33th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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"(invited)" behind a session means that those presentation were invited by the programme committee. They can, of course, be attended by everyone without "invitation

Monday, 09. Sep 2024


0.1Opening Ceremony
Chair:
09. Sep 24 08:30 09:30

0.2ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE: Roberto Cingolani:From cloud computing to multidomain operation in Aeronautics
Chair: D. Mavris ICAS President
09. Sep 24 09:30 10:30

10:30 - 11:00BREAK

1.1Global Sustainable Aviation - Setting the Scene
Chair(s): Wahls, R.
Track 1 Auditorium
15 - Guest lectures
09. Sep 24 11:00 11:25 1.1.1
1253
SUSTAINABLE AVIATION TECHNOLOGY PROGRAMMES IN EUROPE
A. Krein, Clean Aviation, Germany
09. Sep 24 11:25 11:50 1.1.2
1229
UNITED STATES\' AIRCRAFT SUSTAINABILITY RESEARCH & DEVELOPMENT EFFORTS
A. Orton, Federal Aviation Administration, United States; R. Guerrero, United States Air Force, United States; R. Wahls, National Aeronautics and Space Administration, United States
09. Sep 24 11:50 12:15 1.1.3
1255
A VIEW LOOKING IN - AVIATION WEEK\'S ASSESSMENT OF SUSTAINABLE AVIATION R&D IN CHINA AND THE ASIA-PACIFIC REGION
G. Warwick¹, G. Norris¹; ¹Aviation Week, United States
09. Sep 24 12:15 12:40 1.1.4
1269
Q&A - MINI PANEL
Q&A A,
2.1Hydrogen Aircraft 1
Chair(s): Schmollgruber, P.
Track 2 Sala Verde
01.2 - Aircraft Design and Integrated System (Applications)
09. Sep 24 11:00 11:25 2.1.1
0092
GLOBAL SENSITIVITY ANALYSIS OF LIQUID HYDROGEN STORAGE DESIGN PARAMETERS FOR OVERALL AIRCRAFT DESIGN
T. Burschyk¹, B. Fröhler¹, M. Alder¹, T. Zill¹; ¹DLR, Institute for System Architectures in Aeronautics, Germany
09. Sep 24 11:25 11:50 2.1.2
0103
GEOMETRIC OPTIMIZATION OF HYDROGEN AIRCRAFT FUSELAGES IN PRELIMINARY DESIGN
M. Engelmann¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
09. Sep 24 11:50 12:15 2.1.3
0179
RESULTS FROM THE APPU PROJECT: THE POTENTIAL OF LOW-THRESHOLD HYDROGEN-POWERED BLI PROPULSION
A. Heidebrecht¹, M. Hoogreef¹, A.T. Isikveren, SAFRAN S.A., Germany; A. Gangoli Rao¹; ¹TU Delft, Netherlands
3.1Aircraft Design
Chair(s): Rinoie, K.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
09. Sep 24 11:00 11:25 3.1.1
0233
SET-BASED DESIGN TECHNIQUES FOR EVOLVABILITY EXPLORATION DURING CONCEPTUAL AIRCRAFT DESIGN
A.S.J. van Heerden, University of Glasgow, United Kingdom; S. Jimeno Altelarrea¹, A. Riaz¹, X. Chen¹, M.D. Guenov¹, A. Molina-Cristóbal, University of Glasgow Singapore, Singapore; ¹Cranfield University, United Kingdom
Presenter: Sergio Jimeno Altelarrea, Cranfield University
09. Sep 24 11:25 11:50 3.1.2
0614
FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS
Y.-L. Yin¹, K.-S. Zhang¹, H.-L. Qiao¹, A.-L. Che¹, Z.-H. Han¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
09. Sep 24 11:50 12:15 3.1.3
0721
TRANSIENT SIMULATION CALCULATION FOR ELECTRIC THERMAL ANTI-ICING PERFORMANCE OF COMPOSITE WING IN ICING ENVIRONMENT
Z. Dong¹, X. Guo¹, W. Dong¹, P. Wang¹; ¹Shanghai Jiaotong University, China
09. Sep 24 12:15 12:40 3.1.4
0332
TILT-DUCT AIRCRAFT WING AERODYNAMIC DESIGN AND OPTIMIZATION BASED ON ADJOINT METHOD
Y.-T. Zhang¹, S.-R. Xu¹, Z.-J. Zheng¹, Y. Zheng¹, Y.-L. Liu¹; ¹Zhejiang University, China
Presenter: Shangru Xu, Zhejiang University
additional information (interactive) 3.1.R
0068
APPLICATION OF LAMBDA FRAMEWORK FOR AIRCRAFT MULTIDISCIPLINARY DESIGN, ANALYSIS AND OPTIMIZATION
S. Hosseini¹, M.A. Vaziry Zanjany¹, H.R. Ovesy¹, E. Lekzian, Semnan University, Iran; ¹Amirkabir University of Technology, Iran
additional information (interactive) 3.1.R
0575
AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT)
M. Alberti¹, G. Apuleo¹, A. Calia¹, D. Cirio¹, A. Cozzolino¹, F. Gravano¹, M. Mancini¹, F. Nunciato¹, A. Terrile¹; ¹Piaggio Aerospace, Italy
additional information (interactive) 3.1.R
0744
THE INFLUENCE OF DIFFERENT WING MOTIONS ON THE LIFT IN BIO-INSPIRED AERIAL VEHICLES
B.T.V. Carnielo¹, D.D. Bueno¹; ¹São Paulo State University, Brazil
4.1Systems Engineering
Chair(s): Fredriksson, B.
Track 4 Brunelleschi
02 - Systems Engineering and Integration
09. Sep 24 11:00 11:25 4.1.1
0160
AIRCRAFT SYSTEM DESIGN: A MODEL-BASED AND COLLABORATIVE APPROACH
V. Voth¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany
09. Sep 24 11:25 11:50 4.1.2
0053
TECHMAPS – TECHNOLOGY MANAGEMENT FOR THE ARCHITECTING PROCESS OF AIRCRAFT ON-BOARD SYSTEMS
N. Kuelper¹, V. Kriewall¹, K. Beschorner¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany
09. Sep 24 11:50 12:15 4.1.3
0095
MODEL-BASED APPROACH FOR HYDROGEN PRELIMINARY AIRCRAFT DESIGN CONSIDERING SAFETY AND OPERABILITY
A. Sarr¹, J. Jézégou¹, P. de Saqui-Sannes¹; ¹ISAE-SUPAERO, France
09. Sep 24 12:15 12:40 4.1.4
0191
SAFETY ANALYSIS (CCA) OF THE AIR SUPPLY SYSTEM OF A FUEL CELL-POWERED AERO ENGINE FOR ELECTRIC REGIONAL AIRCRAFT
S. Kazula, DLR - Electrified Aero Engines, Germany
additional information (interactive) 4.1.R
0211
RESEARCH ON TECHNOLOGICAL INNOVATION CAPABILITY EVALUATION INDEX FOR AVIATION INDUSTRIES
W. Cheng¹, R. Fan, Aviation Industry Corporation of China, Ltd (AVIC), China; J. Xu¹, H. Zhang¹, Z. Wang¹; ¹Aviation Industry Development Research Center of China (ADR), China
5.1Applied CFD 1
Chair(s): Eliasson, P., Viviani, A.
Track 5 Donatello
03.1 - Aerodynamics – CFD Methods and Validation
09. Sep 24 11:00 11:25 5.1.1
0283
EFFECTIVENESS OF CFD FOR AIRCRAFT DESIGN: STATUS AND PROSPECTS
P. Raj, Virginia Tech, United States
Presenter: Pradeep Raj, Virginia Tech
09. Sep 24 11:25 11:50 5.1.2
1313
EFFECTIVENESS OF CFD FOR AIRCRAFT DESIGN: STATUS AND PROSPECTS PART 2
P. Raj, United States
09. Sep 24 11:50 12:15 5.1.3
0581
COMPUTATIONAL ANALYSIS ON THE EFFECTS OF LEADING EDGE TUBERCLES ON THE PERFORMANCE OF ROTATING PROPELLER
D. Di Pasquale¹, T. Tarun, Indian Institute of Technology(BHU) , India; S. Shubham¹, S.A. Prince¹, A. Proenca¹; ¹Cranfield University, United Kingdom
09. Sep 24 12:15 12:40 5.1.4
1112
INITIAL DEVELOPMENT OF A CFD ICING TOOL
J.R. Teixeira Da Silva¹, M.E.M.C. Lopes¹, A.P.R. Preguica¹, C.F. Rafael¹, P.C. Souza Villela¹, G.A. Lima da Silva, Aerothermal Solutions and Software Distributor LLC, United States; H. Jasak, Cambridge University, United Kingdom; ¹ATS Aerothermal Solutions, Brazil
additional information (interactive) 5.1.R
0531
CONJUGATED HEAT TRANSFER SIMULATION OF BUOYANCY-INDUCED FLOW AND HEAT TRANSFER MECHANISMS IN A COMPRESSOR CAVITY
M. Jian¹, Y. Xiao¹, X. Cheng¹, W. Dong¹; ¹Shanghai Jiao Tong University, China
6.1AI-assisted Flow Analysis
Chair(s): Breitsamter, C.
Track 6 Cimabue
03.3 - Basic Fluid Dynamics and Flow Control
09. Sep 24 11:00 11:25 6.1.1
0741
A CFD STUDY OF THE ACTIVE FLOW CONTROL SYSTEM BEHAVIOUR ON A VERTICAL TAIL SECTION OF AN AIRPLANE, WITH THE AID OF AI
C. Cordoni¹, A. Saporiti¹, M. Boffadossi¹; ¹DAER, Politecnico di Milano, Via La Masa 34, 20156 Milano, Italy, Italy
09. Sep 24 11:25 11:50 6.1.2
1208
GENETIC ALGORITHM OPTIMIZATION OF AN OPPOSITION CONTROL STRATEGY IN A FULLY TURBULENT CHANNEL FLOW
E. Saccaggi¹, G.M. Di Cicca¹; ¹Politecnico di Torino, Italy
Presenter: Enrico Saccaggi, Politecnico di Torino
09. Sep 24 11:50 12:15 6.1.3
0662
FAULT DIAGNOSIS AND TOLERANCE SYSTEM OF FLIGHT STATE PERCEPTION MODEL BASED ON MACHINE LEARNING FOR CO-FLOW JET AIRFOIL
Y.-R. Zhao, China; B.-G. Mi, China; H. Zhan, China; H.-Y. Xu, China
09. Sep 24 12:15 12:40 6.1.4
0282
NUMERICAL INVESTIGATION OF THE FLOW FEATURES ON THE TURRET WITH DIFFERENT CYLINDER HEIGHT IN THE TRANSONIC FLOW
X.-T. Tan¹, H.-Y. Xu¹, Z. Pei¹; ¹Northwest Polytechnic University, China
7.1IFAR Civil Aviation and AAM initiatives
Chair(s): Andreeva Mori, A.
Track 7 Botticelli
15 - Guest lectures
09. Sep 24 11:00 11:25 7.1.1
1223
ADVANCING URBAN AIR MOBILITY: COLLABORATIVE EXCELLENCE AND INFRASTRUCTURE INITIATIVES BY DLR
O. Bertram¹, B. Schuchardt¹, A. König¹, K. Wendt¹, P. Shiva Prakasha¹; ¹DLR, Germany
09. Sep 24 11:25 11:50 7.1.2
1322
NASA’S ADVANCED AIR MOBILITY RESEARCH
P.H. Kopardekar, United States
09. Sep 24 11:50 12:15 7.1.3
0057
IFAR-X: COLLABORATIVE ENGINEERING FRAMEWORK FOR NEXT GENERATION OF AEROSPACE ENGINEERS WORKING ON AIRCRAFT DESIGN
S. Garg¹, A.M.P. Silva², P.F. Albuquerque², E. Nguyen Van, The French Aerospace Lab (Onera), France; K. Kimura³, Y. Sugioka³, M. Jacinto¹, P. Shiva Prakasha¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany ;²Centre of Engineering and Product Development (CEiiA), Portugal ;³Japan Aerospace Exploration Agency (JAXA), Japan
09. Sep 24 12:15 12:40 7.1.4
0079
AIRCRAFT WING STRUCTURAL SIZING COMPUTATIONAL TOOL TAILORED FOR A COLLABORATIVE MULTIDISCIPLINARY DESIGN FRAMEWORK
P.F. Albuquerque¹, A.M.P. Silva¹, A. Pereira¹; ¹CEiiA, Portugal
Presenter: Ana Silva, CEiiA
8.1Complex Flow Phenomena
Chair(s): Gowree, E.
Track 8 Vasari
03.2 - Experimental Aerodynamics
09. Sep 24 11:00 11:25 8.1.1
0853
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A STRUCTURAL-DYNAMICALLY SCALED DELTA WING WITH TRAINING EDGE FLAPS
K. Bantscheff¹, F. Santelli¹, C. Breitsamter¹; ¹Technische Universität München / Lehrstuhl für Aerodynamik, Germany
Presenter: Konstantin Bantscheff, Technische Universität München / Lehrstuhl für Aerodynamik
09. Sep 24 11:25 11:50 8.1.2
0549
EVALUATION OF WIND TUNNEL TEST RESULTS OF TAXIDERMY BLACK-TAILED GULL (LARUS CRASSIROSTRIS)
N. Kishimoto, Kwansei Gakuin University, Japan; D. Wada¹, M. Tamayama¹, Y. Iwami², N. Tomita², T. Ikeda³, Y. Tanahashi³, K. Katagiri, Hiroshima University, Japan; ¹JAXA, Japan ;²Yamashina Institute of Ornithology, Japan ;³Chubu University, Japan
additional information (interactive) 8.1.R
0219
EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT
R. Bardera¹, A.A. Rodríguez-Sevillano², J.C. Matías¹, E. Barroso¹, M. Ojeda², J. Fernández²; ¹Instituto Nacional de Técnica Aeroespacial (INTA)., Spain ;²Escuela Técnica Superior de ingeniería Aeronáutica y del Espacio, Spain
additional information (interactive) 8.1.R
0526
INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION
Y.-F. Wang¹, B.-F. Song¹, Y. Luo¹, X.-Y. Lang¹, W. Wang¹; ¹Northwestern Polytechnical University, China
9.1Micro - nano Structures
Chair(s): , , Kanerva, M.
Track 9 Giotto
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
09. Sep 24 11:00 11:25 9.1.1
0908
EFFICIENT THERMOMECHANICAL SIMULATION FOR METALLIC LATTICE STRUCTURES FABRICATED BY ADDITIVE MANUFACTURING
N. Tsushima, Japan Aerospace Exploration Agency, Japan; M. Kita¹, I. Matsubara¹, M. Ohishi, Ryoyu Systems Co., Ltd., Japan; R. Higuchi, 2The University of Tokyo, Japan; K. Yamamoto¹; ¹3Cybernet Systems Co., Ltd., Japan
09. Sep 24 11:25 11:50 9.1.2
1141
USE OF GRAPHENE MATERIAL IN AIRCRAFT STRUCTURE FOR LIGHTNING STRIKE PROTECTION
P. Jha¹, V.M. Sharma¹, V. Samanyusree¹, A. Sharma¹, S. Maheshwari¹; ¹R. V. College of Engineering, India
09. Sep 24 11:50 12:15 9.1.3
0339
EFFECT OF LASER PRINTING MODE ON SURFACE TOPOGRAPHY, MICROSTRUCTURE AND CORROSION PROPERTY OF ADDITIVE-MANUFACTURED NITI
X. Liu¹, D. Gu¹; ¹Nanjing University of Aeronautics and Astronautics, China
10.1Aerostructures
Chair(s): Guida, M., Bayandor, J.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
09. Sep 24 11:00 11:25 10.1.1
0760
TOWARDS EFFICIENT ANALYSIS OF POSTBUCKLING IN AIRCRAFT STIFFENED STRUCTURES
M.H. Elalfy¹, R. de Breuker¹, S.G.P. Castro¹; ¹TU Delft, Netherlands
09. Sep 24 11:25 11:50 10.1.2
1206
CONCEPTUAL DESIGN AND TOPOLOGY OPTIMIZATION OF A COMPLIANT MORPHING FLAP FOR NEXT GENERATION HYBRID-ELECTRIC REGIONAL AIRCRAFT
M.C. Noviello¹, I. Dimino¹, S. Ameduri¹, A. Concilio¹; ¹The Italian Aerospace Research Centre (CIRA), Italy
Presenter: Maria Chiara Noviello, The Italian Aerospace Research Centre (CIRA)
09. Sep 24 11:50 12:15 10.1.3
0808
HIGH-VELOCITY DROPLET IMPACT STUDIES ON C/SIC AND C/C COMPOSITES
Y. Yue¹, R. Zhao¹, B. Wang¹, Y. Li, Shaanxi Key Laboratory of Impact Dynamics and Engineering Applic, China; ¹School of Aeronautics, Northwestern Polytechnical University, China
09. Sep 24 12:15 12:40 10.1.4
0889
CANCELED - WEIGHT OPTIMIZATION AND STRENGTH ANALYSIS OF AIRBORNE POD BASED ON T300/QY9611 CARBON FIBER COMPOSITE
Z.-C. Dong¹, X.-M. Li, AVIC·Leihua Electronic Technology Research Institute, China; H.-Y. Huang¹; ¹Northwestern Polytechnical University, China
11.1Dynamic Loads
Chair(s): Ricci, S., Toffol, F.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
09. Sep 24 11:00 11:25 11.1.1
0012
POTENTIAL LIMITS OF LOAD ALLEVIATION IN REDUCING THE STRUCTURAL MASS OF A LONG-RANGE TRANSPORT CONFIGURATION
V. Handojo¹, S. Puelm¹; ¹DLR German Aerospace Center, Germany
09. Sep 24 11:25 11:50 11.1.2
0011
CLOSED-LOOP GUST LOADS ANALYSIS OF A SUPERSONIC FIGHTER AIRCRAFT
A. Voß¹, J. Baier¹; ¹DLR Institute of Aeroelasticity, Germany
09. Sep 24 11:50 12:15 11.1.3
0588
DYNAMIC DROP SIMULATION OF THE MAIN LANDING GEAR OF A GENERAL AVIATION AIRCRAFT
N. Li¹, H. Wang¹, Z.Q. Li¹, Z.H. Wang¹; ¹Taiyuan University of Technology, China
09. Sep 24 12:15 12:40 11.1.4
0130
TRADE OFF STUDIES ON WING MANEUVER LOAD ALLEVIATION STRATEGIES BASED ON AILERONS AND WINGLETS MOVABLE SURFACES
R. Pecora, University of Naples Federico II, Italy
additional information (interactive) 11.1.R
0072
FLIGHT LOADS RESEARCH OF TWIN VERTICAL TAIL FOR BLENDED WING-BODY AIRCRAFT BASED ON STRAIN GAUGE CAILBRATION
Z. Guo¹, A. Tang¹, Q. Jing¹; ¹Chinese Flight Test Estsblishment, China
12.1Computational Aeroelasticity 1
Chair(s): Juracka, J., Palacios, R.
Track 12 Petrarca
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
09. Sep 24 11:00 11:25 12.1.1
0066
EFFECTS OF SHOCK IMPINGEMENT LOCATION ON PANEL AEROELASTIC STABILITY IN MACH REFLECTION
Y. He¹, A. Shi¹; ¹Northwestern Polytechnical University, China
09. Sep 24 11:25 11:50 12.1.2
0954
PARAMETERISATION OF NONLINEAR AEROELASTIC REDUCED ORDER MODELS WITH AERODYNAMIC AND STRUCTURAL NONLINEARITY
M. Candon¹, E. Hale¹, M. Balajewicz, Independent Researcher, United States; A. Delgado-Gutierrez¹, V. Muscarello¹, P. Marzocca¹; ¹RMIT University, Australia
Presenter: Pier Marzocca, RMIT University
09. Sep 24 11:50 12:15 12.1.3
0900
EFFICIENT MULTI-FIDELITY REDUCED-ORDER MODELING FOR FLUTTER PREDICTIONS ACROSS MULTIPLE MACH NUMBERS
X. Wang¹, X. Peng¹, H. Liu¹, J. Kou¹, W. Zhang¹; ¹Northwestern Polytechnical University, China
13.1Combustion Heat Transfer 1
Chair(s): Mari, C.
Track 13 Boccaccio
05 - Propulsion
09. Sep 24 11:00 11:25 13.1.1
0450
FAST PREDICTION METHOD FOR RADIAL GROWTH OF LABYRINTH SEAL CLEARANCE BASED ON TRANSIENT THERMAL-FLUID COUPLING NETWORK
Z. Li¹, C. Liu¹, P. Liu¹, Y. Wang¹, X. Jin¹, S. Ding¹; ¹Research Institute of Aero-Engine, Beihang University, China
09. Sep 24 11:25 11:50 13.1.2
0512
BASE FLOW CHARACTERISTICS FOR A SUB-SCALE HIGH-SPEED EXHAUST AT OVER-EXPANDED MODE
S. Tsentis¹, I. Goulos¹, S. Prince¹, V. Pachidis¹, V. Zmijanovic, Reaction Engines Ltd, United Kingdom; ¹Cranfield University, United Kingdom
09. Sep 24 11:50 12:15 13.1.3
0518
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR
B.O. Cakir¹, D. Sanned¹, P. Vauquelin¹, M. Prakash¹, J.-P. Hannappel¹, A. Subash¹, M. Richter¹, X.-S. Bai¹, C. Fureby¹; ¹Lund University, Sweden
09. Sep 24 12:15 12:40 13.1.4
0622
PERFORMANCE ASSESSMENT OF AN ENGINE-INTEGRATED CLOSED-AIR COOLING THERMAL MANAGEMENT SYSTEM IN A NEXT GENERATION FIGHTER CONFIGURATION
T. Matuschek¹, J. Häßy¹, M. Schmelcher¹, A. Görtz¹; ¹German Aerospace Center (DLR), Germany
14.1Air Taxis
Chair(s): Consiglio, M.
Track 14 Puccini
15 - Guest lectures
09. Sep 24 11:00 11:25 14.1.1
1267
RESEARCH RESULTS AND PERSPECTIVES ON NON-COOPERATIVE SENSING FOR SAFE UAM OPERATIONS
F. Vitiello¹, F. Causa¹, R. Opromolla¹, G. Fasano¹; ¹University of Naples Federico II, Italy
09. Sep 24 11:25 11:50 14.1.2
1268
SENSOR UNCERTAINTY MITIGATION FOR DETECT AND AVOID SYSTEMS
E. Theunissen, Netherlands Defence Academy, Netherlands
09. Sep 24 11:50 12:15 14.1.3
1278
PRELIMINARY APPLICATION OF FORMAL VERIFICATION TO AN AUTONOMY ARCHITECTURE FOR UNMANNED AIRCRAFT
L.R. Humphrey¹, C.A. Muñoz¹; ¹NASA, United States
15.1Education and Training Enablers
Chair(s): Kanerva, M.
Track 15 Carducci
14 - Education and Training
09. Sep 24 11:00 11:25 15.1.1
0314
A TIERED CONTINUOUS CULTIVATING SYSTEM FOR AVIATION TECHNOLOGY TALENTS THAT INTEGRATES STEM AND POPULAR SCIENCE EDUCATION
J. Li¹, Y. He, Sichuan Technical Exchange Center, China; X.H. Tang, School of Public Administration, Sichuan University, China; Y.M. Zhou¹, W.F. Huo², J. Zhang², K. Lin², Y. Luo, Mao County Innovation Institute of Intelligent Aircraft Engineer, China; M. Ling, Chenghang Innovation Institute of Intelligent Aerocraft, Chengdu, China; ¹School of Aeronautic Science and Engineering, Beihang University, China ;²Chengdu Xueshang Technology Co., Ltd, China
Presenter: Ji Li, Beihang University/School of Aeronautic Science and Engineering
09. Sep 24 11:25 11:50 15.1.2
0508
DESIGN BUILD AND FLY: A STUDENT APPROACH TO THE CREATION OF AN RC DRONE FOR UNIVERSITY COMPETITION
E. Gaspari¹, E. Bianchini¹, L. Pezzullo¹, A. Giorgi¹, M. Giannetti¹, D.M. Macchini¹, L. Ferrarini¹, F. Bondanese¹, S. Celli¹, T. Strafforello¹, U. Mignemi¹, A. Arnaldi¹, M. Ferrazzani¹, M. Sanna¹, D. Geraci¹, M.R. Chiarelli¹, A.A. Quarta¹, G. Palaia¹, L. Boni¹; ¹University of Pisa, Department of Civil and Industrial Engineeri, Italy
09. Sep 24 11:50 12:15 15.1.3
1263
MICKEY MOUSE AND A GIANT: COMPARISON OF AERONAUTICS EDUCATION IN FINLAND AND CHINA
M. Kanerva¹, Y. Zhang, Tsinghua University, China; R. Yondo Mine¹, L. Qiu, Beihang University, China; M. Wang, BIT, China; ¹Tampere University, Finland
Presenter: Raoul Yondo Mine, Tampere University
09. Sep 24 12:15 12:40 15.1.4
0505
DESIGN AND VISUALIZATION OF A KNOWLEDGE-BASED AIRCRAFT CABIN IN VIRTUAL REALITY
F. Prokic¹, C. Eriksson¹, R.C. Munjuluru¹; ¹Linköping University, Sweden
Presenter: Fredrik Prokic
additional information (interactive) 15.1.R
1098
DESIGNING A FRAMEWORK FOR FLIGHT SIMULATOR TRAINING SCENARIOS. AN EVIDENCE BASED TRAINING APPROACH.
G. Kontos¹, O. Lehmann¹; ¹Abu Dhabi University, United Arab Emirates
16.1Future Maintenance Practices
Chair(s): Kelly, M., Koschlik, A. K.
Track 16 Raffaello
11 - Operations and Sustainment
09. Sep 24 11:00 11:25 16.1.1
0701
COMPARATIVE ANALYSIS OF MACHINE LEARNING ALGORITHMS FOR HEAT EXCHANGERS DIAGNOSIS IN ELECTRIFIED AIRCRAFT
D.F. Migliore¹, G. D'Alessio², S. Caggese², A. De Martin², F. Acerra¹, M. Sorli², M. Fioriti²; ¹Leonardo S.p.A., Italy ;²Politecnico di Torino, Italy
09. Sep 24 11:25 11:50 16.1.2
0083
APPLICATION OF NATURAL LANGUAGE PROCESSING FOR AIRCRAFT DEFECT TRACKING IN MAINTENANCE OPERATIONS
M.J. Scott¹, O. Kirkpatrick¹, W. Verhagen¹, V. Kekoc, Defence Science and Technology Group, Australia; B. Teunisse, Capability Acquisition and Sustainment Group, Australia; J. Zhang¹, H. Fayek¹, P. Marzocca¹; ¹RMIT University, Australia
09. Sep 24 11:50 12:15 16.1.3
0793
TOWARDS TRUSTWORTHY DATA-DRIVEN GAS TURBINE PROGNOSTICS
A. Apostolidis¹, S. Le Dantec, SIGMA Clermont, France; K.P. Stamoulis¹; ¹Amsterdam University of Applied Sciences, Netherlands
09. Sep 24 12:15 12:40 16.1.4
0455
FASTVIBE SW TOOL FOR RIDE-ALONG VIBRATION SURVEY ANALYSIS
S. Bianchi¹, F. Negroni¹, M. Riganti¹; ¹Leonardo Aircraft Division, Italy
additional information (interactive) 16.1.R
0545
LIFE CYCLE ASSESSMENT OF ALTERNATIVE LAUNCH METHODS
S. Wildermuth¹, W. Veraburenon¹, T. Bellier¹, C. Bil¹; ¹RMIT University, Australia
17.1Actuator Systems
Chair(s): Stumpf, E.
Track 17 Galileo
07 - Systems, Subsystems and Equipment
09. Sep 24 11:00 11:25 17.1.1
0735
MODEL-BASED DESIGN OF ACTIVE/ACTIVE ELECTRO-HYDROSTATIC ACTUATION FOR HELICOPTER FLIGHT CONTROLS
M.-W. Sun¹, J. Fu¹, D.-C. Lyu¹, J.-C. Mare, ICA, INSA-Toulouse, France; ¹Beihang University, China
09. Sep 24 11:25 11:50 17.1.2
0146
DEVELOPMENT OF AN ELECTRO-HYDROSTATIC NOSE LANDING GEAR ACTUATION AND STEERING SYSTEM
M.N. Duval¹, T. Lammering¹; ¹Liebherr-Aerospace Lindenberg GmbH, Germany
additional information (interactive) 17.1.R
0674
RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS
X. Hu¹, Y. Fu¹, D. Lyu¹, M. Sun¹, S. Zhao, Beijing Institute of Precision Mechatronics and Controls, Labora, China; J. Fu¹, J. Zhao¹; ¹School of Mechanical Engineering and Automation, Beihang Univers, China
Presenter: Mingwei SUN, Beihang University

12:30 - 13:30LUNCH

0.3GENERAL LECTURE 1. Jim Hileman : Sustainability and Future Mobility
Chair: F. Collier Executive Committee Member
09. Sep 24 13:30 14:30

1.2GSA - Aircraft Concepts & Demonstrations 1
Chair(s): Collier, F.
Track 1 Auditorium
15 - Guest lectures
09. Sep 24 14:30 14:55 1.2.1
1305
JETZERO: RESHAPING AVIATION WITH THE BLENDED WING
SS Savian, JetZero, United States
09. Sep 24 14:55 15:20 1.2.2
1240
X-66: ACCELERATED LEARNING THROUGH FULL SCALE PROTOTYPING
B. Cobleigh, NASA (AFRC), United States; E. Kaduce, Boeing, United States
09. Sep 24 15:20 15:45 1.2.3
1261
BOMBARDIER ECOJET RESEARCH PROJECT; THE QUEST FOR SUSTAINABLE AVIATION
S. McCullough, Bombardier, Canada
09. Sep 24 15:45 16:10 1.2.4
1270
Q&A - MINI PANEL
Q&A A,
2.2Hydrogen Aircraft 2
Chair(s): Schmollgruber, P.
Track 2 Sala Verde
01.2 - Aircraft Design and Integrated System (Applications)
09. Sep 24 14:30 14:55 2.2.1
0826
IMPACT OF HYDROGEN FUEL ON OVERALL DESIGN OF TRANSPORT AIRCRAFT
E. Nguyen Van¹, J. Gauvrit-Ledogar¹, C. Julien², B. Paluch², J.L. Ruan, ONERA/DMPE, France; F. Moens, ONERA/DAAA, France; ¹ONERA/DTIS, France ;²ONERA/DMAS, France
09. Sep 24 14:55 15:20 2.2.2
0251
A PERFORMANCE COMPARISON OF HYDROGEN AIRCRAFT CONCEPTS
N. Wood¹, S. Taylor¹, M. Hales¹, M. Joynt¹, S. Chandran¹, D. Sanjeevekumar¹; ¹GKN AEROSPACE, United Kingdom
09. Sep 24 15:20 15:45 2.2.3
0109
PRELIMINARY SIZING OF HYDROGEN-BURNING JETLINER FOR DIRECT OPERATING COST OPTIMIZATION
H. Mohammadi¹, G. Sirtori¹, L. Trainelli¹; ¹DAER, Politecnico di Milano, Italy
Presenter: Gabriele Sirtori, DAER, Politecnico di Milano
09. Sep 24 15:45 16:10 2.2.4
0358
INVESTIGATING THE FLEXIBLE HYDROGEN AIRCRAFT SYSTEM INTERFACE DESIGN USING THE XR CO-DESIGN APPROACH
F. Reimer¹, M. Fuchs¹, J. Herzig¹, S. Cornelje¹, J. Biedermann¹, B. Nagel¹; ¹DLR, Germany
3.2Design Methods
Chair(s): Nagel, B.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
09. Sep 24 14:30 14:55 3.2.1
1169
A MORPHOLOGICAL ANALYSIS OF METHODS FOR CONCEPTUAL AIRCRAFT DESIGN UNDER UNCERTAINTIES
V.T. Todorov¹, D. Rakov, Blagonravov Institute of Engineering Science, Russia; A. Bardenhagen¹; ¹Technical University of Berlin, Germany
09. Sep 24 14:55 15:20 3.2.2
0216
NUMERICAL AND THEORETICAL INVESTIGATION OF HELICOPTER DITCHING WITH VARIOUS INITIAL VELOCITY AND PITCHING ANGLE
L. Zheng¹, M. Wang², Y. Lu², H. Qiao¹, T. Xiao¹, S. Deng¹; ¹Nanjing University of Aeronautics and Astronautics, China ;²Chinese Aeronautical Establishment, China
09. Sep 24 15:20 15:45 3.2.3
0141
MAXIMUM SPEED OF BATTERY-POWERED TILT-ROTOR AIRCRAFT
N. Roh¹, M. Park¹; ¹Hanwha systems, South Korea
09. Sep 24 15:45 16:10 3.2.4
0420
EFFICIENT MULTI-OBJECTIVE DESIGN OPTIMIZATION OF ROTOR AIRFOILS FOR IMPROVING DYNAMIC STALL CHARACTERISTICS
Z. Lu¹, Z.-H. Han¹, W.-P. Song¹, K.-S. Zhang¹, K.-Y. Zhou¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 3.2.R
0696
AN UNCERTAINTY MULTIDISCIPLINARY PROPAGATION ANALYSIS METHOD FOR CORRELATED HIGH-DIMENSIONAL DATA IN AIRCRAFT DESIGN
S. Du, China; C. Li, China; Y. Liu, China
Presenter: Siyi Du
4.2System of Systems 1
Chair(s): de Laurentis, D., Holmberg, G.
Track 4 Brunelleschi
02 - Systems Engineering and Integration
09. Sep 24 14:30 14:55 4.2.1
1138
COLOSSUS EU PROJECT – COLLABORATIVE SOS EXPLORATION OF AVIATION PRODUCTS, SERVICES AND BUSINESS MODELS: OVERVIEW AND APPROACH
P. Shiva Prakasha¹, N. Naeem¹, K. Amadori, SAAB Aeronautics, Sweden; G. Donelli¹, J. Akbari¹, F. Nicolosi, UNINA, Italy; L. Knöös Franzen, Linkoping University, Sweden; M. Ruocco, Smartup Engineering, Italy; T. Lefebvre, The French Aerospace Lab, France; B. Nagel¹; ¹German Aerospace Center - DLR, Germany
09. Sep 24 14:55 15:20 4.2.2
0402
A SYSTEM OF SYSTEMS AIRCRAFT DESIGN FRAMEWORK: DEMONSTRATION USING A SEAPLANE TRANSPORT NETWORK IN THE GREEK ISLANDS
V. Nugnes¹, C. Varriale, TU Delft, Italy; P. Ratei¹, P. Shiva Prakasha¹, B. Nagel¹; ¹DLR, Italy
09. Sep 24 15:20 15:45 4.2.3
0357
CONCEPT OF OPERATIONS IN AN AGENT-BASED SIMULATION: A SYSTEM-OF-SYSTEMS APPROACH
F. Villas¹, L. Knöös Franzén¹, C. Jouannet², K. Amadori², I. Staack, TU Braunschweig, Germany; ¹Linköping University, Sweden ;²Saab Aeronautics, Sweden
Presenter: Ludvig Knöös Franzén, Linköping University
09. Sep 24 15:45 16:10 4.2.4
0413
SYSTEM OF SYSTEMS ANALYSIS OF AUTONOMOUS AIRCRAFT OPERATIONS IN AIR CARGO FEEDER NETWORKS
P.W. Jansen¹, R.E. Perez¹, J.C.-H. Wang, Ribbit Inc, Canada; ¹Royal Military College of Canada, Canada
Reserve Paper 4.2.R
0041
TECHNICAL RISK MANAGEMENT OF SYSTEM OF SYSTEMS BASED ON TECHNOLOGY READINESS ASSESSMENT
H. Cao¹, W. Cheng¹, C. Xing, Chinese Aeronautics Establishment (CAE), China; G. Song¹; ¹ Aviation Industry Development Research Center of China (ADR) , China
additional information (interactive) 4.2.R
0550
RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS
X. Li¹, L. Deng¹, Y. Ge¹, Y. Pei¹, Y. Gu², L. Cao², A. Shi¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China ;²Shanghai Electro-Mechanical Engineering Institute, China
5.2Applied CFD 2
Chair(s): Martins, J., Kiszkowiak, L.
Track 5 Donatello
03.1 - Aerodynamics – CFD Methods and Validation
09. Sep 24 14:30 14:55 5.2.1
0031
GRID EFFECT ON M823 BOMB AT TRANSONIC REGIME
J. Jiménez-Varona¹, G. Liaño¹; ¹INTA, Spain
09. Sep 24 14:55 15:20 5.2.2
0864
LOW SPEED AERODYNAMICS OF SIX OPTIMISED UNCONVENTIONAL RE-ENTRY VEHICLE AEROSHAPES
S.M. Giannino¹, G. Pezzella¹, A. Viviani¹; ¹Università della Campania Luigi Vanvitelli, Italy
Presenter: Spartaco Giannino, Università della Campania "Luigi Vanvitelli"
09. Sep 24 15:20 15:45 5.2.3
0925
SCALE EFFECT ON WATER LANDING PERFORMANCE OF AMPHIBIOUS AIRCRAFT
H. Zhang¹, J. Chen², F. Wang¹, G. Zhang¹, Z. Shen, Aircraft Strength Research Institute of China, China; Q. Zhu, China Special Vehicle Research Institute, China; G. Wu, Commercial Aircraft Corporation of China Ltd, China; M. Tong²; ¹Jinling Institute of Technology, China ;²Nanjing University of Aeronautics and Astronautics, China
09. Sep 24 15:45 16:10 5.2.4
0929
ANALYSIS OF SUCTION FORCE EFFECT ON DIFFERENT FUSELAGE SHAPE DURING THE WATER DITCHING
J.-Y. Li¹, X.-Y. Wang, Shanghai Electro-Mechanical Engineering Institute, China; J.-C. Chen¹, J. Jiao, China Special Vehicle Research Institute, China; M.-B. Tong¹, C.-L. Yan, Beijing University Of Aeronautics And Astronautics, China; ¹Nanjing University Of Aeronautics And Astronautics, China
additional information (interactive) 5.2.R
0205
APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS
Q. Nguyen Dinh¹, H. Tran The¹, G. Sharma², J. Tanimoto²; ¹Le Quy Don Technical University, Vietnam ;²Kyushu University, Japan
Presenter: Gopal Sharma
additional information (interactive) 5.2.R
0311
SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST
B. Guo¹, Y.F. Lu¹, B. Wang, Chinese Academy of Military Science, China; Z. Guo¹, G.W. Jia¹, D.N. Liu¹; ¹National University of Defense Technology, China
additional information (interactive) 5.2.R
0952
RESEARCH ON AERODYNAMIC PERFORMANCE OF OVERSIZE MODULAR PARAFOIL IN RANDOM WIND FIELD
F. Duan¹, J.-Y. Li¹, Z.-D. Li, Aerospace Life-support Industries Ltd, China; M.-B. Tong¹; ¹Nanjing University of Aeronautics and Astronautics, China
6.2Lift & Flow Separation Control
Chair(s): Vijgens, P.
Track 6 Cimabue
03.3 - Basic Fluid Dynamics and Flow Control
09. Sep 24 14:30 14:55 6.2.1
0228
PASSIVE FLOW CONTROL DEVICES ON LOW-REYNOLDS DU89-134 AIRFOIL
C. Brunelli¹, M. Avirovic¹, B. Janssens¹, B.G. Marinus¹, M. Runacres, Vrije Universiteit Brussel, Belgium; G. May, Von Karman Institute for Fluid Dynamics, Belgium; A. Ecorce², A. Dalbera²; ¹Royal Military Academy, Belgium ;²National Polytechnic Institute of Toulouse , France
09. Sep 24 14:55 15:20 6.2.2
0239
RESEARCH ON UNSTEADY AERODYNAMIC MODELING METHOD OF PREPOSITIVE WING - MAIN WING COMPOSITE SYSTEM AT HIGH ATTACK ANGLE
X. Bai, China; B. Mi, China; J. Zhang, China
09. Sep 24 15:20 15:45 6.2.3
0595
MITIGATING DYNAMIC STALL WITH A MOVABLE LEADING-EDGE: THE NACA0012-IK30 WING
E.A.R. Camacho¹, A.R.R. Silva¹, F.D. Marques, Universidade de São Paulo, Brazil; ¹Universidade da Beira Interior, Portugal
Presenter: Emanuel Camacho, Universidade da Beira Interior
09. Sep 24 15:45 16:10 6.2.4
1053
NUMERICAL STUDY ON ACTIVE FLOW CONTROL SOLUTIONS FOR HIGH LIFT
P. Scavella¹, G. Paolillo¹, T. Astarita¹, G. Cardone¹, C.S. Greco¹; ¹University of Study of Naples Federico II, Italy
7.2Hypersonic Aerodynamics 1
Chair(s): Choudhari, M., Viviani, A.
Track 7 Botticelli
03.1 - Aerodynamics – CFD Methods and Validation
09. Sep 24 14:30 14:55 7.2.1
1026
AERODYNAMIC NUMERICAL/EXPERIMENTAL COMPARISON OF A HYPERSONIC TEST VEHICLE IN MORE&LESS PROGRAM
P. Roncioni¹, M. Marini¹, R. Fusaro², N. Viola², D. Pepelea, INCAS, Romania; B. Cakir, VKI, Belgium; M. Clay, REL, United Kingdom; ¹CIRA, Italy ;²POLITO, Italy
09. Sep 24 14:55 15:20 7.2.2
0644
ANALYSIS ON COMPLEX HYPERSONIC FLOW DURING THE REENTRY OF EXPIRED SPACECRAFT
Z. Han¹, Z.-H. Li, National Laboratory for Computational Fluid Dynamics, China; S.-Y. Chu¹, W.-Y. Cheng¹, C.-S. Wang¹; ¹Aviation Industry Development Research Center of China, China
09. Sep 24 15:20 15:45 7.2.3
0872
ASSESSMENT OF A MACROSCOPIC MODEL FOR THE AEROTHERMODYNAMICS CHARACTERIZATION OF ICE GIANTS ATMOSPHERIC ENTRY
D. Ninni¹, F. Bonelli¹, A. Laricchiuta², G. Colonna², G. Pascazio¹; ¹Politecnico di Bari, Italy ;²CNR ISTP Bari, Italy
09. Sep 24 15:45 16:10 7.2.4
0276
KINETIC MONTE CARLO BASED CATALYTIC VISCOUS WALL BOUNDARY MODELING IN CFD SIMULATION OF HIGH-ENTHALPY NON-EQUILIBRIUM FLOW
Q. Li¹, X. Yang², W. Dong¹, Y. Du²; ¹Shanghai Jiao Tong University, China ;²China Aerodynamics Research and Development Center, China
8.2Airframe Aerodynamics 3
Chair(s): Zhao, H.
Track 8 Vasari
03.4 - Applied Aerodynamics
09. Sep 24 14:30 14:55 8.2.1
0293
EVALUATING INSTALLATION EFFECTS IN SEMI-SPAN WIND TUNNEL EXPERIMENTS USING CARTESIAN-GRID-BASED FLOW SOLVER UTCART
Y. Tamaki¹, Y. Yokoyama¹, T. Imamura¹; ¹The University of Tokyo, Japan
09. Sep 24 14:55 15:20 8.2.2
0414
CHARACTERIZATION OF EXTERNAL LIQUID HYDROGEN TANK INTERFERENCE DRAG
C. Graham¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada
09. Sep 24 15:20 15:45 8.2.3
0348
WIND TUNNEL ANALYSIS OF A SPACE RE-ENTRY VEHICLE AT LOW-SPEED CONDITIONS
N. Montella, University of Campania/ CIRA, Italy; G.A. Vio, The University of Sydney, Australia; L. Iuspa¹, A. Aprovitola¹, G. Pezzella, University of Campania , Italy; A. Viviani¹; ¹University of Campania, Italy
Presenter: Nicolina Montella, Università degli Studi della Campania "L. Vanvitelli" / CIRA
09. Sep 24 15:45 16:10 8.2.4
0102
DESIGN OF A HIGHLY EFFICIENT TRANSPORT NLF AIRCRAFT WITH A BACKWARD SWEPT WING AND A LONG SINGLE-AISLE FUSELAGE
T. Streit¹, J. Ruberte Bailo¹, A. Büscher, Airbus Operations GmbH, Germany; A. Seitz¹; ¹DLR (GERMAN AEROSPACE CENTER), Germany
9.2AAM 1 - Air Mobility Scenarios and Optimisation
Chair(s): Vozella, A., Itoh, E.
Track 9 Giotto
09 - Air Transport System Efficiency
09. Sep 24 14:30 14:55 9.2.1
0850
WHAT-IF SCENARIO ANALYSIS OF REGIONAL AIR MOBILITY OPERATIONS IN SOUTH KOREA
J.C. Lee¹, S.K. Kim, Georgia Institute of Technology, South Korea; S.M. Ahn¹, J.H. Kim, Sejong University, South Korea; ¹Handong Global University, South Korea
09. Sep 24 14:55 15:20 9.2.2
0325
DEVELOPMENT OF LOW ALTITUDE 4-DIMENSIONAL OPERATIONS MANAGEMENT SYSTEM FOR ADVANCED AIR-MOBILITY
T. Iijima¹, N. Matayoshi¹, N. Yokoyama¹, H. Yoshida¹, A. Oosedo¹, S. Kikkawa¹, M. Yawata², S. Nakada², T. Yahata²; ¹JAXA, Japan ;²NEC, Japan
09. Sep 24 15:20 15:45 9.2.3
0464
EXPLORING RIDESHARING IN PASSENGER URBAN AIR MOBILITY: A COMPARATIVE ANALYSIS
A. Edsel¹, S.D. Biswas¹, M. Kilbourne¹, R. Gadre¹, S. Vashi¹, K. Mall¹, W.A. Crossley¹, D.A. DeLaurentis¹, M.D. Patterson², B.E. Sells²; ¹Purdue University, United States ;²NASA Langley Research Center, United States
Presenter: Daniel DeLaurentis, Purdue University
09. Sep 24 15:45 16:10 9.2.4
0326
CLASSIFICATION OF EXTENDED REALITY BASED HUMAN MACHINE INTERFACES SCENARIOS FOR URBAN AIR MOBILITY
M. Gomes Araujo¹, C. Conte², F. De Crescenzio¹, D. Accardo²; ¹University of Bologna, Italy ;²University of Naples Federico II, Italy
Presenter: Millene Gomes Araujo, University of Bologna
10.2Fatigue
Chair(s): Bisagni, C., Blom, A.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
09. Sep 24 14:30 14:55 10.2.1
0229
DEMOCRATIZATION OF FATIGUE EVALUATION FOR REALISTIC RIVETING CONFIGURATIONS USING STATE-OF-THE-ART SIMULATIONS
I. Rivero¹, A. Palomar¹, M. Rebollo¹, J. Domingo¹, M. Lozano¹, Z. Mujika¹, D. Garijo¹, G. Lara¹, A. Capitan¹, J. Gomez-Escalonilla¹; ¹Airbus, Spain
Presenter: Alejandro Palomar, Airbus Defence and Space
09. Sep 24 14:55 15:20 10.2.2
1120
THE FATIGUE LIFE PREDICTION OF THIN-WALLED WELDED JOINTS
M. Sladky¹, M. Machac², J. Papuga², I. Jebacek¹; ¹Faculty of Mechanical Engineering, Brno University of Technology, Czech Republic ;²Faculty of Mechanical Engineering, Czech Technical University, Czech Republic
09. Sep 24 15:20 15:45 10.2.3
0025
SURFACE QUALITY CHALLENGE FOR TI-6AL-4V ADDITIVE MANUFACTURED TOPOLOGIC OPTIMIZED LIGHTWEIGHT STRUCTURE
C. Matias¹, A. Diskin¹, O. Golan, Afeka- Tel-Aviv Academic College of Engineering, Israel; A. Garkun², E. Strokin²; ¹Israel Aerospace Industries, Israel ;²Technion Research & Development Foundation, Israel
09. Sep 24 15:45 16:10 10.2.4
0538
INTEGRATIVE ANALYSIS OF LOW-CYCLE FATIGUE AND CRACK PROPAGATION IN TURBINE BLADES
N.M. Hoang¹, M.D. Ha¹, T.Q. Nguyen¹, P.M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam
additional information (interactive) 10.2.R
0422
STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT
H. Peng¹, B. Wang¹, Y. Zhang¹, L. Ji¹, S. Li¹; ¹AVIC the First Aircraft Institute, China
11.2Structural Design and Optimization 1
Chair(s): Alaimo, A., Pagani, A.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
09. Sep 24 14:30 14:55 11.2.1
0727
NUMERICAL METHOD TO DETERMINE STRUCTURAL ELEMENT REDUCED STIFFNESS FOR DESIRED COMPOSITE WING STRUCTURES CONFIGURATIONS
S. Stammel¹, C. Bisagni¹; ¹Politecnico di Milano, Italy
09. Sep 24 14:55 15:20 11.2.2
0666
SEMI-ANALYTICAL SENSITIVITY METHODS FOR AEROELASTIC SHAPE OPTIMIZATION
G.M. Gagliardi¹, M.D. Kulkarni, Embry-Riddle Aeronautical University, United States; F. Marulo¹; ¹University of Naples Federico II, Italy
09. Sep 24 15:20 15:45 11.2.3
0071
ABSOLUTE NODAL COORDINATE FORMULATION FOR NONLINEAR MULTIBODY MODELING OF FLARED HINGED WINGS
K. Otsuka, Tohoku University, Japan; C.W. Cheng¹, R. Palacios¹; ¹Imperial College London, United Kingdom
09. Sep 24 15:45 16:10 11.2.4
0375
OPTIMIZATION DESIGN OF MULTI-SCALE ACTIVE COOLING STRUCTURE FOR AIRCRAFT
P. Xu¹, Q.-X. Mu¹, W.-N. Zhang¹; ¹AVIC Shenyang Aircraft Design and Research Institute, China
12.2Experimental Aeroelasticity 1
Chair(s): Ricci, S., Toffol, F.
Track 12 Petrarca
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
09. Sep 24 14:30 14:55 12.2.1
0728
COMPUTATIONAL/EXPERIMENTAL AEROELASTIC STUDY FOR AN ALL-MOVABLE HORIZONTAL TAIL WITH TORSION FREE-PLAY
X.-Y. Ai, China; X.-Y. Chen, China; W.-J. Wang, China; J. Liu, China; X.-J. Ran, China; W. Qian, China
09. Sep 24 14:55 15:20 12.2.2
0423
NUMERICAL AND EXPERIMENTAL RESEARCH ON AEROELASTICITY OF HIGH-ASPECT-RATIO WINGS
J. Liu¹, W. Qian¹, X. Hu¹, X. Ai¹, X. Ran¹; ¹Dalian University of Technology, China
09. Sep 24 15:20 15:45 12.2.3
0054
W-WING AEROELASTIC DEMONSTRATOR DESIGN MODIFICATION AND UPGRADE
J. Cecrdle¹, O. Vich¹, J. Starek¹, J. Vlach¹, M. Kolar¹, M. Smid¹; ¹Czech Aerospace Research Centre (VZLU), Czech Republic
09. Sep 24 15:45 16:10 12.2.4
0140
MEASUREMENT OF WING BENDING IN-FLIGHT FROM A T67 SLINGSBY FIREFLY LIGHT AIRCRAFT
N.J. Lawson, The University of Sydney, Australia; G. Zhao¹, S.C. Place¹, R.A. Harrison¹; ¹Cranfield University, United Kingdom
13.2Combustion Heat Transfer 2
Chair(s): Orisamolu, W.
Track 13 Boccaccio
05 - Propulsion
09. Sep 24 14:30 14:55 13.2.1
0712
SUSTAINABLE FUELS SAFETY BOUNDARIES DEMARCATION METHOD
T. Qiu¹, S. Bao¹, S. Ding, Civil Aviation University of China, China; Q. Ma¹, X. Wang¹, C. Gan¹; ¹Beihang University, China
Presenter: Shengyu Bao, Beihang University
09. Sep 24 14:55 15:20 13.2.2
0720
EFFECTS OF SHAPE AND STREAMWISE SPACING OF PIN-FINS ARRAYS ON FLOW AND HEAT TRANSFER
L.W. Li¹, T.L. Dong¹, W.T. Ji¹, J.M. Wu¹; ¹Xi'an Jiaotong University, China
09. Sep 24 15:20 15:45 13.2.3
1012
MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR
L. Zhang, China; T.-T. Jing, China; X. Sun, China; T. Gao, China; Z. Xu, China; F. Qin, China
09. Sep 24 15:45 16:10 13.2.4
0323
NUMERICAL SIMULATION OF HEAT TRANSFER IN MINIATURE RADIALLY ROTATING SODIUM/POTASSIUM HEAT PIPES
G. Li, Tianmushan Laboratory, China; Y. Zhang¹, G. Zhang, Beihang University Research Institute of Aero-Engine, China; S. Huang¹, S. Ding, Civil Aviation University of China, China; ¹Beihang UniversitySchool of Energy and Power Engineering, China
14.2Human Factors 1
Chair(s): Chimetto, P., DeCrescenzio, F.
Track 14 Puccini
10 - Safety and Security
09. Sep 24 14:30 14:55 14.2.1
0089
VALIDATING ASSUMPTIONS ABOUT PILOT RECOGNITION: A PCM-BASED APPROACH FOR AIRCRAFT CERTIFICATION SAFETY ASSESSMENT PROCESS
D.M.C. de Lima¹, D.C. Fernandes¹, M.M. Cardoso Junior¹; ¹Aeronautical Institute of Technology, Brazil
09. Sep 24 14:55 15:20 14.2.2
0279
THE IMPACT OF PIEZOELECTRIC STACK HEATING ON AIRCRAFT DEICING
L. Yuan¹, B. Miao¹, K. Yan¹, C.L. Zhu¹; ¹Nanjing University of Aeronautics and Astronautics, China
09. Sep 24 15:20 15:45 14.2.3
0848
HANDLING QUALITIES RATING SCALE: THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION
M.D. Turazza¹, J.P.C.A Macedo ¹, J.H. Bidinotto¹; ¹EESC/USP, Brazil
09. Sep 24 15:45 16:10 14.2.4
0955
CLASSIFICATION OF COGNITIVE LOAD BASED ON THE PILOT’ VISUAL SCAN PATTERNS
J. Yao, China; Y. Lu, China; Z. Zhong, China; S. Fu, China
15.2Flight Controller Design 1
Chair(s): Shaferman, V.
Track 15 Carducci
06.1 - Flight Dynamics and Control (Control & Modelling)
09. Sep 24 14:30 14:55 15.2.1
0008
LINEAR QUADRATIC PURSUIT AND EVASION DIFFERENTIAL GAME GUIDANCE STRATEGY WITH OBSTACLE AVOIDANCE
X. Wang¹, M. Yang¹, P. Ma¹, T. Chao¹; ¹Harbin Institute of Technology, China
09. Sep 24 14:55 15:20 15.2.2
0043
LEARNING-BASED FULL-ENVELOPE AUTOPILOT DESIGN BASED ON THE KOOPMAN OPERATOR THEORY
Y. Lee¹, J. Kim¹, Y. Kim¹; ¹Seoul National University, South Korea
09. Sep 24 15:20 15:45 15.2.3
0601
INTEGRATING POST-OPTIMAL SENSITIVITIES INTO SUPERVISED TRAINING OF NEURAL NETWORKS
J. Diepolder¹, J.Z. Ben-Asher¹; ¹Technion, Israel
09. Sep 24 15:45 16:10 15.2.4
1044
PREDICTIVE CONTROL DRIVEN TACTICAL MANEUVERING
J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic
Presenter: Jiří Novák, Brno University of Technology
additional information (interactive) 15.2.R
0828
PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT
M. Shin¹, M.-J. Tahk¹, B. Kim¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea
additional information (interactive) 15.2.R
1182
CONTROL ALLOCATION FOR A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT USING DIFFERENTIAL THRUST
C. Döll¹, S. Waitman¹; ¹ONERA, France
16.2UAV Control Systems 2
Chair(s): Munjulury, R., Grabowski, T.
Track 16 Raffaello
06.2 - Flight Dynamics and Control (UAV related)
09. Sep 24 14:30 14:55 16.2.1
0029
HYBRID MODELING APPROACH FOR OPTIMIZATION BASED CONTROL OF MULTIROTOR UNMANNED AERIAL VEHICLES
J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic
09. Sep 24 14:55 15:20 16.2.2
0294
MEDIAL AXIS TRANSFORMATION-BASED CONVEX MODEL PREDICTIVE CONTROL FOR MULTIROTOR INDOOR AUTONOMOUS FLIGHT WITH FIXED ALTITUDE
H.J. Ahn¹, H.C. Bang¹; ¹KAIST, South Korea
09. Sep 24 15:20 15:45 16.2.3
0653
AERODYNAMIC MODEL IDENTIFICATION OF A VTOL TAILSITTER UAV USING SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS
H.-S. Lee¹, D.-W. Lee¹, H.-C. Bang¹; ¹KAIST, South Korea
09. Sep 24 15:45 16:10 16.2.4
0013
ROBUST SLIDING MODE CONTROL FOR UAV FORMATION WITH EXTERNAL DISTURBANCES UNDER EVENT-TRIGGERED STRATEGY
L.H. Wang¹, A.J. Li¹, C.Q. Wang¹, Z. Yury, Samara National Research University, Russia; ¹Northwestern Polytechnical University, China
17.2Energy Supply and Management
Chair(s): Peters, M.
Track 17 Galileo
07 - Systems, Subsystems and Equipment
09. Sep 24 14:30 14:55 17.2.1
0085
SMART ELECTRIC POWER MANAGEMENT ONBOARD FUTURE AIRCRAFT
F. Cuomo¹, C. Musto¹, S. Bozhko, University of Nottingham, United Kingdom; B. Guida, Aeromechs srl, Italy; ¹Leonardo Aircraft, Italy
Presenter: Beniamino Guida, Aeromechs srl
09. Sep 24 14:55 15:20 17.2.2
0270
DESIGNING A HARDWARE-IN-THE-LOOP SIMULATION TEST BED FOR AIRCRAFT ENERGY MANAGEMENT APPLICATIONS
A. Dell’Amico, Linköping University, Sweden
09. Sep 24 15:20 15:45 17.2.3
1072
DUAL STAGE BATTERY SIZING AND PERFORMANCE ASSESSMENT ON-BOARD HYBRID ELECTRIC AIRCRAFT
A. Wise¹, S. Bozhko¹, S. Yeoh¹, S. Sumsurooah¹, C. Manrique, Leonardo S.p.A, Italy; ¹University of Nottingham, United Kingdom
09. Sep 24 15:45 16:10 17.2.4
1205
PRELIMINARY ASSESSMENT FOR STRUCTURAL BATTERY COMPONENTS
G. di Mauro¹, M. Guida¹, G. Olivares², L.M. Gomez², R. Turco¹, R. Tesser¹, S. Mallardo¹, G. Santagata¹, P. Russo¹; ¹Università degli Studi di Napoli Federico II, Italy ;²Jerry Moran Center for Advanced Virtual Engineering & Testing (A, United States
Presenter: Michele Guida, Università degli Studi di Napoli Federico II

16:00 - 16:30BREAK

1.3GSA - Aircraft Concepts & Demonstrations 2
Chair(s): Dubois, S.
Track 1 Auditorium
15 - Guest lectures
09. Sep 24 16:30 17:00 1.3.1
1324
CLEAN AVIATION SHORT MEDIUM RANGE AIRCRAFT CONCEPT
K. Mokaddem, AIRBUS, France
09. Sep 24 17:00 17:30 1.3.2
1254
TOWARDS ZERO CLIMATE IMPACT AVIATION
G. Llewellyn, Airbus, United Kingdom
09. Sep 24 17:30 18:00 1.3.3
1314
ACCELERATING THE CLEAN FUTURE OF FLIGHT
G Teofili, ZeroAvia, United Kingdom
09. Sep 24 18:00 18:30 1.3.4
1271
PANEL DISCUSSION
PD D,
2.3Hydrogen Aircraft 3
Chair(s): Schmollgruber, P., Nicolosi, F.
Track 2 Sala Verde
01.2 - Aircraft Design and Integrated System (Applications)
09. Sep 24 16:30 17:00 2.3.1
0503
CONCEPTUAL AIRCRAFT DESIGN OF A RESEARCH BASELINE WITH DIRECT LIQUID HYDROGEN COMBUSTION
M. Kotzem¹, S. Wöhler¹, T. Burschyk¹, C. Hesse¹, S. Hellbrück¹, T. Zill¹; ¹German Aerospace Center (DLR), Germany
09. Sep 24 17:00 17:30 2.3.2
1060
DESIGN OPTIMISATION OF A BOUNDARY LAYER INGESTION PROPULSOR FOR A MULTI-FUEL HYDROGEN AIRCRAFT
A. Battiston¹, A. Magrini¹, R. Ponza¹, E. Benini¹, B. Türkyilmaz², A. Seitz², A. Heidebrecht, TU Delft, Netherlands; ¹hit09, Italy ;²Bauhaus Luftfahrt, Germany
Presenter: Andrea Battiston, hit09
09. Sep 24 17:30 18:00 2.3.3
1078
MODELLING HYDROGEN FUEL CELL AIRCRAFT IN SUAVE
C. Svensson¹, P. Miltén¹, T. Grönstedt¹; ¹Chalmers University of Technology, Sweden
09. Sep 24 18:00 18:30 2.3.4
1207
PRELIMINARY DESIGN OF A FULL ELECTRIC GENERAL AVIATION AIRCRAFT POWERED WITH FUEL CELL: A CASE STUDY.
G. Cafiero¹, P.J. Comunian¹, A. Lerro¹, F. Ponti², A.N. Damiani Ferretti²; ¹Politecnico di Torino, Italy ;²Università di Bologna, Italy
3.3Novel Design and Analysis 1
Chair(s): Gibson, T.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
09. Sep 24 16:30 17:00 3.3.1
0346
LARGE LANGUAGE MODEL-DRIVEN SIMULATIONS FOR SYSTEM OF SYSTEMS ANALYSIS IN FIREFIGHTING AIRCRAFT CONCEPTUAL DESIGN
J.L. Lovaco¹, R.C. Munjulury¹, I. Staack, Technische Universität Braunschweig, Germany; P. Krus, Linköping University, Sweden; ¹Saab Aeronautics & Linköping University, Sweden
09. Sep 24 17:00 17:30 3.3.2
0611
DATA-DRIVEN MULTI-RANGE MISSION-BASED OVERALL AIRCRAFT CONCEPTUAL DESIGN OPTIMIZATION
L.J. Liu¹, D. Kim, Ecole Nationale de l’Aviation Civile, France; C. Reyner¹, R.P. Liem¹; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China
09. Sep 24 17:30 18:00 3.3.3
0803
CANCELED - ADVANCING ENGINEERING SOLUTIONS THROUGH LARGE LANGUAGE MODELS: A CASE STUDY
E.A. Moura¹, P. Krus, Linköping University, Sweden; R.G.A. Silva¹, L.C.S. Goes¹, A.A. Paula¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
Presenter: Petter Krus, Fluid and Mechatronic Systems/Linköping University
09. Sep 24 18:00 18:30 3.3.4
0626
A DISTRIBUTED UMDO ARCHITECTURE BASED ON SURROGATE MODELS FOR LAUNCH VEHICLE DESIGN
Y. Liu¹, C.N. Li¹, C.L. Gong¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 3.3.R
1036
AIRFOIL PRESSURE PREDICTION BASED ON PHYSICS-INFORMED DEEP LEARNING APPROACH
J.Z. Li¹, Y.J. Yang¹, Y.F. Zhang¹; ¹School of Aerospace Engineering, Tsinghua University, China
4.3System of Systems 2
Chair(s): Prakasha, P., Knöös-Franzen, L.
Track 4 Brunelleschi
02 - Systems Engineering and Integration
09. Sep 24 16:30 17:00 4.3.1
1258
NAVIGATING COMPLEXITY: ADAPTING AEROSPACE DEVELOPMENT IN A DYNAMIC WORLD
C. Jouannet, Saab Aeronautics, Sweden
09. Sep 24 17:00 17:30 4.3.2
0729
MODELING CARGO DEMAND FOR REGIONAL AIR TRANSPORT NETWORKS IN CANADA AND THE UNITED STATES
M.M. Alexiev¹, R.E. Perez¹, P.W. Jansen¹, J.C.-H. Wang, Ribbit Inc., Canada; ¹Royal Military College of Canada, Canada
09. Sep 24 17:30 18:00 4.3.3
0343
RESEARCH ON UNMANNED CLUSTER RECONNECTION DECISION-MAKING METHOD CONSIDERING RESOURCE SUPPLEMENTATION
M. Yao¹, X. Wang¹, L. Kong, Chinese Aeronautical Establishment, China; G. Fu¹, X. Wang¹, J. Yao¹; ¹School of Reliability and Systems Engineering, Beihang Universit, China
Presenter: Mengfei Yao, School of Reliability and Systems Engineering, Beihang Universit
09. Sep 24 18:00 18:30 4.3.4
0554
FROM ONTOLOGY TO SYSTEM ARCHITECTURE: AN MBSE APPROACH TOWARD THE REALIZATION OF URBAN AIR MOBILITY
S. Sinha Roy¹, Y. Huang¹, D. Bekdache¹, T.-Y. Fung¹, B. Beck¹, C. Guariniello¹, D. DeLaurentis¹; ¹Purdue University, United States
Presenter: Daniel DeLaurentis, Purdue University
additional information (interactive) 4.3.R
0962
EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN
Y.-Z. Wang¹, B.-L. Shang¹, P.-F. Li¹, W.-Z. Liu¹, R.-X. Lin¹, K.-A. Xing¹, Y.-T. Deng¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
5.3Applied CFD 3
Chair(s): Prince, S., Azevedo, J.L.
Track 5 Donatello
03.1 - Aerodynamics – CFD Methods and Validation
09. Sep 24 16:30 17:00 5.3.1
0506
IDENTIFICATION METHOD OF LONGITUDINAL COEFFICIENTS BASED ON THE NUMERICAL STUDY OF THE FLOW TOPOLOGY AROUND THE SACCON GEOMETRY
B. Isnard¹, G. Tanguy¹, D. Farcy¹, E. Garnier¹, J.-M. Foucault, LMFL, France; ¹ONERA, France
09. Sep 24 17:00 17:30 5.3.2
0537
AERODYNAMIC CHARACTERISTICS RESEARCH OF A DISTRIBUTED PROPULSION AIRCRAFT
S. Chen¹, Z. Guo¹, G. Jia¹, D. Liu¹; ¹National University of Defense Technology, China
09. Sep 24 17:30 18:00 5.3.3
0904
HYDRODYNAMIC ANALYSIS OF STATIC WATER IMPACT ON WEDGE-SHAPED HULL WATERTIGHT TEST SPECIMEN THROUGH NUMERICAL ANALYSIS
M. Niu, Northwestern Polytechnical University, China; F. Sun, Xi'an Modern Control Technology Research Institute, China; C. Du, AVIC XAC COMMERCIAL AIRCRAFT CO., LTD., China; H. Huang, Northwestern Polytechnical University/Aircraft Strength Reserch , China
09. Sep 24 18:00 18:30 5.3.4
0579
ON THE AERODYNAMIC CHARACTERISTICS OF CRESCENT WING
D.F. Kurtulus¹, B. Anilir¹, D. Raymer, Conceptual Research Corporation, United States; ¹METU, Turkey
additional information (interactive) 5.3.R
0035
A NUMERICAL VIRTUAL FLIGHT PLATFORM DEVELOPMENT AND ITS APPLICATION ON HIGH MANEUVERABILITY FLIGHT VEHICLES
H. Qiao¹, F. Qin¹, S. Deng¹; ¹Nanjing University of Aeronautics and Astronautics, China
additional information (interactive) 5.3.R
0197
APPLICATION OF CONVOLUTIONAL NEURAL NETWORKS IN DETERMINING THE VELOCITY AND PRESSURE FIELDS AROUND AIRFOIL MODELS
G. Sharma¹, T.H. Tran, Le Quy Don Technical University, Vietnam; J. Tanimoto¹; ¹Kyushu University, Japan
6.3Multiphase Flows
Chair(s): Gowree, E., Post, M.
Track 6 Cimabue
03.3 - Basic Fluid Dynamics and Flow Control
09. Sep 24 16:30 17:00 6.3.1
0176
VALIDATION OF MULTIPHASE FLOW SIMULATIONS BY EXPERIMENTAL MEASUREMENTS IN A CHANNEL FLOW
M. Khaled¹, B. Faraji-Tajrishi¹, A. Herrgen, MTU Aero Engines AG, Germany; B. Weigand¹; ¹Institute of Aerospace Thermodynamics, University of Stuttgart, Germany
09. Sep 24 17:00 17:30 6.3.2
0788
STUDY OF THE SCAVENGE PUMP PERFORMANCE FOR TWO-PHASE FLOW IN AN AIRCRAFT ENGINE LUBRICATION SYSTEM
N. Wu¹, J.-P. Hu¹, Y.-G. Lyu¹, J. Wang¹, Y. Tan¹, Z.-X. Liu¹; ¹Northwestern Polytechnical University, China
09. Sep 24 17:30 18:00 6.3.3
0934
STUDY OF DROPLET MOTION AND WATER FILM FLOW CHARACTERISTICS ON SUPERHYDROPHOBIC SURFACES UNDER AIRFLOW SHEARING
H. Zhao¹, D. Zhu¹, S. Wang², S. Chang², L. Yu¹, Y. Wu¹; ¹AVIC Aerodynamics Research Institute, China ;²Beihang University, China
09. Sep 24 18:00 18:30 6.3.4
0969
EXPERIMENTAL SETUP FOR THE INVESTIGATION OF WATER SEPARATION IN ANNULAR FLOW WITHIN A CIRCULAR CHANNEL
R. Haidl¹, B. Weigand¹; ¹Institute of Aerospace Thermodynamics, University of Stuttgart, Germany
additional information (interactive) 6.3.R
0817
EXPERIMENTAL STUDY ON MULTI-ATTITUDE OIL SUPPLY STRUCTURE
Y. Xu¹, Y.-G. Lyu¹, J.-P. Hu¹, Z. Liu¹; ¹Northwestern Polytechnical University, China
7.3IFAR Wildfire / disaster response
Chair(s): Andreeva Mori, A.
Track 7 Botticelli
15 - Guest lectures
09. Sep 24 16:30 17:00 7.3.1
1259
ENHANCING PUBLIC GOOD MISSIONS AND DISASTER RESPONSE WITH ADVANCED AERIAL TECHNOLOGY: OPPORTUNITIES AND CHALLENGES
A. Andreeva-Mori, Japan Aerospace Exploration Agency (JAXA), Japan; D. Sziroczák, Budapest University of Technology and Economics (BME), Hungary; G. Schwoch, German Aerospace Center (DLR), Germany; M.C.R. Murça, Aeronautics Institute of Technology (ITA), Brazil; B. Dziugiel, Lukasiewicz Research Network – Institute of Aviation (ILOT), Poland; J. Homola, National Aeronautics and Space Administration (NASA), United States; V. Kramar, VTT Technical Research Centre of Finland, Finland
09. Sep 24 17:00 17:30 7.3.2
1281
NASA RESEARCH TO EXPAND UAS OPERATIONS FOR DISASTER RESPONSE
K. Ellis¹, M. Johnson¹, N. Neogi¹, J. Homola¹; ¹NASA, United States
09. Sep 24 17:30 18:00 7.3.3
1280
ON-GOING WILDLAND FIRE WORK AT THE NATIONAL RESEARCH COUNCIL OF CANADA WITH A FOCUS ON THE USE OF COTS RPAS FOR REDUCTION OF NON-FIRE PILOT WORKLOAD
G. Leblanc¹, G. Ifimov¹, M. Kalacska², O. Lucanus², J.P. Arroyo-Mora¹, J. Gorman¹, M. Wheatley, Ontario Ministry of Natural Resources and Forestry, Canada; C. McFayden, Natural Resources Canada, Canada; ¹National Research Council of Canada (NRC), Canada ;²Applied Remote Sensing Laboratory, McGill University, Canada
8.3Airframe Aerodynamics 1
Chair(s): Rudnik, R.
Track 8 Vasari
03.4 - Applied Aerodynamics
09. Sep 24 16:30 17:00 8.3.1
0047
MORPHING LEADING-EDGE TUBERCLES ON CESSNA 172 WING
G. Abate¹, H.P. Monner¹; ¹German Aerospace Center (DLR), Germany
09. Sep 24 17:00 17:30 8.3.2
0319
ON THE CHALLENGES OF SURROGATE-BASED AERODYNAMIC SHAPE OPTIMISATION
J. Rasines¹, D. Verstraete¹; ¹The University of Sydney, Australia
09. Sep 24 17:30 18:00 8.3.3
0691
AERODYNAMIC ANALYSIS OF CAMBER MORPHING AIRFOILS USING PARTICLE IMAGE VELOCIMETRY AND COMPUTATIONAL FLUID DYNAMICS METHODS
M. Marciniuk¹, L. Kiszkowiak², P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; L. Malicki¹, K. Strzelecka¹, K. Sibilski², S. Kachel²; ¹Wroclaw University of Science and Technology, Poland ;²Military University of Techology, Poland
09. Sep 24 18:00 18:30 8.3.4
0859
ENGINEERING-BASED TOOL FOR THREE-DIMENSIONAL ESTIMATIONS OF RE-ENTRY VEHICLES AEROTHERMODYNAMICS
P.E. Di Nuzzo, Italy; M. Maione¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy
Presenter: Maria Maione, Department fo Engineering, University fo Campania "L. Vanvitell
additional information (interactive) 8.3.R
0158
MODELLING ASTEROID TRAJECTORY IN EARTH’S ATMOSPHERE
R.H. Morais¹, L.F. Ferreira Marques, ISEC, Portugal; A. Resende Rodrigues da Silva¹, R. Melicio, LAETA-IDMEC, Instituto Superior Técnico, Universidade de Lisboa, Portugal; ¹LAETA-AEROG, Universidade da Beira Interior, Portugal
additional information (interactive) 8.3.R
0639
AERO-KINEMATIC OPTIMIZATION OF HIGH-LIFT DEVICES WITH DOWNWARD DEFLECTION OF SPOILER
C. Wei¹, C. Rao¹, L. Yang¹, T. Zhang¹; ¹Aerodynamics Research Institute, China
9.3AAM 2 - Airspace Integration
Chair(s): Li, M., Maroney, D.
Track 9 Giotto
09 - Air Transport System Efficiency
09. Sep 24 16:30 17:00 9.3.1
1059
ADVANCED HUMAN MACHINE INTERFACES FOR DRONE MONITORING: ASSESSMENT OF THE TECHNOLOGICAL FRAMEWORK FOR THE DESIGN OF AN AUGMENTED REALITY INTERFACE
S. Bagassi¹, T. Fadda¹, M. Corsi¹; ¹University of Bologna, Italy
09. Sep 24 17:00 17:30 9.3.2
0347
CORUS-XUAM: TACKLING URBAN AIR MOBILITY AIRSPACE INTEGRATION CHALLENGES
G. Riccardi¹, L. Brucculeri¹, E. Fornaciari, d-flight, Italy; M. D'Onofrio, Techno Sky, Italy; A. Zilli², D. Leanza², G. Ferrara, Eurocontrol, France; M. Molinario³, G. Esposito³, A. Favier, Pipistrel, Italy; ¹ENAV S.P.A, Italy ;²DTA, Italy ;³NAIS, Italy
Presenter: Giancarlo Ferrara, EUROCONTROL
09. Sep 24 17:30 18:00 9.3.3
1133
AI-ASSISTED DESIGN OF UAV DOCKING STATION NETWORK FOR DUAL USE PURPOSES
A. Avi¹, G. Quaranta¹, A. Valentini, Fondazione Bruno Kessler, Italy; ¹Politecnico di Milano, Italy
09. Sep 24 18:00 18:30 9.3.4
0835
LOW-ALTITUDE INTEGRATED AIRSPACE OPERATIONS OF AIRCRAFT FLYING UNDER VISUAL FLIGHT RULES: THE VERTICAL DIMENSION
A. Andreeva-Mori¹, K. Ohga¹, K. Kobayashi¹; ¹Japan Aerospace Exploration Agency (JAXA), Japan
10.3Low Speed Aerodynamics
Chair(s): Fusaro, R., Zingg, D.
Track 10 Leonardo
03.1 - Aerodynamics – CFD Methods and Validation
09. Sep 24 16:30 17:00 10.3.1
0243
NUMERICAL SIMULATION STUDY ON THE INFLUENCE OF WING SPACING OF DRAGONFLY-INSPIRED FLAPPING WINGS
Y. Luo, China; L. Wang, China; J. Wang, China; X. Lang, China; X. Yang, China
09. Sep 24 17:00 17:30 10.3.2
0463
COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A DIRECT AIR CAPTURE FILTER SYSTEM
M. Panagopoulos¹, N.J. Lawson¹, D.M. D’Alessandro¹, E. Kearns¹; ¹University of Syndey, Australia
09. Sep 24 17:30 18:00 10.3.3
0812
DESIGN OF DUAL-FUSELAGE FLIGHT PLATFORM FOR JET CONTROL FUNCTION VERIFICATION
C.P. Li, China; G. Zhang, China; N. Liu, China; Y. Zhang, China; L. Xu, China; M. Wang, China
11.3Structural Design and Optimization 2
Chair(s): Ikeda, T., De Gaspari, A.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
09. Sep 24 16:30 17:00 11.3.1
0874
AEROELASTIC ISSUES IN THE DESIGN OF HIGH ASPECT RATIO STRUT-BRACED WING AIRCRAFT
E. Roncolini¹, F. Toffol ¹, S. Ricci¹; ¹Politecnico di Milano, Italy
09. Sep 24 17:00 17:30 11.3.2
0389
DYNAMIC BUCKLING ANALYSIS OF THIN-SHELL COMPOSITE STRUCTURES BASED ON ISOGEOMETRIC ANALYSIS
H. Qiu¹, Y. Guo¹, Z. Guan¹, H. Zhu¹, Y. Pan¹; ¹Nanjing University of Aeronautics and Astronautics, China
09. Sep 24 17:30 18:00 11.3.3
0651
EFFICIENT AEROSTRUCTURAL DESIGN OPTIMIZATION COMBINING GRADIENT-ENHANCED KRIGING WITH COUPLED ADJOINT METHOD
H.-J. Guo, China; Z.-H. Han, China; C.-Z. Xu, China; K.-S. Zhang, China; W.-P. Song, China; J.-Q. Luo, China
09. Sep 24 18:00 18:30 11.3.4
1162
BIRD AND DRONE IMPACT DAMAGE PROGNOSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT ENGINE
H. Raza¹, P. Vaghela¹, E. Stumpf, RWTH Aachen, Germany; J. Bayandor¹; ¹University at Buffalo, United States
12.3Aerodynamic Instrumentation and Measurement 1
Chair(s): Benner, M.
Track 12 Petrarca
03.2 - Experimental Aerodynamics
09. Sep 24 16:30 17:00 12.3.1
0757
DESIGN OF MEASUREMENT SETUP FOR HIGH-ALTITUDE IN-FLIGHT EXPERIMENTS ON DU89-134/14 AIRFOIL AT LOW REYNOLDS NUMBER
M. Avirovic¹, C. Brunelli¹, K. Wykes², C. Mengdehl², B.G. Marinus¹, J. Degroote, University of Ghent, Belgium; J. Van Beeck, Von Karman Institute for Fluid Dynamics, Belgium; ¹Royal Military Academy, Belgium ;²Stemme Belgium, Belgium
09. Sep 24 17:00 17:30 12.3.2
0456
UPGRADE OF THE VTI T-38 BLOWDOWN TRISONIC TEST FACILITY: WIND TUNNEL CONTROL SYSTEM
B. Ilic¹, G. Ocokoljic¹, M. Samardžic¹, J. Isakovic, Academy of Applied Technical Studies, Serbia; ¹Military Technical Institute, Serbia
09. Sep 24 17:30 18:00 12.3.3
0070
SURFACE VISUALISATION OF TIME AVERAGED FLOW BEHAVIOUR AROUND RIGID AND FLEXIBLE HEMISPHERES UTILISING UV SENSITIVE OIL
N. Menakath¹, N.J. Lawson¹, G.A. Vio, Defence Science and Technology Group, Australia; ¹The University of Sydney, Australia
09. Sep 24 18:00 18:30 12.3.4
0023
HOT-WIRE ANEMOMETRY OF THE BOUNDARY LAYER PRIOR TO A CAVITY IN RESPONSE TO VARIED UPSTREAM GEOMETRY
C.O.L. Hamilton Smith¹, N.J. Lawson¹; ¹The University of Sydney, Australia
additional information (interactive) 12.3.R
0218
REVITALIZATION OF A FLOW-CELL DEVICE FOR AIR INTAKE TESTING AND ITS INTEGRATION WITH WIND TUNNEL SYSTEMS
D. Damljanovic¹, D. Vukovic¹, L. Petrovic¹; ¹Military Technical Institute, Serbia
13.3Combustion Heat Transfer 3
Chair(s): Mari, C.
Track 13 Boccaccio
05 - Propulsion
09. Sep 24 16:30 17:00 13.3.1
1129
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF NOISE GENERATION IN HYDROGEN AND METHANE-HYDROGEN LAMINAR FLAMES
F.G. Schiavone¹, M. Durand², M. Torresi¹, S.M. Camporeale¹, T. Schuller², D. Laera¹; ¹Polytechnic University of Bari, Italy ;²Institut de Mécanique des Fluides de Toulouse, France
09. Sep 24 17:00 17:30 13.3.2
0341
AN EXPERIMENTAL SIMULATION ON THE INFLUENCE OF DIFFERENT FILM COOLING HOLE SHAPES ON PARTICLE DEPOSITION ON TURBINE VANE
Z. Liu¹, R. Ruan¹, L. Cheng¹, Y. Zhang¹, Z. Liu¹, D. Wu¹; ¹Northwestern Polytechnical University, China
09. Sep 24 17:30 18:00 13.3.3
0708
FUEL CONSUMPTION MONITORING OF TURBOPROP ENGINE
J. Juracka¹, Z. Hubnerova¹; ¹Brno University of Technology, Czech Republic
14.3Hybrid Electric Concepts: H2 Architectures
Chair(s): Bezos OConnor, G.
Track 14 Puccini
05 - Propulsion
09. Sep 24 16:30 17:00 14.3.1
1003
ASSESSING THE TECHNICAL VIABILITY OF ALL-ELECTRIC HYDROGEN-POWERED AIRCRAFTS
P. Marocco¹, M.C. Massaro¹, A.H.A. Monteverde¹, M. Santarelli¹; ¹Politecnico di Torino, Italy
09. Sep 24 17:00 17:30 14.3.2
1103
MODELLING A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE
A. Johansson¹, P. Miltén¹, A. Lundbladh, GKN Aerospace, Sweden; C. Xisto¹; ¹Chalmers University of Technology, Sweden
09. Sep 24 17:30 18:00 14.3.3
0432
CFD-BASED SCOUTING FOR THE DESIGN OF A MULTI-FUEL KEROSENE/HYDROGEN ATMOSPHERIC BURNER
L. Palanti¹, L. Mazzei¹, C. Bianchini¹, S. Link², K. Dave², F. De Domenico², A.G. Rao²; ¹Ergon Research, Italy ;²TU Delft, Netherlands
09. Sep 24 18:00 18:30 14.3.4
0261
MODELLING AND INITIAL ASSESSMENT OF A FUEL CELL AUXILIARY PROPULSION AND POWER UNIT
M.G. Kolb¹, A. Seitz¹, B. Türkyilmaz¹, Y. Ma¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
15.3Flight Controller Design 2
Chair(s): Campos, L.
Track 15 Carducci
06.1 - Flight Dynamics and Control (Control & Modelling)
09. Sep 24 16:30 17:00 15.3.1
0892
DOWNRANGE CONTROL GUIDANCE FOR REENTRY BURN OF REUSABLE LAUNCH VEHICLE
K.-W. Jung¹, C.-H. Lee¹; ¹KAIST, South Korea
09. Sep 24 17:00 17:30 15.3.2
1166
EXPLICIT MODEL FOLLOWING TRAJECTORY CONTROL SYSTEM FOR MULTIPLE VERTICAL TAKEOFF AND LANDING CONFIGURATIONS
A. Comer¹, I. Chakraborty¹; ¹Auburn University, United States
09. Sep 24 17:30 18:00 15.3.3
0839
CONVEX PROGRAMMING APPROACH OF ROBUST POWERED DESCENT GUIDANCE THROUGH DYNAMIC TUBE MPC
J.-I. Jang¹, C.-H. Lee¹, S. He, BIT, China; ¹KAIST, South Korea
09. Sep 24 18:00 18:30 15.3.4
0185
SYSTEM ARCHITECTURE AND EVALUATION METHOD OF HUMAN-MACHINE COLLABORATION IN FLIGHT CONTROL SYSTEM
J. Che¹, X. Chen¹, S. Che, Northwestern Polytechnical University, China; J. Li¹, Z. Sun¹; ¹Flight Automatic Control Research Institute, AVIC, China
additional information (interactive) 15.3.R
0805
PILOT INDUCED OSCILLATIONS AND FLIGHT PHASES IDENTIFICATION OF THE SPACE SHUTTLE AND TRANSPORT AIRPLANES
S. Kolb, CREA, France
additional information (interactive) 15.3.R
1119
A NOLINEAR MODEL PREDICTIVE CONTROL METHOD FOR AIRBREATHING HYPERSONIC VEHICLE BASED ON KOOPMAN OPERATOR
C.R. Li¹, W.Q. Li¹, Y. Li¹, S. Tang¹; ¹Northwestern Polytechnical University, China
16.3UAV Navigation and Path Planning
Chair(s): Kwiek, A., Krus, P.
Track 16 Raffaello
06.2 - Flight Dynamics and Control (UAV related)
09. Sep 24 16:30 17:00 16.3.1
0897
HARDWARE-IN-THE-LOOP SIMULATION FRAMEWORK FOR THE EVALUATION OF AUTONOMOUS FLIGHT FUNCTIONS
D. Pla Guerrero¹, A. Hegde¹, J. Wan, Flanders Make, Belgium; E. Allegaert¹, Y. Lemmens¹; ¹Siemens Digital Industries Software, Belgium
Presenter: Elias Allegaert, Siemens Digital Industries Software
09. Sep 24 17:00 17:30 16.3.2
0610
FLIGHT CONTROL SYSTEM KNOWLEDGE GRAPH CONSTRUCTION BASED ON AERONAUTICAL DOMAIN KNOWLEDGE AUGMENTED LARGE LANGUAGE MODEL
Y. Fan, China; Y. Sun, China; B. Mi, China
09. Sep 24 17:30 18:00 16.3.3
1020
AN UAV MANEUVERING DECISION-MAKING ALGORITHM BASED ON DEEP TRANSFER REINFORCEMENT LEARNING
K. Li¹, K. Zhang¹, H. Liu², Y. Li², Q. Wang¹; ¹Northwestern Polytechnical University, China ;²Shenyang Aircraft Design and Research Institute, China
additional information (interactive) 16.3.R
0664
AUTONOMOUS LANDING OF A QUADROTOR ON A MOVING TARGET WITH OCCLUSION AVOIDANCE MANEUVER
D. Kim¹, H.J. Kim¹; ¹Seoul National University, South Korea
additional information (interactive) 16.3.R
0972
ULTRA-LOW-ALTITUDE PENETRATION PATH PLANNING FOR FIXED-WING AIRCRAFT BASED ON NMP ALGORITHM
H.-X. Huang¹, D.-B. Li¹, P.-Y. Qi¹, Y.-X. Shang¹; ¹beihang university, China
additional information (interactive) 16.3.R
1209
AN OPTICAL FLOW BASED GUIDANCE ALGORITHM FOR A QUADROTOR UAV MOVING INSIDE CIRCULAR CORRIDORS
A. Bagherzadeh¹, F. Saghafi¹; ¹Sharif University of Technology, Iran
17.3Sensors and Test Rig Design
Chair(s): Stumpf, E.
Track 17 Galileo
07 - Systems, Subsystems and Equipment
09. Sep 24 16:30 17:00 17.3.1
0056
HYBRID AIR DATA SYSTEM ARCHITECTURE: FROM DESIGN TO FLIGHT TEST VERIFICATION
M. Rovelli¹, A. Brandl¹, S. Di Bitonto¹, F. Di Donfrancesco¹, E. Maruccia¹, I. Viglietti¹, D. Marchetti¹; ¹Leonardo, Italy
09. Sep 24 17:00 17:30 17.3.2
0171
DEVELOPMENT AND TESTING OF AN ACTUATION SYSTEM FOR A MORPHING CONTROL SURFACE
M. Schäfer¹, R. Keimer¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany
09. Sep 24 17:30 18:00 17.3.3
0483
PRELIMINARY ANALYSIS OF TEMPERATURE EFFECTS AND MANEUVER-INDUCED DEFORMATIONS ON FBG OPTIC FIBER INTEGRATED SYSTEMS
A. Aimasso¹, M. Bertone¹, C. Ferro¹, M.D.L. Dalla Vedova¹, P. Maggiore¹; ¹Politecnico di Torino, Italy
09. Sep 24 18:00 18:30 17.3.4
0737
NUMERICAL METHOD FOR DESIGNING AND MODELING AN EXHAUST CLUSTER FOR A SMALL TURBOJET ENGINE TEST CELL
T.-G. Nguyen¹, Q.-H. Nghiem¹, P.-M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam

Tuesday, 10. Sep 2024


0.4ICAS IFAR LECTURE Air Traffic Management as a key for sustainable aviation Speakers: Bruno Sainjon, ONERA FR, Antonio Blandini, CIRA IT, Markus Fischer, DLR GE, Robert A. Pearce, NASA USA, Reginald Tan, A*STAR SIN, Michel Peters, NLR NL
Chair: G. Holmberg ICAS Executive Committee Member
10. Sep 24 08:30 09:30

09:30 - 10:00BREAK

1.4GSA - Regional Fuel Flexible and Hybrid Flight Demos (Lessons Learned)
Chair(s): Jankovsky, A., Bezos O Connor, G.
Track 1 Auditorium
15 - Guest lectures
10. Sep 24 10:00 10:30 1.4.1
1242
FUEL CELL BASED POWERTRAINS
J. Ludvik, Honeywell, United States
10. Sep 24 10:30 11:00 1.4.2
1266
CLEAN AVIATION HIGH VOLTAGE NETWORK AND DEMONSTRATION
R. Foley, RTX/Collins, United States
10. Sep 24 11:00 11:30 1.4.3
1303
P&W APPROACH TO SUSTAINABILITY
J-M Thomassin, Pratt & Whitney Canada, Canada
10. Sep 24 11:30 12:00 1.4.4
1321
PANEL DISCUSSION: ADDITONAL: SUSAN YING, ERIKA HOLTZ, GABRIELE TEOFILI, DAVID SERCOMBE
D. P.,
2.4Progress toward BWB Concept Test and Development
Chair(s): Collier, F.
Track 2 Sala Verde
15 - Guest lectures
10. Sep 24 10:00 10:30 2.4.1
1292
OBJECTIVES OF THE UNITED STATES FULL SCALE BLENDED WING BODY FLIGHT DEMONSTRATION
F. Collier, NASA (LaRC), United States
10. Sep 24 10:30 11:00 2.4.2
1293
TECHNICAL APPROACH FOR A BWB AIRLINER TO MEET MARKET DEMANDS
M. Page, JetZero, United States
10. Sep 24 11:00 11:30 2.4.3
1294
TECHNICAL FINDINGS TO DATE TO SUPPORT MARKET DEMANDS OF A BWB AIRLINER
M. Page, JetZero, United States
10. Sep 24 11:30 12:00 2.4.4
1295
GROUND AND SCALED FLIGHT TEST PLANS TO SUPPORT DEVELOPMENT OF A BWB AIRLINER
M. Page, JetZero, United States
10. Sep 24 12:00 12:30 2.4.5
1296
PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS
J. Ahuja¹, C. Perron¹, R.D.B. Rivera¹, J.C. Tai¹, D.N. Mavris¹; ¹Georgia Tech, United States
Reserve Paper 2.4.R
1319
PERFORMANCE COMPARISON OF THE BLENDED WING BODY AND TUBE AND WING CONFIGURATIONS EXTRA
J. Tai, Georgia Tech, United States
3.4MDAO
Chair(s): Nagel, B.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
10. Sep 24 10:00 10:30 3.4.1
0687
ROBUST SCHUR-COMPLEMENT SOLVERS AND LARGE-SCALE MULTIDISCIPLINARY DESIGN OPTIMIZATION
M.A.S. Abdul-Kaiyoom¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States
10. Sep 24 10:30 11:00 3.4.2
0285
PROCESSES, METHODS AND TOOLS SUPPORTING THE DEVELOPMENT OF AERONAUTICAL SYSTEMS
L. Boggero¹, J. Bussemaker¹, G. Donelli¹, F. Torrigiani¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
10. Sep 24 11:00 11:30 3.4.3
0059
MDAX : ENHANCEMENTS IN A COLLABORATIVE MDAO WORKFLOW FORMULATION TOOL
S. Garg¹, J.H. Bussemaker¹, L. Boggero¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
10. Sep 24 11:30 12:00 3.4.4
0825
SURROGATE-ASSISTED HIERARCHICAL OPTIMIZATION METHOD FOR VARIABLE SWEEP FLIGHT VEHICLE TRAJECTORY
N.-H. Ye¹, T. Long¹, B. Fu, Xi’an Modern Control Technology Research Institute, China; R.-H. Shi, Beijing Institute of Technology Chongqing Innovation Center, China; ¹Beijing Institute of Technology, China
10. Sep 24 12:00 12:30 3.4.5
0496
RAPID DESIGN OF UNCONVENTIONAL AIRCRAFT USING SOFTWARE TOOLS COUPLED IN OPTIMIZATION LOOP – LESSONS LEARNED
T. Goetzendorf-Grabowski¹, A. Kwiek¹, J. Mieloszyk, ?ukasiewicz Research Network – Institute of Aviation, Poland; A. Tarnowski¹; ¹Warsaw University of Technology, Poland
4.4MBSE
Chair(s): Prakasha, P.
Track 4 Brunelleschi
02 - Systems Engineering and Integration
10. Sep 24 10:00 10:30 4.4.1
0076
REQUIREMENTS UNCERTAINTY PROPAGATION IN CONCEPTUAL DESIGN USING BAYESIAN NETWORKS
A. Spinelli¹, A. Sharma, Centre for Aeronautics, Cranfield University, United Kingdom; T. Kipouros¹; ¹Centre for Propulsion and Thermal Power, Cranfield University, United Kingdom
10. Sep 24 10:30 11:00 4.4.2
0318
APPLICATION OF SYSML IN THE DEVELOPMENT OF AIRCRAFT CABIN HEALTH MANAGEMENT
A. Hechelmann¹, T. Mannchen¹; ¹Baden-Wuerttemberg Cooperative State University (DHBW) Ravensbur, Germany
10. Sep 24 11:00 11:30 4.4.3
0510
AUTOMATION OF ENGINEERING INTEROPERABILITY FOR AIRCRAFT SYSTEM DESIGN
F. During¹, R.C. Munjulury¹, R. Hällqvist, System Simulation and Concept Development, Saab Aeronautics, Sweden; ¹FLUMES, Linköping University, Sweden
10. Sep 24 11:30 12:00 4.4.4
0860
AUTOMATIC SYSTEM REQUIREMENTS VERIFICATION FOR THE MBSE-ORIENTED AIRCRAFT DESIGN PROCESS
A. Dagna¹, S. Centomo², E. Brusa¹, C. Delprete¹, R. Gentile²; ¹Politecnico di Torino, Italy ;²Leonardo LABS, Leonardo S.p.A., Italy
10. Sep 24 12:00 12:30 4.4.5
1139
AN MBSE ENABLED MDAO APPROACH FOR THE CONCEPTUAL DEVELOPMENT OF COMPLEX SYSTEMS
M. Fouda¹, L. Willrodt¹, H. Almeida¹, J. Cortez¹, O. Hussein¹, F. Castaneda¹, H. Dhouib¹, C. Dahik¹, V. Drouet¹, R. Brook¹; ¹Capgemini Engineering, Germany
Presenter: Mahmoud Fouda, Capgemini Engineering
additional information (interactive) 4.4.R
0603
A MODEL BASED SYSTEM ENGINEERING APPROACH TOWARDS AIRCRAFT DIGITAL CERTIFICATION
C. Mirabella¹, M. Tuccillo¹, P. Della Vecchia¹; ¹Università degli Studi Federico II, Italy
additional information (interactive) 4.4.R
0843
A SEMANTIC MODEL-BASED SYSTEMS ENGINEERING APPROACH FOR SUPERSONIC BUSINESS JET CONCEPTUAL DESIGN
Z. Cui¹, M. Luo¹, J. Lu¹, J. Wang¹; ¹Beihang University, China
5.4Supersonic and Hypersonic Aircraft 1
Chair(s): Melkert, J.
Track 5 Donatello
01.2 - Aircraft Design and Integrated System (Applications)
10. Sep 24 10:00 10:30 5.4.1
1251
BREAKING THE SOUND BARRIER: ACHIEVING QUIET SUPERSONIC FLIGHT OVER LAND
P. Coen, United States
10. Sep 24 10:30 11:00 5.4.2
0064
DUAL-STREAM JET NOISE TEST WITH INTERNAL MIXER DESIGN VARIATIONS FOR LTO NOISE OF SUPERSONIC AIRCRAFT
R. Habing¹, M.-J. Van der Meulen¹, M. Huet, ONERA / DAAA, France; R. Jaron, DLR, Germany; F. Petrosino², M. Barbarino², O. Zaporozhets, Institute of Aviation, Poland; ¹NLR, Netherlands ;²CIRA, Italy
10. Sep 24 11:00 11:30 5.4.3
0820
THE FUTURE OF CIVIL SUPERSONIC TRANSPORT IN EUROPE: THE SENECA AND MORE&LESS PROJECTS
R. Jaron, DLR, Germany; N. Viola, Politecnico di Torino, Italy
10. Sep 24 11:30 12:00 5.4.4
0566
POTENTIAL OF THE RANGE EXTENSION OF SUPERSONIC TRANSPORT
Z. Lei, SUWA UNIVERSITY OF SCIENCE, Japan
10. Sep 24 12:00 12:30 5.4.5
1032
ESATTO: THE HOLISTIC FRAMEWORK TO SUPPORT THE DESIGN OF SUSTAINABLE SUPERSONIC AVIATION
R. Fusaro¹, G. Piccirillo¹, D. Ferretto¹, G. Saccone, Italian Aerospace Research Center, Italy; D. Bodmer², J. Jäschke², M. Cremaschi, ENVISA, Italy; N. Viola¹; ¹Politecnico di Torino, Italy ;²Hamburg University of Technology, Germany
Reserve Paper 5.4.R
0597
AERODYNAMIC DESIGN OF A SUPERSONIC TRANSPORT CONFIGURATION CONSIDERING AVERAGE LOUDNESS IN THE WHOLE BOOM CARPET
Q. Chen¹, Z.-H. Han¹, J.-L. Qiao¹, Y.-L. Ding¹, K.-S. Zhang¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China
Presenter: Qing Chen, Northwestern Polytechnical University
6.4Transition Modeling
Chair(s): Coder, J., Halila, G.
Track 6 Cimabue
03.1 - Aerodynamics – CFD Methods and Validation
10. Sep 24 10:00 10:30 6.4.1
0081
TRANSITION MODELING IN SUPPORT OF CFD VISION 2030 - HIGHLIGHTS OF RECENT EFFORTS AT THE NASA LANGLEY RESEARCH CENTER
M. Choudhari¹, E. Beyak¹, N. Hildebrand¹, F. Li¹, E. Vogel¹, P. Paredes, National Institute of Aerospace, United States; V. Srivastava², B. Venkatachari²; ¹NASA Langley Research Center, United States ;²Analytical Mechanics Associates, United States
10. Sep 24 10:30 11:00 6.4.2
1179
EVALUATION OF CFD TRANSITION MODELING FOR TRANSONIC, NATURAL-LAMINAR-FLOW DESIGN
J.G. Coder, Pennsylvania State University, United States
10. Sep 24 11:00 11:30 6.4.3
0327
ON THE CHOICE OF TURBULENCE MODEL FOR THE SIMULATION OF AIRFOILS AT REYNOLDS NUMBER BELOW 200,000
S. Shahjahan¹, B. Emmerson¹, D. Verstraete¹; ¹The University of Sydney, Australia
10. Sep 24 11:30 12:00 6.4.4
0354
FLUIDODYNAMIC ANALYSIS OF LOW REYNOLDS NUMBER FLOWS
N. Verde, Italy; F. Capoluongo, Italy; P. Catalano, CIRA, Italy; G. Pezzella, University of Campania , Italy; A. Viviani, University of Campania, Italy
Presenter: Giuseppe Pezzella, Department of Engineering, University of Campania \"L. Vanvit
10. Sep 24 12:00 12:30 6.4.5
0681
BOUNDARY-LAYER SUCTION AND AERODYNAMIC SHAPE OPTIMIZATION FOR HYBRID LAMINAR FLOW CONTROL ON A FIN
H. Wu¹, W. Song¹, H. Nie¹, Z. Han¹; ¹National Key Laboratory of Aircraft Configuration Design, China
additional information (interactive) 6.4.R
1144
CANCELED - BOUNDARY LAYER TRANSITION AND RE-LAMINARIZATION IN MACH 6 NOZZLE OF A SHOCK TUNNEL–A NUMERICAL STUDY
S. Malekipour¹, M. Mohammadi-Amin¹, I. Bahman-Jahromi¹; ¹Aerospace Research Institute, Iran
Presenter: Shahed Malekipour, ARI
7.4empty
Chair(s): ,
Track 7 Botticelli
8.4Airframe Aerodynamics 2
Chair(s): Rivers, M.
Track 8 Vasari
03.4 - Applied Aerodynamics
10. Sep 24 10:00 10:30 8.4.1
0677
FINITE-STATE AEROELASTIC MODELLING OF MORPHING WING THROUGH UNSTEADY LIFTING-LINE THEORY
R. Giansante¹, G. Bernardini¹, M. Gennaretti¹; ¹Roma Tre University, Italy
10. Sep 24 10:30 11:00 8.4.2
0189
DECOUPLING STORE AND PARENT AERODYNAMICS FOR FAST PREDICTION OF SUBSONIC STORE TRAJECTORIES
N. Mthembu¹, H. Ndlovu¹, B. Ndebele¹, K. Jamison¹, L. Zwane¹; ¹CSIR, South Africa
Presenter: Ndumiso Mthembu, CSIR
10. Sep 24 11:00 11:30 8.4.3
0370
WIND-TUNNEL TESTS OF INNOVATIVE TAILPLANE CONFIGURATIONS
F. Nicolosi¹, P. Della Vecchia¹; ¹University of Naples Federico II, Italy
10. Sep 24 11:30 12:00 8.4.4
0679
FAST PREDICTION OF PRESSURE DISTRIBUTION FOR 3D CONFIGURATION BASED ON LARGE LANGRAGE MODEL
B.W. Shu, Northwestern Polytechnical University, China; Z.H. Gao, China; J.T. Huang, China; X. Chen, China; W. Zhang, China; H. Zhao, China
Presenter: Hua Zhao, Northwestern Polytechnical University
10. Sep 24 12:00 12:30 8.4.5
0605
RESEARCH ON AERODYNAMIC DESIGN OF ENGINE NACELLE UNDER THE INFLUENCE OF PROPELLER SLIPSTREAM FOR THE TURBOPROP AIRCRAFT
R.-F. Xu¹, W.-P. Song¹, X.-H. Li², R.-Z. Qian², Y.-J. Zhang², J.-H. Xu¹, X.-L. Li¹; ¹Northwestern Polytechnical University, China ;²AVIC The First Aircraft Institute, China
Presenter: Xin-Long Li, Northwestern Polytechnical University
additional information (interactive) 8.4.R
0551
LONG-WAVE INSTABILITY OF AIRCRAFT WAKE VORTEX UNDER SHEAR CROSSWIND
Z. Xu¹, D. Li¹, J. Cai¹, J. Han, N, China; ¹Northwestern Polytechnical University School of Aeronautics, China
9.4ERC
Chair(s): Symeonidis, G.
Track 9 Giotto
15 - Guest lectures
10. Sep 24 10:00 10:30 9.4.1
1226
EUROPEAN RESEARCH COUNCIL (ERC) - FUNDING OPPORTUNITIES AND REPRESENTATIVE PROJECT HIGHLIGHTS
G. Symeonidis, European Research Council Executive Agency (ERCEA), Belgium
10. Sep 24 10:30 11:00 9.4.2
1239
TOWARDS A FIRST-PRINCIPLE BASED QUANTITATIVE DESCRIPTION OF TURBULENCE WITHOUT THE NEED FOR ADHOC MODELS
T.M. Schneider, EPFL, Switzerland
10. Sep 24 11:00 11:30 9.4.3
1234
METAMATERIALS FOR CONTROL OF FLUID FLOWS
M. Kotsonis, Delft University of Technology, Netherlands
10. Sep 24 11:30 12:00 9.4.4
1232
THERMOACOUSTIC INSTABILITY IN AERO-ENGINE COMBUSTORS
A. Morgans, United Kingdom
10. Sep 24 12:00 12:30 9.4.5
1230
NABUCCO TAKE-OFF: MULTI-STABLE PANELS FOR AN ADAPTIVE WING
C. Bisagni, Politecnico di Milano, Italy
10.4Impact
Chair(s): Filippi, M., Kanerva, M.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
10. Sep 24 10:00 10:30 10.4.1
0841
HIGH TEMPERATURE BALLISTIC IMPACT TEST TECHNOLOGY BASED ON ELECTROMAGNETIC LAUNCH
C. Zhang¹, J. Liu¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
10. Sep 24 10:30 11:00 10.4.2
1111
IMPACT TOLERANCE OF CERAMIC MATRIX COMPOSITES FOR AEROSPACE APPLICATIONS
G. Janszen¹, A.M. Caporale¹, L. Cavalli, Petroceramics S.p.A., Italy; M. De Stefano Fumo, CIRA, Italy; A. Airoldi¹; ¹Politecnico di Milano, Italy
10. Sep 24 11:00 11:30 10.4.3
0878
INFLATABLE SPACE SHIELD STRUCTURE FOR SPACE HABITATION MODULE
J.-H. Cha, Chosun Uni., South Korea
10. Sep 24 11:30 12:00 10.4.4
0461
CANCELED - DAMAGE CHARACTERISTICS AND MECHANISM OF CARBON FIBER REINFORCED COMPOSITES IMPACTED BY HIGH-SPEED WATERJETS
Y. Li, School of Aeronautics, Northwestern Polytechnical University, China; N. Hou¹, X. Wang¹; ¹School of Civil Aviation, Northwestern Polytechnical University, China
10. Sep 24 12:00 12:30 10.4.5
0748
DAMAGE AND MECHANICAL REPAIR OF COMPOSITE LAMINATES: EFFECTS OF EMBEDDED DEFECTS AND LOW VELOCITY IMPACTS
G. Zhang, China; M. Tong, China; B. Yan, China; F. Wang, China; H. Zhang, China
Presenter: Guijia Zhang
Reserve Paper 10.4.R
1006
IMPACT RESPONSES AND FAILURE MECHANISMS OF ALMGB14 UNDER DYNAMIC LOADS
Y. Lu¹, W. Wang¹, Y. Zhang, Hangzhou Zhiyuan Research Institute, China; Z. Zhang, Northwest Institute of Mechanical and Electrical Engineering, China; ¹Northwestern Polytechnical University, China
Presenter: YANYAN LU, School of Aeronautics, Northwestern Polytechnical University
11.4Vibrations and Damping
Chair(s): Rade, D., Pecora, R.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
10. Sep 24 10:00 10:30 11.4.1
0814
DETECTION OF DELAMINATIONS IN DAMAGED COMPOSITE PLATES VIA LOCAL DAMAGE RESONANCE APPROACH
F. Nicassio¹, A.P. Fontanella², M. Cinefra², G. Scarselli¹; ¹University of Salento, Italy ;²Politecnico of Bari, Italy
10. Sep 24 10:30 11:00 11.4.2
0832
FREE VIBRATIONS OF CYLINDRICAL SHELLS WITH CUTOUTS BY A SINGLE-DOMAIN RITZ FORMULATION
A. Milazzo, University of Palerrmo, Italy; M. Lo Cascio, University of Palermo, Italy
10. Sep 24 11:00 11:30 11.4.3
0365
LARGE-SCALE STRUCTURAL DYNAMIC TOPOLOGY OPTIMIZATION DESIGN FOR AIRCRAFT VIBRATION REDUCTION UNDER RANDOM EXCITING RESPONSE
S. Xiao¹, L.-Y. Liu¹, H.-M. Xue¹, M.-Q. Wang¹, D.-Y. Chen¹; ¹AVIC Shenyang Aircraft Design and Research Institute, China
Presenter: Huimin Xue, AVIC Shenyang Aircraft Design and Research Institute
10. Sep 24 11:30 12:00 11.4.4
1106
ACTIVE CONTROL DAMPING WITH THE USE OF VOICE COIL ACTUATORS
G. Cardellino¹, T. Melz¹, R. Feldmann¹, C. Adams, Technical University of Graz, Austria; F. Franco², G. Petrone², S. De Rosa²; ¹Technical University of Darmstadt, Germany ;²Universitä degli Studi di Napoli Federico II, Italy
10. Sep 24 12:00 12:30 11.4.5
0905
ANALYTICAL STUDY ON HYDROSTATIC RESPONSE CHARACTERISTICS DURING WATER LANDINGS OF AMPHIBIOUS AIRCRAFT
F. Sun, Xi'an Modern Control Technology Research Institute, China; Y.-H. Zheng¹, S.-S. Zhu¹; ¹Northwestern Polytechnical University, China
12.4Trajectory Planning and Weather
Chair(s): Reynolds, T., Mori, R.
Track 12 Petrarca
09 - Air Transport System Efficiency
10. Sep 24 10:00 10:30 12.4.1
1247
TOWARDS SUSTAINABLE AVIATION WITH EFFICIENT AIRSPACE OPERATIONS
W.J. Coupe¹, S. Saxena¹; ¹NASA Ames Research Center, United States
Presenter: William Coupe
10. Sep 24 10:30 11:00 12.4.2
0137
COMPARING CONVECTIVE WEATHER IMPACTS ON AIR TRAFFIC MANAGEMENT OPERATIONS IN UNITED STATES, CANADA & EUROPE
G. Enea¹, T. Reynolds¹, J. Venuti¹, T. Polishchuk², V. Polishchuk², A. Lemetti², A. Lau³, J. Solzer³, T. Bölle³; ¹MIT Lincoln Laboratory, United States ;²Linköping University, Sweden ;³German Aerospace Center (DLR), Germany
10. Sep 24 11:00 11:30 12.4.3
0380
RELATIONSHIPS BETWEEN AIRCRAFT ROUTES AND TURBULENCE-RELATED WEATHER DATA
Y. Nakamura¹, A. Senoguchi¹; ¹Electronic Navigation Research Institute, Japan
Presenter: Yoichi Nakamura, Electronic Navigation Research Institute
10. Sep 24 11:30 12:00 12.4.4
0406
ROUTE PLANNING FOR VOLCANIC ASH AND RADIOACTIVITY IN-SITU DRONE MEASUREMENTS USING A GENETIC ALGORITHM AND KRIGING
K.A. Buchtal¹, A. Lau¹, D. Ebert², J. Richters², K. Schneiders²; ¹German Aerospace Center (DLR), Institute of Air Transport, Germany ;²German Weather Service (DWD), Radioactivity Monitoring, Germany
10. Sep 24 12:00 12:30 12.4.5
0950
INTEGRATING ECO-EFFICIENT FLIGHT PLANNING IN AIRCRAFT CONCEPTUAL DESIGN: MINIMAL NOX ROUTES FOR HIGH-SPEED AIRCRAFT USING HYDROGEN
F. Borgna¹, V. Borio¹, R. Fusaro¹, N. Viola¹, G. Saccone, Italian Aerospace Research Centre (CIRA), Italy; ¹Politecnico di Torino, Italy
13.4Propellers, Fans, Compressors 1
Chair(s): Mogilka, P.
Track 13 Boccaccio
05 - Propulsion
10. Sep 24 10:00 10:30 13.4.1
0135
ON THE WATER ENHANCED TURBOFAN CONCEPT: PART B – FLOW PATH AND MASS ASSESSMENT
J. Häßy¹, A. Görtz¹, M. Schmelcher¹, J. Schmeink¹, M. El-Soueidan¹; ¹DLR, Germany
10. Sep 24 10:30 11:00 13.4.2
0157
DESIGN AND ANALYSIS OF A SCALED COMPOSITE UHBR FAN BLADE FOR WIND TUNNEL TESTS
B.A.T. Noordman¹, W.J. Vankan¹; ¹Royal Netherlands Aerospace Centre, Netherlands
10. Sep 24 11:00 11:30 13.4.3
0199
ON THE WATER ENHANCED TURBOFAN CONCEPT: PART A - THERMODYNAMICS AND OVERALL ENGINE DESIGN
A. Görtz¹, J. Häßy¹, M. Nickl², A. Lessis², M. Schmelcher¹, M. El-Soueidan¹; ¹German Aerospace Center, Germany ;²Bauhaus Luftfahrt e.V., Germany
10. Sep 24 11:30 12:00 13.4.4
0263
UNSTEADY AERODYNAMICS OF A COUPLED COMPACT INTAKE-FAN IN CROSSWIND
L. Lobuono¹, D. MacManus¹, R. Christie¹, L. Boscagli¹; ¹Cranfield University, United Kingdom
10. Sep 24 12:00 12:30 13.4.5
0272
KNOWLEDGE-BASED TURBINE DISK MODELING – A CONCEPTUAL DESIGN PROCESS CALIBRATED TO THE NASA ENERGY EFFICIENT ENGINE
P. Wehrel¹, J. Schmeink¹, J. Häßy¹; ¹German Aerospace Center (DLR), Germany
14.4Hybrid Electric Regional Aircraft Concepts
Chair(s): Bezos OConnor, G., Jankovsky, A.
Track 14 Puccini
05 - Propulsion
10. Sep 24 10:00 10:30 14.4.1
0153
STUDY OF HYBRIDISATION SCENARIOS FOR TURBOPROP AIRCRAFT IN THE GENERAL AVIATION SEGMENT
F. Lutz¹, J. Jézégou¹, M. Budinger², A. Reysset²; ¹ISAE-SUPAERO, France ;²INSA Toulouse, France
10. Sep 24 10:30 11:00 14.4.2
1125
INSTRUMENTATION OF A SUBESCALE GROUND EFFECT VEHICLE, VOLITAN, TO MEASURE FLIGHT PROPULSION EFFICIENCY
C. Fischer, 1Instituto Federal de São Paulo and Aeronautics Institute of Tec, Germany; M.A.R. Diaz¹, L. Souza¹, R.G.A. da Silva¹, L.C.S. Goes¹; ¹Aeronautics Institute of Technology, Brazil
10. Sep 24 11:00 11:30 14.4.3
1109
A SENSITIVITY ANALYSIS ON THE ENDURANCE EQUATION FOR HYBRID-ELECTRIC AIRCRAFT
A. Batra¹, R. Raute, Dept. Ind. Elec. Eng. University of Malta, Malta; R. Camilleri¹; ¹INSTITUTE OF AEROSPACE TECHNOLOGIES (IAT), UNIVERSITY OF MALTA, Malta
10. Sep 24 11:30 12:00 14.4.4
1069
DESIGN APPROACH FOR HYBRID ELECTRIC PROPULSION CONCEPTS OF MID-RANGE AIRCRAFT INCLUDING SUSTAINABLE AVIATION FUELS
K. Ziaja¹, D. Lieder², J. Göing², J. Friedrichs², F. di Mare¹; ¹Ruhr University Bochum, Germany ;²Technische Universität Braunschweig, Germany
10. Sep 24 12:00 12:30 14.4.5
0161
HYDROGEN-POWERED SOLID OXIDE FUEL CELL - GAS TURBINE SYSTEM FOR AERONAUTICAL APPLICATION
D. Kierbel¹, T. Neuland¹, P.-E. Roux¹, P. Nehter¹, J. Hollmann², C.N. Dagli², P. Köhler², S. Kabelac², A.G. Rao³, F. de Domenico³, M. Hoogreef³, L. Van Biert³, F. Yin³, C. Rossignol*, L. Dessemond*, M.C. Steil*, P. Maasº, F. Winterº, C. Warschº, S.S. Ventura, German Aerospace Center, Germany; ¹AIRBUS SAS, Germany ;²Leibniz University Hannover, Germany ;³Technische Universiteit Delft, Netherlands ;*Univ. Grenoble Alpes, Univ. Savoie Mont Blanc, France ;ºBauhaus Luftfahrt e.V., Germany
Presenter: Pascal Köhler, Leibniz University of Hanover, Germany
15.4Structural Modelling
Chair(s): Carrera, E., Bayandor, J.
Track 15 Carducci
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
10. Sep 24 10:00 10:30 15.4.1
0360
REDESIGN OF AN AERONAUTICAL COMPOSITE STIFFENED PANEL WITH THE DOUBLE-DOUBLE DESIGN APPROACH
A. Riccio¹, A. Garofano¹, G. Rigliaco¹, M. Boccaccio², F. Acerra²; ¹University of Campania “Luigi Vanvitelli”, Italy ;²Leonardo S.p.A., Italy
10. Sep 24 10:30 11:00 15.4.2
0252
MACRO, MESO AND MICRO SCALE ENERGY EVALUATION IN LAMINATED AND COMPOSITE STRUCTURES USING THE COMPONENT-WISE APPROACH
S. Saputo¹, R. Augello¹, E. Carrera, Germany; ¹Department of Aeronautics and Aerospace Engineering, Politecnico, Italy
10. Sep 24 11:00 11:30 15.4.3
0032
ELECTROMAGNETIC INDUCTION HEATING OF TP-CFRP LAMINATES: FEM MODELLING AND VALIDATION
W.J. Vankan¹, N. van Hoorn¹, A.J. de Wit¹, T.P.A. Koenis¹; ¹NLR, Netherlands
10. Sep 24 11:30 12:00 15.4.4
0250
ON AN EFFICIENT GLOBAL/LOCAL STOCHASTIC METHODOLOGY FOR FAILURE PREDICTION OF AIRCRAFT COMPOSITE STRUCTURES
P. Minigher, INEGI / University of Porto / University of Girona, Italy; A. Arteiro¹, A. Turon, University of Girona, Spain; J. Fatemi, Airbus NL, Netherlands; S. Guinard, Airbus SAS, France; L. Barrière, Saint Exupéry, France; P.P. Camanho¹; ¹INEGI / University of Porto, Portugal
10. Sep 24 12:00 12:30 15.4.5
0393
FATIGUE CRACK LIFE PREDICTION BASED ON BAYESIAN DYNAMIC UPDATE
Y. Zhang, China; Y. Ning, China; B. Wang, China; H. Peng, China
16.4Advanced Maintenance Data Management
Chair(s): Raddatz, F., Stamoulis, K.
Track 16 Raffaello
11 - Operations and Sustainment
10. Sep 24 10:00 10:30 16.4.1
0198
THE JOURNEY TOWARDS CONDITION-BASED MAINTENANCE: A FRAMEWORK FOR THE HORIZONTAL TAIL ACTUATOR OF AN ADVANCED JET TRAINER AIRCRAFT
L. Baldo¹, A. De Martin¹, M. Terner, Leonardo S.p.A. Aircraft Division, Italy; M. Sorli¹; ¹DIMEAS, Politecnico di Torino, Italy
10. Sep 24 10:30 11:00 16.4.2
0657
HOLISTIC AND SCALABLE SMART OPTIMIZATION FRAMEWORK FOR PRESCRIPTIVE MAINTENANCE
A. Giacotto¹, A.C. Pereira Mesquita¹, H. Costa Marques¹, A. Martinetti, University of Twente, Netherlands; ¹ITA, Brazil
10. Sep 24 11:00 11:30 16.4.3
0993
HYDROGEN TANKERING: TOOLS FOR ECONOMIC AND ENVIRONMENTAL IMPACT SCENARIO STUDIES
G. Sirtori¹, L. Trainelli¹, Z. Lahmam¹; ¹DAER, Politecnico di Milano, Italy
10. Sep 24 11:30 12:00 16.4.4
0367
AN EMPIRICAL AND CUSTOMISABLE FLEET RENEWAL MODEL FOR PROSPECTIVE SCENARIOS USING OPEN-ACCESS DATA
P. Viry¹, T. Planès¹, S. Delbecq¹, L. Joly, ISAE-SUPAERO, Université de Toulouse, France; A. Salgas¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France
10. Sep 24 12:00 12:30 16.4.5
0159
A NOVEL DEEP MULTIMODAO INFORMATION FUSION MODEL FOR AERO-ENGINE STATE PREDICTION
Y. Huang¹, G. Sun¹, J. Tao¹, J. Feng¹; ¹Fudan University, China
additional information (interactive) 16.4.R
0165
DIGITALISATION AND SUSTAINABILITY IN CABIN DESIGN: SYNERGIES AND DEPENDENCIES
M.C. Berschik¹, S. Wehrend¹, F.N. Laukotka¹, D. Krause¹; ¹Hamburg University of Technology, Germany
17.4Systems Safety Aspects
Chair(s): Stumpf, E.
Track 17 Galileo
07 - Systems, Subsystems and Equipment
10. Sep 24 10:00 10:30 17.4.1
0037
CANCELED - RESEARCH ON FATIGUE LIFE OF HEAT EXCHANGER BASED ON STRESS SIMULATION
L. Hu¹, Y.-L. Han, Nanjing University of Aeronautics and Astronautics, China; F. Meng¹; ¹Nanjing Engineering Institute of Aircraft Systems, China
Presenter: Liang Hu, Nanjing Engineering Institute of Aircraft Systems
10. Sep 24 10:30 11:00 17.4.2
0149
HYDROGEN SAFETY: A COMPARATIVE ANALYSIS OF LEAK DETECTION SENSORS
O. Petrella¹, A. Martucci¹, P. Caruso¹, L. Travascio¹, A. Vozella¹; ¹CIRA, Italy
Presenter: Pasquale Caruso, CIRA
10. Sep 24 11:00 11:30 17.4.3
0678
VIBRATION ANAYLYSIS AND INFLUENCING FACTOR STUTY OF HELICOPTER HYDRAULIC PIPELINNE
S. Yang¹, S. Huang¹, Y. Wang¹, Y.-P. Huang¹; ¹CHRDI, China
10. Sep 24 11:30 12:00 17.4.4
0178
SENS4ICE EU PROJECT HYBRID ICE DETECTION ARCHITECTURES DEMONSTRATION RESULTS
C.W. Schwarz¹, C. Deiler¹, J. Lucke¹, T. Jurkat-Witschas¹, A. Orazzo², B. Thillays²; ¹DLR, Germany ;²Safran Aerosystems, France
10. Sep 24 12:00 12:30 17.4.5
0046
FLIGHT TEST RESULTS FOR PERFORMANCE-BASED ICE DETECTION
C. Deiler, DLR, Germany

12:30 - 13:30LUNCH

0.5GENERAL LECTURE 3: Marco Ferrogalini: Airbus DDMS - the digital transformation program enabling Airbus to pioneer sustainable aerospace for a safe and united world
Chair: R. Gerhards ICAS Executive Committee Member
10. Sep 24 13:30 14:30

1.5GSA - Aerodynamic Technology
Chair(s): Vijgen, P.
Track 1 Auditorium
15 - Guest lectures
10. Sep 24 14:30 14:55 1.5.1
1231
APPLICATION OF LAMINAR FLOW CONTROL FOR ENHANCED PERFORMANCE AND REDUCED EMISSIONS
J. Crouch, Boeing, United States
10. Sep 24 14:55 15:20 1.5.2
1298
HIGH ASPECT RATION WING CONCEPTS
P. Schmollgruber, ONERA, France
10. Sep 24 15:20 15:45 1.5.3
1246
RIBLETS IN AVIATION- FIRST EVER INDUSTRIALIZATION WITH AEROSHARK
J.U. Müller, Lufthansa, Germany
10. Sep 24 15:45 16:10 1.5.4
1273
Q&A - MINI PANEL
QA A,
2.5X-57
Chair(s): Borer, N., Schultz, V.
Track 2 Sala Verde
15 - Guest lectures
10. Sep 24 14:30 14:55 2.5.1
1287
THE NASA X-57 “MAXWELL” DISTRIBUTED ELECTRIC PROPULSION FLIGHT DEMONSTRATOR PROJECT
H. Maliska, NASA, United States
10. Sep 24 14:55 15:20 2.5.2
1288
X-57 TRACTION POWER AND COMMAND SYSTEMS DEVELOPMENT
S. Clarke¹, J. Terry¹, K. Harris¹, D. Avanesian¹; ¹NASA, United States
10. Sep 24 15:20 15:45 2.5.3
1289
FLIGHT PERFORMANCE ESTIMATES FOR THE NASA X-57 DISTRIBUTED ELECTRIC PROPULSION FLIGHT DEMONSTRATOR
N. Borer, NASA, United States
10. Sep 24 15:45 16:10 2.5.4
1290
DISTRIBUTED THRUST TAKEOFF FOR THE NASA X-57 MOD IV FLIGHT DEMONSTRATOR
N.K. Borer¹, R.D. Wallace², J.R. Reynolds², D.E. Cox¹, C. Sales², T.L. Williams², W.M. Ringelberg²; ¹NASA Langley Research Center, United States ;²NASA Armstrong Flight Research Center, United States
3.5Novel Design and Analysis 2
Chair(s): Bagassi, S.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
10. Sep 24 14:30 14:55 3.5.1
0431
DATA-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION AND MULTI-FIDELITY DESIGN EXPLORATION USING CONDITIONAL DIFFUSION-BASED GEOMETRY SAMPLING METHOD
A. Yang¹, J. Zhang, Shanghai Artificial Intelligence Laboratory, China; J. Li, Institute of High Performance Computing, A*STAR, Singapore; R. Liem¹; ¹Hong Kong University of Science and Technology, Hong Kong SAR of China
Presenter: Aobo Yang, Hong Kong University of Science and Technology
10. Sep 24 14:55 15:20 3.5.2
0484
LATENT SPACE CORRELATION FOR INTERPRETABLE AIRFOIL PARAMETERIZATION USING VARIATIONAL AUTOENCODERS
K. Swannet¹, C. Varriale¹, N.A.K. Doan¹; ¹Delft University of Technology, Netherlands
10. Sep 24 15:20 15:45 3.5.3
0561
RESEARCH ON MULTI-ATTRIBUTE DECISION MAKING AND VERIFICATION METHODS FOR SYSTEMS CONFRONTATION
Y. Tong¹, M. Luo¹, Z. Cui¹, Z. Liu¹, Z. Ji¹; ¹Beihang University, China
10. Sep 24 15:45 16:10 3.5.4
0625
EXPLORATION OF EFFICIENT HYPERPARAMETERS ADAPTION OF SUPPORT VECTOR REGRESSION FOR AERODYNAMIC DESIGN
K.-S. Zhang¹, H.-L. Qiao¹, P.-H. Wang¹, Y.-Q. Du¹, Z.-H. Han¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
4.5Hybrid Aircraft Power System
Chair(s): Padulo, M.
Track 4 Brunelleschi
01.1 - Aircraft Design and Integrated System (Basics and Theory)
10. Sep 24 14:30 14:55 4.5.1
0080
DUCTED HEAT EXCHANGER THERMAL AND AERODYNAMIC SHAPE OPTIMIZATION
E.J. Adler¹, A.H.R. Lamkin¹, J.R.R.A. Martins¹; ¹University of Michigan, United States
10. Sep 24 14:55 15:20 4.5.2
0175
ANALYZING THE IMPACTS OF SUSTAINABLE POWERTRAINS FOR SHORT-HAUL COMMUTER AIRLINES
F. Salucci¹, N. Prabhakar¹, D. Karbowski¹; ¹Argonne National Laboratory, United States
10. Sep 24 15:20 15:45 4.5.3
1067
LOCAL AIR QUALITY AND NOISE OPTIMIZATION OF A LARGE ASPECT RATIO WINGS WITH DISTRIBUTED HYBRID ELECTRIC PROPULSION
R. Cavallaro¹, P. Norczyk Simon¹, A. Cini¹; ¹Universidad Carlos III de Madrid, Spain
10. Sep 24 15:45 16:10 4.5.4
0303
POWER MANAGEMENT SUPPLY OPTIMIZATION FOR HYBRID-ELECTRIC REGIONAL AIRCRAFT
G. Palaia¹, K. Abu Salem¹; ¹Polytechnic of Turin, Italy
Presenter: Giuseppe Palaia, Polytechnic of Turin
5.5Sustainable Aviation 1
Chair(s): Ying, S.
Track 5 Donatello
01.2 - Aircraft Design and Integrated System (Applications)
10. Sep 24 14:30 14:55 5.5.1
0398
ESTABLISHING THE DLR-F25 AS A RESEARCH BASELINE AIRCRAFT FOR THE SHORT-MEDIUM RANGE MARKET IN 2035
S. Wöhler¹, J. Häßy¹, V. Kriewall, TUHH, Germany; ¹DLR, Germany
10. Sep 24 14:55 15:20 5.5.2
0636
BATTERY PERFORMANCE METRICS FOR LARGE ELECTRIC PASSENGER AIRCRAFT
R. de Vries¹, R.E. Wolleswinkel¹, D. Rosen Jacobson¹, M. Bonnema², S. Thiede²; ¹Elysian Aircraft, Netherlands ;²University of Twente, Netherlands
10. Sep 24 15:20 15:45 5.5.3
1085
CONCEPTUAL DESIGN OF A ZERO-EMISSION REGIONAL AIRCRAFT FOR ENHANCED SHORT-HAUL MOBILITY
L. Trainelli¹, C.E.D. Riboldi¹, Y.M. Khan¹, F. Salucci, Argonne National Laboratory, United States; G. Sirtori¹; ¹DAER, Politecnico di Milano, Italy
Presenter: Lorenzo Trainelli, DAER, Politecnico di Milano
additional information (interactive) 5.5.R
1021
DESIGN OF REMOTE-CONTROLLED GROUND BASED AIRCRAFT TUG
I. Kopec¹, D. Matyja¹; ¹Polish Air Force University, Poland
6.5Aeroelastic Applications of CFD
Chair(s): Cesnik, C. E. S., Azevedo, J.L.
Track 6 Cimabue
03.1 - Aerodynamics – CFD Methods and Validation
10. Sep 24 14:30 14:55 6.5.1
0181
DATA-DRIVEN UNSTEADY AERODYNAMIC MODELS FOR AEROELASTIC STABILITY ANALYSES
A.C.N. Carloni, Instituto Tecnológico de Aeronáutica, Brazil; J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil
10. Sep 24 14:55 15:20 6.5.2
0641
NUMERICAL STUDY OF FLOWS OVER LAUNCH VEHICLES WITH VARIOUS FAIRING BY SECOND-MOMENT CLOSURE DETACHED-EDDY SIMULATION
Q. Li¹, G. Wang¹, M. Qin¹, L. Xu¹; ¹Northwestern Polytechnical University, China
10. Sep 24 15:20 15:45 6.5.3
0823
NUMERICAL ANALYSIS OF GENERALIZED AERODYNAMIC FORCES CONSIDERING LAMINAR-TURBULENT TRANSITION ON A NLF WING
C. Sebastia Saez¹, J. Martin Ferres¹, M. Hornung¹; ¹Technical University of Munich, Germany
10. Sep 24 15:45 16:10 6.5.4
1004
LINEAR SYSTEM TECHNIQUES APPLIED TO NONLINEAR AEROSERVOELASTIC ANALYSES
M.V.G. Muniz¹, J.A.A. Lyrio, Aeronautics Institute of Technology, Brazil; J.L.F. Azevedo¹; ¹Institute of Aeronautics and Space, Brazil
additional information (interactive) 6.5.R
0791
SURROGATE MODELING OF VORTEX SHEDDING TURBINE IN LOW REYNOLDS NUMBER
J.L. Kurniawan¹, M. Hu¹; ¹Institut Teknologi Bandung, Indonesia
additional information (interactive) 6.5.R
1084
PREDICTION OF TRANSIENT DEFORMATION BY COUPLING CFD AND FEM ANALYSIS USING MACHINE LEARNING BASED CORRELATION FUNCTION
J. Parez¹, P. Kovar¹, T. Vampola¹; ¹Czech Technical University in Prague, Czech Republic
Presenter: Jan Pařez, Czech Technical University in Prague
7.5AI in Structural Analysis
Chair(s): Monaco, E., Bayandor, J.
Track 7 Botticelli
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
10. Sep 24 14:30 14:55 7.5.1
0169
TRAIN ON SYNTHETIC - TEST ON REAL: DOMAIN ADAPTATION FOR STRAIN-BASED DAMAGE DETECTION ON AN AIRCRAFT WING
P. Conen¹, F. Raddatz¹, G. Wende¹; ¹DLR, Germany
10. Sep 24 14:55 15:20 7.5.2
0307
MACHINE LEARNING AND NUMERICAL OPTIMIZATION OF BIO-INSPIRED 3D-PRINTABLE SANDWICH CORE CELL
B. Omede'¹, A.M. Grande¹; ¹Politecnico di Milano, Italy
10. Sep 24 15:20 15:45 7.5.3
0435
FLUID-STRUCTURE INTERACTION OF TWO-PHASE SCATTERER METAMATERIALS FOR VIBRATION SELF-SUPPRESSION
W.H. Yuan¹, Y.J. Chai¹, X.W. Yang¹, F. Ripamonti, Politecnico di Milano, Italy; X. Wang¹, Y.M. Li¹; ¹Xi’an Jiaotong University, China
Presenter: Wenhan Yuan, Xi’an Jiaotong University
10. Sep 24 15:45 16:10 7.5.4
0351
A PHASE FIELD BASED DEEP LEARNING APPROACH FOR MECHANICAL PROPERTY PREDICTION OF SINTERED SILVER IN POWER ELECTRONICS
B.R. Yang¹, B. Wan¹, G.C. Fu¹, X.H. Wang¹, X.H. Wang¹, J. Yao¹; ¹Beihang University, China
8.5AI-assisted Airfoil and Wing Performance Predictions
Chair(s): Clark, A.
Track 8 Vasari
03.4 - Applied Aerodynamics
10. Sep 24 14:30 14:55 8.5.1
0448
DATA MINING ANALYSIS ON AERODYNAMIC STEALTH DESIGN PRINCIPLES OF AIRFOIL PROFILES
S.-Y. Jin¹, Z.-H. Gao¹, S.-S. Chen¹, Y.-Q. Wang, China Aerodynamics Research and Development Center, China; ¹ Northwestern Polytechnical University, China
10. Sep 24 14:55 15:20 8.5.2
0852
INTELLIGENT RECONSTRUCTION METHOD OF AIRFOIL FLOW FIELD BASED ON DEEP ATTENTION NETWORK
K. Zuo¹, X. Yuan, China Aerodynamics Research and Development Center, China; W. Zhang¹, Z. Ye¹; ¹Northwestern Polytechnical University, China
10. Sep 24 15:20 15:45 8.5.3
0958
CORRELATION MODELLING OF SURFACE INVISCID FLOW CHARACTERISTICS AND FRICTION DISTRIBUTION BASED ON MACHINE LEARNING
S. Zhao¹, W. Zhang¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
10. Sep 24 15:45 16:10 8.5.4
1080
DYNAMIC STALL PREDICTION THROUGH COMBINING PHYSICAL MODELS AND MACHINE LEARNING
W. Zhang¹, X. Wang¹, J. Kou¹, Z. Liu, The China Aerodynamics Research and Development Center, China; ¹ Northwestern Polytechnical University, China
Presenter: Weiwei Zhang
9.5UAV Systems
Chair(s): Viola, N.
Track 9 Giotto
07 - Systems, Subsystems and Equipment
10. Sep 24 14:30 14:55 9.5.1
1028
MULTI SENSOR AND MULTI TASK ALLOCATION BASED ON IMPROVED WHALE OPTIMIZATION ALGORITHM
B. Yuan¹, S. Zhang¹, B. Wang, School of Electronic and Information, Northwestern Polytechnica, China; K. Zhang, School of Electronic and Information, Northwestern Polytechnical, China; ¹College of Aerospace Science and Engineering, National Universit, China
10. Sep 24 14:55 15:20 9.5.2
1050
PRELIMINARY DESIGN OF POWER CONTROL STRATEGIES FOR THE HYBRID-ELECTRIC PROPULSION SYSTEM OF A LIGHTWEIGHT FIXED-WING UAV
G. Di Rito¹, A. Suti¹; ¹University of Pisa - Dept. of Civil and Industrial Engineering, Italy
Presenter: Gianpietro Di Rito, University of Pisa - Dept. of Civil and Industrial Engineering
10. Sep 24 15:20 15:45 9.5.3
1093
DEVELOPMENT OF UAVS/DRONES EQUIPPED WITH THERMAL SENSORS FOR THE SEARCH OF INDIVIDUALS LOST UNDER RUBBLE DUE TO EARTHQUAKE COLLAPSES OR ANY EVENTUALITY REQUIRING SUCH CAPABILITIES
J.A. Herrera Velasco, National Autonomous University of Mexico (UNAM), Mexico; H.S. Delgado Guevara, UNAM, Mexico
10. Sep 24 15:45 16:10 9.5.4
0156
MEASURING THE ANGLE OF ATTACK – PRACTICAL CONSIDERATIONS FOR THE DEVELOPMENT OF FAULT DETECTION RESIDUALS
C. Raab¹, N. Fezans¹; ¹DLR (German Aerospace Center) - Institute for Flight Systems, Germany
Presenter: Christian Raab, DLR - Institute of Flight Systems
10.5Damage
Chair(s): Marklund, P.O., Alaimo, A.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
10. Sep 24 14:30 14:55 10.5.1
1203
VIBRATION OF COMPOSITE SHELLS OF REVOLUTION USING EQUIVALENT SINGLE LAYER APPROACH
E. Carrera , Politecnico, Italy; V.V. Zozulya, iMex, Ukraine
10. Sep 24 14:55 15:20 10.5.2
1158
DAMAGE TOLERANCE OF A CURVED COMPOSITE STIFFENED PANEL FABRICATED BY AN OUT OF AUTOCLAVE – LIQUID RESIN INFUSION PROCESS
D. Fanteria¹, L. Boni¹, F. Romano, 2CIRA S.C.p.A., Italian Aerospace Research Centre, Italy; ¹University of Pisa, Italy
10. Sep 24 15:20 15:45 10.5.3
1146
NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES
M. Khella¹, S. Ghiasvand¹, P. Ballarin¹, F. Panzeri¹, S. Piacquadio¹, A. Airoldi¹; ¹Politecnico di Milano, Italy
Presenter: Maikel Khella, Politecnico di Milano
10. Sep 24 15:45 16:10 10.5.4
1108
INVESTIGATING THE EFFECT OF DELAMINATION-INDUCED FRICTIONAL CONTACT ON THE DYNAMIC BEHAVIOR OF LAMINATE STRUCTURES
S. Kiasat¹, A.S. Nobari, Aeronautics Engineering Department, Imperial College, United Kingdom; M. Filippi¹, E. Carrera¹; ¹POLITECNICO DI TORINO, Italy
Presenter: Shabnam Kiasat, Politecnico di Torino
11.5Experimental Aeroelasticity 2
Chair(s): Cesnik, C., Ricci, S.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
10. Sep 24 14:30 14:55 11.5.1
0784
STUDY OF AEROELASTIC PROBLEM OF RUDDER SYSTEM WITH ELECTRIC ACTUATOR AND STRUCTURAL NONLINEARITIES
W. Qian¹, W.-Z. Feng, Dalian University of Technology, China; C.-X. Han¹, X.-Y. Ai¹; ¹Daian University of Technology, China
10. Sep 24 14:55 15:20 11.5.2
0299
NOVEL TEST RIG TO DEMONSTRATE A MULTI FUNCTIONAL FLAP MECHANISM OFFERING A 2ND DEGREE OF FREEDOM
J. Docter¹, H. Pijlman¹, D. de Wit², J. Vervliet², J. Katarzynski¹, R. Postma¹, K.-J. Bisschop¹, J. Vroon¹; ¹NLR, Netherlands ;²Asco Industries, Belgium
Presenter: Hermen Hermen, NLR
10. Sep 24 15:20 15:45 11.5.3
0580
GUST LOAD ALLEVIATION IN A SCALED UAV DEMONSTRATOR
A. Herwig¹, M. Haupt¹, T. Brack¹, J. Bustamante¹, S. Heimbs¹; ¹Cluster of Excellence SE²A – Techniche Universität Braunschweig, Germany
10. Sep 24 15:45 16:10 11.5.4
0430
REDUCED ORDER MODELLING OF UNSTEADY AERODYNAMICS FOR GROUND FLUTTER TEST SYSTEM
W.-Z. Feng¹, J.-H. Zhang¹, Z.-H. Liang¹, W. Qian¹; ¹Dalian University of Technology, China
Presenter: Wei-Zhe Feng, Dalian University of Technology
additional information (interactive) 11.5.R
0530
EXPERIMENTAL INVESTIGATION AND NUMERICAL ANALYSIS OF THE EFFECT OF TEMPERATURE ON THE MECHANICAL PROPERTIES OF AEROSPACE COMPOSITE-METAL HYBRID JOINTS
R. Hou¹, B.T. Wang, Department of Strength Design, The First Aircraft Institute of A, China; Z.X. Zhu¹, W.C. Gao¹; ¹Department of Astronautical Science and Mechanics, HIT, China
12.5Loads and Aeroelasticity of Rotorcraft and Propellers
Chair(s): Alaimo, A., Cerdle, J.
Track 12 Petrarca
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
10. Sep 24 14:30 14:55 12.5.1
0418
ROTOR DYNAMIC LOADS CHARACTERISTIC ANALYSIS WITH BLADE TIP TWIST DISTRIBUTION
Z. Yu¹, J. Huang¹, Q. Jiang¹, F. Fan, CHRDI , Germany; S. Huang¹; ¹CHRDI, China
10. Sep 24 14:55 15:20 12.5.2
1017
INVESTIGATING AN OPTIMAL AEROELASTIC DESIGN FOR AIRCRAFT WINGS WITH DISTRIBUTED PROPELLERS MADE OF COMPOSITES
M. Abouhamzeh, University of Wolverhampton, United Kingdom; Y. Ma, Bauhaus Aviation Research Institute, Germany
10. Sep 24 15:20 15:45 12.5.3
0730
EXPERIMENTAL VALIDATION OF THE DYNAMIC FINITE ELEMENT MODEL OF A 1:8 SCALE SEAPLANE USING A LASER DOPPLER VIBROMETER (LDV)
F. Lovero¹, G. Biggi¹, S. Lombardi¹, M.A.C. Costa¹, V. Amore¹, E. Cestino¹; ¹Politecnico di Torino, Italy
10. Sep 24 15:45 16:10 12.5.4
1241
DRIVETRAIN INFLUENCE ON THE LEAD-LAG MOTION OF HELICOPTER ROTORS
F. Weiss, DLR, Germany
13.5Propellers, Fans, Compressors 2
Chair(s): Mogilka, P.
Track 13 Boccaccio
05 - Propulsion
10. Sep 24 14:30 14:55 13.5.1
0281
A MOMENTUM-INTEGRAL METHOD TO CALCULATE WINDAGE LOSSES ON A ROTATING DRUM WITH SUPERPOSED FLOW
H. Tuo¹, P. Liu¹, S. Ding¹, T. Qiu¹, C. Liu¹, R. Cheng, AECC Shenyang Engine Research Institute, China; ¹Research Institute of Aero-Engine, Beihang University, China
10. Sep 24 14:55 15:20 13.5.2
0342
AERODYNAMIC OPTIMIZATION OF HIGH-ALTITUDE PROPELLER COMBINED WITH MACHINE LEARNING METHOD
D. Li¹, Z. Ge¹, R. Cui¹, L. Yang¹, C. Wei¹, W. Song, Northwestern Polytechnical University, China; ¹AVIC Aerodynamics Research Institute, China
10. Sep 24 15:20 15:45 13.5.3
0419
AERODYNAMIC PERFORMANCE OF BLADELESS DUCTED FAN BASED ON EJECTION EFFECT WITH DIFFERENT DESIGN VARIABLES
K. Han, China; S. Yu, China; J. Huang, China; J. Bai, China; Y. Qiu, China
14.5Pedagogy in Education
Chair(s): Kanerva, M.
Track 14 Puccini
14 - Education and Training
10. Sep 24 14:30 14:55 14.5.1
0324
TRANSFORMATIVE PEDAGOGY: CO-TEACHING COURSE CLUSTERS THROUGH COMPETITIVE TEAM DESIGNS FOR INNOVATIVE TALENT DEVELOPMENT IN AEROSPACE EDUCATION
M. Luo¹, H. Liu¹, X. Zhang¹, Z. Cui¹; ¹Beihang University, China
Presenter: ZHIYANG CUI, Beihang University
10. Sep 24 14:55 15:20 14.5.2
0867
LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS
I. Jonsson¹, C. Xisto¹, V. Chernoray¹, A. Capitao Patrao¹; ¹Chalmers University Of Technology, Sweden
10. Sep 24 15:20 15:45 14.5.3
1185
INTEGRATING UNMANNED AERIAL SYSTEMS INTO THE INTELLIGENT SYSTEMS ENGINEERING CURRICULUM
O.D. Dantsker, Indiana University, United States
10. Sep 24 15:45 16:10 14.5.4
1264
DLR DESIGN CHALLENGE 2024: DESIGN OF A COST AND ENERGY EFFICIENT REGIONAL AIRCRAFT
C. Ehrich¹, L. Kriebel¹, T. Schulz¹, M. Tekkel¹, L. Wauer¹, L. Wenz¹, L. Kugler², S. Müller², C. Niro²; ¹Technical University of Berlin, Germany ;²German Aerospace Center (DLR), Germany
15.5Flight Control 2
Chair(s): Silvestre, F.
Track 15 Carducci
06.1 - Flight Dynamics and Control (Control & Modelling)
10. Sep 24 14:30 14:55 15.5.1
0424
A COMPARSION OF TRAJECTORY GENERATION ALGORITHMS FOR A TERRAIN FOLLOWING FLIGHT
H. Lee¹, S. Lee¹; ¹Korea Aerospace University, South Korea
10. Sep 24 14:55 15:20 15.5.2
0364
A GENETIC ALGORITHM FOR TRAJECTORY GENERATION IN ENGINE-OUT EMERGENCY LANDING SCENARIOS OF COMMERCIAL AIRCRAFT
J. Gauci, University of Malta, Malta; B. Zammit, Malta; M. Galea, Malta
10. Sep 24 15:20 15:45 15.5.3
0478
ATTITUDE CONTROL DESIGN FOR A FLYING-CRAWLING INTEGRATED FLAPPING-WING MICRO AIR VEHICLE
Z.Y. Yuan¹, W.Y. Yang¹, J.X. Xuan¹; ¹nwpu, China
10. Sep 24 15:45 16:10 15.5.4
0468
TRAJECTORY OPTIMIZATION FOR LONG-RANGE AIR-LAUNCHED GLIDING VEHICLES USING CONVEX PROGRAMMING
C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea
additional information (interactive) 15.5.R
1115
OPTIMAL APPROACH AND DEPARTURE TRAJECTORIES WITH ACOUSTIC FOOTPRINT ASSESSMENT FOR AN AIR MOBILITY QUAD-ROTOR
C. Varriale¹, F. Yunus¹, M. Snellen¹; ¹Delft University of Technology, Netherlands
16.5Collaborative and Other UAV Operations
Chair(s): Doll, C., Watanabe, Y.
Track 16 Raffaello
06.2 - Flight Dynamics and Control (UAV related)
10. Sep 24 14:30 14:55 16.5.1
0713
INCREMENTAL NONLINEAR DYNAMIC INVERSION CONTROLLER FOR A FLYING WING OPERATED IN AN AIRBORNE WIND ENERGY SYSTEM
D.F. Duda¹, H. Fuest¹, J. Müller¹, T. Islam¹, D. Moormann¹; ¹RWTH Aachen Unitversity, Germany
10. Sep 24 14:55 15:20 16.5.2
0795
ADVANCED SOLUTIONS AND CHALLENGES IN MULTI-DRONE SYSTEMS FOR SEARCH AND RESCUE MISSIONS: TECHNICAL APPROACHES AND UNRESOLVED MATTER
E. D'Amato, Università degli Studi di Napoli Parthenope, Italy
10. Sep 24 15:20 15:45 16.5.3
0084
HAWK-INSPIRED COOPERATIVE ENCIRCLEMENT GUIDANCE OF FIXED-WING UAV SWARM WITH LIMITED COMMUNICATION IN THREAT SCENARIO
B.-Y. Qin¹, D. Zhang¹, S. Tang¹; ¹Northwestern Polytechnical University, China
10. Sep 24 15:45 16:10 16.5.4
0608
A SIMULINK APPROACH TO MODELING HETEROGENEOUS DRONE FORMATIONS FOR AGENT-BASED SIMULATION
G. Raspaolo, Italy; G. D'Alterio, Italy; I. Notaro, Italy; E. D'Amato, Italy
Presenter: Immacolata Notaro
17.5Displays and Assistance Systems
Chair(s): Viola, N.
Track 17 Galileo
07 - Systems, Subsystems and Equipment
10. Sep 24 14:30 14:55 17.5.1
0786
ENHANCED AIRCRAFT TAKEOFF/LANDING SAFETY USING DEEP LEARNING MODEL IN RUNWAY ASSISTANCE SYSTEM
N.L. Ywet¹, A.A. Maw¹, J.W. Han¹, J. Chung, Toronto Metropolitan University, Canada; J.W. Chang, Korea Aerospace University, South Korea; J.-W. Lee¹; ¹Konkuk University, South Korea
10. Sep 24 14:55 15:20 17.5.2
1187
NONLINEAR BEHAVIOR IN AIRCRAFT FUEL GAUGE READINGS: AN EXPLORING ANALYSIS
M.A.D. Di Marzo¹, O.A. Gonzatto Junior¹, H.N. Najafabadi, Linköping University – LiU, Sweden; J.H. Bidinotto¹; ¹University of São Paulo - USP, Brazil
10. Sep 24 15:20 15:45 17.5.3
0244
INTEGRITY MONITORING OF TIGHTLY INTEGRATED BDS/SINS USING MULTI-HYPOTHESIS SOLUTION SEPARATION (MHSS) ALGORITHM
S. Sun¹, H. Wang¹, R. Liu¹, S. Kuang¹, W. Chen¹; ¹Civil Aviation University of China, China
10. Sep 24 15:45 16:10 17.5.4
0425
DEVELOPMENT OF THRUST CONTROL SYSTEM FOR SPACECRAFT’S DOCKING MANEUVER
H. Lee¹, H. Lee¹, S. Lee¹; ¹Korea Aerospace University, South Korea

16:00 - 16:30BREAK

1.6GSA - Structures and Manufacturing
Chair(s): Scott, M.
Track 1 Auditorium
15 - Guest lectures
10. Sep 24 16:30 17:00 1.6.1
1237
NASA HI-RATE COMPOSITE AIRCRAFT MANUFACTURING (HICAM) PROJECT OVERVIEW
R. Young, NASA (LaRC), United States
Presenter: Tom Reynolds
10. Sep 24 17:00 17:30 1.6.2
1302
SUSTAINABLE HIGH RATE COMPOSITE MANUFACTURE
P C Crothers, Boeing Aerostructures Australia, Australia
10. Sep 24 17:30 18:00 1.6.3
1318
FUSELAGE, CABIN & CARGO AND EMPENNAGE OF TOMORROW @ AIRBUS COMMERCIAL - NEW FUSELAGE DESIGN & MATERIALS
Y. C. Roth, Airbus, Germany
10. Sep 24 18:00 18:30 1.6.4
1283
WING OF TOMORROW - LONGER, LEANER, LIGHTER
M. Cantrell, Airbus, United Kingdom
2.6Active Flow Control Flight Demonstrations
Chair(s): Post, M., Vijgen, P.
Track 2 Sala Verde
15 - Guest lectures
10. Sep 24 16:30 17:00 2.6.1
1248
AFC FLIGHT-DEMONSTRATOR X-65 PROGRAM OVERVIEW
M.L. Post, DARPA/TTO, United States
10. Sep 24 17:00 17:30 2.6.2
1312
INTEGRATING ACTIVE FLOW CONTROL ON AIRCRAFT
J. F. Langford, Aurora Flight Sciences, A Boeing Company, United States
10. Sep 24 17:30 18:00 2.6.3
1262
THE PATH TO TRANSITION ACTIVE FLOW CONTROL TECHNOLOGY
R. Woszidlo, The Boeing Company, United States
10. Sep 24 18:00 18:30 2.6.4
1297
PERSPECTIVES ON FLOW CONTROL APPLICATIONS FOR LARGE TRANSPORT AIRCRAFT
D. Reckzeh, Airbus, Germany
3.6Design of Sustainable Aircraft 1
Chair(s): Rinoie, K.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
10. Sep 24 16:30 17:00 3.6.1
1114
EU IMPACT MONITOR PROJECT - OVERVIEW AND APPROACH
P. Shiva Prakasha¹, P. Ratei¹, M. Van Eenige¹, T. Lefebvre, The French Aerospace Lab, France; M. Alder¹, U. Gupta, Cranfield University , United Kingdom; M. Antonio Solazzo, CIRA, Italy; B. Nagel¹; ¹German Aerospace Center - DLR, Germany
10. Sep 24 17:00 17:30 3.6.2
0254
EVALUATION OF ASWING FOR OVERALL AIRCRAFT DESIGN OF UNCONVENTIONAL CONFIGURATIONS. APPLICATION TO JOINED WINGS WITH FOLDING WINGTIPS
R. Jan¹, S. Delbecq¹, E. Benard¹; ¹ISAE-Supaero, France
10. Sep 24 17:30 18:00 3.6.3
1134
IDENTIFICATION OF THE IMPACT OF BLOWING ON THE AERODYNAMIC MODEL OF AN AIRPLANE WITH DISTRIBUTED ELECTRIC PROPULSION
S. Cacciola¹, L. Bottà¹, C.E.D. Riboldi¹, L. Trainelli¹; ¹Politecnico di Milano, Italy
10. Sep 24 18:00 18:30 3.6.4
0470
MULTIDISCIPLINARY PRELIMINARY DESIGN PROCESS OF HYBRID-ELECTRIC SEAPLANE
M. Tuccillo¹, P. Della Vecchia¹; ¹University of Naples Federico II, Italy
additional information (interactive) 3.6.R
0042
TRANSLATING THE CONCEPT OF SUSTAINABILITY FOR THE DETERMINATION OF REQUIREMENTS FOR THE DESIGN OF FUTURE AIRCRAFT
L. Paletti¹, L. Boggero¹, G. Wende¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
Presenter: Ligeia Paletti, German Aerospace Center (DLR)
additional information (interactive) 3.6.R
1046
PERFORMANCE ENHANCEMENTS BETWEEN DIFFERENT APPLICATIONS OF ALTERNATIVE FUELS AND NOVEL AIRCRAFT CONFIGURATIONS
J.L.C. Chan¹, Y. Sun¹, H. Smith, Cranfield University , United Kingdom; ¹Cranfield University, United Kingdom
4.6LH 2 Aircraft System
Chair(s): Nagel, B., Imamura, T.
Track 4 Brunelleschi
01.1 - Aircraft Design and Integrated System (Basics and Theory)
10. Sep 24 16:30 17:00 4.6.1
0488
EXPLORATION AND EVALUATION OF KNOWLEDGE-BASED ENGINEERING APPROACH FOR LIQUID HYDROGEN TANK INTEGRATION IN EXISTING FUSELAGE
N. Bhargav¹, V. Elangovan¹, R.C. Munjulury, Linköping University, Sweden; C. Hesse², P. Satwan²; ¹Linköping University/DLR, Germany ;²Institute for System Architectures in Aeronautics, DLR, Germany
10. Sep 24 17:00 17:30 4.6.2
0301
INCREMENTAL TRADE-OFF STUDY OF A HYDROGEN FUEL CELL-BASED PROPULSION SYSTEM USING MDAO TECHNIQUES
R. di Giuseppe, ISAE-Supaero, SafranTech, France; S. Delbecq¹, V. Pauvert, SafranTech, France; V. Pommier-Budinger¹; ¹ISAE-SUPAERO, France
10. Sep 24 17:30 18:00 4.6.3
1002
METHODOLOGIES FOR THE PRELIMINARY SIZING OF HYDROGEN-POWERED AIRCRAFT AND SUPPORTING AIRPORT INFRASTRUCTURES
L. Trainelli¹, C.E.D. Riboldi¹, G. Sirtori¹; ¹DAER, Politecnico di Milano, Italy
10. Sep 24 18:00 18:30 4.6.4
0736
CFD STUDY OF AIR SUPPLY SYSTEM FOR COOLING OF A HYDROGEN POWERED UNMANNED SEAPLANE AND REDUCTION OF THE RESULTING DRAG
A. Marsano¹, F. Bustos Ortega¹, G. Santarella¹, S.G. Soundararajan¹, F. Giargia¹; ¹Politecnico di Torino, Italy
5.6Sustainable Aviation 2
Chair(s): Ying, S.
Track 5 Donatello
01.2 - Aircraft Design and Integrated System (Applications)
10. Sep 24 16:30 17:00 5.6.1
1170
INTEGRATED SIZING OF AN ELECTRIFIED TILT-WING AIRCRAFT FOR VERTICAL AND CONVENTIONAL TAKEOFF AND LANDING
A.A. Mishra¹, B. Kunwar¹, I. Chakraborty¹; ¹Auburn University, United States
10. Sep 24 17:00 17:30 5.6.2
0366
IMPACT OF WELL-TO-TANK EFFICIENCY AND EMISSIONS ON HYBRID AIRCRAFT DESIGN OPTIMIZATION
M. Blandino¹, M.M. Molinari¹, J. Liberatori¹, P.P. Ciottoli¹, R. Malpica Galassi¹; ¹Sapienza Università di Roma, Italy
10. Sep 24 17:30 18:00 5.6.3
0166
MASS AND POWER ESTIMATIONS IN PRELIMINARY FLIGHT CONTROL SYSTEM DESIGN
S.M. Lübbe¹, M. Schäfer¹, O. Bertram¹; ¹German Aerospace Center (DLR), Germany
10. Sep 24 18:00 18:30 5.6.4
1155
CANCELED - ON THE TECHNOLOGIES FOR THE GREENING OF ALL CLASSES OF AIR TRANSPORT
L.M.B.C. Campos¹, J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal; P.A. Serrão¹; ¹IDMEC/CCTAE - IST, Portugal
Presenter: Pedro Serão
6.6Numerical Methods in Aerodynamics
Chair(s): Coder, J., Azevedo, J.L.
Track 6 Cimabue
03.1 - Aerodynamics – CFD Methods and Validation
10. Sep 24 16:30 17:00 6.6.1
0247
ENHANCING EFFICIENCY FOR UNSTEADY CFD COMPUTATIONS IN AERONAUTICS
M. Carlsson¹, P. Eliasson¹, P. Weinerfelt¹; ¹Saab, Sweden
Presenter: Magnus Carlsson, SAAB AB
10. Sep 24 17:00 17:30 6.6.2
1181
ANALYSIS OF THE R FAMILY OF LIMITERS APPLIED TO HIGH-ORDER FR/CPR SCHEMES FOR THE SIMULATION OF SUPERSONIC FLOWS
F.B. Oliveira, Instituto Tecnologico de Aeronautica, Brazil; J.L.F. Azevedo, Instituto de Aeronautica e Espaco, Brazil; Z.J. Wang, University of Kansas, United States
10. Sep 24 17:30 18:00 6.6.3
0694
A HIGH-PRECESION PSEUDO ARC-LENGTH METHOD WITH POSITIVE VALUE PRESERVATION PROPERTIES BASED ON TV SPLITTING
C. Wang¹, P. Li¹, L. He¹, G. Li¹, H. Dai¹; ¹Chinese Aeronautical Establishment, China
10. Sep 24 18:00 18:30 6.6.4
0676
A BOUNDARY INTEGRAL EQUATION FORMULATION FOR POTENTIAL COMPRESSIBLE FLOWS AROUND DEFORMABLE BODIES
E. Levati¹, C. Pasquali¹, G. Bernardini¹, M. Gennaretti¹; ¹Roma Tre University, Italy
7.6High speed flows
Chair(s): Gowree, E.
Track 7 Botticelli
03.2 - Experimental Aerodynamics
10. Sep 24 16:30 17:00 7.6.1
0710
EXPERIMENTAL INVESTIGATION OF THE DLR-F23 CONFIGURATION AT TRANSONIC SPEEDS USING FAST-RESPONSE PRESSURE-SENSITIVE PAINT
P. Hartl¹, M. Ritschel¹, M. Braune¹, H. Mai¹; ¹German Aerospace Center (DLR), Germany
10. Sep 24 17:00 17:30 7.6.2
0447
ASSESSING THE SONIC BOOM OF A FULL-SIZE AIRCRAFT FROM FREE FLIGHT TESTS ON A SUB-SCALE MODEL
G. Fasulo¹, L. Federico¹; ¹Italian Aerospace Research Centre (CIRA), Italy
10. Sep 24 17:30 18:00 7.6.3
0540
EFFECT OF FREESTREAM DISTURBANCES ON BOUNDARY LAYER TRANSITION IN HYPERSONIC WIND TUNNEL
J. Yuan¹, S. Yu¹, Z. Qian¹; ¹AVIC Aerodynamics Research Institute, China
10. Sep 24 18:00 18:30 7.6.4
0390
ELECTRIC FIELD MEASUREMENT IN GLOW DISCHARGE PLASMA INTERACTING WITH SHOCK WAVE IN HYPERSONIC FLOW
N. Cao Van¹, H. Itoh¹, M. Mizoguchi¹, A. Uenaka¹; ¹National Defense Academy of Japan, Japan
8.6Aerodynamics of Propulsion System Integration
Chair(s): Tamaki, Y.
Track 8 Vasari
03.4 - Applied Aerodynamics
10. Sep 24 16:30 17:00 8.6.1
0134
SIMULATION OF AN INSTALLED PROPELLER BY MEANS OF STEADY AND UNSTEADY BODY-FORCE MODELING
H. Pantel¹, F. Falissard¹, G. Dufour, ISAE-SUPAERO, France; ¹ONERA, France
10. Sep 24 17:00 17:30 8.6.2
0264
EXPERIMENTAL MEASUREMENTS OF SLIPSTREAM DEFORMATION FOR AN INSTALLED DISTRIBUTED PROPELLER CONFIGURATION.
R.R. Duivenvoorden¹, F. do Nascimento Monteiro¹, T. Sinnige¹; ¹Delft University of Technology, Netherlands
10. Sep 24 17:30 18:00 8.6.3
0632
AERODYNAMIC PERFORMANCE AND INTERACTION EFFECTS OF AN OVER-THE-WING DISTRIBUTED-PROPELLER SYSTEM IN CRUISE CONDITIONS
R. de Vries¹, T. Sinnige¹, L.L.M. Veldhuis¹; ¹Delft University of Technology, Netherlands
10. Sep 24 18:00 18:30 8.6.4
0028
CANCELED - ON THE INFLUENCE OF PROPELLER MODELLING STRATEGY FOR INTERACTIONAL AERODYNAMICS
Z. Li¹, V. Maltsev¹, A.H. Aval¹, A. Da Ronch¹; ¹University of Southampton, United Kingdom
9.6AAM 3 - Vertiports and Infrastructure
Chair(s): Li, M.
Track 9 Giotto
09 - Air Transport System Efficiency
10. Sep 24 16:30 17:00 9.6.1
0155
COMPARING THE CAPACITY OF DIFFERENT VERTIPORT TOPOLOGIES USING DISCRETE EVENT SIMULATION
E. Wille, RWTH Aachen University, Germany
Presenter: Eva Wille
10. Sep 24 17:00 17:30 9.6.2
0953
DEMAND CAPACITY BALANCING FOR URBAN AIR MOBILITY USING MULTIAGENT SIMULATION
G. Sato, Electronic Navigation Research Institute, Japan
10. Sep 24 17:30 18:00 9.6.3
0745
DESIGN OF A UAM GROUND INFRASTRUCTURE NETWORK WITH RESPECT TO MAINTENANCE CAPACITY REQUIREMENTS
M. Swaid, German Aerospace Center (DLR), Germany; S. Papakonstantinou¹, D. Kloock-Schreiber¹, V. Gollnick¹; ¹Hamburg University of Technology (TUHH), Germany
10. Sep 24 18:00 18:30 9.6.4
0686
AIRPORT INFRASTRUCTURE SIZING FOR A REGIONAL ELECTRIC AVIATION NETWORK
F. Vehlhaber¹, M. Salazar¹; ¹Eindhoven University of Technology, Netherlands
10.6NDT / Optimization
Chair(s): Concilio, A., Kanerva, M.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
10. Sep 24 16:30 17:00 10.6.1
1076
STIMULATED THERMOGRAPHY AS NON-DESTRUCTIVE TESTING TO ASSESS THE STRUCTURAL INTEGRITY OF AERONAUTICAL COMPONENT IN CFRP
G. Masciopinto¹, E. D'Accardi¹, D. Palumbo¹, U. Galietti¹; ¹Polytechnic University of Bari, Italy
Presenter: Umberto Galietti, Polytechnic University of Bari
10. Sep 24 17:00 17:30 10.6.2
0818
NUMERICAL ANALYSIS OF PROCESS-INDUCED DEFORMATIONS AND STRESSES IN AERONAUTICAL COMPOSITE COMPONENTS
R. Masia¹, M. Petrolo¹, E. Zappino¹, N. Zobeiry, University of Washingthon, United States; E. Carrera¹; ¹Politecnico di Torino, Italy
10. Sep 24 17:30 18:00 10.6.3
0280
CANCELED - CONCURRENT TOPOLOGY OPTIMIZATION OF CROSS-SECTION TOPOLOGY AND FIBER ORIENTATION FOR ROTATING COMPOSITE BEAMS
Y.-F. Luo¹, M.-L. Hao¹, X. Li¹, Q.-H. Li¹; ¹Shandong University, China
10. Sep 24 18:00 18:30 10.6.4
0544
ELASTIC/PLASTIC SEMI-ANALYTICAL METHOD FOR ARBITRARY CURVED SURFACES OF SCARF REPAIRED COMPOSITES
Y. Liu¹, B. Liu¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 10.6.R
0933
A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING
D.-B. Li, China; H.-X. Huang, China; X.-C. Liu, China; P.-Y. Hou, China; H.-H. Liao, China
11.6Adaptive and Morphing Aircraft
Chair(s): Rade, D., Pecora, R.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
10. Sep 24 16:30 17:00 11.6.1
0385
MULTI-OBJECTIVE DESIGN OPTIMIZATION OF A MORPHING AILERON FOR A HYBRID ELECTRIC REGIONAL AIRCRAFT
A. De Gaspari¹, V. Cavalieri¹, M. Corti¹, S. Ricci¹; ¹Politecnico di Milano, Italy
10. Sep 24 17:00 17:30 11.6.2
0513
ADAPTIVE WING FLUTTER SUPPRESSION BY MEANS OF MULTIPLE TRAILING EDGE CONTROL SURFACES - A COMPARATIVE STUDY
C.R. Vindigni¹, G. Mantegna¹, A. Esposito¹, C. Orlando¹, A. Alaimo¹; ¹Kore University of Enna, Italy
10. Sep 24 17:30 18:00 11.6.3
0565
DESIGN OF A BODY FREEDOM FLUTTER FLIGHT MODEL WITH CONVENTIONAL CONFIGURATION
X. Tian¹, Y. Gu¹, Z. Yang¹; ¹Northwestern Polytechnical University, China
10. Sep 24 18:00 18:30 11.6.4
0801
CANCELED - DESIGN AND TEST OF A MORPHING LEADING EDGE FOR A LARGE-SCALE CIVIL AIRCRAFT
Z. Wang, China; X. Sun, China; Y. Yang, China; J. Zhou, China; C. Li, China; J. Xue, China; J. Xiang, China; D. Li, China
additional information (interactive) 11.6.R
1015
MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON\\\\\\\'S RATIO HONEYCOMB
S.-Y. Sun¹, H.-Z. Wang¹, R. Yang¹, W. Qian¹; ¹Dalian University of Technology, China
12.6Structural Design and Optimization 3
Chair(s): Ikeda, T., Han, J.H.
Track 12 Petrarca
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
10. Sep 24 16:30 17:00 12.6.1
0486
ADVANCED MULTIDISCIPLINARY DESIGN OF NEXT-GENERATION GREEN AIRCRAFT
L. Pustina¹, R.M. Galassi¹, M. Blandino¹, F. Mastroddi¹; ¹Sapienza University of Rome, Italy
10. Sep 24 17:00 17:30 12.6.2
0405
OPTIMIZATION OF COMPOSITE WING STRUCTURE FOR TILT-DUCT AIRCRAFT CONSIDERING DISCRETE AND CONTINUOUS DESIGN VARIABLES
S.-R. Xu, China; Y.-T. Zhang, China; J.-F. Zhang, China; Y. Zheng, China; Y.-L. Liu, China
10. Sep 24 17:30 18:00 12.6.3
1142
A PRELIMINARY METHODOLOGY TO ASSESS GUST SPECTRA VIA SATELLITE DATA
E. Carrera¹, A. Pagani¹, M. Valente¹, G. Palaia¹; ¹Politecnico di Torino, Italy
Presenter: Erasmo Carrera, Politecnico di Torino
10. Sep 24 18:00 18:30 12.6.4
0642
AEROELASTIC DIVERGENCE AND FLUTTER ANALYSIS OF A WING WITH ALL MOVING WING TIP
W. Wang¹, W. Qian¹, X. Ai¹; ¹Dalian University of Technology, China
13.6Propellers, Fans, Compressors 3
Chair(s): Mogilka, P.
Track 13 Boccaccio
05 - Propulsion
10. Sep 24 16:30 17:00 13.6.1
0726
GRADIENT-BASED OPTIMIZATION OF AN AXIAL COMPRESSOR UNDER INLET DISTORTION USING BODY-FORCE MODELING
C. Dosne¹, R. Barrier¹, S. Bourasseau¹, M. Carini¹, A. Dumont¹, J. Peter¹; ¹ONERA, France
10. Sep 24 17:00 17:30 13.6.2
0896
EFFECT OF POPULAR ADDITIVE MANUFACTURING TECHNOLOGIES ON THE PERFORMANCE AND ACOUSTICS OF UAV PROPELLERS
J. García-Tíscar¹, P. Quintero¹, F.N. Ramírez¹, A. Cremades, KTH Royal Institute of Technology, Sweden; ¹Universitat Politècnica de València, Spain
14.6Attainability of Hybrid Electric Vehicles
Chair(s): Bezos OConnor, G., Orisamolu, W.
Track 14 Puccini
05 - Propulsion
10. Sep 24 16:30 17:00 14.6.1
1027
SAFETY-DRIVEN BASELINING OF HYBRID ELECTRIC AIRCRAFT ELECTRICAL POWER SYSTEM ARCHITECTURES
K. Fong¹, P. Norman¹, C.E. Jones¹; ¹University of Strathclyde, United Kingdom
10. Sep 24 17:00 17:30 14.6.2
0738
EVALUATION AND SIMULATION OF PARALLEL HYBRID ELECTRIC PROPULSION WITH REAL FLIGHT DATA
H. Murphy¹, C. Gallagher¹, C. Stuart¹, S. Spence¹, S. Fitzgerald, Ryanair DAC, Ireland; ¹Dept. of Mechanical Engineering, Trinity College Dublin, Ireland
10. Sep 24 17:30 18:00 14.6.3
1054
PROJECTION OF KEY POWERTRAIN COMPONENT FIGURES OF MERIT FOR OVERALL ASSESSMENT OF ELECTRIC FLIGHT SCENARIOS
A. Link¹, S. de Graaf¹; ¹German Aerospace Center (DLR), Germany
10. Sep 24 18:00 18:30 14.6.4
0442
AIRPORT CHARGING SYSTEM DESIGNS AND POWER MANAGEMENT FOR MEGAWATT-LEVEL CHARGING OF BATTERY-ELECTRIC AIRCRAFT
J. Hellgren¹, M. Persson¹, H. Alfredsson¹; ¹RISE Research Institutes of Sweden, Sweden
Presenter: Jonas Hellgren, RISE Research Institutes of Sweden
15.6Flight Modeling and Simulation
Chair(s): Grabowski, T,
Track 15 Carducci
06.1 - Flight Dynamics and Control (Control & Modelling)
10. Sep 24 16:30 17:00 15.6.1
0355
STUDY ON CONFIGURATIONS OF AIRBORNE LAUNCH SYSTEM FOR DELIVERY OF SMALL PAYLOAD TO LOW EARTH ORBIT
T. Goetzendorf-Grabowski¹, L. Kiszkowiak², A. Kwiek¹, P. Zalewski², K. Chudy², M. Figat¹; ¹Warsaw University of Technology, Poland ;²Military University of Technology, Poland
10. Sep 24 17:00 17:30 15.6.2
0819
ASSISTED AND AUTOMATED AERIAL REFUELLING – OVERVIEW OF THE CONDUCTED RESEARCH AT THE GERMAN AEROSPACE CENTER (DLR)
T. Jann¹, N. Fezans¹, A. Koloschin¹, S.-O. Schmidt¹, P. Link¹, J. Ament¹, S. Krause¹; ¹German Aerospace Center (DLR), Institute of Flight Systems, Germany
10. Sep 24 17:30 18:00 15.6.3
1167
CANCELED - ON THE EXTRAPOLATION OF STABILITY DERIVATIVES FOR DIFFERENT AIRSPEEDS AND ANGLES-OF-ATTACK AND SIDESLIP
L.M.B.C. Campos¹, J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal; P.A. Serrão¹; ¹IDMEC/CCTAE - IST, Portugal
10. Sep 24 18:00 18:30 15.6.4
0317
INFLUENCE OF CONTROL POWER RATE ON HIGH-ALPHA ROLL MANOEUVRABILITY
P. Månsson, Saab AB, Sweden
additional information (interactive) 15.6.R
0223
STRUCTURED H-INFINITY DESIGN OF PREDICTORS FOR THE MONITORING OF AN AIRCRAFT IN ITS FLIGHT ENVELOPE
K.H. Kienitz, Instituto Tecnologico de Aeronautica, Brazil; A. Gonzalez Sorribes¹, R. Sanz Diaz¹, C. Braga de Mendonça, Boeing Brasil, Brazil; P.J. Garcia¹; ¹Universitat Politecnica de Valencia, Spain
additional information (interactive) 15.6.R
0621
DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE
C. Zhai¹, B. Song¹, Q. Fu¹, J. Xuan¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
additional information (interactive) 15.6.R
0627
DATA-DRIVEN MODEL DISCOVERY AND CONTROL OF HIGH-PERFORMANCE TRAINER AIRCRAFT VIA SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS
M.-W. Kang¹, D.-W. Lee², S.-H. Yun¹, H.-C. Bang²; ¹ADD, South Korea ;²KAIST, South Korea
additional information (interactive) 15.6.R
0938
GROUND EFFECT ON A SLENDER 65º DELTA WING WITH SIDESLIP, IMAGE METHOD, USING EULER
R.K. Nangia¹, T. Nangia¹; ¹Nangia, United Kingdom
16.6Advanced Manufacturing Technology 1
Chair(s): Lin, K., Jiang, L.
Track 16 Raffaello
08 - Manufacturing and Supply Chain Management
10. Sep 24 16:30 17:00 16.6.1
0260
REDESIGN AND MACHINING OF LEADING EDGE OF TRANSONIC COMPRESSOR BLADE IN ROBOTIC GRINDING OPERATION
H. Li¹, L. Zou¹, W. Wang¹, L. Gui¹; ¹Chongqing University, China
Presenter: Lai Zou, Chongqing University
10. Sep 24 17:00 17:30 16.6.2
1194
DESIGN OF A SUSTAINABLE FLEXFORMING PROCEDURE FOR AERO ENGINE COMPONENTS IS ALLOY 718
P. Ottosson¹, E.-L. Westman¹, I. Nygren, Quintus Technologies, Sweden; T. Pettersson, Permanova LaserTool in Blekinge, Sweden; F. Niklasson², L.-E. Brattström²; ¹RISE Research Institutes of Sweden, Sweden ;²GKN Aerospace Engine Systems Sweden, Sweden
10. Sep 24 17:30 18:00 16.6.3
0378
PRESERVING HUMAN EXPERTISE: EXPLORING MIXED REALITY TRAJECTORY PLANNING FOR ROBOTIC BELT GRINDING
W.-X. Wang¹, H.-L. He¹, T.-Y. Zhou, Cardiff University, United Kingdom; L. Wan¹; ¹Chongqing University, China
Presenter: Wenxi WANG, Chongqing University
10. Sep 24 18:00 18:30 16.6.4
0487
A DIGITAL METHOD FOR THE COMPENSATED MOLD DESIGN OF COMPOSITE PARTS
E. Delsol¹, I. Taouil¹, W. Azoti², B. Castanie², P. Olivier², L. Ratsifandrihana, Segula, France; ¹Segula - ICA, France ;²ICA, France
17.6Thermal Management
Chair(s): Stumpf, E.
Track 17 Galileo
07 - Systems, Subsystems and Equipment
10. Sep 24 16:30 17:00 17.6.1
0529
ANGLE AND DISTANCE EFFECT ON PHOSPHOR THERMOMETRY
Q. Yin¹, Y. Quan¹, L. Ma¹, J. Liu¹, J. Chai¹, J. Liu¹, L. Zhang¹; ¹Beihang University, China
10. Sep 24 17:00 17:30 17.6.2
1010
VOID FRACTION CALCULATION MODEL BASED ON TWO-PHASE FLOW PATTERNS IN THE SCAVENGE PIPE
J.-W. Xie¹, P.-F. Zhu¹, J.-P. Hu¹, Y.-G. Lyv¹, Z.-X. Liu¹; ¹Northwestern Polytechnical University, China
10. Sep 24 17:30 18:00 17.6.3
1030
A STUDY ON THE AIRLOCK MECHANISM OF THE OIL SUPPLY PUMP IN AERO-ENGINE LUBRICATING OIL SYSTEM
S. Zhang, China; P.-F. Zhu, China; H. Fan, China; Z.-X. Liu, China
10. Sep 24 18:00 18:30 17.6.4
0295
POTENTIAL APPLICATION OF PHASE CHANGE MATERIALS FOR THERMAL MANAGEMENT SYSTEM OF NEXT GENERATION AIRCRAFT
E. Revello¹, M. Boccaccio, Leonardo Labs, Italy; F. Acerra, Leonardo SpA, Italy; A. Monteverde¹; ¹Politecnico di Torino, DISAT, Italy

Wednesday, 11. Sep 2024


0.6ICAS LECTURE FOR INNOVATION IN AERONAUTICS: Helen Webber: Ongoing Innovation at Reaction Engines
Chair: C. Atkin ICAS Programme Committee Chair
11. Sep 24 08:30 09:30

0.7INTERACTIVE PRESENTATIONS (Coffee Break 09:30-10:00)
Chair:
11. Sep 24 09:30 11:00

1.7GSA - Propulsion & Energy 1
Chair(s): Haselbach, F.
Track 1 Auditorium
15 - Guest lectures
11. Sep 24 11:00 11:25 1.7.1
1233
BARRIERS TO MW CLASS ELECTRIFIED POWERTRAIN AIRCRAFT PROPULSION SYSTEMS
G. Bezos O Connor, NASA (LaRC), United States
11. Sep 24 11:25 11:50 1.7.2
1245
NASA HYBRID THERMALLY EFFICIENT CORE (HYTEC) PROJECT OVERVIEW
A.L. Nerone¹, J.M. Haglage¹, L.M. Nakley¹, R. Tornabene¹; ¹NASA (GRC), United States
11. Sep 24 11:50 12:15 1.7.3
1265
JAXA EN-CORE PROJECT OVERVIEW AND ACHIEVEMENTS
T. Yamane, Japan Aerospace Exploration Agency, Japan
11. Sep 24 12:15 12:40 1.7.4
1274
Q&A - MINI PANEL
QA A,
2.7High Lift Common Research Model Ecosystem (CRM-HL) 1
Chair(s): Slotnick, J.
Track 2 Sala Verde
15 - Guest lectures
11. Sep 24 11:00 11:25 2.7.1
1210
A CFD VALIDATION ECOSYSTEM TO ADVANCE THE PREDICTION OF LOW-SPEED AERODYNAMICS
J.P. Slotnick, Boeing, United States
11. Sep 24 11:25 11:50 2.7.2
1212
CHALLENGES IN GEOMETRY DEVELOPMENT FOR THE CRM-HL ECOSYSTEM
A.M. Clark¹, D.S. Lacy¹; ¹Boeing Commercial Airplanes, United States
11. Sep 24 11:50 12:15 2.7.3
1213
NASA CONTRIBUTIONS TO THE HIGH LIFT COMMON RESEARCH MODEL ECOSYSTEM
M. Rivers, United States
11. Sep 24 12:15 12:40 2.7.4
1214
THE CRM-HL ECOSYSTEM - DLR CONTRIBUTIONS
R. Rudnik¹, S. Pülm¹, F. Schmidt¹, J. Wild¹, A. Schröder¹, C. Spehr¹, P. Mühlmann¹; ¹DLR, Germany
3.7Design of Sustainable Aircraft 2 (Climate Impact)
Chair(s): Bagassi, S.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
11. Sep 24 11:00 11:25 3.7.1
0399
CLIMATE IMPACT AND ECONOMIC ASSESSMENT OF LIQUID HYDROGEN AND SYNTHETIC KEROSENE LONG-RANGE AIRCRAFT CONCEPTS
S. Wöhler¹, K. Buchtal¹, M. Iwanizki¹, J. Häßy¹, K. Dahlmann¹, C. Lois¹, M. Hepperle¹; ¹DLR, Germany
11. Sep 24 11:25 11:50 3.7.2
0585
SUSTAINABLE AVIATION IN NORDIC COUNTRIES
C. Jouanet¹, K. Amadori¹, E. Espinoza Juarez¹; ¹Linköpings University, Sweden
11. Sep 24 11:50 12:15 3.7.3
0088
A PROPOSAL TOWARDS A STEP CHANGE FROM ECO-DRIVEN TO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT COMPONENTS
A. Filippatos¹, D.N. Markatos¹, A. Theochari¹, S. Malefaki¹, T. Kalampoukas¹, S.G. Pantelakis¹; ¹University of Patras, Greece
11. Sep 24 12:15 12:40 3.7.4
0723
ON THE EXISTENCE OF A FAMILY OF IDEAL AIRCRAFT CONFIGURATIONS
R.J. Huyssen, CSIR, South Africa; G.R. Spedding, University of Southern California, United States
4.7LH 2 Fuel Tank Configurations
Chair(s): Padulo, M., Imamura, T.
Track 4 Brunelleschi
01.1 - Aircraft Design and Integrated System (Basics and Theory)
11. Sep 24 11:00 11:25 4.7.1
0193
CRYOGENIC TANK SIZING MODEL FOR THE CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT
G. Licheva¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada
11. Sep 24 11:25 11:50 4.7.2
0590
HYDROGEN STORAGE SYSTEM DESIGN: CASE STUDIES FOR AIRBORNE APPLICATION
F. Mazzoni¹, G. Accardo², R. Biga², E. Brusa¹, C. Delprete¹, C.A. Manrique-Escobar², V. Vercella²; ¹Politecnico di Torino, Italy ;²Leonardo S.p.A., Italy
11. Sep 24 11:50 12:15 4.7.3
0439
INTEGRATING CRYOGENIC TANKS MODEL IN HYDROGEN AIRCRAFT DESIGN FOR PARAMETRIC PERFORMANCE ANALYSIS
R. Parello, ONERA/ISAE-SUPAERO, France; S. Defoort, ONERA, France; E. Benard¹, Y. Gourinat¹; ¹ISAE-SUPAERO, France
11. Sep 24 12:15 12:40 4.7.4
0515
HYDROGEN AIRLINER TANK OPTIMISATION
P. De Felipe¹, C. Cumpsty¹, I. Iturriaga¹, H. Dance¹; ¹ZeroAvia, United Kingdom
5.7Sustainable Aviation 3
Chair(s): Ying, S.
Track 5 Donatello
01.2 - Aircraft Design and Integrated System (Applications)
11. Sep 24 11:00 11:25 5.7.1
1090
ARCHITECTURE DESIGN FOR A COMMERCIALLY VIABLE HYDROGEN-ELECTRIC POWERED RETROFITTED REGIONAL AIRCRAFT
B. Rietdijk¹, M. Selier¹; ¹Conscious Aerospace, Netherlands
11. Sep 24 11:25 11:50 5.7.2
0222
ENVIRONMENTAL IMPLICATIONS OF HYBRID-ELECTRIC REGIONAL AIRCRAFT: EMISSIONS AND CLIMATE CHANGE
K. Abu Salem¹, G. Palaia¹; ¹Politecnico di Torino, Italy
11. Sep 24 11:50 12:15 5.7.3
0091
CLEANSKY2/ CLEAN AVIATION LARGE PASSENGER AIRCRAFT FOR MORE SUSTAINABLE COMMERCIAL FUSELAGE TECHNOLOGIES – MAJOR ACHIEVEMENTS
Y.C. Roth¹, R. Herrmann¹, C. Sanchez Santos, Aernnova, Spain; M. Uellendahl, Airbus Aerostructures, Germany; J. Koopman, GKN Fokker Aerospace, Netherlands; A. Henneberg, Diehl Aviation, Germany; J. Kos, Royal Netherlands Aerospace Centre, Netherlands; I.F. Villegas, Delft University of Technology, Netherlands; A. Choudhary, SAMXL, Netherlands; L. Larsen, DLZ Zentrum für Leichtbauproduktionstechnologie, Germany; S. Ferstl, Premium Aerotec, Germany; B. Diehl, Fraunhofer, Germany; F. Emanuelsson, Saab Aerospace Systems, Sweden; J.-B. Sinechal¹, M. Pleth¹, K. Atherton¹; ¹Airbus, Germany
11. Sep 24 12:15 12:40 5.7.4
0813
ANALYSIS OF BATTERY WEIGHT REQUIREMENTS IN THE DESIGN OF HYBRID ELECTRIC POWERED AIRCRAFT
D. Liu¹, Z. Chen¹, Z. Guo¹, B. Zhu¹, G. Jia¹, X. Yang¹; ¹National University of Defense Technology, China
6.7Shock Interactions
Chair(s): Stumpf, E., Fu, S.
Track 6 Cimabue
03.3 - Basic Fluid Dynamics and Flow Control
11. Sep 24 11:00 11:25 6.7.1
0067
A BRIEF REVIEW OF PANEL AEROELASTICITY WITH SHOCK INTERACTION
A. Shi, China; Y. He, China; E.H. Dowell, United States
Presenter: Yiwen He
11. Sep 24 11:25 11:50 6.7.2
0792
ACTIVE-PASSIVE HYBRID CONTROL OF SHOCK BUFFET
C.Q. Gao, China; K. Ren, China; W.W. Zhang, China
11. Sep 24 11:50 12:15 6.7.3
0569
WALL TEMPERATURE EFFECTS ON AERODYNAMIC HEATING MECHANISMS IN SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION
Z.Y. Tang, China; H.N. Xu, China; X.Y. Li, China; J. Ren, China
7.7EVTOL Concepts
Chair(s): Bezos O Connor, G., Cinar, G.
Track 7 Botticelli
15 - Guest lectures
11. Sep 24 11:00 11:25 7.7.1
0973
PSYCHOACOUSTICAL ANALYSIS OF SYNTHESIZED MOTOR-PROPELLER ROTOR SYSTEM NOISE
J.H. Jeong, Korea Aerospace Research Institute, South Korea; J.W. Ko, Korea Aerospace University, South Korea
11. Sep 24 11:25 11:50 7.7.2
0329
INFLUENCE OF MOTOR CHARACTERISTICS ON OPTIMAL PROPROTOR DESIGN
S. Shahjahan¹, D. Verstraete¹; ¹The University of Sydney, Australia
11. Sep 24 11:50 12:15 7.7.3
0940
NOVEL SOFTWARE-DRIVEN VARIABLE-PITCH AND LEVEL FLIGHT CONTROL SYSTEM: PRINCIPLES AND APPLICATIONS FOR SMALL AIRCRAFT WITH A QUADROTOR CASE STUDY
X. Xiong¹, S. Wu¹; ¹International WYNNBEAR Advanced AeroTech Innovation, United States
11. Sep 24 12:15 12:40 7.7.4
1132
CHALLENGES OF INTEGRATING PHOTOVOLTAIC CELLS ONTO THE WINGS OF AN UNMANNED SOLAR-POWERED AIRCRAFT
R. Lopusiewicz¹, N. Ksiazek¹; ¹AGH University of Krakow, Poland
Presenter: Roza Lopusiewicz, AGH University of Krakow
8.7Airframe Aeroacoustics
Chair(s): de Vries, R.
Track 8 Vasari
03.4 - Applied Aerodynamics
11. Sep 24 11:00 11:25 8.7.1
0361
SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT
A. Glorioso¹, F. Petrosino², M. Barbarino², G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy ;²CIRA, Italy
Presenter: Antimo Glorioso, University of Campania
11. Sep 24 11:25 11:50 8.7.2
0373
SPARSE POLYNOMIAL CHAOS-BASED SONIC BOOM UNCERTAINTY QUANTIFICATION AND AERODYNAMIC/SONIC BOOM ROBUST DESIGN OPTIMIZATION UNDER MULTI-PARAMETER UNCERTAINTIES
S. Wang¹, H. Zhao¹, K. Gan¹, Z. Gong¹, Y. Gan¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
11. Sep 24 11:50 12:15 8.7.3
0471
NUMERICAL EVALUATION FOR FAN-NOISE SHIELDING EFFECTS ON AFT-FUSELAGE MOUNTED AND EMBEDDED ENGINES
T. Ikeda¹, R. Furuya, Ryoyu Systems, Japan; M. Murayama¹; ¹JAXA, Japan
11. Sep 24 12:15 12:40 8.7.4
0069
REFINED PREDICTIONS COMPARED WITH THE PROPULSION AIRFRAME AEROACOUSTICS AND AIRCRAFT SYSTEM NOISE FLIGHT RESEARCH TEST DATA
R.H. Thomas¹, Y. Guo, NASA Langley Reseach Center, United States; E.H. Nesbitt¹, I.A. Clark¹, J.C. June¹; ¹NASA Langley Research Center, United States
9.7Trajectory Management
Chair(s): Enea, G., Harigae, M.
Track 9 Giotto
09 - Air Transport System Efficiency
11. Sep 24 11:00 11:25 9.7.1
0685
SPEED GATED INTERCEPT PROCEDURE STUDY FOR INTEGRATION OF INCREASING DIVERSE OPERATIONS (IDO) AT EUROPEAN AIRPORTS
T. Welsch¹, M.-M. Temme¹; ¹DLR, Germany
11. Sep 24 11:25 11:50 9.7.2
0968
VALIDATING FLOW-BASED EN ROUTE AMAN COUPLING ESCAPE LIGHT WITH AIRTOP SOFTWARE
K. Sekine¹, P. Bouchaudon, EUROCONTROL Innovation Hub, France; T. Tatsukawa¹, K. Fujii¹, E. Itoh, The University of Tokyo, Japan; ¹Tokyo University of Science, Japan
11. Sep 24 11:50 12:15 9.7.3
1165
CANCELED - ON THE POSITION ACCURACY NEEDED FOR SAFE SEPARATION OF FLIGHT ALONG CORRIDORS
L.M.B.C. Campos¹, J.M.G. Marques, Escola de Ciências e Tecnologias, Universidade de Évora, Portugal; P.A. Serrão¹; ¹IDMEC/CCTAE - IST, Portugal
11. Sep 24 12:15 12:40 9.7.4
1177
FEASIBILITY STUDY ON OPERATIONAL FLIGHT PLANS ADAPTED FOR TRAJECTORY BASED OPERATION
A. Harada, Kyushu University, Japan; N. Takeichi, Tokyo Metropolitan University, Japan; T. Masuki¹, H. Nakahata¹, S. Inohata¹, N. Nagata¹, A. Yasuda¹; ¹Japan Airlines Co., Ltd., Japan
10.7Structural Measurement Techniques
Chair(s): Petrone, G., Camanho, P.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
11. Sep 24 11:00 11:25 10.7.1
0923
LASER SHEAROGRAPGY-PREDICTION AND OPTIMIZING ITS FLAW DETECTION CAPABILITIES USING AN ADVANCED HYBRID APPROACH
Y. Elbaz, Technion, I.I.T.., Israel; H. Abramovich, Technion, I.I.T., Israel
11. Sep 24 11:25 11:50 10.7.2
0633
FATIGUE PROPERTIES OF ADDITIVELY MANUFACTURED TOOL STEEL
C.M. Johnston¹, L.C. Tshabalala¹, M. Davids, University of the Witwatersrand, South Africa; ¹CSIR, South Africa
11. Sep 24 11:50 12:15 10.7.3
0830
DEVELOPMENT AND ANALYSIS OF THE THEORY OF COMPOSITE EXPANSION RING UNDER ELECTROMAGNETIC LOADING
Z.-X. Liu¹, J. Liu¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
additional information (interactive) 10.7.R
0525
DEVELOPMENT OF A MACHINE LEARNING-BASED STRESS SPECTRUM ESTIMATION TECHNIQUE FOR FATIGUE MONITORING
E.G. Park, South Korea; S.H. Jeong, South Korea; J.Y. Cho, South Korea; J.H. Kim, South Korea
additional information (interactive) 10.7.R
0739
FULLY-EMBEDDED PRESSURE SENSOR FOR AERODYNAMICS SURFACES BASED ON FBG TECHNOLOGY
P.E. Boffa¹, E. Casciaro¹, P. Bettini¹; ¹Politecnico di Milano, Italy
11.7Aeroelastic Tailoring 1
Chair(s): Petrolo, M., Filippi, M.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
11. Sep 24 11:00 11:25 11.7.1
1097
STOCHASTIC BUCKLING ANALYSES OF LAMINATED COMPOSITE PLATES UNDER HYGROTHERMAL, GEOMETRIC AND MATERIAL UNCERTAINTIES MODELED AS NON-GAUSSIAN RANDOM FIELDS
H.E.A.A. Santos, Embraer S.A., Brazil; D.A. Rade, Aeronautics Institute of Technology, Brazil
11. Sep 24 11:25 11:50 11.7.2
0479
SANDWICH COMPOSITES SKIN PANEL OPTIMIZATION FOR THE COMMON RESEARCH MODEL WING
Y.M. Meddaikar¹, J.K.S. Dillinger¹, W.R. Krüger¹, R. De Breuker, Delft University of Technology, Netherlands; G.H. Silva¹, P.H. Cabral², A.P. do Prado²; ¹DLR - Institute of Aeroelasticity, Germany ;²Embraer S.A., Brazil
11. Sep 24 11:50 12:15 11.7.3
0167
AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING AEROELASTIC TAILORING BASED ON VIRTUALLY-GENERATED ALLOWABLES AND HIGH ORDER FINITE ELEMENTS FOR IMPROVED COMPOSITE WING DESIGN
P.H. Cabral¹, A.P. do Prado¹, E. Carrera², A. Pagani², A. Racionero Sánchez-Majano², M. Enea²; ¹Embraer S.A., Brazil ;²Politecnico di Torino, Italy
12.7Structural Design and Optimization 4
Chair(s): Cooper, J.E., Pagani, A.
Track 12 Petrarca
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
11. Sep 24 11:00 11:25 12.7.1
0111
STRUCTURAL AND AEROELASTIC OPTIMISATION OF A LARGE AIRCRAFT WING WITH A PASSIVE TWIST WINGTIP
Y.J. Pan¹, M. Alam¹, A. Spinelli¹, E. Bragado Aldana¹; ¹Cranfield University, United Kingdom
11. Sep 24 11:25 11:50 12.7.2
0115
DEVELOPMENT OF A MASS EVALUATION TOOL FOR CLASSICAL AND DISRUPTIVE AIRCRAFT STRUCTURES
V. Priasso¹, A. Lannoo¹; ¹DMAS, ONERA, France
Presenter: Valentin Priasso, ONERA
11. Sep 24 11:50 12:15 12.7.3
1035
STRUCTURAL DESIGN OF NEXT-GENERATION REGIONAL GREEN AIRCRAFT
L. Pustina¹, F. Mastroddi¹, P. Della Vecchia, University of Naples “Federico II”, Italy; G. Cerino, LEONARDO, Aircraft Division, Italy; ¹Sapienza University of Rome, Italy
11. Sep 24 12:15 12:40 12.7.4
0837
MULTIPHYSICS MODELING FOR SAFE BATTERIES USING LS-DYNA
G. Di Mauro¹, M. Guida¹, G. Olivares², L.M. Gomez²; ¹University of Naples Federico II, Italy ;²Jerry Moran Center, AVET, NIAR, WSU, United States
13.7High Speed and Cavity Flows
Chair(s): Barbarino, M., Viviani, A.
Track 13 Boccaccio
03.1 - Aerodynamics – CFD Methods and Validation
11. Sep 24 11:00 11:25 13.7.1
0877
AERO-THERMAL ANALYSIS OF A REUSABLE LAUNCH VEHICLE DURING RE-ENTRY MANOEUVRER
A. Assonitis¹, R. Paciorri ¹, V. Orlandini¹, A. Neri, ESA ESRIN, Italy; ¹University of Rome La Sapienza , Italy
Presenter: Valerio Orlandini, University of Rome La Sapienza
11. Sep 24 11:25 11:50 13.7.2
0709
RESEARCH ON AIRSPEED CORRECTION TECHNOLOGY OF EJECTION SEAT BASED ON CFD
L. Jin¹, G. Feng¹, L. Wu¹; ¹Overall Technology R&D Department, AVIC Aerospace Life-support I, China
11. Sep 24 11:50 12:15 13.7.3
0558
AEROACOUSTIC CAVITY FLOW ENERGY HARVESTING
J.M. Kirkness-Duncombe¹, N.J. Lawson¹, G.A. Vio², S.D. Moss², D.J. Munk²; ¹The University of Sydney, Department of Aeronautical Engineering, Australia ;²Defence Science and Technology Group, Aerospace Division, Australia
11. Sep 24 12:15 12:40 13.7.4
0783
NUMERICAL INVESTIGATION OF THE INTERACTION OF OPPOSING JETS AND SUPERSONIC FREE FLOWS
Z.K. Liu¹, Y.L. Liu¹, Q.Z. Li¹, G. Wang¹; ¹Northwestern Polytechnical University, China
14.7Accident Prevention & Survivability 1
Chair(s): Boucher, A.
Track 14 Puccini
10 - Safety and Security
11. Sep 24 11:00 11:25 14.7.1
0127
FROM THA TO REAL-TIME MONITORING: INTEGRATING NEW VIEW OF SAFETY INTO FLIGHT TEST PROGRAMS
T.F. Macedo¹, M.M. Cardoso Junior¹; ¹Technological Institute of Aeronautics, Brazil
Presenter: MOACYR Cardoso-Junior, Technological Institute of Aeronautics
11. Sep 24 11:25 11:50 14.7.2
0214
REMOTE OBSERVATION EXPERIMENT OF VOLCANIC ASH USING POLARIZATION LIDAR
H. Inokuchi¹, H. Oikawa¹, G. Morimoto, Metro Weather Co., Ltd, Japan; S. Inaka¹; ¹JAXA, Japan
11. Sep 24 11:50 12:15 14.7.3
0700
COMPARATIVE ANALYSIS OF EVTOL, DRONE AND GROUND TRANSPORTATION SYSTEMS FOR EMERGENCY DELIVERY OF BLOOD-DERIVED MEDICATION
D. Angelini¹, E. Cestino¹, D. Cestino², F. Cattel²; ¹Politecnico di Torino, Italy ;²A.O.U. Città della Salute e della Scienza di Torino, Italy
11. Sep 24 12:15 12:40 14.7.4
0707
ENABLING AIRWORTHINESS SECURITY BY A HOLISTIC SECURITY ENGINEERING PROCESS AT VARIOUS AIRCRAFT DESIGN LEVELS
M. Blecken¹, H. Hintze¹, R. God¹; ¹Hamburg University of Technology, Germany
15.7Innovative UAV Technologies
Chair(s): Grabowski, T.
Track 15 Carducci
06.2 - Flight Dynamics and Control (UAV related)
11. Sep 24 11:00 11:25 15.7.1
0516
DYNAMICS OF THE MECHANISM FOR VENTILATION ACROSS FEATHERS IN FLAPPING WING UAV
R.C. Silva¹, D.D. Bueno¹; ¹UNESP, Brazil
11. Sep 24 11:25 11:50 15.7.2
0778
TRAJECTORY OPTIMIZATION OF EVTOL VEHICLES FOR URBAN AIR MOBILITY USING INDIRECT METHODS
K. Mall¹, R. Gadre¹, J. Gerardus¹, D.A. DeLaurentis¹; ¹Purdue University, United States
11. Sep 24 11:50 12:15 15.7.3
0984
IN-FLIGHT VIBRATION SIGNAL BASED DETECTION AND LOCALIZATION FOR UAV PROPELLER ANOMALIES UNDER UNCERTAINTY VIA MACHINE LEARNING TYPE METHODS
I.A. Iliopoulos¹, J.S. Korolis¹, S.D. Fassois¹, J.S. Sakellariou¹; ¹University of Patras, Greece
11. Sep 24 12:15 12:40 15.7.4
0548
STUDY ON CONTROL PERFORMANCE OF A NEW TYPE OF TILT-ROTOR AIRCRAFT
K. Miyabe¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu Univercity, Japan
additional information (interactive) 15.7.R
0578
DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE
L. Wang¹, X. Yang¹, Y. Luo¹, H. Chen¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
16.7Advanced Manufacturing Technology 2
Chair(s): Lin, K., Jiang, L.
Track 16 Raffaello
08 - Manufacturing and Supply Chain Management
11. Sep 24 11:00 11:25 16.7.1
1152
AN ONTOLOGY-BASED APPROACH FOR THE CO-DEVELOPMENT AND OPTIMIZATION OF AIRCRAFT CABIN DESIGN AND ASSEMBLY ARCHITECTURES
Y. Ghanjaoui¹, J.H. Bussemaker¹, J. Biedermann¹, B. Nagel¹; ¹DLR, Germany
11. Sep 24 11:25 11:50 16.7.2
1127
FRICTION RIVETING OF THERMOPLASTIC COMPOSITE WITH A CNC MACHINE: EXPERIMENTAL WORK
I. Tan¹, G. Cohen¹, A.-C. Araujo¹, A. Daidié¹; ¹Institut Clément Ader, France
11. Sep 24 11:50 12:15 16.7.3
0306
PRELIMINARY RESULTS FOR AN INSTRUCTION DESIGN PROCEDURE IN AERONAUTICAL MANUFACTURING
M. Bartolomei¹, F. Barravecchia¹, L. Mastrogiacomo¹, F. Franceschini¹, F. Acerra², D.M. Gatta², D. Cannizzaro²; ¹Politecnico di Torino, Italy ;²Leonardo S.p.A, Italy
11. Sep 24 12:15 12:40 16.7.4
0262
SURFACE MORPHOLOGY AND MICROSTRUCTURAL FEATURES OF ELECTRON BEAM SURFI-SCULPTED TI-6AL-4V ALLOY
K. Li¹, P. Fu¹, Z. Tang¹, B. Zhang¹, Y. Ma, Chongqing University of Technology, China; ¹AVIC Manufacturing Technology Institute, China
17.7Digital Processes for Non-Destructive Evaluation
Chair(s): Couldrick, J., Marzocca, P.
Track 17 Galileo
11 - Operations and Sustainment
11. Sep 24 11:00 11:25 17.7.1
0020
MIXED REALITY FOR AIRCRAFT STRUCTURAL DENT AND BUCKLE NON-DESTRUCTIVE EVALUATION
A.-K. Koschlik¹, M.J. Scott², T. Keser¹, F. Rauscher¹, H. Meyer¹, W. Verhagen², P. Marzocca², F. Raddatz¹, G. Wende¹; ¹DLR, Germany ;²RMIT, Australia
11. Sep 24 11:25 11:50 17.7.2
0152
CINNABAR PROJECT - AUGMENTED REALITY WORKFLOW FOR AIRCRAFT DENT & BUCKLE INSPECTION
T. Keser¹, R. Schmied-Kowarzik¹, A.-K. Koschlik¹, L. Kaschub², M.J. Scott, RMIT University, Australia; R. Rodeck², G. Wende²; ¹German Aerospace Center (DRL), Germany ;²German Aerospace Center (DLR), Germany
11. Sep 24 11:50 12:15 17.7.3
0164
CINNABAR PROJECT: EXAMINING REQUIREMENTS FOR USER ACCEPTANCE OF AIRCRAFT STRUCTURE INSPECTION IN AUGMENTED REALITY
R. Schmied-Kowarzik¹, T. Keser¹, L. Kaschub¹, A.-K. Koschlik¹, R. Rodeck¹, G. Wende¹; ¹German Aerospace Center (DLR), Germany
11. Sep 24 12:15 12:40 17.7.4
0125
CINNABAR PROJECT – COST-BENEFIT ANALYSIS OF DIGITAL PROCESSES FOR NON-DESTRUCTIVE INSPECTIONS OF AIRCRAFT STRUCTURES
J. Aigner¹, A.-K. Koschlik¹, H. Meyer¹, F. Raddatz¹, G. Wende¹; ¹German Aerospace Center (DLR), Germany
additional information (interactive) 17.7.R
0065
DIGITAL TWIN OF AN AIRCRAFT LANDING GEAR TO ENHANCE FAILURE ANALYSIS AND MANAGE PREDICTIVE MAINTENANCE
D.Y. Sabag¹, O. Yakimenko, Naval Postgraduate School, United States; H. Alian¹; ¹Israeli Air Force, Israel

12:30 - 13:30LUNCH

0.8GENERAL LECTURE 2 ISABE: Frank Haselbach: ISABE and the runway towards sustainable aviation
Chair: S. Bagassi ICAS Executive Committee Member
11. Sep 24 13:30 14:30

1.8GSA - Propulsion & Energy 2
Chair(s): Murphy, A.
Track 1 Auditorium
15 - Guest lectures
11. Sep 24 14:30 14:55 1.8.1
1308
SAFRAN PROPULSION STRATEGY AND ROADMAP FOR FUTURE SUSTAINABLE AVIATION
D Dijoud, France
11. Sep 24 14:55 15:20 1.8.2
1257
MTU’S ROADMAP TOWARDS SUSTAINABLE PROPULSION
F. Donus, MTU, Germany
11. Sep 24 15:20 15:45 1.8.3
1306
DELIVERING THE ROLLS-ROYCE NET ZERO ROADMAP
T Newby, Rolls-Royce plc, United Kingdom
11. Sep 24 15:45 16:10 1.8.4
1275
Q&A - MINI PANEL
QA A,
2.8High Lift Common Research Model Ecosystem (CRM-HL) 2
Chair(s): Rivers, M.
Track 2 Sala Verde
15 - Guest lectures
11. Sep 24 14:30 14:55 2.8.1
1216
BOEING CONTRIBUTIONS TO THE CRM-HL ECOSYSTEM
K. Hood, United States
11. Sep 24 14:55 15:20 2.8.2
1215
TEST SUMMARY OF THE FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL
T. Hashioka¹, Y. Murahashi¹, H. Yasuda¹, Y. Sawaki¹, S. Onda¹, Y. Tsuchimoto¹, Y. Nishizaki¹, W. Suzuki¹, T. Kawamura¹; ¹Kawasaki Heavy Industries, Ltd., Japan
11. Sep 24 15:20 15:45 2.8.3
1238
ACTIVITY PLANS USING CRM-HL AT JAXA
M. Kohzai, Japan
11. Sep 24 15:45 16:10 2.8.4
1284
PANEL DISCUSSION
P D, United States
3.8AI in Systems Design
Chair(s): Conway, S., Jouannet, C.
Track 3 Michelangelo
02 - Systems Engineering and Integration
11. Sep 24 14:30 14:55 3.8.1
0514
LARGE LANGUAGE MODEL IN AIRCRAFT SYSTEM DESIGN
P. Krus, Linköping University, Sweden
11. Sep 24 14:55 15:20 3.8.2
0869
APPLYING MODEL-BASED SYSTEM ENGINEERING AND DEVOPS ON THE IMPLEMENTATION OF AN AI-BASED COLLISION AVOIDANCE SYSTEM
T. Stefani¹, J.M. Christensen¹, E. Hoemann¹, A. Anilkumar Girija¹, F. Köster, DRL, Germany; T. Krüger¹, S. Hallerbach¹; ¹DLR, Germany
11. Sep 24 15:20 15:45 3.8.3
0397
A HUMAN-CENTERED SYSTEMS ENGINEERING APPROACH FOR INTEGRATING ARTIFICIAL INTELLIGENCE IN AVIATION: A REVIEW OF AI SYSTEMS
L.D.O. Morais¹, P. Krus, Linköping University, Sweden; L. Pereira¹; ¹UFABC, Brazil
11. Sep 24 15:45 16:10 3.8.4
1116
AN AUTONOMOUS SYSTEM FOR DOCKING AND BATTERY SWAPPING IN UAVS
I. Kute¹, J. Dagli¹, E. Khot¹, R. Verma¹, P. Gupta¹, D. Shukla¹, R. Pant¹; ¹Indian Institute of Technology Bombay, India, India
additional information (interactive) 3.8.R
0148
AUTOMATING THE VERIFICATION OF GEOMETRIC REQUIREMENTS FOR AIRCRAFT FUEL SYSTEMS USING KNOWLEDGE-BASED ENGINEERING
B. Boden¹, M. Padilha¹, T. Burschyk¹, C. Cabaleiro de la Hoz¹, E. Moerland¹, M. Fioriti, Politecnico di Torino, Germany; ¹DLR, Germany
4.8Unmanned Aerial Systems and Advanced Aerial Mobility 1
Chair(s): Lott, M.
Track 4 Brunelleschi
01.2 - Aircraft Design and Integrated System (Applications)
11. Sep 24 14:30 14:55 4.8.1
0151
A DESIGN APPROACH FOR A MODEL-SCALE VTOL POWERED BY TWO PIVOTING KEROSENE TURBINES
T. Müller¹, V. Gollnick¹; ¹Institute of Air Transportation Systems, Germany
11. Sep 24 14:55 15:20 4.8.2
0172
ENERGY AND EMISSION ANALYSIS OF AN AIR-TAXI SERVICE USING DYNAMIC EVTOL SYSTEM MODELS
N. Prabhakar¹, F. Salucci¹, D. Karbowski¹; ¹Argonne National Laboratory, United States
11. Sep 24 15:20 15:45 4.8.3
0267
SCALED FLIGHT TESTING FOR EVALUATING DISTRIBUTED ELECTRIC PROPULSION
H. Jentink, Royal Netherlands Aerospace Centre NLR, Netherlands; C. Döll, ONERA, France; P. Iannelli, CIRA, Italy; M. Hoogreef, TU Delft, Netherlands; D. Kierbel, Airbus, France
11. Sep 24 15:45 16:10 4.8.4
0352
DETERMINISTIC HYBRID POWER RATIOS CONSIDERING VARIOUS FAILURE CASES FOR QUAD TILTROTOR AIRCRAFT
M. Park¹, N. Roh¹; ¹Hanwha systems, South Korea
Presenter: Minjun Park, Hanwha Systems
Reserve Paper 4.8.R
0036
RETROFITTING A JET DRIVEN UAV TO FORM A MULTI-PURPOSE TEST PLATFORM
D. Teubl¹, T.B. Sissing¹, M. Hornung¹; ¹Chair of Aircraft Design, Technical University of Munich, Germany
Reserve Paper 4.8.R
0785
A STUDY ON BATTERY SEPARATION DRONES TO EXTEND ENDURANCE
H. Kim¹, T. Kim, Seoul Digital University, South Korea; C. Son¹; ¹Cheongju University, South Korea
5.8Hypersonic Aerodynamics 2
Chair(s): Pezzella, G., Halila, G.
Track 5 Donatello
03.1 - Aerodynamics – CFD Methods and Validation
11. Sep 24 14:30 14:55 5.8.1
0363
LAUNCH SYSTEM ASSESSMENT OF AN EXPERIMENTAL HYPERSONIC SCRAMJET VEHICLE
F. Cascone¹, P. Roncioni¹, O. Russo¹, M. Marini¹, S. Di Benedetto¹, M. Albano², R. Bertacin², G. Ranuzzi²; ¹CIRA, Italy ;²ASI, Italy
Presenter: Pietro Roncioni, CIRA
11. Sep 24 14:55 15:20 5.8.2
0576
STABILITY CHARACTERISTICS OF CROSSFLOW MODES IN HYPERSONIC BOUNDARY LAYER WITH EXPANSION CORNER
P. Lu¹, Y. Xi¹, J. Sun¹, S. Fu¹; ¹Tsinghua University, China
11. Sep 24 15:20 15:45 5.8.3
0907
NUMERICAL INVESTIGATION OF HYPERSONIC FLOWS
C.-S. Dikmen¹, M.-N. Yüksel¹, M. Yumusak¹; ¹Roketsan, Turkey
11. Sep 24 15:45 16:10 5.8.4
1175
DETACHED EDDY SIMULATION OF HYPERSONIC SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE-CYLINDER-FLARE
R.O. Bura, Republic Indonesia Defense University, Indonesia; A. Riyadl, National Research and Innovation Agency, Indonesia
Presenter: Romie Bura, Republic of Indonesia Defense University
6.8Lift & Wake Characteristics
Chair(s): Breitsamter, C.
Track 6 Cimabue
03.3 - Basic Fluid Dynamics and Flow Control
11. Sep 24 14:30 14:55 6.8.1
0034
NUMERICAL SIMULATION OF FLOWS AROUND AN AIRFOIL DURING ACCELERATED AND DECELERATED FLIGHT
R. Yamashita, The University of Tokyo, Japan
11. Sep 24 14:55 15:20 6.8.2
0655
NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF HOVERING ROTOR IN GROUND EFFECT
X.-L. Li¹, J.-H. Xu¹, W.-P. Song¹, S.-Q. Han, Sichuan University, China; Z.-H. Han¹; ¹ Northwestern Polytechnical University, China
11. Sep 24 15:20 15:45 6.8.3
0995
NONLINEAR DROPLET DYNAMICS IN IDEALIZED TRAILING VORTICES
O. Avni¹, Y. Dagan¹; ¹Technion - Israel Institute of Technology, Israel
11. Sep 24 15:45 16:10 6.8.4
1153
FLYING WING CIRCULATION DISTRIBUTIONS, AERODYNAMIC PERFORMANCE AND WAKE ROLL-UP
H.W.M. Hoeijmakers¹, M.P.J Sanders¹, L.H. Groot Koerkamp¹, A. van Garrel¹, C.H. Venner¹; ¹University of Twente, Netherlands
7.8Rotary Wing and VTOL Aerodynamics
Chair(s): Xi, Y.
Track 7 Botticelli
03.2 - Experimental Aerodynamics
11. Sep 24 14:30 14:55 7.8.1
0412
ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP
V. Gollnick¹, J. Luehrmann¹, F. Danquah¹, A. Semke¹, T. Mueller¹, J. Thoeben¹; ¹Hamburg University of Technology, Germany
11. Sep 24 14:55 15:20 7.8.2
0978
AERODYNAMIC INTERACTION EFFECTS OF TILTROTOR EVTOL AIRCRAFT
C. Moreira¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
11. Sep 24 15:20 15:45 7.8.3
0257
PIV AND AERODYNAMIC FORCES ANALYSIS OF A HELICOPTER OPERATING AROUND A BUILDING BY WIND-TUNNEL EXPERIMENTS
R. Bardera¹, J.C. Matias¹, E. Barroso¹; ¹Instituto Nacional de Técnica Aeroespacial, Spain
11. Sep 24 15:45 16:10 7.8.4
0790
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON AERODYNAMIC PERFORMANCE OF A MARS ROTOR SYSTEM
Y. Liu¹, J. Xiao¹, N.A. Benai-dara¹, Z. Chen¹, N. Qin, University of Sheffield, United Kingdom; ¹NUAA, China
8.8Propeller Noise and Performance
Chair(s): Huyssen, J.
Track 8 Vasari
03.4 - Applied Aerodynamics
11. Sep 24 14:30 14:55 8.8.1
0857
A HYBRID APPROACH FOR RECONSTRUCTION OF TRANSONIC BUFFET AERODYNAMIC NOISE: INTEGRATING RANDOM FOREST AND COMPRESSIVE SENSING ALGORITHM
Q. Zhang, Northwestern Polytechnical University, China; W. Zhang, Northwestern Polytec, China
11. Sep 24 14:55 15:20 8.8.2
0411
AEROACOUSTICS INVESTIGATION OF PROPELLER LEADING EDGE TUBERCLES APPLIED TO ADVANCED AIR MOBILITY
D. Skrna, Austria; M. de Rosa Jacinto, Brazil; M. Berens, Germany
Presenter: Dominik Skrna, Technische Universität Wien
11. Sep 24 15:20 15:45 8.8.3
0507
OPERATIONAL LIMITS ASSESSMENT FOR HIGH-ALTITUDE LONG-ENDURANCE UAVS CONSIDERING PROPELLER ICING EFFECT
Y.H. Kim, South Korea; J.-H. Shin, South Korea; C.J. Woo, South Korea; C.K. Son, South Korea; K.J. Yee, South Korea
11. Sep 24 15:45 16:10 8.8.4
0901
NUMERICAL SIMULATION OF THE RESPONSE CHARACTERISTICS OF THE WING STRUCTURE OF A SEAPLANE PLANING IN WAVE
Z.-W. Lu¹, Y.-H. Li¹, J.-C. Chen¹, M.-B. Tong¹, B. Wu¹; ¹Nanjing University of Aeronautics and Astronautics, China
additional information (interactive) 8.8.R
0665
NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES
D. Guagliardo¹, E. Cestino¹, A. Virdis¹, A. Alfero¹, V. Sapienza¹; ¹Politecnico of Turin, Italy
9.8Climate Impact of Air Transport Systems
Chair(s): Finck, T,, Andreeva-Mori, A.
Track 9 Giotto
09 - Air Transport System Efficiency
11. Sep 24 14:30 14:55 9.8.1
0410
OVERVIEW OF FACTORS RELATED TO AIRCRAFT OPERATION ASSOCIATED WITH A NEGATIVE IMPACT ON THE ENVIRONMENT
D. Kacik, Warsaw University of Technology, Poland
11. Sep 24 14:55 15:20 9.8.2
0377
A COMPREHENSIVE METHODOLOGY FOR PERFORMING PROSPECTIVE LIFE CYCLE ASSESSMENTS OF FUTURE AIR TRANSPORT SCENARIOS
F. Pollet¹, T. Planès¹, S. Delbecq¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France
11. Sep 24 15:20 15:45 9.8.3
0096
MITIGATING THE CLIMATE IMPACT OF AVIATION BY OPERATIONAL MEANS - A COMPARATIVE STUDY FOR DIFFERENT WEATHER SITUATIONS
Z.L. Zengerling¹, M. Mendiguchia Meuser¹, A. Lau¹, V. Gollnick, Hamburg University of Technology (TUHH), Germany; ¹German Aerospace Center (DLR), Germany
11. Sep 24 15:45 16:10 9.8.4
0126
CHARACTERISING THE ROLE OF FLEET RENEWAL ON THE PATHWAY TO 2050: A EUROPEAN AIRLINE CASE STUDY
N. Barry¹, C. Gallagher¹, S. Fitzgerald, Ryanair, Ireland; C. Stuart¹; ¹Trinity College Dublin, Ireland
10.8SHM
Chair(s): Zappino, E., Marklund, P.O.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
11. Sep 24 14:30 14:55 10.8.1
0120
CONVOLUTIONAL NEURAL NETWORKS ALGORITHMS FOR STRUCTURAL HEALTH MONITORING OF AIRCRAFTS COMPOSITES PANELS
E. Monaco¹, F. Ricci¹; ¹Università di Napoli , Italy
11. Sep 24 14:55 15:20 10.8.2
0654
IMPROVING SHAPE SENSING OF AERONAUTICAL STRUCTURES WITH STRAIN PRE-EXTRAPOLATION AND SENSOR PLACEMENT OPTIMIZATION
E. Del Priore¹, L. Lampani¹; ¹Sapienza University of Rome, Italy
11. Sep 24 15:20 15:45 10.8.3
1135
STRUCTURAL HEALTH MONITORING OF CFRP DURING FATIGUE LOAD VIA THE ASSESSMENT OF CRACK DENSITY BY MEANS OF THERMOGRAPHY
R. De Finis, Università del Salento, Italy; D. Palumbo¹, U. Galietti¹; ¹Politecnico di Bari, Italy
11. Sep 24 15:45 16:10 10.8.4
1081
EMBEDDED SENSORS FOR AIRCRAFT PREDICTIVE MAINTENANCE: SHM SYSTEM INTEGRATION & TRADE-OFF ANALYSIS
V.M. Sharma¹, P. Jha¹, V. Samanyusree¹, A. Sharma¹, S. Maheshwari¹, G.S. Mamatha¹; ¹RV College of Engineering, India
additional information (interactive) 10.8.R
0316
THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW
W. Stryczniewicz¹, T. Kwiatkowski¹, I. Kaminska², M. Chojnacki², K. Fronc²; ¹?ukasiewicz Research Network - Institute of Aviation, Poland ;²Institute of Physics Polish Academy of Sciences, Poland
11.8Aeroelastic Tailoring 2
Chair(s): Petrolo, M., Filippi, M.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
11. Sep 24 14:30 14:55 11.8.1
0162
FAST TRANSONIC CORRECTIONS FOR PANEL METHODS USING VISCOUS-INVISCID INTERACTION
A. Crovato¹, P. Dechamps¹, A.P. Prado², P.H. Cabral², V.E. Terrapon¹, G. Dimitriadis¹; ¹University of Liège, Belgium ;²Embraer S.A., Brazil
11. Sep 24 14:55 15:20 11.8.2
0150
EXPLORING MULTI-FIDELITY AEROELASTIC TAILORING: PROSPECT AND MODEL ASSESSMENT
H.F. Maathuis¹, S.G.P. Castro¹, R. De Breuker¹; ¹Delft University of Technology, Netherlands
11. Sep 24 15:20 15:45 11.8.3
0322
A-BASIS AND B-BASIS BUCKLING ALLOWABLES FOR AN AIRCRAFT COMPOSITE WING
R.A.S. Cardoso¹, M.S. Reis¹, L.P.S. Ferreira, FEMTO-ST, France; M.P. Alves¹, S.K. Ha, Hanyang University, South Korea; C.A. Cimini Jr.¹; ¹Federal University of Minas Gerais, Brazil
11. Sep 24 15:45 16:10 11.8.4
0192
ENHANCING THE PERFORMANCE OF SLENDER STRUCTURES WITH GEOMETRIC CONSTRAINTS: A CASE STUDY WITH THE ROORDA FRAME
L. Zhu¹, J. Shen, University of Exeter, United Kingdom; R.M.J. Groh¹, M. Schenk¹, A. Pirrera¹; ¹University of Bristol, United Kingdom
12.8Composites 1
Chair(s): Zhang, C., Petrolo, M.
Track 12 Petrarca
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
11. Sep 24 14:30 14:55 12.8.1
0245
CANCELED - ENERGY DISSIPATION BEHAVIOR AND LIFE PREDICTION OF CARBON FIBER REINFORCED COMPOSITE MATERIALS SUBJECTED TO FATIGUE LOAD
J. Huang, China; Q. Yun, China; A. Li, China
11. Sep 24 14:55 15:20 12.8.2
0259
A MESO-SCALED SIMULATION ON THE THICKNESS EFFECT OF TWO-DIMENSIONAL TRIAXIALLY BRAIDED COMPOSITES UNDER TENSILE LOADS
Y. Bai¹, P. Liu¹, Z.-Q. Zhao¹, C. Zhang¹; ¹Northwesterm Polytechnical University, China
Presenter: Zhenqiang Zhao, Northwestern Polytechnical University
11. Sep 24 15:20 15:45 12.8.3
0290
MULTIAXIAL TESTING OF AERONAUTIC COMPOSITE STRUCTURES AT INTERMEDIATE SCALE
B. Castanié¹, J.-C. Passieux¹, J.-N. Périé¹, C. Bouvet¹, J.-E. Dufour¹, J. Serra¹; ¹Institut Clément Ader, France
11. Sep 24 15:45 16:10 12.8.4
0296
DYNAMIC AND STABILITY ANALYSES OF ROTATING THIN-WALLED FILAMENT WOUND GLASS FIBRE COMPOSITE CYLINDERS WITH METAL LINER
R. Hu, China; Z. Yuan, China; C. Zhang, China
Presenter: Ruiqi Hu
13.8Supersonic / Hypersonic Propulsion 1
Chair(s): Orisamolu, W.
Track 13 Boccaccio
05 - Propulsion
11. Sep 24 14:30 14:55 13.8.1
1147
DESIGN SPACE EXPLORATION OF NEXT-GENERATION SUPERSONIC BUSINESS JET ENGINE WITH A FOCUS ON LANDING AND TAKE-OFF (LTO) NOISE
D. Del Gatto¹, S. Adamidis¹, C. Mourouzidis¹, S. Brown¹, V. Pachidis¹; ¹Cranfield University, United Kingdom
Presenter: Dario Del Gatto, Cranfield University
11. Sep 24 14:55 15:20 13.8.2
0235
RAMJET/SCRAMJET TEST BENCH WITH CAVITY INJECTION OF HYDROGEN
F. Strauss¹, T. Nilsson, Lund University, Sweden; K. Manassis¹; ¹German Aerospace Center DLR, Germany
Presenter: Thommie Nilsson, Lund University
11. Sep 24 15:20 15:45 13.8.3
0255
PROPULSIVE CFD ANALYSIS OF THE SCRAMJET HYPERSONIC EXPERIMENTAL VEHICLE
O. Russo¹, P. Roncioni¹, M. Marini¹, S. Di Benedetto¹, G. Ranuzzi², S. Pizzurro², M. Albano²; ¹Italian Aerospace Research Centre (CIRA), Italy ;²Italian Space Agency (ASI), Italy
11. Sep 24 15:45 16:10 13.8.4
0920
EXPERIMENTAL AND NUMERICAL INVESTIGATION ON SEPARATION CHARACTERISTICS OF SERPENTINE CONVERGENT-DIVERGENT NOZZLE
M.-X. Wang¹, L. Zhou¹, J.-W. Shi¹, W.-J. Deng¹, H. Xiao¹; ¹Northwestern Polytechnical University, China
14.8Accident Prevention & Survivability 2
Chair(s): Vozella, A., Mori, R.
Track 14 Puccini
10 - Safety and Security
11. Sep 24 14:30 14:55 14.8.1
0049
IDENTIFICATION OF FACTORS CONTRIBUTING TO UNFAVORABLE LANDINGS
R. Mori, Kobe University, Japan
11. Sep 24 14:55 15:20 14.8.2
0416
HELICOPTER ACCIDENTS IN BRAZIL: AN ANALYSIS OF MAINTENANCE FROM THE PERSPECTIVE OF HUMAN FACTORS
F. de Assis da Silva Junior¹, J.M. Vieira da Fonseca¹, I.N.M. da Silva¹, A.V. Gaspar¹, M.M. Cardoso Junior¹; ¹Technological Institute of Aeronautics, Brazil
Presenter: MOACYR cardoso-Junior, Technological Institute of Aeronautics
11. Sep 24 15:20 15:45 14.8.3
0599
SENSITIVITY ANALYSIS OF SAFETY FACTORS BASED ON MODEL OF AVIATION RECIPROCATING ENGINE TURBOCHARGING SYSTEM
Z. Wang, China; G. Li, China; Y. Teng, China; T. Xu, China; Y. Zhang, China
Presenter: ZiLu Wang
11. Sep 24 15:45 16:10 14.8.4
1082
CANCELED - ANALYZING THE STATISTICAL CORRELATION OF PHYSIOLOGICAL PARAMETERS WITH TUC IN PILOTS PRIOR TO HYPOBARIC TRAINING
S.-J. Wu, Taiwan, China; C.-T. Kuo, Taiwan, China; N.-S. Chen, Taiwan, China; C.-J. Su, Taiwan, China; K.-K. Jen, Taiwan, China; S.-T. Hsieh, Taiwan, China; C.-Y. Lai, Taiwan, China; C.-L. Kuo, Taiwan, China
Reserve Paper 14.8.R
0074
STUDY ON THE BALLISTIC-RESISTANT AIRWORTHINESS STANDARDS FOR COMMERCIAL AIRCRAFT COCKPIT DOOR
T. Hu¹, J. Song¹, N. Yue¹, Z. Zhang², Y. Zhang², T. Chen²; ¹Airworthiness Technology Research & Management Center, China ;²Shanghai Aviation Airworthiness Certification Center, China
Presenter: Tao Hu, Airworthiness Technology Research & Management Center
additional information (interactive) 14.8.R
0587
A METHOD FOR AUTOMATIC GENERATING SAFETY ANALYSIS BASED ON AVIATION PISTON ENGINE MODEL
G. Li¹, Y.-D. Teng¹, Z.-L. Wang¹, T.-G. Xu¹, S.-T. Ding, Civil Aviation University of China,, China; ¹Beihang University, China
additional information (interactive) 14.8.R
1186
IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM
T.-J. Jiang¹, Z.-P. Luo¹, Z. Kan¹, J.-W. Xiang¹, X.-C. Liu², C.-Y. Bai², X.-L. Xi²; ¹Beihang University, China ;²Aircraft Strength Research Institute, China
15.8UAV Control Applications
Chair(s): , , Bil, C.
Track 15 Carducci
06.2 - Flight Dynamics and Control (UAV related)
11. Sep 24 14:30 14:55 15.8.1
0980
IN-FLIGHT MEASUREMENT OF WING SURFACE PRESSURE DISTRIBUTION ON A FIXED-WING UAV AND ITS APPLICATION TO FLIGHT CONTROL
Y. Hayashi¹, J.-H. Kim¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan
11. Sep 24 14:55 15:20 15.8.2
0879
MODEL PREDICTIVE CONTROL DRIVEN AERIAL GRASPING WITH SOFT OPERATIONAL CONSTRAINTS
J. Novák ¹, J. Hanák¹, P. Chudý¹; ¹BUT, Czech Republic
11. Sep 24 15:20 15:45 15.8.3
0794
FUZZING ON TARGET DETECTION SYSTEM OF UNMANNED AERIAL VEHICLE
H. Dai¹, Z. Wang¹, J. Ding¹, G. Li¹, C. Wang¹, L. He¹, H. Liu, Swinburne University of Technology, Australia; ¹Chinese Aeronautical Establishment, China
11. Sep 24 15:45 16:10 15.8.4
1176
FLIGHT PATH RECONSTRUCTION OF A FLEXIBLE WING UAV WITH WING MOUNTED VANES
V.P. Fernandes¹, T.R. Paula¹, R.C. Nascimento¹, R.G.A. Silva¹, L.C.S. Góes¹; ¹ITA - Instituto Tecnológico de Aeronáutica, Brazil
16.8Additive Manufacturing
Chair(s): Liu, X., Jiang, L.
Track 16 Raffaello
08 - Manufacturing and Supply Chain Management
11. Sep 24 14:30 14:55 16.8.1
0964
LIGHT WEIGHT DESIGN AND LASER ADDITIVE MANUFACTURING OF METAL BIPOLAR PLATES FOR THE APPLICATION OF AIRCRAFT FUEL CELL
K.J. Lin, China; Y. Xu, China; D.D. Gu, China; J.H. Shan, China; K.Y. Shi, China; W.L. Zhang, China
11. Sep 24 14:55 15:20 16.8.2
0593
EFFECTS OF PROCESSING STRATEGIES ON SURFACE QUALITY AND MECHANICAL PROPERTIES IN HYBRID ADDITIVE MANUFACTURING OF IN718 ALLOY
T. Wang¹, C. Wang¹, J.-J. Li¹, W.-X. Wang¹; ¹Chongqing University, China
11. Sep 24 15:20 15:45 16.8.3
0313
BUILDING METHODS FOR A COMPOSITE CONSTRUCTED VTOL USING 3D PRINTING TECHNIQUES
T. Müller¹, V. Gollnick¹; ¹Institute of Air Transportation Systems, Germany
11. Sep 24 15:45 16:10 16.8.4
0022
THE PRODUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS FOR AEROSPACE APPLICATIONS
J. Shipley¹, A. Magnusson¹, J. Gårdstam¹, C. Beamer¹, A. Cassese¹; ¹Quintus Technologies, Sweden
17.8Environmental Impact of Aircraft Operations
Chair(s): Conte, C., Wilkinson, G.
Track 17 Galileo
11 - Operations and Sustainment
11. Sep 24 14:30 14:55 17.8.1
0292
CLIMATE RESILIENCE – THE IMPACT OF EXTREME WEATHER EVENTS - A CASE STUDY: HEATHROW AIRPORT
M. Osund-Ireland¹, B. Elzen¹, W.A. Ireland¹; ¹Susteer AB, Sweden
11. Sep 24 14:55 15:20 17.8.2
0452
SUSTAINABLE ENGINE MAINTENANCE: EVALUATING THE ECOLOGICAL IMPACT OF LIFE LIMITED PART REPLACEMENT
A. Oestreicher¹, A. Rahn¹, J. Ramm¹, J. Städing², C. Keller², K. Wicke¹, G. Wende¹; ¹DLR, Germany ;²MTU Maintenance, Germany
11. Sep 24 15:20 15:45 17.8.3
0671
FACTORS INFLUENCING THE CLIMATE-RELEVANT ENVIRONMENTAL IMPACT OF AIR TRANSPORT COMPARED TO RAIL AND ROAD TRANSPORT
J. Roesing, RWTH Aachen University, Germany
11. Sep 24 15:45 16:10 17.8.4
0680
E-KEROSENE POTENTIAL FOR COMMERCIAL AVIATION DECARBONIZATION
G. Quaresma¹, L.B. Magalhães, ISEC, ISEC Lisboa, Portugal; A.F. Ferreira, IDMEC-LAETA, Mechanical Engineering Department, IST/UL, Portugal; A. Silva¹; ¹AEROG-LAETA, Aerospace Sciences Department, UBI, Portugal
additional information (interactive) 17.8.R
0350
ENSURING THE NEXT GENERATION GREEN AIRCRAFT’ SUSTAINABILITY FROM THE DESIGN PHASE VIA A LIFE-CYCLE COST ANALYSIS
E. Stefana¹, E. De Paola¹, L. Pustina¹, R. Patriarca¹, F. Mastroddi¹; ¹Sapienza University of Rome, Italy

16:00 - 16:30BREAK

1.9GSA - Propulsion & Energy 3
Chair(s): Newby, A.
Track 1 Auditorium
15 - Guest lectures
11. Sep 24 16:30 17:00 1.9.1
1307
PRATT & WHITNEY SUSTAINABILITY STRATEGY & DEMONSTRATORS
A. J. Murphy, Pratt & Whitney, United States
11. Sep 24 17:00 17:30 1.9.2
1235
GE AEROSPACE: RISING TO THE CHALLENGE FOR MORE SUSTAINABLE FLIGHT
R. Seele, GE Aerospace, United States
11. Sep 24 17:30 18:00 1.9.3
1315
FUTURE LANDSCAPE OF AVIATION ENERGY – US PERSPECTIVE
M. R. Berube, Department of Energy EERE, United States
11. Sep 24 18:00 18:30 1.9.4
1276
PANEL DISCUSSION
PD D,
2.9Japanese R&D on GX and DX in Aviation
Chair(s): Rinoie, K.
Track 2 Sala Verde
15 - Guest lectures
11. Sep 24 16:30 17:00 2.9.1
1221
OVERVIEW OF JAPANESE R&D ACTIVITIES ON GREEN TRANSFORMATION AND DIGITAL TRANSFORMATION IN AVIATION
S. Watanabe Watanabe, Japn Aerospace Exploration Agency, Japan
11. Sep 24 17:00 17:30 2.9.2
0836
DEVELOPMENT OF CORE TECHNOLOGIES FOR HYDROGEN AIRCRAFT
M. Kazari, Kawasaki Heavy Industries,Ltd., Japan
11. Sep 24 17:30 18:00 2.9.3
0856
AIRCRAFT DX IN COMMERCIAL AVIATION SYSTEMS
Y. Yamaguchi, Mitsubishi Heavy Industries, Ltd./Commercial Aviation Systems, Japan
11. Sep 24 18:00 18:30 2.9.4
0971
DEVELOPMENT OF AIRCRAFT SYSTEM ELECTRIFICATION AND HYBRID ELECTRIC PROPULSION
N. Seki¹, T. Inoue¹; ¹IHI Corporation, Japan
3.9Design of Unconventional Configurations
Chair(s): Kanazaki, M.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
11. Sep 24 16:30 17:00 3.9.1
0462
STRUT-BRACED WING INDUCED DRAG MODELING FOR REGIONAL TURBOPROP AIRCRAFT DESIGN
G. Grazioso, University of Naples Federico II, Italy; A. De Marco, University of Naples, Italy
11. Sep 24 17:00 17:30 3.9.2
0273
STEADY ANALYSIS OF THREE-SURFACE AIRPLANES: IMPROVING THE AERODYNAMIC PERFORMANCE THROUGH REDUNDANT LONGITUDINAL CONTROL
S. Cacciola¹, C.E.D. Riboldi¹, C. Spitale¹; ¹Politecnico di Milano, Italy
11. Sep 24 17:30 18:00 3.9.3
0371
LONGITUDINAL STABILITY PARAMETERS FOR FLYING BOOM AERIAL REFUELING
L.H. Peristy¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada
11. Sep 24 18:00 18:30 3.9.4
0495
ON THE FUTURE OF TRANSONIC FLIGHTS: CURVED PLANFORM WINGS FOR BUFFET-ONSET CONTROL
M.R. Chiarelli¹, S. Bonomo¹, G. Cascinelli¹; ¹Department of Civil and Industrial Engineering, Pisa, Italy
Reserve Paper 3.9.R
0643
INVESTIGATION ON AERODYNAMIC DESIGN OF VTOL AIRCRAFT PROPELLER
L.D. Deng¹, W.P. Song¹, J.H. Xu¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
4.9Unmanned Aerial Systems and Advanced Aerial Mobility 2
Chair(s): Lott, M.
Track 4 Brunelleschi
01.2 - Aircraft Design and Integrated System (Applications)
11. Sep 24 16:30 17:00 4.9.1
0477
DEVELOPMENT OF A SERVO-DRIVEN FLAPPING-WING AIR VEHICLE WITH FOLDING-WING MECHANISM
E.-H. Lee¹, H.-H. Yang¹, S.-G. Lee¹, J.-H. Han¹; ¹KAIST, South Korea
11. Sep 24 17:00 17:30 4.9.2
0536
PRELIMINARY DESIGN EXPLORATION OF PROSPECTIVE MULTIROTOR AEROBOTS FOR MARS
V. Youhanna¹, L. Felicetti¹, D. Ignatyev¹; ¹Cranfield University, United Kingdom
11. Sep 24 17:30 18:00 4.9.3
0564
MISSION-BASED OPTIMAL PROPELLER SELECTION FOR VTOL SUAV CONFIGURATION
C. Reyner¹, C. Lee¹, D. Kim, Ecole Nationale de l’Aviation Civile, France; R.P. Liem¹; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China
11. Sep 24 18:00 18:30 4.9.4
0573
MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM
Y. Shiratsuchi¹, K. Kaneko, The University of Tokyo, Japan; S. Okada, Tokyo University of Agriculture and Technology, Japan; A. Oyama², K. Yamada², H. Tanaka², M. Sato¹; ¹Kogakuin University, Japan ;²Japan Aerospace Exploration Agency, Japan
5.9CFD and Sustainable Aviation
Chair(s): Fusaro, R., Kiszkowiak, L.
Track 5 Donatello
03.1 - Aerodynamics – CFD Methods and Validation
11. Sep 24 16:30 17:00 5.9.1
0062
APPLICATION OF DIFFERENT NUMERICAL TOOLS AND NUMERICAL METHODS FOR PREDICTION OF HEAT EXCHANGER RAMAIR-CONCEPTS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT CONFIGURATIONS
A.-R. Hübner¹, J. Kirz¹, K. Weinman¹; ¹German Aerospace Center (DLR), Germany
11. Sep 24 17:00 17:30 5.9.2
0502
TOWARDS REFINED CONTRAIL SIMULATIONS OF FORMATION FLIGHT SCENARIOS
J. Pauen¹, S. Unterstrasser¹, A. Stephan¹; ¹DLR, Germany
11. Sep 24 17:30 18:00 5.9.3
1009
PERFORMANCE AND ACOUSTIC ANALYSIS OF A DISTRIBUTED ELECTRIC PROPULSION UNMANNED AIRCRAFT
R. Navarro¹, L.M. García-Cuevas¹, J. García-Tíscar¹, F.N. Ramírez¹; ¹Universitat Politècnica de València, Spain
11. Sep 24 18:00 18:30 5.9.4
1048
HIGH FIDELITY MODELING OF ACOUSTIC LINERS FOR AERONAUTICAL APPLICATIONS
L. Pinelli¹, M. Marconcini¹, A. Arnone ¹, D. Bacci, Oxford Thermofluids Institute, University of Oxford, United Kingdom; ¹Department of Industrial Engineering, University of Florence, Italy
6.9Low Reynolds Number Aerodynamics
Chair(s): Prince, S., Halila, G.
Track 6 Cimabue
03.1 - Aerodynamics – CFD Methods and Validation
11. Sep 24 16:30 17:00 6.9.1
0863
PRELIMINARY DESIGN OF A FIXED-WING DRONE FOR MARS EXPLORATION ACTIVITIES
G. Barbato¹, G. Pezzella¹, A. Viviani¹; ¹Università della Campania Luigi Vanvitelli, Italy
Presenter: Gennaro Barbato, Università della Campania \\\"Luigi Vanvitelli\\\"
11. Sep 24 17:00 17:30 6.9.2
1198
PARELLEL UNSTEADY REYNOLDS-AVERAGED NAVIER-STOKES (URANS) STUDEIS OF THE PERFORMANCE OF ONR WATERJET AXWJ-2
S.E. Monroe, Clarkson University, United States
11. Sep 24 17:30 18:00 6.9.3
0930
NUMERICAL INVESTIGATION ON THE LIQUID SLOSHING DAMPING INSIDE A TANK WITH A FLEXIBLE ANTI-SLOSHING DEVICE
F. Rossetti¹, L. Pirillo¹, M. Cimini, ENEA, Italy; M. Bernardini¹, F. Stella¹; ¹Sapienza University, Italy
Presenter: Lorenzo Pirillo, Sapienza University
11. Sep 24 18:00 18:30 6.9.4
0752
THE EFFECTS OF INITIAL STRESS ON AERODYNAMIC PERFORMANCE OF FLEXIBLE MEMBRANE-SKELETON WINGS WITH FSI SIMULATION
Y.-Y. Guo¹, W.-Q. Yang¹, J.-L. Xuan¹, W. Wang¹, D. Xue¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 6.9.R
0104
VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA
M. Turner¹, J. Sharpe¹, M. Kopacz¹, D. Standingford¹, C. Sequeira², B. Sanby², C. Rider²; ¹Zenotech, United Kingdom ;²Flare Bright, United Kingdom
7.9Fan and Nozzle Flow Control
Chair(s): Vijgens, P.
Track 7 Botticelli
03.3 - Basic Fluid Dynamics and Flow Control
11. Sep 24 16:30 17:00 7.9.1
0849
MECHANISM STUDY ON THE IMPACT OF PULSED JET AT THE BLADE TIP LEADING EDGE ON THE FLOW FIELD IN COMPRESSOR
Y. Yang, Civil Aviation Flight University of China, China; H. Zhang¹, W. Lu, Nanjing Tech University, China; C. Zhang¹, C. Xu¹, G. Huang¹; ¹Nanjing University of Aeronautics and Astronautics, China
11. Sep 24 17:00 17:30 7.9.2
0870
IMPLEMENTATION OF ACTIVE FLOW CONTROL ON A SHORT-INLET UHBR ENGINE NACELLE
S. Hayböck¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
11. Sep 24 17:30 18:00 7.9.3
0944
NUMERICAL STUDY OF THE FLOWFIELD IN A DIFFERENTIALLY-THROTTLED LINEAR AEROSPIKE
J. Hassan ¹, R. Marsilio¹, G.M. Di Cicca¹, M. Ferlauto¹; ¹Dept. of Mech. and Aerospace Engineering, Politecnico di Torino, Italy
11. Sep 24 18:00 18:30 7.9.4
1123
ON THE OPTIMIZATION OF (GENERALIZED) IMPEDANCE FOR ACOUSTIC LINERS
E. De Bono, France; A.D. Fernandes, Italy; G. Petrone, Italy; M. Ouisse, France; R. Teloli, Italy; S. De Rosa, Italy
Presenter: Arthur Diniz
8.9Applications of Aerodynamic Optimisation
Chair(s): Streit, T.
Track 8 Vasari
03.4 - Applied Aerodynamics
11. Sep 24 16:30 17:00 8.9.1
0227
AERODYNAMIC SHAPE OPTIMIZATION OF FILLETED INTERSECTIONS WITH SURFACE MESH DEFORMATION
H.M. Hajdik¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States
11. Sep 24 17:00 17:30 8.9.2
0298
NOVEL GRADIENT-ENHANCED MULTI-FIDELITY SURROGATE MODEL ASSISTED ROBUST MULTIDISCIPLINARY DESIGN OPTIMIZATION OF TAILLESS FLYING WING
H. Zhao¹, K.-K. Wang¹, Z.-Y. Gong¹, K.Y. Gan¹; ¹Northwestern Polytechnical University, China
Presenter: Huan Zhao
11. Sep 24 17:30 18:00 8.9.3
0394
DESIGN AND AERODYNAMIC OPTIMIZATION OF A THIN-HAUL AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION: ZETHA
G. Beghetto¹, M. Boffadossi¹; ¹Politecnico di Milano, Italy
Presenter: Giacomo Beghetto, DAER, Politecnico di Milano
11. Sep 24 18:00 18:30 8.9.4
1150
ABOUT MODELLING OF EMPIRICAL CORRELATIONS WITHIN AERODYNAMIC PROFILES USING HIGHER ORDER ARTIFICIAL NEURAL NETWORKS
P. Kovar, Center of Advanced Aerospace Technology, Czech Republic; J. Fürst, Department of Technical Mathematics, Faculty of Mechanical Engin, Czech Republic
additional information (interactive) 8.9.R
0265
LOCALIZED AERODYNAMIC SHAPE OPTIMIZATION FOR AUTOMOTIVE APPLICATIONS
M. Nayman¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada
9.9Airspace Management
Chair(s): Ellis, K., Johnson, M.
Track 9 Giotto
09 - Air Transport System Efficiency
11. Sep 24 16:30 17:00 9.9.1
1137
WEATHER-AWARE INTEGRATED AIRPORT/AIRSPACE CAPACITY PREDICTION TECHNOLOGIES
T. Reynolds¹, K.C. Woodrow¹, H. Iskenderian¹, D. Johnson¹, M. Matthews¹, J. Venuti¹, M. Worris¹, G. Enea¹, B. Crawley, NAV CANADA, Canada; ¹MIT Lincoln Laboratory, United States
Presenter: Gabriele Enea, MIT Lincoln Laboratory
11. Sep 24 17:00 17:30 9.9.2
0782
PROBING AND MODELING LARGE-SCALE AIRLINE NETWORK DISRUPTIONS: 2022 SOUTHWEST AIRLINES SCHEDULING CRISIS
M. Peng¹, A. Kamat¹, V. Tran, Harvard University, United States; C. Dawson², C. Fan², M.Z. Li¹; ¹University of Michigan, United States ;²Massachusetts Institute of Technology, United States
Presenter: Max Zhaoyu Li
11. Sep 24 17:30 18:00 9.9.3
0966
TIME-BASED CONTROL TO REDUCE TRAJECTORY COMPLEXITY IN THE FLOW-CENTRIC AIR TRAFFIC CONTROL PARADIGM
K. Tominaga¹, N. Inoue¹, M. Schultz, University of the Bundeswehr Munich, Germany; Y. Zeng, Nanyang Technological University Singapore, Singapore; E. Itoh¹; ¹The University of Tokyo, Japan
Presenter: Eri Itoh, The University of Tokyo
11. Sep 24 18:00 18:30 9.9.4
1038
APPLICATIONS AND CHALLENGES FOR AIRBORNE AD-HOC COMMUNICATION NETWORKS IN ORP AIRSPACES USING THE L-BAND
T. Marks¹, A. Hillebrecht¹, M.A. Bellido-Manganell¹; ¹German Aerospace Center, Germany
Presenter: Alexander Hillebrecht, German Aerospace Center
10.9Structures at Extreme Temperatures
Chair(s): Giglio, M., Petrolo, M.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
11. Sep 24 16:30 17:00 10.9.1
0858
DESIGN OF HYDROGEN STORAGE SYSTEMS IN NEW-GENERATION REGIONAL AIRCRAFT
V. Memmolo¹, L.M. Cardone¹, G. Petrone¹, S. De Rosa¹; ¹Università degli Studi di Napoli Federico II, Italy
11. Sep 24 17:00 17:30 10.9.2
1052
THERMAL AND MECHANICAL CYCLING OF THIN-PLY COMPOSITES FOR CRYOGENIC APPLICATIONS
M.S. Loukil¹, J. Xu¹, E. Marklund², M. Merzkirch², F. Moreau³, F. Ohlsson³; ¹Linköping University, Sweden ;²Research Institutes of Sweden RISE, Sweden ;³Oxeon AB, Sweden
11. Sep 24 17:30 18:00 10.9.3
0105
NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL
N. Monokrousos¹, L. Könözsy¹, V. Pachidis¹, E. Sozio², F. Rossi²; ¹Cranfield University, United Kingdom ;²Pangea Aerospace, Spain
11. Sep 24 18:00 18:30 10.9.4
0438
OPTIMIZATION OF POST-PROCESSING HEAT TREATMENT FOR LPBF MODIFIED 2024 ALUMINIUM ALLOY
M. Bona¹, A.M. Grande¹; ¹Politecnico di Milano, Italy
additional information (interactive) 10.9.R
0275
ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT
R. Szczepaniak¹, P. Przybylek¹, D. Szczechula¹, A. Krzyzak¹, A. Komorek¹, G. Woroniak, Bialystok University of Technology, Poland; ¹Polish Air Force University, Poland
11.9Aeroelastic Tailoring 3
Chair(s): Petrolo, M., Filippi, M.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
11. Sep 24 16:30 17:00 11.9.1
0170
THE EFFECTS OF ENGINE MASS AND LOCATION ON THE FLUTTER CHARACTERISTICS OF AIRCRAFT WINGS
J.R. Banerjee¹, A. Ananthapuvirajah¹, P.H. Cabral, Embraer S.A., Brazil; ¹City, University of London, United Kingdom
11. Sep 24 17:00 17:30 11.9.2
0114
INFLUENCE OF SKIN CURVATURE ON WINGBOX OPTIMIZATION WITH NONLINEAR STRUCTURAL STABILITY CONSTRAINTS
F.M.A. Mitrotta¹, A. Pirrera¹, T. Macquart¹, J.E. Cooper¹, A. Pereira do Prado², P.H. Cabral²; ¹University of Bristol, United Kingdom ;²Embraer, Brazil
11. Sep 24 17:30 18:00 11.9.3
0875
RANDOM MATRIX MODELLING FOR UNCERTAINTY QUANTIFICATION IN PRESTRESSED STRUCTURES
A. Mannoosseril¹, S. Adhikari¹, A.P. Prado², P.H. Cabral²; ¹James Watt School of Engineering, University of Glasgow, United Kingdom ;²Embraer S.A., São José dos Campos, Brazil, Brazil
11. Sep 24 18:00 18:30 11.9.4
1178
FLUID-SOLID INTERACTIVE MODELLING OF FABRIC-BASED ATMOSPHERIC ENTRY SIZED AERODYNAMIC DECELARATORS
E. Malof¹, J. Bayandor¹; ¹University at Buffalo CRASH Lab, United States
12.9Composites 2
Chair(s): Yondomine, R.
Track 12 Petrarca
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
11. Sep 24 16:30 17:00 12.9.1
0058
PROCESS MODELLING OF COMPOSITES USING A MULTISCALE FRAMEWORK
G.M. Odegard, Michigan Technological University, United States; M. Maiaru, Columbia University, United States
11. Sep 24 17:00 17:30 12.9.2
0213
MICROMECHANICAL MODELING OF THE VISCOELASTIC-VISCOPLASTIC RESPONSE OF FIBER-REINFORCED COMPOSITES
T. Nan¹, G.J. Yun, Seoul National University, North Korea; C. Zhang¹; ¹Northwestern Polytechnical University, China
11. Sep 24 17:30 18:00 12.9.3
0584
A DYNAMIC TEST METHODOLOGY FOR DETERMINING THE LONGITUDINAL COMPRESSIVE RESPONSE OF CARBON FIBER COMPOSITE TOWS
J. Gu¹, Y. Bai¹, Z. Zhao¹, C. Zhang¹; ¹Northwestern Polytechnical University, China
11. Sep 24 18:00 18:30 12.9.4
1099
INVESTIGATION ON VARIABLE-HEIGHT PROTRUSION ARRANGEMENT OF METAL–COMPOSITE HYBRID JOINTS UNDER A TENSILE LOAD
Y. Zhao, China; W. Wang, China; X. Wan, China
13.9Supersonic / Hypersonic Propulsion 2
Chair(s): Orisamolu, W.
Track 13 Boccaccio
05 - Propulsion
11. Sep 24 16:30 17:00 13.9.1
0195
MODEL-BASED CONCEPTUAL DESIGN AND EVALUATION OF A SOLID-FUEL SCRAMJET VEHICLE
M. Bhardwaj¹, S. Rajashankar¹, N. Ananthkrishnan¹, A. Sharma¹, W.-D. Ki², H.-J. Namkoung²; ¹Yanxiki Tech, India ;²Hyundai Rotem, South Korea
Presenter: Hyuck-Joon Namkoung, Hyundai Rotem
11. Sep 24 17:00 17:30 13.9.2
0919
AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD
Q.-L. Li¹, L. Zhou¹, Z.-X. Wang¹, X.-B. Zhang¹, S. Huang¹; ¹Northwestern Polytechnical University, China
11. Sep 24 17:30 18:00 13.9.3
0188
DESIGN OF A WIND TUNNEL MODEL FOR A REUSABLE LAUNCH VEHICLE DURING ITS LANDING BURN
A.T. Hoang¹, N.J. Lawson¹, T. Bykerk, German Aerospace Center (DLR), Germany; ¹The University of Sydney, Australia
Presenter: Nicholas J. Lawson, The University of Sydney
11. Sep 24 18:00 18:30 13.9.4
0924
COMPARISON OF LIFE CYCLE COST FOR MACH 8 AND MACH 5 HYPERSONIC PASSENGERS AIRCRAFT
L. Pugliese¹, D. Ferretto¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy
14.9Monitoring
Chair(s): Kügler, D.
Track 14 Puccini
10 - Safety and Security
11. Sep 24 16:30 17:00 14.9.1
0106
DECODING AN IN-FLIGHT REFUELING INCIDENT: AVIATION COMPLEXITY THROUGH STAMP/CAST AND ACCIMAP METHODS
J.G. Fowler¹, D.C. Fernandes¹, D.M.C. de Lima¹, G.V. da Rocha¹, M.M. Cardoso Júnior¹; ¹Aeronautic Institute of Technology, Brazil
Presenter: Daniella Castro Fernandes, Aeronautic Institute of Technology
11. Sep 24 17:00 17:30 14.9.2
0719
DYNAMIC RESPONSE MONITORING OF FLIGHT CONTROL WITH INCREMENTAL NONLINEAR DYNAMIC INVERSION
H. Hofsäß¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
11. Sep 24 17:30 18:00 14.9.3
0287
INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF WINGS UNDER ICING CONDITIONS AT VARIOUS SWEEP ANGLES
X. Xu¹, Y. Zhang¹, G. Chen¹, X. Ma, Xi'an Jiaotong UniversityXi'an Jiaotong University, China; ¹Xi'an Jiaotong University, China
11. Sep 24 18:00 18:30 14.9.4
0027
SLEEPINESS IN BRAZILIAN AVIATION: A PROBLEM-SOLVING APPROACH
V. Gomes¹, T. Paiva¹, A. Herculano¹, T. Dias¹, M.M. Cardoso-Junior¹, M.C. Belderrain¹; ¹ITA, Brazil
15.9UAV Design and Performance
Chair(s): Kiszkowiak, L., Krus, P.
Track 15 Carducci
06.2 - Flight Dynamics and Control (UAV related)
11. Sep 24 16:30 17:00 15.9.1
0310
FLIGHT MECHANICAL ANALYSIS OF A VERY FLEXIBLE HIGH-ALTITUDE PLATFORM UNDER UNCERTAINTY CONSIDERATIONS
Y.J. Hasan¹, N. Fezans¹, A. Voß, DLR Institute of Aeroelasticity, Germany; ¹DLR Institute of Flight Systems, Germany
11. Sep 24 17:00 17:30 15.9.2
0947
FLIGHT PERFORMANCE AND DYNAMICS OF AN UNCONVENTIONAL SOLAR POWERED UAS
G. Charruaz¹, A. Borgia¹, A. Braghin¹, T. Bussi¹, A. Esposito¹, A. Pescosolido¹; ¹Politecnico di Torino, Italy
11. Sep 24 17:30 18:00 15.9.3
0724
ON THE DEVELOPMENT OF THE STRUCTURAL DIGITAL TWIN OF AN UNMANNED AERIAL VEHICLE
X. Zhou¹, M. Dziendzikowski², K. Dragan², M. Giglio³, L. Dong¹, C. Sbarufatti³; ¹Beihang University, China ;²Instytut Techniczny Wojsk Lotniczych, Poland ;³Politecnico di Milano, Italy
11. Sep 24 18:00 18:30 15.9.4
1100
DYNAMIC FREE FLIGHT TESTS WITH A SUB-SCALE AIRPLANE DESIGNED ACCORDING TO THE FROUDE NUMBER
C. Fischer, Instituto Federal de São Paulo and Aeronautics Institute of Tec, Brazil; A.S. Davi, Lilium GmbH, Germany; R.G.A. da Silva¹, L.C.S. Goes¹; ¹Aeronautics Institute of Technology, Brazil
additional information (interactive) 15.9.R
0231
MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS
H. Shi¹, S. Li, AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China; Z. Huang¹, S. Li¹, A. Li¹, Y. Zhou¹; ¹BEIHANG UNIVERSITY, China
16.9Advanced Manufacturing Technology 3
Chair(s): Liu, X., Jiang, L.
Track 16 Raffaello
08 - Manufacturing and Supply Chain Management
11. Sep 24 16:30 17:00 16.9.1
0248
THERMAL AND GRINDING PERFORMANCE OF 3D PRINTED COMPLIANCE GRINDING TOOLS WITH ROTARY-ENHANCED HEAT TRANSFER STRUCTURE
M.C. Li, China; S. Yan, China; K.F. Zhang, China; W. Wang, China; L. Zou, China; Y. Huang, China
Presenter: Wenxi Wang
11. Sep 24 17:00 17:30 16.9.2
0672
CYBER-PHYSICAL SYSTEM IMPLEMENTATION FOR THE AR-ASSISTED AIT OF AEROSPACE COMPONENTS
J. Pesce¹, A. Carini¹, M. Marinacci¹, M. Boscia¹, P. Marzioli¹, M. Pasquali¹, M. Eugeni¹, M. Mecella¹, P. Piergentili¹, P. Gaudenzi¹; ¹Sapienza University of Rome, Italy
11. Sep 24 17:30 18:00 16.9.3
0799
DESIGN AND DEVELOPMENT OF THE VISUAL AND AUDITORY LAYER FOR DIFFERENT CABIN/COCKPIT LAYOUT
A. Alaimo, Kore Università di Enna, Italy; S. Bagassi¹, E. Carrera, Politecnico di Torino, Italy; T. Fadda¹, M.C. Moruzzi¹; ¹Università di Bologna, Italy
17.9Advanced Air Mobility Operations
Chair(s): Homola, J.
Track 17 Galileo
11 - Operations and Sustainment
11. Sep 24 16:30 17:00 17.9.1
0705
MRO FOR VTOLS IN A FUNCTIONAL SEQUENCES SOLUTION SPACE
S. Papakonstantinou¹, D. Kloock-Schreiber¹, M. Ziegler², A.N. Mishra, Hamburg University of Technology, Germany; P.K. Jaisawal¹, U. Wieczorek², V. Gollnick¹; ¹Hamburg University of Technology, ILT, Germany ;²Airbus Protect, Germany
Presenter: Stephanos Papakonstantinou, TUHH/ILT
11. Sep 24 17:00 17:30 17.9.2
0379
ASSESSMENT OF A HIGHLY PARAMETERIZED STEADY-STATE MICROSCALE WIND SIMULATOR FOR URBAN AIR MOBILITY APPLICATIONS
D.S. Nithya¹, G. Quaranta¹, V. Muscarello², M. Liang²; ¹Politecnico di Milano, Italy ;²RMIT University, Australia
11. Sep 24 17:30 18:00 17.9.3
0110
A DESIGN OF VFR APPROACH AND DEPARTURE PROCEDURES OF UAM AT VERTIPORTS ADJACENT TO THE AIRPORT
S. Kim¹, O. Park¹, H.-S. Shin¹; ¹Cranfield University, United Kingdom
11. Sep 24 18:00 18:30 17.9.4
0500
ENVIRONMENTAL AND ECONOMIC ASSESSMENT OF AN EVTOL AIRCRAFT FLEET FOR URBAN AIR MOBILITY
M. Fioriti¹, M. Borghi¹, G. Pavan¹; ¹Politecnico di Torino, Italy
Presenter: Marco Fioriti, Politecnico di Torino

18:30 - 20:00SPEED MENTORING

Thursday, 12. Sep 2024


0.9GENERAL LECTURE 4: Bob Pearce: Aviation Transformations: Research for the Future of Flight
Chair: J.L. Azevedo ICAS Past President
12. Sep 24 08:30 09:30

09:30 - 10:00BREAK

1.10GSA - Airliner OEM Strategy Overview
Chair(s): Krein, A.
Track 1 Auditorium
15 - Guest lectures
12. Sep 24 10:00 10:30 1.10.1
1310
AIRBUS COMMERCIAL AVIATION SUSTAINABILITY STRATEGY
I. Bloy, AIRBUS, France
12. Sep 24 10:30 11:00 1.10.2
1227
THE CHALLENGE OF SUSTAINABILITY IN COMMERCIAL AVIATION
T. Beezhold, Boeing, United States
12. Sep 24 11:00 11:30 1.10.3
1301
EMBRAER SUSTAINABILITY STRATEGY
CS Silva, Embraer, Brazil
12. Sep 24 11:30 12:00 1.10.4
1244
ATR COMMERCIAL AVIATION SUSTAINABILITY STRATEGY
D. Cuchet, ATR, France
12. Sep 24 12:00 12:30 1.10.5
1277
PANEL DISCUSSION
PD D,
2.10Integrated CFD Validation Experiments for Low-Speed Aerodynamics
Chair(s): Slotnick, J.
Track 2 Sala Verde
15 - Guest lectures
12. Sep 24 10:00 10:30 2.10.1
1217
HIGH-LIFT PREDICTION WORKSHOPS: RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS
C.L. Rumsey, NASA Langley Research Center, United States
12. Sep 24 10:30 11:00 2.10.2
1218
CFD VALIDATION EXPERIMENTS AT DLR: OVERVIEW AND LESSONS-LEARNED
C. Grabe, DLR, Germany
12. Sep 24 11:00 11:30 2.10.3
1219
THE BEVERLI HILL EXPERIMENTS FOR SMOOTH-BODY TURBULENT FLOW SEPARATION - RETROSPECTIVE, LESSONS LEARNED, AND FUTURE PROSPECTS
C.J. Roy¹, K.T. Lowe¹, W.J. Devenport¹, A. Borgoltz¹, A. Gargiulo, University of Virginia, United States; ¹Virginia Tech, United States
12. Sep 24 11:30 12:00 2.10.4
1220
SYSTEMATIC CFD VERIFICATION - RESULTS FROM THE 2024 HIGH FIDELITY CFD VERIFICATION WORKSHOP
M. Galbraith, United States
12. Sep 24 12:00 12:30 2.10.5
1311
PANEL DISCUSSION
P D,
3.10Wing Design
Chair(s): Gibson, T.
Track 3 Michelangelo
01.1 - Aircraft Design and Integrated System (Basics and Theory)
12. Sep 24 10:00 10:30 3.10.1
0097
PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM
B.M.H.J. Fröhler¹, A.A. Pohya¹, J. Häßy¹, T. Kilian¹, A.H. Bismark¹, M. Radestock, Germany; D. Cruz Palacios, Aernnova Aerospace, Spain; ¹German Aerospace Center (DLR), Germany
12. Sep 24 10:30 11:00 3.10.2
0415
A COST-EFFICIENT PREDICTIVE METHOD FOR AERODYNAMIC PERFORMANCE DEGRADATION OF HORIZONTAL TAIL UNDER ICING CONDITIONS
S. Corcione¹, A. De Marco¹, V. Cusati¹; ¹University of Naples Federico II, Italy
12. Sep 24 11:00 11:30 3.10.3
0943
FUEL-BASED THERMAL MANAGEMENT SYSTEM ARCHITECTURES AND TANK TEMPERATURE EVOLUTION MODELS FOR AVIATION
S. Favre¹, F. Di Fede, Leonardo Labs, Leonardo S.p.A., Italy; E. Brusa¹, C. Delprete¹; ¹Politecnico di Torino, Italy
12. Sep 24 11:30 12:00 3.10.4
0951
SCOPING OF AN AIR SUPPLY CONFIGURATION FOR ACTIVE FLOW CONTROL ON A COMMERCIAL TRANSPORT AIRPLANE HIGH-LIFT SYSTEM
C.P. van Dam, University of California - Davis, United States; S.S. Hosseini¹, S.A. Pandya¹; ¹NASA Ames Research Center, United States
12. Sep 24 12:00 12:30 3.10.5
0862
OPTIMIZATION PROCEDURE FOR THE WING OF A MARS EXPLORATION DRONE
A. Viviani¹, A. Aprovitola¹, L. Iuspa², G. Pezzella²; ¹Università della Campania Luigi Vanvitelli , Italy ;²Università della Campania Luigi Vanvitelli , Italy
Presenter: Andrea Aprovitola, Università della Campania
Reserve Paper 3.10.R
0572
DESIGN OPTIMIZATION OF A WIG CRAFT’S HIGH LIFT DEVICE CONSIDERING GROUND EFFECT
Y.H. Wang¹, W.P. Song¹, H. Nie¹, K.F. Zheng¹, Z.H. Han¹; ¹Northwestern Polytechnical University, China
4.10Supersonic and Hypersonic Aircraft 2
Chair(s): Melkert, J.
Track 4 Brunelleschi
01.2 - Aircraft Design and Integrated System (Applications)
12. Sep 24 10:00 10:30 4.10.1
0882
SONIC BOOM COMPARATIVE STUDY BETWEEN MACH 4.7 OUTDOOR EXPERIMENTAL TESTS AND NUMERICAL SIMULATIONS
G. Fasulo¹, L. Federico¹, F. Petrosino¹, S. Graziani², N. Viola², S. Hengy³, B. Martinez³, M. Albisser³; ¹Italian Aerospace Research Centre (CIRA), Italy ;²Politecnico di Torino, Italy ;³French-German research institute of Saint-Louis (ISL), France
12. Sep 24 10:30 11:00 4.10.2
0121
LANDING AND TAKEOFF NOISE PREDICTION OF CONCEPTUAL SUPERSONIC AIRCRAFT
M. Graebert¹, R. Jaron¹, M. Plohr¹, S. Zenkner¹, C. Richter², C. Stöhr², C. Villena Munoz, Cranfield University, United Kingdom; M.-J. van der Meulen³, R. Habing³, M. Huet, ONERA, France; F. Petrosino*, M. Barbarino*, F. Fischer, MTU, Germany; O. Zaporozhets, Institute of Aviation, Poland; ¹DLR, Germany ;²Rolls-Royce Deutschland, Germany ;³NLR, Netherlands ;*CIRA, Italy
Presenter: Matti Graebert, DLR
12. Sep 24 11:00 11:30 4.10.3
0975
SENECA’S AIRCRAFT EMISSIONS EVALUATION AND THEIRS ENVIRONMENTAL
E. Terrenoire¹, M. Muller¹, E. Ramirez Correra², P. Leyland², K. Synylo³, A. Krupko³, O. Zaporozhets, ILOT, Poland; D. Lee*, B. Owen*, L. Lim*, A. Skowron*, R. Rodriguez DE Leon*, D. Marsh*, S. Matthes, DLR, Germany; P. Madden, RR UK, United Kingdom; S. Bake, RR DE, Germany; C. Mourouzidis, CU, United Kingdom; ¹ONERA, France ;²AEDS, Switzerland ;³NAU, Ukraine ;*MMU, United Kingdom
12. Sep 24 11:30 12:00 4.10.4
0758
DESIGN OF THE SENECA MACH 1.8 SUPERSONIC AIRLINER WITH MULTI-FIDELITY AERODYNAMIC ANALYSIS FOR NOISE-OPTIMISED TAKE-OFF TRAJECTORIES
C. Villena Muñoz¹, C. Lawson¹, A. Riaz¹, A. Sharma¹; ¹Cranfield University, United Kingdom
12. Sep 24 12:00 12:30 4.10.5
0927
CONCEPTUAL DESIGN METHODOLOGY FOR LOW-SUPERSONIC LH2-POWERED PASSENGERS AIRCRAFT
E. Sunzeri¹, D. Ferretto¹, N. Viola¹; ¹Politecnico di Torino, Italy
Reserve Paper 4.10.R
0129
THERMODYNAMIC DESIGN AND EMISSIONS MODEL OF A MACH 1.8 SUPERSONIC AIRLINER ENGINE
M. Plohr¹, S. Zenkner¹, S. Bake², D. Zeitz²; ¹DLR Institute of Propulsion Technology, Germany ;²Rolls-Royce Deutschland Ltd & Co KG, Germany
5.10Aerodynamic Optimization
Chair(s): Pezzella, G., Zingg, D.
Track 5 Donatello
03.1 - Aerodynamics – CFD Methods and Validation
12. Sep 24 10:00 10:30 5.10.1
0465
SHAPING SUSTAINABLE AVIATION WITH CFD-BASED DESIGN OPTIMIZATION
J.R.R.A. Martins¹, M.A.S. Abdul-Kaiyoom¹, E.J. Adler¹, A.C. Gray¹, H. Hajdik¹, E. Jonsson¹, A.H.R. Lamkin¹, B. Pacini¹, A. Yildirim¹; ¹University of Michigan, United States
12. Sep 24 10:30 11:00 5.10.2
0078
ADJOINT-BASED TRANSONIC WING AERODYNAMIC SHAPE OPTIMIZATION INVESTIGATIONS
L.V. Rezende Sanches, Universidade Federal do Paraná, Brazil; G.L. Olichevis Halila¹, F. Issamu Kitadani Odaguil¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; ¹Embraer, Brazil
12. Sep 24 11:00 11:30 5.10.3
0124
INVESTIGATING THE INFLUENCE OF AN INBOARD PROPELLER’S VERTICAL OFFSET ON A TRAILING WING’S LIFT AND DRAG DISTRIBUTIONS
S.S. Chauhan¹, G. Padovany da Silva, Universidade Federal do Parana, Brazil; G.L. Olichevis Halila, Embraer, Brazil; J.R.R.A. Martins¹, J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil; ¹University of Michigan, United States
Presenter: Gustavo Luiz Olichevis Halila, Embraer
12. Sep 24 11:30 12:00 5.10.4
0618
A SEQUENTIAL LOCAL ENUMERATION-BASED IMPROVED LATIN HYPERCUBE SAMPLING METHOD FOR BALLISTIC CONSTRAINT DESIGN SPACE
H. Zeng¹, Z.-H. Han¹, C.-Z. Xu¹, Y. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
12. Sep 24 12:00 12:30 5.10.5
0824
EFFICIENT SHAPE OPTIMIZATION IN AERONAUTICS: INTEGRATING PARAMETRIC CAD AND MESH MORPHING FOR ENHANCED AERODYNAMIC PERFORMANCE
A. Lopez¹, G. Magrì², U. Cella¹, G. Urso, RBF Morph srl, Italy; F. Della Barba², M.-E. Biancolini¹; ¹Università di Roma Tor Vergata, Italy ;²Università degli studi di Padova, Italy
6.10Boundary Layer Transition & control
Chair(s): Prince, S., Vijgen, P.
Track 6 Cimabue
03.3 - Basic Fluid Dynamics and Flow Control
12. Sep 24 10:00 10:30 6.10.1
0543
RESEARCH ON EFFICIENT ACTIVE T-S WAVE GENERATION METHOD IN BOUNDARY LAYER
P. Li¹, Z. Cao¹, D. Li¹; ¹Northwestern Polytechnical University, China
12. Sep 24 10:30 11:00 6.10.2
0553
NUMERICAL STUDY ON ACOUSTIC RECEPTIVITY OF COMPRESSIBLE LAMINAR FLOW OVER A FLAT PLATE WITH MODIFIED SUPER-ELLIPSE LEADING EDGE
B.Z. Xu¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China
12. Sep 24 11:00 11:30 6.10.3
0574
CROSSFLOW AND GÖRTLER INSTABILITIES IN HYPERSONIC BOUNDARY LAYERS
Y. Xi¹, S. Fu¹; ¹School of Aerospace Engineering, Tsinghua University, China
12. Sep 24 11:30 12:00 6.10.4
0918
ON THE INFLUENCE OF BASE FLOW CHARACTERISTICS ON CROSSFLOW INSTABILITY IN SWEPT BOUNDARY LAYERS
Z.-M. Xu¹, Z.-H. Han¹, H. Nie¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China
12. Sep 24 12:00 12:30 6.10.5
0987
ON THE INFLUENCE OF SURFACE ROUGHNESS ON BOUNDARY-LAYER TRANSITION FOR SWEPT WINGS
V. Prieto, ONERA and ISAE-SUPAERO, France; M. Forte, ONERA, France; E.R. Gowree, ISAE-SUPAERO, France
Presenter: Erwin Ricky Gowree, ISAE-SUPAERO
additional information (interactive) 6.10.R
0426
NUMERICAL INVESTIGATION ON THE EFFECT OF REYNOLDS NUMBER ON TANDEM DROPLET
S.-T. Peng¹, F.-Z. Chen¹, H. Yan¹, X.-Q. Sun¹; ¹Northwestern Polytechnical University, China
7.10EAP Regulation and Standards Opportunities and Challenges
Chair(s): Schultz, V., Schlickenmaier, H.
Track 7 Botticelli
15 - Guest lectures
12. Sep 24 10:00 10:30 7.10.1
0834
A CALL TO ACTION TO ENGAGE THE COMMUNITY TO MEET THE CHALLENGES THAT MUST BE TACKLED TO MAKE ELECTRIFIED AIRCRAFT PROPULSION REAL
V.P. Schultz, NASA Langley Research Center, United States; H. Schlickenmaier, HS Advanced Concepts LLC, United States; L. Daelemans, European Union Aviation Safety Authority, Germany; C. Genster, Diamond Aircraft, Austria; M. Walz, Federal Aviation Administration,, United States; E. Holtz, Harbour Air, Canada; S. Ying, Ampaire, United States
12. Sep 24 10:30 11:00 7.10.2
1320
PANEL DISCUSSION: VINCENT SCHOLTZ, HERBERT SCHLICKENMAIER, LILIAN DAELEMANS, MICHAEL WALTZ, CHRISTOPH GENSTER, EDWARD LOVELACE, ERIKA HOLTZ
P. D.,
8.10Airfoil and Wing Performance
Chair(s): Manfriani, L.
Track 8 Vasari
03.4 - Applied Aerodynamics
12. Sep 24 10:00 10:30 8.10.1
0116
SUMMARY OF DLR RESULTS FROM THE SEVENTH AIAA DRAG PREDICTION WORKSHOP
S. Keye¹, O. Brodersen¹, S. Melber-Wilkending¹; ¹German Aerospace Center (DLR), Germany
12. Sep 24 10:30 11:00 8.10.2
0957
MULTI-FIDELITY SURROGATE MODELING BASED ON DATA EXTENSION USING POD AND ANN
W. Wang¹, X. Jia¹, C. Gong¹, C. Li¹; ¹Northwestern Polytechnical University, China
Presenter: Chunna Li, Northwestern Polytechnical University
12. Sep 24 11:00 11:30 8.10.3
0501
FLIGHT TEST AND CFD STUDY OF THE EFFECT OF WING BOUNDARY LAYER TRANSITION ON AILERON BALANCE
L. Manfriani¹, X. Liu¹; ¹ZHAW, Switzerland
12. Sep 24 11:30 12:00 8.10.4
1110
TRANSFER LEARNING FOR REDUCED-ORDER MODELING OF TRANSONIC FLOWS USING MULTIFIDELITY DATA
J. Kou¹, C. Ning¹, W. Zhang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 8.10.R
0690
RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS
K.-Y. Zhou¹, S.-Q. Zhang, Jilin Chongtong Chengfei New Material Co., LTD, China; W.-P. Song¹, J.-H. Xu¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China
9.10Airport and ATC Operations
Chair(s): Kithmal Wickramasinghe, N., Mori, R.
Track 9 Giotto
09 - Air Transport System Efficiency
12. Sep 24 10:00 10:30 9.10.1
0963
DEVELOPMENT OF A NEW OPERATIONAL FRAMEWORK TO ACCOMMODATE STOCHASTIC AIR TRAFFIC FLOW AT TOKYO INTERNATIONAL AIRPORT
D. Iwata, The University of Tokyo, Japan; E. Itoh, The University of Tokyo/Electronic Navigation Research Institute, Japan
12. Sep 24 10:30 11:00 9.10.2
0061
ATM CONTROLLER SUPPORT IN CASE OF SPACIOUS SEVERE WEATHER CONSTELLATIONS ILLUSTRATED USING TWO AIRSPACE EXAMPLES
L. Nöhren¹, O. Gluchshenko¹, M.-M. Temme¹, K. Muth¹; ¹DLR, Germany
12. Sep 24 11:00 11:30 9.10.3
1016
EXTENDED REALITY IN AIRPORT CONTROL TOWERS: FROM CONCEPT DESIGN TO PRELIMINARY ASSESSMENT OF AN INNOVATIVE HUMAN-MACHINE INTERFACE FOR AIR TRAFFIC CONTROL OPERATORS
S. Bagassi¹, M. Corsi¹, T. Fadda¹; ¹University of Bologna, Italy
12. Sep 24 11:30 12:00 9.10.4
0985
A ROADMAP FOR TRANSFORMING TRADITIONAL ATCO TEAMS INTO COLLABORATIVE HUMAN-MACHINE TEAMS
T. Finck, German Aerospace Center, Germany
12. Sep 24 12:00 12:30 9.10.5
0845
MODELING TECHNIQUE FOR THE EVALUTAION OF ENVIRONMENTAL EFFECT OF FLIGHT-PATH NEAR AIRPORTS: THE CASE STUDY OF A NEW ROUTE AT NAPLES AIRPORT
M. Viscardi, University of Naples, Italy
10.10Challenge of High AR Wings 1: Aeroelastic Issues
Chair(s): Cooper, J.E., Ricci, S.
Track 10 Leonardo
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
12. Sep 24 10:00 10:30 10.10.1
0403
FINITE ELEMENT MODEL UPDATE OF VERY FLEXIBLE AIRCRAFT BASED ON GROUND VIBRATION TESTS
C.E.S. Cesnik¹, S. Sharqi¹; ¹University of Michigan, United States
12. Sep 24 10:30 11:00 10.10.2
0604
PRELIMINARY STRUCTURAL DESIGN OF A HIGH ASPECT RATIO RANSPORT AIRCRAFT WITH LAMINAR WING
M.R. Ritter¹, M. Schmalz¹, M. Fehrs¹; ¹German Aerospace Center (DLR), Germany
12. Sep 24 11:00 11:30 10.10.3
0740
NUMERICAL INVESTIGATION OF PASSIVE AND ACTIVE ALLEVIATION OF DYNAMIC LOADS ON HIGH-ASPECT-RATIO-WING VEHICLES
C.W. Cheng¹, S. Duessler¹, R. Palacios¹, G. Wilson¹; ¹Imperial College London, United Kingdom
12. Sep 24 11:30 12:00 10.10.4
0386
CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT: HIGH ASPECT RATIO WINGS AND FLOATING WINGTIPS
F. Healy¹, H. Gu¹, D. Rezgui¹, J. Cooper¹; ¹University of Bristol, United Kingdom
12. Sep 24 12:00 12:30 10.10.5
0147
GUST LOAD PASSIVE ALLEVIATION BY MEANS ON NONLINEAR, BUCKLING DRIVEN, STRUCTURAL RESPONSE
F. Toffol¹, C. Bisagni¹; ¹Politecnico di Milano, Italy
11.10Computational Aeroelasticity 2
Chair(s): Juracka, J., Palacios, R.
Track 11 Dante
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
12. Sep 24 10:00 10:30 11.10.1
1001
HIGHER-ORDER 1D STICK MODELS FOR THE FLUTTER ANALYSIS OF AIRCRAFT STRUCTURES
E. Zappino¹, M. Santori¹, M. Petrolo¹, E. Carrera¹; ¹Politecnico di Torino, Italy
12. Sep 24 10:30 11:00 11.10.2
1140
A FORMULATION FOR WING AEROELASTIC ANALYSIS BASED ON THE UNSTEADY VLM AND STRUCTURAL DISCONTINUOUS GALERKIN TECHNIQUE
F. Montano¹, I. Benedetti¹, V. Gulizzi¹; ¹Università degli Studi di Palermo, Italy
Presenter: Ivano Benedetti, Università degli Studi di Palermo
12. Sep 24 11:00 11:30 11.10.3
0854
COUPLED THERMOELASTIC ANALYSIS OF BEAM STRUCTURES USING A REFINED 1D FINITE ELEMENT MODEL
M. Filippi¹, R. Azzara¹, M. Santori¹, M. Petrolo¹, E. Carrera¹; ¹Politecnico di Torino, Italy
12. Sep 24 11:30 12:00 11.10.4
0446
ANALYSIS AND STUDY ON FLUTTER CHARACTERISTICS OF WINGS UNDER TYPICAL FRAGMENT DAMAGE
M. Zhang¹, H. Zhan¹, B. Mi¹, Y. Zhang¹, Y. Liu¹; ¹Northwestern Polytechnical University, China
12. Sep 24 12:00 12:30 11.10.5
0922
REVIEW ON NONLINEAR AEROELASTIC ANALYSIS WITH FREEPLAY
Y. Sun¹, Z. Han¹, H. Cao¹, W. Cheng¹, Z. Wu², C. Yang²; ¹Aviation Industry Development Research Center of China, China ;²School of Aeronautic Science and Engineering, Beihang University, China
Presenter: Zheng Han, Aviation Industry Development Research Center of China
additional information (interactive) 11.10.R
0445
INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY
Y. Zhang¹, H. Zhan¹, B. Mi¹, M. Zhang¹; ¹Northwestern Polytechnical University, China
12.10Human Factors 2
Chair(s): Conway, S.
Track 12 Petrarca
10 - Safety and Security
12. Sep 24 10:00 10:30 12.10.1
0131
INSIGHTS INTO HUMAN FATIGUE: STATISTICAL ANALYSIS IN AIRCRAFT MAINTENANCE
J.C. Silva, Brazil; A. Barqueira, Portugal; L.B. Magalhães, Portugal; L.F.F.M. Santos, Portugal
12. Sep 24 10:30 11:00 12.10.2
0183
PILOT FATIGUE DETECTION USING BP NEUTRAL NETWORKS
C.-R. Huang¹, H.-L. Shi¹; ¹AVIC Aerospace Life-Support Industries, Ltd., China
12. Sep 24 11:00 11:30 12.10.3
0202
ASSESSING MENTAL WORKLOAD AND INTERFACE USABILITY IN MILITARY PILOTS: AN ADVANCED EYE-TRACKING METHODOLOGY
A.C. Russo, Universidade de São Paulo, Brazil; A. Sarmento¹, I.S. Rehder¹, M.M. Cardoso-Junior¹, E. Villani¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
Presenter: Moacyr Machado Cardoso-Junior, Instituto Tecnológico de Aeronáutica
12. Sep 24 11:30 12:00 12.10.4
0743
METAMODELLING OF THE WORKLOAD ASSESSMENT IN SIMULATED FLIGHTS USING THE KRIGING METHOD
A. Esposito¹, G. Iacolino¹, C. Orlando¹, A. Alaimo¹; ¹Kore University of Enna, Italy
12. Sep 24 12:00 12:30 12.10.5
0132
A SYSTEMATIC REVIEW OF HUMAN FACTORS AND AI INFLUENCING OPERATOR PERFORMANCE IN MUM-T ENVIRONMENTS
I. de Souza Rehder¹, M.M. Cardoso Júnior¹, E. Villani¹; ¹Aeronautical Institute of Technology, Brazil
Presenter: Emilia Villani, Aeronautical Institute of Technology
13.10System-Wide Benefits of MW Class Hybrid Electric Aircraft
Chair(s): James, K., Meade, A.
Track 13 Boccaccio
15 - Guest lectures
12. Sep 24 10:00 10:30 13.10.1
0781
OPTIMIZING FLEET ASSIGNMENT DECISIONS FOR REGIONAL AIRLINES WITH HYBRID ELECTRIC AIRCRAFT UPTAKE
B. Chan, University of Pennsylvania, United States; Y. Deng¹, N. Tran¹, H. Wu¹, M. Ikeda, RTX Research Center, United States; G. Cinar¹, M.Z. Li¹; ¹University of Michigan, United States
Presenter: Max Zhaoyu Li
12. Sep 24 10:30 11:00 13.10.2
0884
SIZING AND PERFORMANCE ANALYSIS OF A MW-CLASS ELECTRIFIED AIRCRAFT PROPULSION (EAP) SYSTEM FOR A PARALLEL HYBRID TURBOPROP CONCEPT
D.D.V. Pham¹, C. Recine¹, R.H. Jansen, NASA Glenn Research Center, United States; ¹NASA Ames Research Center, United States
12. Sep 24 11:00 11:30 13.10.3
1172
REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS
J. Gladin¹, E. Aydin¹, J. Kenny¹, A. Burell¹, J. Decroix¹, T. Zaidi¹, R. Gautier¹, D. Mavris¹; ¹ASDL, United States
12. Sep 24 11:30 12:00 13.10.4
1188
VEHICLE ASSESSMENT AND SYSTEM-WIDE BENEFIT ANALYSES OF HYBRID-ELECTRIC COMMERCIAL AIRCRAFT – ELECTRIFIED POWERTRAIN FLIGHT DEMONSTRATION PROJECT (EPFD)
K.D. James¹, A. Meade¹; ¹NASA Ames Research Center, United States
12. Sep 24 12:00 12:30 13.10.5
1285
PANEL DISCUSSION
P D, United States
14.10Morealis
Chair(s): Kuegler, D.
Track 14 Puccini
10 - Safety and Security
12. Sep 24 10:00 10:30 14.10.1
0099
MOREALIS – A HOLISTIC APPROACH TO ENHANCE SAFETY FOR MICRO-AIRCRAFT OPERATIONS
R.O. Kuchar¹, W. Scholz², B. Dörfler, Rödel Aerospace Systems, Germany; P. Herrmann², P. Jamakatel, University of the Bundeswehr Munich , Germany; J. Karger², J.J. Kiam³, J. Klennert*, M. Klennert*, M. Lindlar, German Aerospace Center (DLR-ME), Germany; M.S. May¹, D. Milz¹, N. Mummº, D. Nospes³, L. Peterº, G. Looye¹, A. Schulte³, P. Stütz³; ¹German Aerospace Center (DLR-SR), Germany ;²SFL GmbH., Germany ;³University of the Bundeswehr Munich, Germany ;*STAR Healthcare Management GmbH., Germany ;ºAmazilia Aerospace GmbH., Germany
12. Sep 24 10:30 11:00 14.10.2
0268
GENERATION AND COMMUNICATION OF STRATEGIC PLANS AT DIFFERENT LEVELS OF ABSTRACTION FOR INTELLIGENT ASSISTANCE SYSTEMS IN GENERAL AVIATION
P. Jamakatel¹, J.J. Kiam ¹; ¹University of the Bundeswehr Munich, Germany
12. Sep 24 11:00 11:30 14.10.3
0460
PILOT SAFETY – SUPPORT BY BIOMEDICAL MONITORING IN PILOTS WITH HEALTH RISKS
M. Lindlar¹, J. Klennert, STAR Healthcare Management GmbH, Germany; S. Plath¹; ¹German Aerospace Center, Germany
12. Sep 24 11:30 12:00 14.10.4
0517
MIXED FLIGHT CONTROL LAYOUT FOR ULTRALIGHT GENERAL AVIATION AIRCRAFT
M. May¹, D. Milz¹, W. Scholz², P. Herrmann², J. Karger², L. Peters³, N. Mumm³, R. Kuchar¹; ¹DLR, Germany ;²SFL GmbH, Germany ;³Amazilia Aerospace GmbH, Germany
12. Sep 24 12:00 12:30 14.10.5
0706
SENSOR AND COVERAGE PATH PLANNING FOR THE MONITORING OF AIRCRAFT EMERGENCY LANDING SITES
D. Nospes¹, P. Stütz¹; ¹University of the Bundeswehr Munich, Germany
15.10UAV Control Systems 1
Chair(s): Logan, M., Bil, C.
Track 15 Carducci
06.2 - Flight Dynamics and Control (UAV related)
12. Sep 24 10:00 10:30 15.10.1
1300
APPLICATION OF UAS TECHNOLOGIES TO CREATE RESILIENT RURAL COMMUNITIES
M.J. Logan, NASA, United States
12. Sep 24 10:30 11:00 15.10.2
0459
ENHANCING QUADCOPTER CONTROL: A MODEL REFERENCE ADAPTIVE CONTROL APPROACH WITH NEURAL NETWORKS
S.R. Bassolillo¹, G. Raspaolo², L. Blasi², E. D'Amato¹; ¹Università degli Studi di Napoli Parthenope, Italy ;²Università degli Studi della Campania L. Vanvitelli, Italy
Presenter: Egidio D\'Amato, Università degli Studi di Napoli Parthenope
12. Sep 24 11:00 11:30 15.10.3
0271
ONBOARD TRAJECTORY OPTIMIZATION FOR RADIUS TO FIX TURNS
D.M. Gierszewski¹, P. Piprek¹, F. Holzapfel, Technische Universität München, Germany; ¹ Technische Universität München, Germany
12. Sep 24 11:30 12:00 15.10.4
1136
ADAPTIVE CONTROL AND MISSION PLANNER DESIGN FOR UAV OPERATIONS WITH BATTERY MANAGEMENT
A. Boldrini¹, G. Gozzini¹, D. Invernizzi¹; ¹Politecnico di Milano, Italy
Presenter: Giovanni Gozzini, Politecnico di Milano
12. Sep 24 12:00 12:30 15.10.5
0570
PASSIVE FAULT TOLERANT CONTROL OF A DUAL-SYSTEM UAV IN TRANSITION FLIGHT
J. Cai¹, M. Lovera¹; ¹Politecnico di Milano, Italy
additional information (interactive) 15.10.R
0535
A NOVEL APPROACH TO AUTOMATED TRACKING CONTROL OF HYBRID TILTING ROTOR UAVS USING LQG CONTROLLER AND STATE MACHINE
J.L. Kurniawan¹, P.B.A. Baylon¹, R.A. Sasongko¹; ¹Institut Teknologi Bandung, Indonesia
16.10Student Final
Chair(s): ,
Track 16 Raffaello
15 - Guest lectures
17.10Flight Control 1
Chair(s): Rogalski, T., Lee, C.
Track 17 Galileo
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 24 10:00 10:30 17.10.1
0044
APPLICATION OF CLUSTERING TECHNIQUES IN OPTIMISATION-BASED FLIGHT CONTROL SYSTEM CLEARANCE
P. Piprek¹, P.M. Dias¹, J. Tonti¹, D. Schwalb¹; ¹Airbus Defence and Space GmbH, Germany
12. Sep 24 10:30 11:00 17.10.2
0861
SELF-DRIVING AND MODEL-BASED EXTREMUM SEEKING CONTROL IN TIGHT FORMATION FLIGHT FOR FUEL SAVING
D.B. Rossato, Faculdade de Tecnologia SENAI, Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil
Presenter: Daniel Rossato, Faculdade de Tecnologia SENAI
12. Sep 24 11:00 11:30 17.10.3
0891
APPLICATION OF A MORE INTEGRATED TOTAL ENERGY CONTROL SYSTEM FOR IMPROVING AIRCRAFT AND ENGINE CONTROL EFFICIENCY
T. Giusti Degaspare, Embraer S.A., Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil
Presenter: Karl Heinz Kienitz, Instituto Tenológico de Aeronáutica
12. Sep 24 11:30 12:00 17.10.4
1014
FLYING V DIRECTIONAL FLIGHT CONTROL: AN EXPERIMENTAL INVESTIGATION
R. Vos¹, N. Johnson¹, S. Nolet¹; ¹TU Delft, Netherlands
12. Sep 24 12:00 12:30 17.10.5
1087
REENTRY TRAJECTORY DESIGN FOR DEFORMABLE HYPERSONIC VEHICLES BASED ON NEURAL NETWORKS
C.-K. Zhou¹, Z.-F. Luo¹, T. Zhang¹; ¹SUN YAT-SEN UNIVERSITY, China
Reserve Paper 17.10.R
0613
AILERON-FLAP-INTEGRATED ROLL CONTROL LAW BY OPTIMIZED CONTROL ALLOCATION FOR FLEXIBLE TRANSPORT AIRCRAFT
H. Wilke¹, G.C. Silva¹, F.J. Silvestre¹; ¹Technische Universität Berlin, Germany
additional information (interactive) 17.10.R
0494
A MODEL PREDICTIVE CONTROL ALGORITHM FOR THE FORMATION CONTROL OF NANOSATELLITES IN LEO ORBIT
C. Santoro¹, S.R. Bassolillo, University of Naples Parthenope, Italy; A. Ferraro, University of Reggio Calabria Mediterranea, Italy; L. Blasi¹, I. Notaro¹; ¹University of Campania L. Vanvitelli, Italy
additional information (interactive) 17.10.R
0977
MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF
Y. Liu¹, Y.-H. Nong², X. Liu, Shanghai Aircraft Airworthiness Certification Center, China; Z.-H. Cheng², M.-X. Zhang¹; ¹Northwestern Polytechnical University, China ;²AVIC General Huanan Aircraft Industry, China
additional information (interactive) 17.10.R
1070
TRAJECTORY DESIGN FOR ASTEROID SAMPLE RETURN COMBINING BALLISTIC CAPTURE AND AEROBRAKING
Z.-F. Luo¹, Y.-J. Lian, National University of Defense Technology, China; C. Zhang, Chinese Academy of Sciences, China; T. Zhang¹; ¹Sun Yat-sen University, China

12:30 - 13:30LUNCH

1.11GSA - Airspace & Operational Efficiency
Chair(s): Bastin, M.
Track 1 Auditorium
15 - Guest lectures
12. Sep 24 13:30 14:00 1.11.1
1299
NASA SUSTAINABLE FLIGHT NATIONAL PARTNERSHIP OPERATIONS RESEARCH
A. Sultan, NASA (ARMD), United States
12. Sep 24 14:00 14:30 1.11.2
1256
HOW CAN EUROPE BECOME THE MOST EFFICIENT AND ENVIRONMENTALLY-FRIENDLY SKY TO FLY IN THE WORLD?
A. Boschen, SESAR Joint Undertaking, Germany
12. Sep 24 14:30 15:00 1.11.3
1252
RECENT FLIGHT EXPERIMENTS SHOW THE CLIMATE BENEFITS OF SUSTAINABLE AVIATION FUELS (SAF) AND ADVANCED ENGINE TECHNOLOGIES
R. Moore, NASA (LaRC), United States; C. Voigt, DLR, Germany
12. Sep 24 15:00 15:30 1.11.4
1279
AI DRIVEN DECISION SUPPORT IN OPERATIONS STEERING
C. Most, Lufthansa, Germany
2.11Challenge of High AR Wings 2: Design, Aerodynamic and Control Aspects
Chair(s): Ricci, S., Atkin, C.
Track 2 Sala Verde
15 - Guest lectures
12. Sep 24 13:30 14:00 2.11.1
0855
STRUT-BRACED DRY WING CONCEPT FOR HYDROGEN-POWERED AIRCRAFT
M. Méheut¹, D. Losada Costoso¹, F. Moens¹, O. Atinault¹, C. Julien¹, L. Vertonghen¹, L. Coelho¹, V. Priasso¹, A. Lannoo¹, S. Defoort¹, E. NGuyen Van¹, C. David¹, D. Glenis¹, J. Sodja², S. de Boer², J. Schwingel³, D. Eisenhut³; ¹ONERA, France ;² Delft University of Technology, Netherlands ;³University of Stuttgart, Germany
12. Sep 24 14:00 14:30 2.11.2
1225
OPTIMAL WING ASPECT RATIO OF HIGHLY EFFICIENT LONG-RANGE AIRCRAFT
T.F. Wunderlich, German Aerospace Center (DLR), Germany
12. Sep 24 14:30 15:00 2.11.3
0108
NASA TRANSONIC TRUSS-BRACED WING STUDIES
D.P. Wells¹, G.M. Gatlin¹, J.C. June¹, T.V. Marien¹; ¹NASA Langley Research Center, United States
12. Sep 24 15:00 15:30 2.11.4
1286
EXPLORING ROLL MANEUVERABILITY OF FUTURE AIRCRAFT WITH HIGH AR WINGS
D. Sanghi¹, C.E.S. Cesnik¹, C. Riso¹; ¹University of Michigan, United States
3.11Unmanned Aerial Systems and Advanced Aerial Mobility 3
Chair(s): Lott, M., Nicolosi, F.
Track 3 Michelangelo
01.2 - Aircraft Design and Integrated System (Applications)
12. Sep 24 13:30 14:00 3.11.1
1156
CONCEPTUAL DESIGN AND SIZING OF A SOLAR POWERED QUAD-ROTOR FIXED WING HYBRID UAV FOR EXPLORATION OVER MARS
A. Kalgutkar¹, P. Gupta¹, P. Priyadarshi, Vikram Sarabhai Space Centre, India, India; R.S. Pant¹; ¹Indian Institute of Technology Bombay, India, India
12. Sep 24 14:00 14:30 3.11.2
0284
INNOVATIVE UAVS WITH CONFIGURATION OF LIKING BOTH PLANE AND KITE FOR WIND POWER
Z.X. Yao, Shenyang Aircraft Design and Research Institute, China
12. Sep 24 14:30 15:00 3.11.3
0557
FRAMEWORK DEVELOPMENT FOR CONCEPTUAL DESIGN AND CONFIGURATION ANALYSIS OF EVTOL AIRCRAFT
R.Y. Yanev¹, I. Staack¹; ¹Technische Universität Braunschweig, Germany
12. Sep 24 15:00 15:30 3.11.4
0568
ANALYSIS OF STEALTH ENHANCEMENT DESIGN PROCESS AND METHODS FOR UNMANNED AERIAL VEHICLE
G. Jia, China; D. Hu, China; Z. Guo, China; Y. Lu, China; D. Liu, China
4.11Unconventional Aircraft
Chair(s): Gerhards, R.
Track 4 Brunelleschi
01.2 - Aircraft Design and Integrated System (Applications)
12. Sep 24 13:30 14:00 4.11.1
0217
FROM THEORY TO FLIGHT: THE BOX-WING CONFIGURATION IMPLICATIONS FOR THE NEXT-GENERATION AIRCRAFT
K. Abu Salem¹, G. Palaia¹, A. Frediani, SkyBox Engineering, Italy; ¹Politecnico di Torino, Italy
12. Sep 24 14:00 14:30 4.11.2
0649
PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS
C.E.D. Riboldi¹, M. Belan¹, S. Cacciola¹, R. Terenzi¹, S. Trovato¹, D. Usuelli¹, G. Familiari¹; ¹Dept. of Aerospace Science and Technology, Politecnico di Milano, Italy
Presenter: Raffaello Terenzi, DAER - Politecnico di Milano
12. Sep 24 14:30 15:00 4.11.3
0910
GENERAL DESIGN CONSIDERATIONS FOR SOLAR-ELECTRIC HIGH-ALTITUDE LONG-ENDURANCE AIRCRAFT
A. Bierig¹, F. Nikodem¹, D. Rothe¹; ¹DLR, Germany
12. Sep 24 15:00 15:30 4.11.4
0939
CONTINUING DEVELOPMENT OF A NOVEL CERTIFIABLE AIRLINER “GONDOLA” USING LIQUID HYDROGEN
R.K. Nangia, Nangia Aero, United Kingdom; L. Hyde, Consulting, United Kingdom; J.E. Cooper, Bristol University, United Kingdom
5.11Aeroacoustic Analysis
Chair(s): Barbarino, M., Kiszkowiak, L-
Track 5 Donatello
03.1 - Aerodynamics – CFD Methods and Validation
12. Sep 24 13:30 14:00 5.11.1
0583
JET NOISE ABATEMENT VIA SURROGATE MODEL-BASED AEROACOUSTIC OPTIMISATION USING LARGE EDDY SIMULATION
G. Yang, University of Bristol, United Kingdom
12. Sep 24 14:00 14:30 5.11.2
0556
NUMERICAL STUDIES ON NOISE-SHIELDING EFFECTS OF A BLENDED-WING-BODY AIRCRAFT USING BOUNDARY ELEMENT METHOD
H.Y. Wang¹, C.T. Mutasa¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China
12. Sep 24 14:30 15:00 5.11.3
0309
AERODYNAMICS AND AEROACOUSTIC ANALYSIS OF A SUPERSONIC SLENDER-BODY GEOMETRY
M. De Rosa¹, A. Glorioso¹, G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy
Presenter: Maria De Rosa, University of Campania "Luigi Vanvitelli"
12. Sep 24 15:00 15:30 5.11.4
0682
MEASUREMENTS OF T-S WAVES DUE TO ACOUSTIC DISTURBANCES IN EXPERIMENTS
Z. Cao¹, P.F. Li¹, D. Li¹; ¹Northwestern Polytechnical University, China
6.11Turbulence Modeling
Chair(s): Choudhari, M., Zingg, D.
Track 6 Cimabue
03.1 - Aerodynamics – CFD Methods and Validation
12. Sep 24 13:30 14:00 6.11.1
1197
UNCERTAINTY ANALYSIS OF THE AERODYNAMIC PERFORMANCE OF EVTOL PROPELLERS VIA REYNOLDS STRESS TENSOR PERTURBATION
G. Gori¹, A. Zanotti¹; ¹Department of Aerospace Science and Technology, PoliMI, Italy
12. Sep 24 14:00 14:30 6.11.2
0822
ASSESSMENT OF AN ADAPTIVE ONE-EQUATION TURBULENCE MODEL FOR LEADING-EDGE VORTEX FLOWS ON MULTIPLE SWEPT DELTA WINGS
M. Zieher¹, D. Sedlacek¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
12. Sep 24 14:30 15:00 6.11.3
0607
EFFECTS OF GEOMETRY PARAMETERS ON AERODYNAMIC CHARACTERISTICS OF ROTOR AIRFOIL IN REVERSE FLOW
C.-P. Liu¹, W.-P. Song¹, S.-Q. Han, Sichuan University, China; Z.-H. Han¹; ¹Northwestern Polytechnical University, China
12. Sep 24 15:00 15:30 6.11.4
1190
ASSESSMENT OF EXPLICIT ALGEBRAIC REYNOLDS STRESS MODELS APPLIED TO AERONAUTICAL FLOWS
T. Chagas Silva, Instituto Tecnológico de Aeronáutica, Brazil; J.L.F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil
7.11ICAS Digital Pioneering Initiative
Chair(s): Nagel, B.
Track 7 Botticelli
15 - Guest lectures
12. Sep 24 13:30 14:00 7.11.1
1325
PIONEERING THE EXCHANGE OF KNOWLEDGE
B Nagel, Germany
12. Sep 24 14:00 14:30 7.11.2
1326
DIGITAL COLLABORATION FOR SUSTAINABLE AVIATION
A.S.J. van Herden, United Kingdom
12. Sep 24 14:30 15:00 7.11.3
1327
HARNESSING THE POWER OF METAVERSE TO REVOLUTIONIZE AIRCRAFT AND MRO RESEARCH
K.K. Koschlik, Germany
12. Sep 24 15:00 15:30 7.11.4
1328
MANAGING DIGITAL COMPLEXITY
C. Jouannet, Sweden
8.11Aerodynamics of Unconventional Configurations
Chair(s): Kiszkowiak, L.
Track 8 Vasari
03.4 - Applied Aerodynamics
12. Sep 24 13:30 14:00 8.11.1
0232
LOW-SUBSONIC AERODYNAMIC ANALYSES OF A NONPLANAR BWB MODEL: AN EXPERIMENTAL AND CFD STUDY
M. Nikbay¹, K. Kontis², H. Aleisa², B. Pirlepeli¹; ¹Istanbul Technical University, United Kingdom ;²University of Glasgow, United Kingdom
12. Sep 24 14:00 14:30 8.11.2
0333
ASPECT RATIO AND ADVANCE RATIO EFFECTS ON AERODYNAMIC CHARACTERISTICS OF FLEXIBLE FLAPPING WINGS
R. Addo-Akoto¹, S.-G. Lee¹, J.-S. Han, Chungnam National University, South Korea; J.-H. Han¹; ¹KAIST, South Korea
Presenter: Reynolds A.-A, KAIST
12. Sep 24 14:30 15:00 8.11.3
0401
NUMERICAL STUDY ON THE FIRST-STAGE RE-ENTRY TRAJECTORY USING AN INFLATABLE BALLUTE
V. Orlandini¹, R. Paciorri¹, A. Assonitis¹, A. Bonfiglioli, Università degli Studi della Basilicata, Italy; ¹University of Rome La Sapienza, Italy
12. Sep 24 15:00 15:30 8.11.4
1201
AERODYNAMIC ANALYSIS OF A FLAP-BASED DEPLOYABLE RE-ENTRY SYSTEM UNDER RAREFIED CONDITIONS
D. Vera Sepúlveda¹, R. Cassineli Palharini¹, E. Gaglio, Scuola Superiore Meridionale, Italy; R. Savino, University of Naples “Federico II”, Italy; ¹Universidad Técnica Federico Santa Marpia, Chile
additional information (interactive) 8.11.R
0449
SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV
Y. Li¹, X. Xu¹, Z. Zhou¹, Y. Bai¹, H. Wang¹, B. Xu¹; ¹Northwestern Polytechnical University, China
Presenter: Yunlong Li
additional information (interactive) 8.11.R
0473
RESEARCH ON OPTIMAL TORSIONAL DEFORMATION OF FLAPPING WING
J. Liu¹, D. Xue¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
9.11Optimal Operations
Chair(s): Homola, J., Andreeva-Mori, A.
Track 9 Giotto
09 - Air Transport System Efficiency
12. Sep 24 13:30 14:00 9.11.1
0142
ESTIMATING THE IMPACT OF NUMERICAL WEATHER PREDICTION DATA MODELS ON SHORT-HAUL MINIMUM COST TRACKS
N.K. Wickramasinghe¹, Y. Nakamura¹, A. Senoguchi¹; ¹Electronic Navigation Research Institute, Japan
12. Sep 24 14:00 14:30 9.11.2
0763
PAIRWISE SWAPPING SEQUENCE OPTIMIZATION BY METROPOLIS-HASTING ALGORITHM WITH QUANTUM ANNEALING FOR AIR TRAFFIC CONTROL
N. Yoshikawa, Mitsubishi Electric Corporation, Japan
12. Sep 24 14:30 15:00 9.11.3
0946
AUTOMATED OPERATION OF HIGH-PERFORMANCE FIXED-WING DRONES: A POTENTIAL GAME-CHANGER FOR GREEN AERIAL SERVICES
M. Spieck, Thelsys, Germany; J.H. Binnebesel¹, J. Mehnen¹; ¹mb+Partner, Germany
12. Sep 24 15:00 15:30 9.11.4
1007
STRUCTURED ANALYSIS ESTIMATION FOR ELECTRICAL ENERGY DEMAND ON AIRPORT OPERATIONS FOR HYBRID REGIONAL AND ELECTRIC TOWING PARAMETERIZED BY MOVEMENT METRICS CONSIDERING UPCOMING ELECTRIC INTENSIVE TECHNOLOGIES AND EMISSION REDUCTIONS IN THE UPCOMING D
T. Oliveira¹, A. Carvalho¹; ¹The Boeing Company, Brazil
10.11Bonding / Mechanical Behaviour
Chair(s): Zappino, E., Jokinen, J.
Track 10 Leonardo
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
12. Sep 24 13:30 14:00 10.11.1
1222
PATCHBOND II - CERTIFICATION OF ADHESIVE BONDED REPAIRS FOR PRIMARY AEROSPACE COMPOSITE STRUCTURES
J. Jokinen, Tampere University, Finland; T. Thorvaldsen, Norwegian Defence Research Establishment, Norway; P. Nijhuis, Royal Netherlands Aerospace Centre, Netherlands; M. Kadlec¹, R. Ruzek¹, L. Munch, University of Stuttgart, Institute of Aircraft Design, Germany; M. Hoffmann, Airbus Defence and Space GmbH, Germany; T. Viitanen, Technical Research Center of Finland Ltd, Finland; M. Wallin, Patria Aviation, Finland; G. Sagvolden, Light Structures AS, Norway; C. Sbarufatti², L. Martulli², A. Bernasconi²; ¹Czech Aerospace Research Centre, Czech Republic ;²Politecnico di Milano, Department of Mechanical Engineering, Italy
12. Sep 24 14:00 14:30 10.11.2
0407
HOT-WET CONDITIONING AND THE SENSITIVITY OF MECHANICAL TESTING WITHIN SURFACE TREATMENT QUALIFICATION FOR AIRCRAFT
D. Blanco Garde¹, F. Mews¹, J. Jokinen¹, N. Pournoori¹, M. Kanerva¹; ¹Tampere University, Finland
12. Sep 24 14:30 15:00 10.11.3
0300
STABLE LOCALIZED CORROSION IN A 7075-T6 ALUMINUM ALLOY FSW JOINT: MECHANISM AND MITIGATION
K. Li¹, Y. Ma, Chongqing University of Technology, China; Y. Han¹; ¹AVIC Manufacturing Technology Institute, China
Presenter: Kai Li, AVIC Manufacturing Technology Institute
12. Sep 24 15:00 15:30 10.11.4
0796
INVESTIGATION ON THE MECHANISM OF THERMAL CYCLING FAILURE IN C/SIC COATING COMPOSITE MATERIALS
Y. Ma, China; X. Zha, China; P. Cheng, China; J. Xie, China; L. Li, China; X. Liu, China
Presenter: Yanbin Ma, Avic Aircraft Strength Research Institute
11.11Aerodynamic Instrumentation and Measurement 2
Chair(s): Manfriani, L.
Track 11 Dante
03.2 - Experimental Aerodynamics
12. Sep 24 13:30 14:00 11.11.1
0894
DESIGN OF A HIGH ENTHALPY HYPERSONIC NOZZLE FOR “GHIBLI” PLASMA WIND TUNNEL
D. Guida¹, A. Smoraldi¹, A. Schettino, C.I.R.A., Germany; ¹CIRA Italian Aerospace Research Centre, Italy
12. Sep 24 14:00 14:30 11.11.2
0634
SPARSE RECONSTRUCTION OF SURFACE LOADS ON AIRCRAFT USING POD AND RBFNN
X. Jia¹, C. Gong¹, C. Li¹; ¹Northwestern Polytechnical University, China
12. Sep 24 14:30 15:00 11.11.3
0840
DEVELOPMENT OF UNSTEADY PRESSURE-SENSITIVE PAINT FOR LOW REYNOLDS NUMBER WIND TUNNEL TESTS IN LOW-PRESSURE ENVIRONMENTS
S. Takaya¹, K. Shibata¹, D. Numata¹; ¹Tokai University, Japan
12.11Composites 3
Chair(s): Pagani, A.
Track 12 Petrarca
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
12. Sep 24 13:30 14:00 12.11.1
0045
STUDY ON LOW-VELOCITY IMPACT BEHAVIOR AND RESIDUAL PERFORMANCE PREDICTION OF CFRP T-JOINTS
J. Zhou, China; C. Zhang, China
12. Sep 24 14:00 14:30 12.11.2
0212
THE RESISTANCE TO THE HIGH-VELOCITY IMPACT OF THE INTRA-LAYER HYBRID PLAIN WEAVE COMPOSITES
H. Wu¹, Y. Bai¹, S.-L. Fang¹, Z.-Q. Zhao¹, C. Zhang¹; ¹Northwestern Polytechnical University, China
12. Sep 24 14:30 15:00 12.11.3
0215
MODELING THE TEMPERATURE-RISE BEHAVIOR OF 2D TRIAXIAL BRAIDED COMPOSITES UNDER IMPACT LOADS
C. Zhang¹, P. Liu¹, Y.-L. Li¹; ¹Northwestern Polytechnical University, China
12. Sep 24 15:00 15:30 12.11.4
0225
THE EFFECT OF TARGET THICKNESS ON THE BALLISTIC BEHAVIOR OF HYBRID CFRP/KFRP COMPOSITES
S. Zhao¹, J. Huang¹, C. Zhang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 12.11.R
0806
EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT
M. Mucha¹, D. Sikorski, 41st Training Air Base, Poland; R. Szczepaniak¹, R. Babel¹, A. Krzyzak¹, T. Zahorski¹; ¹Polish Air Force University, Poland
13.11Propellers, Fans, Compressors 4
Chair(s): Mari, C.
Track 13 Boccaccio
05 - Propulsion
12. Sep 24 13:30 14:00 13.11.1
0143
FLOW CHARACTERISTICS OF THE INLET IN TURBOPROP ENGINE WITH THE INFLUENCE OF SANDS
B. Mi¹, H. Zhan¹, J. Yu, No. 5715 Factory of PLA, China; ¹Northwestern Polytechnical University, China
12. Sep 24 14:00 14:30 13.11.2
1011
DEEP LEARNING BASED FAST PREDICTION OF AERODYNAMIC PARAMETERS FOR DUCTED PROPELLERS
L. Liu¹, L. Zeng¹, T. Wang¹, Z. Gao¹, X. Shao¹; ¹Zhejiang University, China
12. Sep 24 14:30 15:00 13.11.3
1157
LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION
M. Crona¹, S. Dinger¹, P. Samuelsson¹, H. Strömfeldt¹, I. Jonsson¹; ¹Chalmers University of Technology, Sweden
12. Sep 24 15:00 15:30 13.11.4
0523
CANCELED - PRELIMINARY COUPLING EFFECTS OF A NOVEL INTEGRATED SELF-SUPERCHARGED PROPULSION SYSTEM
X. Xiong¹, S. Wu¹; ¹International WYNNBEAR Advanced AeroTechInnovation, United States
14.11Navigation, Comms & Radar
Chair(s): Toebben, H.
Track 14 Puccini
10 - Safety and Security
12. Sep 24 13:30 14:00 14.11.1
0519
CANCELED - ADVANCED RADAR-BASED COUNTER-UAV SOLUTIONS FOR ENHANCED AIRCRAFT SECURITY IN AIRPORT ENVIRONMENTS
V. Miliotis, Bianor Services Ltd & MSB Technologies P.C., Bulgaria; T. Punchev, Bianor Services Ltd, Bulgaria; I.D. Gavardinas, Hellenic Air Force & University of Thessaly, Greece; P. Koutidis, Hellenic Air Force, Greece; B. Papaspyros, Hellenic Air Force Engineers Scientific Society, Greece; P. Chatzimisios, International Hellenic University, Greece
Presenter: VASILEIOS MILIOTIS, Bianor Services Ltd and MSB Technologies
12. Sep 24 14:00 14:30 14.11.2
0559
A FAST INFORMATION THEORETICALLY SECURE RADIO COMMUNICATION PROTOCOL BASED ON GNSS POSITIONING
S. Morioka, Interstellar Technologies Inc., Japan; S. Obana, Hosei University, Japan; M. Yoshida, NICT, Japan
12. Sep 24 14:30 15:00 14.11.3
0617
MUTUAL POSITION PLAUSIBILITY CHECKING IN FLYING AD-HOC NETWORKS USING DISTANCE MEASUREMENTS
T. Marks, German Aerospace Center, Germany; K. Fuger, Hamburg University of Technology, Germany
15.11Flight Systems Dynamics
Chair(s): Viola, N.
Track 15 Carducci
07 - Systems, Subsystems and Equipment
12. Sep 24 13:30 14:00 15.11.1
0467
FAILURE HANDLING ON A SPLIT-FLAP ULTRALIGHT GENERAL AVIATION AIRCRAFT WITH HYBRID NONLINEAR DYNAMIC INVERSION
D. Milz¹, M. May¹, J. Martins¹, R. Kuchar¹, G. Looye¹; ¹German Aerospace Center (DLR), Germany
12. Sep 24 14:00 14:30 15.11.2
0932
EXPLORING A CATEGORY OF LIMIT CYCLE OSCILLATIONS IN AIRCRAFT HYDRAULIC SYSTEMS
S. Yang¹, Y. Long, School of Energy and Power Engineering, Beihang University, China; Z. Hu¹; ¹Institute for Aero Engine, Tsinghua University, China
12. Sep 24 14:30 15:00 15.11.3
0520
SIMPLIFIED MODELS OF PILOT BIOMECHANICS FOR ROTORCRAFT VERTICAL BOUNCE ANALYSIS
T. Aresi¹, A. Zanoni¹, G. Cassoni¹, P. Masarati¹; ¹Politecnico di Milano, Italy
12. Sep 24 15:00 15:30 15.11.4
0440
ENHANCED SAFETY THROUGH AI: AN ASSESSMENT OF ADVERSARIAL REINFORCEMENT LEARNING FOR CONTROL OF COMPLEX AIRCRAFT
C. Koopman¹, D. Zammit-Mangion¹; ¹University of Malta, Malta
16.11Manufacturing Management and Supply Chain Managment
Chair(s): Lin, K., Liu, X.
Track 16 Raffaello
08 - Manufacturing and Supply Chain Management
12. Sep 24 13:30 14:00 16.11.1
0589
VALUE-DRIVEN TRADESPACE EXPLORATION FOR AIRCRAFT DESIGN, MANUFACTURING AND SUPPLY CHAIN
G. Donelli¹, J.M.G.D. Mello², F.I.K. Odaguil², T. Van der Laan, GKN/Fokker, Netherlands; L. Boggero¹, B. Nagel¹; ¹German Aerospace Center DLR, Germany ;²Embraer, Brazil
12. Sep 24 14:00 14:30 16.11.2
0804
UNCERTAINTY PROPAGATION IN VALUE-DRIVEN DECISION-MAKING FOR THE AIRCRAFT, MANUFACTURING AND SUPPLY CHAIN DESIGN
G. Ascione¹, G. Donelli¹, L. Boggero¹, B. Nagel¹; ¹DLR, Germany
Presenter: Pina Donelli, DLR
12. Sep 24 14:30 15:00 16.11.3
0100
A SUPPORTING FRAMEWORK FOR AIRCRAFT MRO OPERATIONS. CAPACITY PLANNING, TASKS TRACEABILITY AND DISEMBARKED ITEMS TRACKING
F. Martone¹, G. Zazzaro¹, M. Inverno¹, S. De Luca, Atitech S.p.A., Italy; F. Mainieri, Major Bit Consulting s.r.l., Italy; G. Romano¹; ¹C.I.R.A. Italian Aerospace Research Centre, Italy
12. Sep 24 15:00 15:30 16.11.4
0190
COMPUTER VISION ALGORITHMS FOR THE IDENTIFICATION OF DAMAGES ON FULL-SCALE AIRCRAFT COMPONENTS
S. Merola ¹, M. Guida¹, F. Marulo¹; ¹University of Naples Federico II, Italy
17.11Flight Test and Equipment
Chair(s): Kim, Y., Kordos, D.
Track 17 Galileo
06.1 - Flight Dynamics and Control (Control & Modelling)
12. Sep 24 13:30 14:00 17.11.1
0646
VALIDATION OF ENERGY CHARACTERISTICS IN FLIGHT CONTROL SYSTEM BASED ON A MULTIDISCIPLINARY VIRTUAL PLATFORM
Y. Wang¹, M. Sun¹, J. Fu¹; ¹Beihang University, China
12. Sep 24 14:00 14:30 17.11.2
1151
RESULTS OF THE SCALED FLIGHT DEMONSTRATOR FLIGHT TESTS
P. Schmollgruber¹, C. Toussaint¹, P. Iannelli, CIRA, Italy; H. Jentink, Royal NLR, Netherlands; D. Kierbel, Airbus S.A.S., France; ¹ONERA, France
12. Sep 24 14:30 15:00 17.11.3
0647
FAULT DETECTION FOR AN AIRCRAFT ELEVATOR
F.C. Antoniazzi¹, A.G.P. Sarmento¹, E. Villani¹; ¹Aeronautical Institute of Technology, Brazil
Presenter: Emília Villani, Aeronautical Institute of Technology
12. Sep 24 15:00 15:30 17.11.4
0890
ENERGY PREDICTION DURING APPROACH AND LANDING BASED ON LONG SHORT-TERM MEMORY MODEL
J.-Q. Yan, School of Aeronautics, Northwestern Polytechnical University, China
additional information (interactive) 17.11.R
0491
DATA ORIENTED EVALUATION OF FLIGHT CHARACTERISTIC MODELS BY USING BAYES FACTOR
M. Naruoka¹, T. Ninomiya¹; ¹Japan Aerospace Exploration Agency, Japan

15:30 - 16:00BREAK

0.10VON KARMAN LECTURE: Pedro Cabral: Aeroelastic Tailoring Project
Chair: D. Mavris ICAS President
12. Sep 24 16:00 17:00

17:00 - 17:45CLOSING CEREMONY