33th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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Thursday, 08. Sep 2022


0.1General lecture V: ICAS/IFAR „Transforming Aviation towards Zero Emission - to mitigate the climate impact“ I. Yimer, NRC Canada, B. Sainjon, ONERA France, M. Fischer, DLR Germany, Y. Watanabe, JAXA Japan, P. Krus, SARC Sweden
Chair: D. Mavris ICAS PC Chair
08. Sep 22 08:00 09:30

09:30 - 10:00Coffee Break

1.1Selected Highlights from Clean sky/Clean Aviation 1 (invited)
Chair(s): Krein, A.
A1
15 - Guest lectures
08. Sep 22 10:00 10:30 1.1.1 CS2 PROGRAMME OVERVIEW
S. Dubious, France
08. Sep 22 10:30 11:00 1.1.2 SUSTAINABLE TECHNOLOGIES FOR COMMERCIAL AIRCRAFT OF TOMORROW - INTEGRATED MULTIFUNCTIONAL FUSELAGE DEMONSTRATOR
Y.C. Roth, Germany
08. Sep 22 11:00 11:30 1.1.3 OPEN FAN ENGINE ARCHITECTURE FOR NEXT GENERATION SMR
C. DIETTE, Safran Aircraft Engines, France
08. Sep 22 11:30 12:00 1.1.4 PROGRESS IN WING DESIGN, STATUS AND PERSPECTIVES
J. LERY, Dassault Aviation, France; M. WERNER, Airbus, Germany; E. COUSTOLS, ONERA, France
08. Sep 22 12:00 12:30 1.1.5 THE CLEAN SKY 2 TECHNOLOGY EVALUATOR 1ST GLOBAL ASSESSMENT RESULTS
J.F. Brouckaert, Belgium
2.1Sustainable Aircraft 2
Chair(s): Gibson, T.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
08. Sep 22 10:00 10:30 2.1.1 COMBINED APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER IN PRELIMINARY AIRCRAFT DESIGN
T. Effing¹, V. Schmitz¹, F. Schültke¹, F. Peter, Bauhaus Luftfahrt e.V, Germany; E. Stumpf¹; ¹RWTH Aachen University, Germany
08. Sep 22 10:30 11:00 2.1.2 CLEAN-SKY 2 LARGE PASSENGER AIRCRAFT PLATFORM 1 ADVANCED ENGINE AND AIRCRAFT CONFIGURATIONS
D. KIERBEL, AIRBUS, France
08. Sep 22 11:00 11:30 2.1.3 AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN
Thomas Streit¹, Martin Kruse¹, Thomas Kilian¹, Ilias Petropoulos, ONERA, France; Judith v Geyr¹; ¹DLR, Germany
08. Sep 22 11:30 12:00 2.1.4 ECONOMICS OF SUSTAINABLE REGIONAL AIR MOBILITY
P De Felipe¹, D Yang¹; ¹Imperial College London, United Kingdom
08. Sep 22 12:00 12:30 2.1.5 TOWARD A GREENER AIRCRAFT ARCHITECTURE
F Vidal de Saint Jean, Dassault Aviation, France
Reserve Paper 2.1.R DEVELOPMENT OF INNOVATIVE AND ECO-FRIENDLY AIRFRAME TECHNOLOGIES TO IMPROVE AIRCRAFT LIFE CYCLE ENVIRONMENTAL FOOTPRINT
L.A.S.A Prado¹, S. Coskun¹, T.S.G. Das¹, A. Kötter¹; ¹Capgemini Engineering / Altran Deutschland und SAS KG, Germany
Presenter: Luis Antonio Sanchez de Almeida Prado, Capgemini Engineering / Altran Deutschland und SAS KG
3.1Hybrid-Electric Aircraft & LH2 3
Chair(s): Gerhards, R.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
08. Sep 22 10:00 10:30 3.1.1 SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART I: INITIAL DESIGNS
M.F.M. Hoogreef¹, V.O. Bonnin¹; ¹Delft University of Technology, Netherlands
08. Sep 22 10:30 11:00 3.1.2 SCALABILITY ANALYSIS OF RADICAL TECHNOLOGIES TO VARIOUS AIRCRAFT CLASS - PART II: SENSITIVITY ANALYSIS
V.O. Bonnin¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands
08. Sep 22 11:00 11:30 3.1.3 REGIONAL TRANSPORT AIRCRAFT DESIGN USING TURBO-ELECTRIC DISTRIBUTED PROPULSION SYSTEM
V. Polepeddi¹, P. Raj¹, Mathias Emeneth, PACE America, United States; ¹Virginia Tech, United States
08. Sep 22 11:30 12:00 3.1.4 RETROFITTING EXISTING AIRCRAFT WITH HYDROGEN PROPULSION
E. Fourquet-Beramendi¹, A.S.J. van Heerden¹, I. Roumeliotis¹, S. Brown¹, V. Pachidis¹; ¹Cranfield University, United Kingdom
Presenter: Elorie Fourquet-Beramendi, Airbus
08. Sep 22 12:00 12:30 3.1.5 ARRIVING AT CERTIFIABLE NOVEL AIRLINER USING LIQUID HYDROGEN & EFFICIENCY METRICS
Raj (Dr) Nangia, Nangia, United Kingdom; Leslie (Mr) Hyde, Consulting, United Kingdom
4.1CFD Applications 2
Chair(s): Kiszkowiak, L., Viviani, A.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
08. Sep 22 10:00 10:30 4.1.1 STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL
Carlos Tavera Guerrero¹, Nenad Glodic¹, Hans Mårtensson, GKN Aerospace Sweden AB, Germany; ¹KTH, Sweden
08. Sep 22 10:30 11:00 4.1.2 LARGE EDDY SIMULATION OF A LYNX HELICOPTER LANDING IN THE BARROSO CORVETTE SHIP
D. M. Pio¹, C.F. Rafael¹, P. S. C. Villela¹, G. A. L. da Silva¹, M. J. M. Guedes, Marinha do Brasil, Brazil; M. Ferro, Laboratorio Nacional de Computacao Cientifica - LNCC, Brazil; ¹Aerothermal Solutions - ATS, Brazil
08. Sep 22 11:00 11:30 4.1.3 NUMERICAL INVESTIGATIONS OF ROTORCRAFT PRESSURE ERROR CORRECTION BY UTILIZATION OF AIR DAMS
A.-O. Sezer, Turkish Aerospace, Turkey; M. Elfarra, Ankara Y?ld?r?m Beyaz?t University, Turkey
08. Sep 22 11:30 12:00 4.1.4 TRANSONIC FLOW OVER DELTA WING USING ENTROPIC LATTICE BOLTZMANN METHOD
M Dhake¹, C Thantanapally¹, S Arcidiacono¹, S Ansumali¹; ¹SankhyaSutra Labs Ltd, India
Presenter: Chakradhar Thantanapally, SankhyaSutra Labs Limited
08. Sep 22 12:00 12:30 4.1.5 CFD TAKE-OFF ANALYSIS OF A SEAPLANE HULL THROUGH A DYNAMIC MULTIPHASE MODEL
M. Sinisi¹, G. Occhipinti¹, G. Cantanna¹, A. Caramazza¹, G. Dilonardo¹, E. Cestino¹; ¹Politecnico di Torino, Italy
Reserve Paper 4.1.R EFFECTS OF TWO WINGLET TIP GEOMETRIES ON THE FLOW AND AERODYNAMIC PERFORMANCE OF A HYDRAULIC AXIAL TURBINE
D. S. Tonon¹, J. T. Tomita¹, C. Bringhenti¹, D. F. C. Barbosa¹, L. H. L. Whitacker¹, L. E. N. Almeida, AVIBRAS, Brazil; ¹Aeronautics Institute of Technology , Brazil
Reserve Paper (interactive) 4.1.R VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA
D. Standingford¹, C. Sequeira², M. Allan¹, G. Furse², J. Sharpe¹; ¹Zenotech, United Kingdom ;²Flare Bright, United Kingdom
Reserve Paper (interactive) 4.1.R COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHODS.
G. Muchla¹, A. Kwiecien¹; ¹Faculty of Power and Aeronautical Engineering, WUT, Poland
Presenter: Adrianna Kwiecien, Faculty of Power and Aeronautical Engineering, WUT
Reserve Paper (interactive) 4.1.R REDESIGNING AND SIMULATION EVALUATION ON LARGE-FLOW HIGH-TEMPERATURE HIGH-PRESSURE BYPASS SURGE-OUT SYSTEM
Zhi-peng:Z.-P Li, AECC Shenyang Engine Research Institute, China
5.1Turbulence Modelling
Chair(s): Eliasson, P., Halila, G.
C 2
03.1 - Aerodynamics – CFD Methods and Validation
08. Sep 22 10:00 10:30 5.1.1 AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 1 (invited)
A Rizzi¹, DS Henningson¹; ¹KTH, Sweden
08. Sep 22 10:30 11:00 5.1.2 AERONAUTICAL CFD AND TURBULENCE - PROGRESS AND CHALLENGES PART 2 (invited)
A Rizzi¹, D. Henningson¹; ¹KTH, Sweden
08. Sep 22 11:00 11:30 5.1.3 OPEN CAVITY SIMULATIONS UNDER SIDESLIP CONDITIONS
Karthick Rajkumar¹, Joseph Radtke¹, Eike Tangermann¹, Markus Klein¹; ¹University of the Bundeswehr Munich, Germany
08. Sep 22 11:30 12:00 5.1.4 APPLICATION OF GP AND ANN APPROACHES FOR RECONSTRUCTION OF TURBULENT JET FLOW FIELDS
V. Gryazev, United Kingdom; U. Armani, United Kingdom; A.R. Murali, France; A.P. Markesteijn, United Kingdom; S.A. Karabasov, United Kingdom; V. Toropov, United Kingdom; S.E. Naghibi, United Kingdom; V. Riabov, Japan
08. Sep 22 12:00 12:30 5.1.5 UNSTEADY SIMULATIONS OF MASSIVELY SEPARATED FLOW AROUND NACA0021 AIRFOIL USING A TRANSITIONAL IDDES MODEL
Y. Wang, China; S.-Q. Zhang, China; W.-P. Song, China; Z.-H. Han, China
Reserve Paper 5.1.R INVESTIGATION ON THE INFLUENCES OF TURBULENCE MODEL AND OPERATING CONDITIONS ON THE CENTRIFUGAL NOZZLE PERFROMANCE
Da Mo¹, Hongjun Lin¹, Caiyun Liang¹, Shoutang Shang¹, Jiaohui Xia, Aero Engine Academy of China, China; Yixiong Liu¹; ¹AECC Shenyang Engine Research Institute, China
6.1Wind Tunnel Testing Technology 1
Chair(s): ,
C 3
03.2 - Experimental Aerodynamics
08. Sep 22 10:00 10:30 6.1.1 EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS
J. Stegmüller¹, S. Hayböck¹, P. Hartl¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
08. Sep 22 10:30 11:00 6.1.2 OPTIMIZATION OF AN ACTIVE DAMPING SYSTEM FOR USE WITH A SINGLE STRUT MOUNT
J. L. Pereira, National Research Council Canada, Canada
08. Sep 22 11:00 11:30 6.1.3 WIND-TUNNEL TEST ON LEADING-EDGE VORTEX OF LOW-ASPECT-RATIO FLAPPING PLATES
J.-S. Han¹, C. Breitsamter¹; ¹Technical University of Munich, Germany
08. Sep 22 11:30 12:00 6.1.4 POWERED WIND TUNNEL TESTING WITH HYDRAULIC MOTORS
D. Steiling¹, P. Aschwanden¹, J. Müller¹, T. Jax¹; ¹RUAG AG, Switzerland
Presenter: Peter Aschwanden, RUAG AG
08. Sep 22 12:00 12:30 6.1.5 EXPERIMENTING ROTORCRAFT FLIGHT IN COMPLEX ENVIRONMENTAL CONDITIONS USING WIND TUNNEL: HELICOPTER SHIP LANDING CASE
A. Zanotti¹, G. Gibertini¹, G. Quaranta¹; ¹Politecnico di Milano, Italy
Reserve Paper 6.1.R RESEARCH ON VIRTUAL FLIGHT TEST OF LARGE-SCALE LOW-SPEED WIND TUNNEL
W.-Y. Yanling, Aerodynamics Research Institute,Harbin, China
7.1Fatigue Analysis
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
08. Sep 22 10:00 10:30 7.1.1 INCREMENTAL FATIGUE DAMAGE MODEL: APPLICATION TO PLANE PROBLEMS WITH NON-PROPORTIONAL LOADING
Z Kapidzic¹, S. B. Lindström, Linköping University, Sweden; J Lundgren¹; ¹Saab AB, Sweden
08. Sep 22 10:30 11:00 7.1.2 FATIGUE OF STANDARD SPECIMENS – THE INFLUENCE OF THE STRESS GRADIENT ON THE S-N CURVE IN DIFFERENT AL2024 KT=2.0 DESIGNS
S Sieberer¹, J Homan, Fatec Engineering, Netherlands; M Schagerl¹; ¹Johannes Kepler University Linz, Austria
08. Sep 22 11:00 11:30 7.1.3 FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES
L. Boni ¹, F Bovecchi¹, D. O. Busse, AIRBUS Operations GmbH, Germany; D. Furfari, IRBUS Operations GmbH, Germany; ¹University of Pisa, Italy
08. Sep 22 11:30 12:00 7.1.4 FATIGUE CHARACTERIZATION OF ADHESIVE JOINTS IN AEROPLANES-THE DEVELOPMENT OF A NEGATIVE LOAD RATIO (R<0) TESTING METHOD
O Orell¹, J Jokinen¹, M Kanerva¹; ¹Tampere University, Finland
08. Sep 22 12:00 12:30 7.1.5 FATIGUE DAMAGE MODEL OF HIGH TEMPERATURE POLYMER COMPOSITES IN AERO-ENGINES
Vivek Richards Pakkam Gabriel¹, Patrik Fernberg¹; ¹Luleå University of Technology, Sweden
Reserve Paper 7.1.R FATIGUE CRACK PROPAGATION IN ADDITIVELY MANUFACTURED POLYMER PARTS
H.H El Fazani¹, J. Laliberté¹, J. Coil¹; ¹Carleton University , Canada
8.1Vibration and Damping 1
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
08. Sep 22 10:00 10:30 8.1.1 DEVELOPMENT OF A PREDICTIVE DAMAGE METHODOLOGY FOR HYBRID WING BODY AIRCRAFT STRUCTURES
H. Raza¹, C. Harey¹, P. Vaghela¹, J. Bayandor¹; ¹CRASH Lab, University at Buffalo, United States
Presenter: Christopher Harley, CRASH Lab, Dept. of MAE, University at Buffalo
08. Sep 22 10:30 11:00 8.1.2 NUMERICAL ANALYSIS AND COMPARISON WITH RESULTS OF FRACTURE TESTS OF LUG MANUFACTURED IN COMPOSITE MATERIAL
G. C. Fonseca, Embraer Minas Gerais, Brazil; S. F. M. Almeida, Instituto Tecnológico de Aeronáutica, Brazil
08. Sep 22 11:00 11:30 8.1.3 ENHANCEMENT OF FLEXIBLE STRATEGY FOR AUGMENTING DESIGN POINTS FOR COMPUTER EXPERIMENTS AND APPLICATION TO A MDO OF A FAN-BLISK
A. Tamkan¹, P. Flassig¹, M Meyer, Rolls-Royce Deutschland, Germany; ¹Technische Hochschule Brandenburg, Germany
08. Sep 22 11:30 12:00 8.1.4 TRANSIENT AND FREE-VIBRATION ANALYSIS OF LAMINATED SHELLS THROUGH THE DISCONTINUOUS GALERKIN METHOD
G. Guarino¹, V. Gulizzi¹, A. Milazzo¹; ¹1University of Palermo, Department of Engineering, Italy
08. Sep 22 12:00 12:30 8.1.5 DESIGN AND STUDY ON NOISE REDUCTION PROPERTIES OF A MULTISTAGE BIONIC MEMBRANE-TYPE ACOUSTIC METAMATERIAL
X. J. Zhang¹, D. Guo¹, H. Y. Huang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 8.1.R MODELING AND ANALYSES OF A MULTI-FUNCTIONAL PIEZO-SMA-COMPOSITE WING
G.C. Silva, Technische Universität Berlin, Germany
Reserve Paper 8.1.R A NEW APPROACH TO SHAPING THE PUSHROD TUBE AS THE MAIN COMPONENT OF THE CONTROL SYSTEM, OPTIMIZATION, AND MANUFACTURING.
W. Grendysa, Warsaw University of Technology, Poland
9.1Propellers, Fan Compressors
Chair(s): Piro, N.
C 4
05 - Propulsion
08. Sep 22 10:00 10:30 9.1.1 AEROELASTIC TAILORING OF COMPRESSOR BLADES
A.-P. Chalke¹, N Glodic¹, M Gutierrez Salas¹; ¹KTH Royal Institute of Technology, Sweden
08. Sep 22 10:30 11:00 9.1.2 RAPID AEROACOUSTIC PLANFORM DESIGN OPTIMIZATION OF INSTALLED PROPELLERS
T. Sinnige¹, W. de Gruijl¹, W. de Haan¹, G. Eitelberg¹; ¹Delft University of Technology, Netherlands
08. Sep 22 11:00 11:30 9.1.3 PERFORMANCE BENEFITS OF A FAN ON BLADE – FLADE – FOR A VARIABLE CYCLE ENGINE
Marcelo Assato, IAE, Brazil; Ali Altar Inceer¹, Lucilene Moraes¹, Jesuino Takachi Tomita², Cleverson Bringhenti², Pedro Bravo-Mosquera, USP, Brazil; Daniel Rosell, SAAB Aeronautcs, Sweden; Tomas Grönstedt¹; ¹Chalmers University, Sweden ;²ITA, Brazil
08. Sep 22 11:30 12:00 9.1.4 STATUS OF GKN AEROSPACE\\\'S ENGINE MODULE DEMONSTRATORS IN THE CLEAN SKY-2 PROJECT
Robert Lundberg¹, Lars Ellbrant¹, Patrik Johansson¹, Ulf Johansson¹, Mattias Billson¹, Bernhard Gustafsson¹; ¹GKN Aerospace Sweden AB, Sweden
Presenter: Lars Ellbrant, GKN Aerospace Sweden AB
08. Sep 22 12:00 12:30 9.1.5 STUDY ON THE OBJECTIVE FUNCTION OF THE PROFILED ENDWALL OPTIMIZATION OF AN EMBEDDED COMPRESSOR STATOR
Jiayu Wang¹, Dejun Meng¹, Dongmin Feng¹, Qingwei Zhao¹; ¹Shenyang Engine Research Institute of AECC, China
Reserve Paper 9.1.R DESIGN AND EFFICIENCY ANALYSIS OF EVTOL CONTRA-ROTATING PROPELLER
N.-X Qiao¹, T.-L Ma¹, X.-S Wang¹, J.-C Fu¹; ¹Beihang University, China
Reserve Paper 9.1.R EXPERIMENTAL STUDY ON THE EFFECT OF INTERSTAGE BLEEDING ON THE PERFORMANCE OF FULL-SCALE MULTISTAGE AXIAL COMPRESSOR
Z.-B. Zhang¹, Y.-H. Zhang¹, Y.-H. Chen¹; ¹Shenyang Engine Research Institute, China
Reserve Paper 9.1.R EXPERIMENTAL STUDY OF FLAT BAFFLE INLET TOTAL-PRESSURE DISTORTION IN A THREE-STAGE FAN
CHEN Yehui¹, ZHANG Zhibo¹, WANG Anni¹; ¹AECC Shenyang Engine Institute, China
Presenter: Yehui CHEN, AECC Shenyang Engine Institute
Reserve Paper (interactive) 9.1.R SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR
Jia Bobo¹, Zhang Zhibo¹, Li Hongxin, AECC, China; ¹AECC Shenyang Engine Institute, China
10.1Flight Control
Chair(s): Bang, H.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
08. Sep 22 10:00 10:30 10.1.1 INCREMENTAL NONLINEAR DYNAMIC CONTROL WITH SPARSE NON-PARAMETRIC BAYESIAN REGRESSION OF DAMAGED AIRCRAFT
L Kim¹, D Lee¹, H Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea
08. Sep 22 10:30 11:00 10.1.2 FAULT-TOLERANT CONTROL FOR AIRCRAFT WITH STRUCTURAL DAMAGE USING GAUSSIAN PROCESS REGRESSION
D.-W. LEE¹, L.-S KIM¹, H.-J. AHN¹, H.-C. BANG¹; ¹KAIST, South Korea
08. Sep 22 11:00 11:30 10.1.3 EFFECTIVENESS ANALYSIS OF DOBC Q-FILTER PARAMETERS FOR A MULTICOPTER UAV
H.J. Jeaong¹, C.S. Roh¹, Y.H. Jang¹, J.Y Suk¹, S.K. Kim¹; ¹Department of Aerospace Engineering, Chungnam National Universit, South Korea
08. Sep 22 11:30 12:00 10.1.4 CONVEX PROGRAMMING-BASED OPTIMAL THREE-DIMENSIONAL MID-COURSE GUIDANCE WITH LOSSLESS CONVEXIFICATION
C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹KAIST, South Korea
11.1MBSE 2
Chair(s): Isaksson, O., Fredriksson, B.
27
02 - Systems Engineering and Integration
08. Sep 22 10:00 10:30 11.1.1 HETEROGENEOUS SYSTEMS MODELLING IN SUPPORT OF INCREMENTAL DEVELOPMENT
R. Hällqvist¹, J. Naeser¹, J. Wallén Axehill¹, E. Herzog¹; ¹Saab AB, Sweden
08. Sep 22 10:30 11:00 11.1.2 A MODEL BASED SYSTEMS ENGINEERING APPROACH TO STREAMLINED NOISE CERTIFICATION OF TRANSPORT-TYPE AIRCRAFT
D Kim¹, F Karagoz¹, S Datta¹, M Balchanos¹, D Anvid¹, E Harrison¹, D Mavris¹; ¹Georgia Institute of Technology, United States
08. Sep 22 11:00 11:30 11.1.3 A HOLISTIC AIRCRAFT CABIN METAMODEL AS AN APPROACH TOWARDS AN INTERCONNECTED DIGITISED CABIN LIFECYCLE
M. C. Berschik¹, M. Blecken¹, H. Kumawat¹, J.-E. Rath¹, D. Krause¹, R. God¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany
08. Sep 22 11:30 12:00 11.1.4 A COLLABORATIVE DESIGN METHOD FOR CIVIL AIRCRAFT BASED ON AN ENDURING AND EVOLUTIONARY AUTHORITATIVE SOURCE OF TRUTH
X Sun¹, M Luo¹, Z Cui¹, Z Ji¹, H Liu¹; ¹Beihang University, China
12.1Student Final
Chair(s): Rein Weston, K.
24 + 25
15 - Guest lectures
13.1Operation
Chair(s): ,
35 + 36
09 - Air Transport System Efficiency
08. Sep 22 10:00 10:30 13.1.1 DESIGN & VALIDATION OF A FLIGHT CENTRIC WORKLOAD MODEL INCLUDING ATC TASK CHANGE & CONSIDERING INFLUENCING FACTORS
T. Finck¹, M.-C. Névir, Technische Universität Dresden, Germany; C. Kluenker¹; ¹German Aerospace Center, Germany
08. Sep 22 10:30 11:00 13.1.2 REDUCED TRANSMISSION RISKS FOR PASSENGER OPERATIONS DURING COVID-19 PANDEMIC
Michael Schultz, Universität der Bundeswehr München, Germany; Majid Soolaki, University of Westminster, United Kingdom; Oliver Michler, Dresden University of Technology, Germany; Eri Itoh, University of Tokyo, Japan
08. Sep 22 11:00 11:30 13.1.3 VOICE PROJECT: REDUCED SEPARATIONS AND IMPROVED EFFICIENCY BASED ON VHF COMMUNICATIONS OVER LEO SATELLITES
E. Delgado Pinedo¹, R-F. Flores Acedo¹, S. Lora García¹, D. Polo Álvarez¹; ¹Indra Sistemas, S.A., Spain
08. Sep 22 11:30 12:00 13.1.4 V/A-R AIR GESTURES HMI INTERACTION IN AIRPORT CONTROL TOWERS
S. Bagassi¹, M. Corsi¹, F. Galuppi¹; ¹University of Bologna, Italy
14.1Sustainment Systems
Chair(s): Scott, M., Koschlik, A.K.
38
11 - Operations and Sustainment
08. Sep 22 10:00 10:30 14.1.1 MODEL-BASED SYSTEMS ENGINEERING FOR FUTURE DIGITAL FLIGHT LINES
M.A. Kelly, Lockheed Martin Aeronautics, United States
08. Sep 22 10:30 11:00 14.1.2 MACHINE LEARNING ENABLED MIXED REALITY SYSTEMS – FOR EVALUATION AND VALIDATION OF AUGMENTED EXPERIENCE IN AIRCRAFT MAINT
T. Gulrez¹, V. Kakoc¹, G. Emmanuel², M. Schumacher², T. Mills¹; ¹Defence Science and Technology Group, Australia ;²Airbus Australia Pacific, Australia
08. Sep 22 11:00 11:30 14.1.3 GRAPH-BASED KNOWLEDGE REPRESENTATION AND ALGORITHMS FOR AIR AND MAINTENANCE OPERATIONS
E. Olsson¹, O. Candell¹, P. Funk², R. Sohlberg², M. Castaño, Luleå University of Technology, Sweden; M. Gustafsson¹, P. Bladh¹; ¹Saab Aeronautics, Sweden ;²Mälardalen University, Sweden
08. Sep 22 11:30 12:00 14.1.4 AUGMENTED REALITY FOR AIRCRAFT FATIGUE NON-DESTRUCTIVE EVALUATION
Michael Scott¹, Stephan Koschel¹, Wim Verhagen¹, Oleg Levinski, Defence Science and Technology Group, Australia; Pier Marzocca¹; ¹RMIT University, Australia
08. Sep 22 12:00 12:30 14.1.5 ATTENTION GUIDANCE AI-SYSTEM FOR REMOTE TOWER OPERATIONS
G.L Söderholm, Linköpings University, Sweden
Reserve Paper 14.1.R REAL-TIME TRAJECTORY PLANNING SYSTEM USING HYBRID DATASET FOR ROBOTIC OPERATIONS
SY Yildirim, Cranfield University, United Kingdom
Reserve Paper (interactive) 14.1.R ECONOMIC PERFORMANCE EVALUATION OF AIRCRAFT MAINTENANCE USING DATA-DRIVEN APPROACH
X. Zhao, Nanjing University of Aeronautics and Astronautics, China

12:30 - 13:30Lunch Break

1.2Selected Highlights from Clean sky/Clean Aviation 2 (invited)
Chair(s): Krein, A.
A1
15 - Guest lectures
08. Sep 22 13:30 14:00 1.2.1 CA PROGRAMME RATIONALE AND OVERVIEW
R. van Manen, Netherlands
08. Sep 22 14:00 14:30 1.2.2 ULTRA-EFFICIENT AIRCRAFT AND PROPULSION ARCHITECTURES FOR LOW-EMISSION SHORT/MEDIUM RANGE [SMR] AIRCRAFT
M. Calvo Blanco, Spain
08. Sep 22 14:30 15:00 1.2.3 HYBRID-ELECTRIC AND FULL ELECTRIC ARCHITECTURES FOR LOW-EMISSION HYBRID-ELECTRIC REGIONAL [REG] AIRCRAFT
A. Marino, Italy
08. Sep 22 15:00 15:30 1.2.4 DISRUPTIVE TECHNOLOGIES TO ENABLE ZERO-CARBON HYDROGEN–POWERED [HPA] SHORT RANGE AIRCRAFT
P. Trinchieri, Italy
2.2Wing Design
Chair(s): Gibson, T.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
08. Sep 22 13:30 14:00 2.2.1 AERODYNAMIC CHARACTERISTICS OF BOX WINGS FOR AN INNOVATIVE EVTOL CONFIGURATION
Eiji SHIMA, Japan Aerospace Exploration Agency, Japan; Koichi YONEZAWA, Central Research Institute of Electric Power Industry, Japan; Ryoma NISHIDA¹, Shusuke HONDA ¹, Makoto SATO ¹; ¹Kogakuin University, Japan
08. Sep 22 14:00 14:30 2.2.2 IMPACT OF NO. OF WING STATIONS ON TWIST OF BWB CONCEPTUAL DESIGN IN A MDAO ENVIRONMENT TO MATCH TARGET LIFT DISTRIBUTION
B. Fröhler¹, M. Iwanizki¹, P. Balack¹, J. Häßy¹, D. Silberhorn1¹; ¹German Aerospace Center (DLR), Germany
08. Sep 22 14:30 15:00 2.2.3 CS2 – MANTA – MULTI-FUNCTIONAL FLAP MECHANISM OFFERING A SECOND DEGREE OF FREEDOM
M Desmet¹, J. Vervliet¹, D. De Wit¹, R. Seidler, Deutsches Zentrum Fuer Luft und Raumfahrt E.V., Germany; J. Docter, Netherlands Aerospace Centre, Netherlands; B. Everaert¹; ¹Asco Industries nv/sa, Belgium
08. Sep 22 15:00 15:30 2.2.4 INFLUENCES OF CHANGING THE INSTALLING POSITIONS OF MULTIPLE WINGLETS ON AERODYNAMIC CHARACTERISTICS
E Kobayashi¹, K Chiba¹; ¹The University of Electro-Communications, Japan
Reserve Paper 2.2.R DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING
N. Ma¹, F.-M. Meng¹, J.-H. Meng¹, L. Liu¹; ¹Beijing Institute of Technology, China
Reserve Paper 2.2.R AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION
Krittin Khankwa¹, Tharathep Phiboon¹, Atthaphon Ariyarit¹, Rattaporn Kasemsri¹, Masahiro Kanazaki, Tokyo Metropolitan University, Japan; ¹Suranaree University of Technology, Thailand
3.2Supersonic and Hypersonic Aircraft 2
Chair(s): Viola, N.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
08. Sep 22 13:30 14:00 3.2.1 COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION
R. Scigliano¹, V. De Simone¹, R. Fusaro², D. Ferretto², M. Marini¹, N. Viola²; ¹Italian Aerospace Research Center - CIRA scpa, Italy ;²Politecnico di Torino (PoliTo), Italy
08. Sep 22 14:00 14:30 3.2.2 HYPERSONIC AIRCRAFT AND MISSION CONCEPT RE-DESIGN TO MOVE FROM MACH 8 TO MACH 5 OPERATIONS
N. Viola¹, R. Fusaro¹, D. Ferretto¹, O. Gori¹, M. Marini², P. Roncioni², B. O. Cakir³, A. C. Ispir³, B. H. Saracoglu³; ¹Politecnico di Torino, Italy ;²CIRA, Italy ;³VKI, Belgium
Presenter: Oscar Gori, Politecnico di Torino
08. Sep 22 14:30 15:00 3.2.3 LTO NOISE AND SONIC BOOM PREDICTIONS IN EARLY CONCEPTUAL DESIGN PHASES
G. Piccirillo¹, S. Graziani¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy
08. Sep 22 15:00 15:30 3.2.4 SIMPLIFIED MODELS FOR THE PRELIMINARY AERODYNAMIC CHARACTERIZATION OF HIGH-SPEED VEHICLES TO SUPPORT MISSION ANALYSIS
O. Gori, Politecnico di Torino, Italy
Reserve Paper 3.2.R “CONCORDE-NEO”: A BIOFUEL PROPELLED SUPERSONIC COMMERCIAL AIRCRAFT WITH CONCORDE CONFIGURATION
F. Fornaseri¹, M. Borghi¹, G. Clinca¹, F. A. D'Amico¹, E. Versino¹; ¹Politecnico di Torino, Italy
4.2Transition and Flow Stability
Chair(s): Coder, J., Halila, G.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
08. Sep 22 13:30 14:00 4.2.1 ACCURATE TWO-DIMENSIONAL STEADY-STATES FOR THE SUPERSONIC FLOW OVER A COMPRESSION CORNER
R D Santos¹, L. S. de B. Alves¹, N Cerulus², H. R. Quintanilha Jr², V. Theofilis²; ¹UFF, Brazil ;²UoL, United Kingdom
08. Sep 22 14:00 14:30 4.2.2 NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION IN AN INTERCONNECTING COMPRESSOR DUCT
A Capitao Patrao¹, B González Lozano¹, I Jonsson¹, C Xisto¹; ¹Chalmers University of Technology, Sweden
08. Sep 22 14:30 15:00 4.2.3 ANALYSIS OF A LAMINAR SEPARATION BUBBLE ON A NACA0009 AIRFOIL AT DIFFERENT BACKGROUND NOISE LEVELS
J.S. Kern¹, A. Hanifi¹, D.S. Henningson¹; ¹FLOW, Department of Engineering Mechanics, KTH Royal Institute o, Sweden
08. Sep 22 15:00 15:30 4.2.4 A STUDY ON THE NUMERICAL SIMULATION OF FLOW TRANSITION INCLUDING CROSSFLOW EFFECTS
A. R. S. Righi, ITA, Brazil; G. L. O. Halila¹, J. L. F. Azevedo¹; ¹IAE, Brazil
Reserve Paper 4.2.R WAVE-PACKETS WITH STEADY TRIPLE-DECK SOLUTIONS
Diego Exposito¹, Sudhir L. Gai¹, Andrew J. Neely¹; ¹UNSW Canberra, Australia
5.2Aeroacoustics and Sonic Boom Predictions
Chair(s): Zhou, B., Viviani, A.
C 2
03.1 - Aerodynamics – CFD Methods and Validation
08. Sep 22 13:30 14:00 5.2.1 COMPUTATIONALLY ECONOMICAL METHODS FOR LANDING GEAR NOISE SIMULATIONS
R. A. Spencer, CFMS Ltd, United Kingdom; M. R. Allan, Zenotech Ltd, United Kingdom
08. Sep 22 14:00 14:30 5.2.2 PROPELLER AEROACOUSTIC MODELS IN VARIABLE-FIDELITY DESIGN OPTIMIZATION
W. A. Klimczyk¹, A. Sieradzki¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland
08. Sep 22 14:30 15:00 5.2.3 NUMERICAL PREDICTION OF FOCUS BOOM GENERATED BY MANEUVERS
S Han¹, Y Xu¹; ¹Chinese Aeronautical Establishment, China
08. Sep 22 15:00 15:30 5.2.4 INVERSE DESIGN METHOD OF LOW-BOOM SUPERSONIC AIRCRAFT FROM NEARFIELD SONIC BOOM
J.-L. Qiao, Northwestern Polytechnical University , China
Reserve Paper 5.2.R IN-FLIGHT MEASUREMENTS AND ESTIMATION OF SONIC BOOM SIGNATURE OF SUPERSONIC AIRCRAFT
Lixia Qu, China; Shuo Han, China; Yahui Song, China; Yue Xu, China; Yuelin Zhang, China; Yuhang Wang, China
6.2Wind Tunnel Testing Technology 2
Chair(s): ,
C 3
03.2 - Experimental Aerodynamics
08. Sep 22 13:30 14:00 6.2.1 WALL INTERFERENCE CORRECTIONS USING NONLINEARLEAST-SQUARES OPTIMISATION
Simon Noel¹, David Birch², John Doherty², Tanmay Tipnis¹; ¹QinetiQ, United Kingdom ;²University of Surrey, United Kingdom
08. Sep 22 14:00 14:30 6.2.2 A BLOWDOWN-INDUCTION FACILITY FOR HYPERSONIC FLOW SIMULATION DRIVEN BY A HIGH VELOCITY OXYGEN FUEL GUN
A. ESPOSITO , DEPT.OF INDUSTRIAL ENGINEERING UNIVERSITY OF NAPLES FEDERICO II, Italy; C. ALLOUIS , STEMS-CNR, Italy; M. LAPPA, Dept of Mech. and Aer.Engineering, University of Strathclyde, United Kingdom
08. Sep 22 14:30 15:00 6.2.3 RECENT ACTIVITIES ON FLOW QUALITY ASSESSMENT AT THE EUROPEAN TRANSONIC WINDTUNNEL
J. H. You¹, M. C.N. Wright¹, H. Quix¹; ¹European Transonic Windtunnel GmbH, Germany
08. Sep 22 15:00 15:30 6.2.4 INVESTIGATION ON CORRECTION OF TUNNEL WALL INTERFERENCE FOR DYNAMIC AIRFOIL TEST IN LOW-SPEED WIND TUNNEL
Yuqin Jiao, China
Presenter: Yuqin Jiao
Reserve Paper 6.2.R DEVELOPMENT AND VERIFICATION OF OSCILLATING BLADE GUST GENERATOR IN LOW-SPEED WIND TUNNEL
Chen BU¹, Zhanyuan MA¹, Ying ZHANG¹, Li LI¹; ¹AVIC Aerodynamics Research Institute, China
7.2Metallic Structures
Chair(s): ,
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
08. Sep 22 13:30 14:00 7.2.1 FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE
Sture Olsson¹, Björn Carlsson¹; ¹Quintus Technologies AB, Sweden
08. Sep 22 14:00 14:30 7.2.2 INFLUENCE OF KEYHOLE TIG WELDING PARAMETERS ON THE WELD GEOMETRY OF NEWLY-DEVELOPED SUPERALLOY VDM 780
Achmad Ariaseta, Sweden; Nima Sadeghinia, Sweden; Joel Andersson, Sweden
08. Sep 22 14:30 15:00 7.2.3 USE OF FRICTION STIR WELDING ON PRIMARY STRUCTURES OF AIRCRAFTS INSTEAD OF RIVETED JUNCTION
D. Desgaches, Stelia Aerospace, France
08. Sep 22 15:00 15:30 7.2.4 EXPERIMENTAL INVESTIGATIONS ON TENSILE PROPERTIES OF ALUMINUM HONEYCOMB SANDWICH STRUCTURE WITH SINGLE-SIDED REPAIRING
Yan Bing¹, Zhang Guijia¹, Tong Mingbo ¹, Li Lei¹, Yu Dingchang¹, Zhu Shuhua¹, Wu Zhangyu², Wang Hao², Jin Tao, China Special Vehicle Research Institute, China; ¹Nanjing University of Aeronautics & Astronautics, China ;²Nanjing University of Aeronautics and Astronautics, China
Presenter: Bing Yan
Reserve Paper 7.2.R ELECTROMAGNETIC INTERFERENCE SHIELDING EFFECTIVENESS OF THE THIN CNF/SICF COMPOSITE
Xiaojing JIA¹, Huan DU¹, Liguo ZHANG¹, Zhenquan ZHONG¹, Xinquan ZHANG¹; ¹AVIC The first Aircraft Institute, China
Reserve Paper 7.2.R RESEARCH ON THE DUCTILE FRACTURE OF AL7085 AND TC11 UNDER COMPLEX STRESS STATE
Y.J. LIU, AVIC the First Aircraft Institute, China
Reserve Paper (interactive) 7.2.R HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS
Muhammad Atif¹, Muhammad Aamir Raza¹, Xianzhe Shi¹, Muhammad Zakir Sheikh¹, Jianghua Shen, Joint International Research Center of Impact Dynamics and Its E, China; Yulong Li, School of Civil Aviation, Northwestern Polytechnical University, China; ¹Northwestern Polytechnical University, China
8.2Vibration and Damping 2
Chair(s): ,
Balcony
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
08. Sep 22 13:30 14:00 8.2.1 NUMERICAL NONLINEAR VIBRATION-BUCKLING INVESTIGATION OF STRUCTURES SUBJECTED TO MECHANICAL AND THERMAL LOADINGS
R. Azzara¹, M. Filippi¹, A. Pagani¹, E. Carrera¹; ¹Politecnico di Torino, Italy
08. Sep 22 14:00 14:30 8.2.2 GROUND VIBRATION TESTING OF A HIGH ASPECT RATIO WING WITH REVOLVING CLAMP
G. Dessena¹, D.I. Ignatyev¹, J.F. Whidborne¹, A. Pontillo, University of Bristol, United Kingdom; L. Zanotti Fragonara¹; ¹Cranfield University, United Kingdom
08. Sep 22 14:30 15:00 8.2.3 UPDATING OF JET TRAINER AIRCRAFT DYNAMIC MODEL TO RESULTS OF GROUND VIBRATION TEST
J. Cecrdle, Czech Aerospace Research Centre (VZLU), Czech Republic
08. Sep 22 15:00 15:30 8.2.4 DYNAMIC STRSS SIMULATION AND ASYMMETRY STATOR DESIGN FOR A FAN BLISK
Yixiong Liu¹, Kening Xu, Aero Engine Academy of China, China; Yuzhi Chen¹, Yunwu Wu¹, Qing Du¹, Da Mo¹; ¹AECC Shenyang Engine Research Institute, China
Reserve Paper 8.2.R DECORATION OF CARBON NANOTUBE - GRAPHENE 3D NANOSTRUCTURES AND THEIR ENHANCEMENTS IN POLYMER MATRIX
C Chenxi, Civil Aviation University of China, China
9.2Propulsion System & Aircraft Performance 2
Chair(s): Mari, C.
C 4
05 - Propulsion
08. Sep 22 13:30 14:00 9.2.1 TECHNOLOGY MATURATION FOR NEXT GENERATION SMR ENGINE
C. DIETTE, Safran Aircraft Engines, France; E. OBERT, Safran, France; G. MARION, Safran Transmission Systems, France; H. DE FRANSSU, Safran Nacelles, France; A. FREZET, Avio Aero, Italy; B. WALTHER, GE Deutschland, Germany; A. SJUNNESSON, GKN Aeropsace Engie Systems, Sweden
Presenter: Christophe DIETTE, Safran Aircraft Engines
08. Sep 22 14:00 14:30 9.2.2 NOVEL AIRCRAFT PROPULSION AND AVAILABILITY OF ALTERNATIVE, SUSTAINABLE AVIATION FUELS IN 2050
J. Kos¹, J.A. Posada-Duque², B. Peerlings¹, N. Ben Salah², M.N.A. Lim¹, W.F. Lammen¹, I. Stepchuk, TU Delft, Faculty of Technology and Policy Management, Netherlands; E.S. Sman¹, M.P.M. Palmeros-Parada²; ¹Royal Netherlands Aerospace Centre, Netherlands ;²TU Delft, Faculty of Applied Sciences, Netherlands
08. Sep 22 14:30 15:00 9.2.3 MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM
Tomas Grönstedt¹, Carlos Xisto¹, Xn Zhao¹, Isak Jonsson¹, Magnus Genrup², Avo Reinap², Nenad Glodic³, Mauricio Guiterrez Salas³, Marcus Lejon*, Richard Avellan*, Mårtensson Hans*; ¹Chalmers University, Sweden ;²Lund University, Sweden ;³Royal Institute of Technology, Sweden ;*GKN Aerospace, Sweden
08. Sep 22 15:00 15:30 9.2.4 LOW BPR TURBOFAN PERFORMANCE WITH POWER EXTRACTION
D. H. Rosell, Saab Aeronautics, Sweden; U. T. Grönstedt, Chalmers Univerity of Technology, Sweden; P. D. Bravo-Mosquera¹, F. Martini Catalano¹; ¹University of Sao Paulo, Brazil
Reserve Paper 9.2.R ANALYSIS OF THE OPERATION OF THE PULSEJET ENGINE
Jon Tegner, FOI, Sweden
Reserve Paper (interactive) 9.2.R ANALYSIS AND SIZING OF A GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT
M. Bruno¹, R. Cambertoni¹, A. Pellegrino¹, P. Petrachi¹, C. Spampinato¹; ¹Polytechnic of Turin, Italy
Presenter: Cristina Spampinato, Polytechnic of Turin
Reserve Paper (interactive) 9.2.R TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS
B.-O. Schröder¹, P. González¹, F. Silvestre¹; ¹TU Berlin, Germany
Presenter: Pedro González, TU Berlin
Reserve Paper (interactive) 9.2.R COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTION
F. Petrosino¹, M. Barbarino¹; ¹CIRA, Italy
10.2Flight Modelling
Chair(s): Rogalski, T., Ochi, Y.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
08. Sep 22 13:30 14:00 10.2.1 ON LATERAL-LONGITUDINAL CONTROL COUPLING FOR SHORT- AND LONG-FUSELAGE BWB AIRCRAFT CONFIGURATIONS
L.M.B.C. Campos, Instituto Superior Técnico, Universidade de Lisboa, Portugal
08. Sep 22 14:00 14:30 10.2.2 OPEN-LOOP SUBSPACE IDENTIFICATION OF A FLEXIBLE UNMANNED AERIAL SYSTEM
R C M Carvalho Machado, ITA, Brazil
08. Sep 22 14:30 15:00 10.2.3 LATERAL-DIRECTIONAL FORCE AND MOMENTS MODELING OF NUMERICAL RESULTS USING NEURO-FUZZY HYBRIDZED WITH DIFFERENTIAL EVOLUT
V.T. Santana¹, I. Staack, Linköping University, Sweden; R. M. Finzi¹; ¹Federal University of Uberlândia, Brazil
11.2Systems Architecting
Chair(s): Petersson, A., Holmberg, G.
27
02 - Systems Engineering and Integration
08. Sep 22 13:30 14:00 11.2.1 TOWARDS CORRECT-BY-CONSTRUCTION DESIGN OF SAFETY-CRITICAL EMBEDDED AVIONICS SYSTEMS
I. Sander¹, I. Söderquist², M. Ekman², R. Jordao¹, F. Bahrami¹, R. Chen¹, A. Åhlander²; ¹KTH Royal Institute of Technology, Sweden ;²Saab AB, Sweden
08. Sep 22 14:00 14:30 11.2.2 CONCEPT LEVEL EXPLORATION OF IMA-BASED NETWORKED PLATFORMS WITH MIXED TIME-SENSITIVE COMMUNICATION REQUIREMENTS
R. Saar de Moraes¹, S. Nadjm-Tehrani¹; ¹Linköping University, Sweden
08. Sep 22 14:30 15:00 11.2.3 SYSTEMS ARCHITECTING ASSISTANT (SARA) - ENABLING A SEAMLESS PROCESS CHAIN FROM REQUIREMENTS TO OVERALL SYSTEMS DESIGN
N. Kuelper¹, J. Broehan¹, T. Bielsky¹, F. Thieleke¹; ¹Hamburg University of Technology, Germany
12.2Icing
Chair(s): ,
24 + 25
07 - Systems, Subsystems and Equipment
08. Sep 22 13:30 14:00 12.2.1 EXPERIMENTAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR
A. Hatamoto, Japan; K. Emori, Japan; H. Nishida, Japan
08. Sep 22 14:00 14:30 12.2.2 THE SENS4ICE EU PROJECT – SAFER AVIATION IN ICING ENVIRONMENT – PROJECT OVERVIEW AND INITIAL RESULTS
C. W. Schwarz, DLR, Germany
08. Sep 22 14:30 15:00 12.2.3 STRESS AND ENERGY RELEASE RATE INFLUENCE ON ICE SHEDDING WITH RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS
G Gastaldo¹, V Palanque, ISAE-Supaero and ONERA, France; M Budinger, INSA/ICA, France; V Budinger¹; ¹ISAE-Supaero, France
08. Sep 22 15:00 15:30 12.2.4 NUMERICAL SIMULATION OF ICE ACCRETION ON PITOT TUBE
Krzysztof Szilder¹, Peter Forsyth¹; ¹National Research Council, Canada
Reserve Paper 12.2.R EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF CFRP COMPOSITE ON ELECTROTHERMAL ANTI-ICING SYSTEM
Xiaofeng Guo¹, Qian Yang¹, Haoran Zheng¹, Wei Dong¹; ¹Shanghai Jiaotong University, China
13.2UTM / UAM
Chair(s): ,
35 + 36
09 - Air Transport System Efficiency
08. Sep 22 13:30 14:00 13.2.1 NEW ENTRANTS’ AIRSPACE INTEGRATION IN JAPAN: JAXA’S ONGOING CONTRIBUTION
Naoki Matayoshi, Japan Aerospace Exploration Agency, Japan
08. Sep 22 14:00 14:30 13.2.2 ON KEY PARAMETERS FOR THE ATTRACTIVENESS OF ON-DEMAND INTER-CITY AIR MOBILITY
T. Ehlers¹, S. Hagemann², V. Gollnick², K. Lütjens¹; ¹German Aerospace Center, Germany ;²Hamburg University of Technology, Germany
08. Sep 22 14:30 15:00 13.2.3 THE AUTOMATION EVOLVES: CONCEPT FOR A HIGHLY AUTOMATED CONTROLLER WORKING POSITION
I Gerdes¹, M Jameel¹, R Hunger¹, L Christoffels¹, H Gürlük¹; ¹German Aerospace Center DLR, Germany
08. Sep 22 15:00 15:30 13.2.4 AN OPERATIONAL CONCEPT FOR THE INTEGRATION OF URBAN AIR MOBILITY VEHICLES INTO THE AIR TRAFFIC CONTROL PROCESSES
Isabel C. Metz¹, Sebastian Schier-Morgenthal¹; ¹German Aerospace Center DLR, Germany
14.2UAV Design
Chair(s): ,
38
06.2 - Flight Dynamics and Control (UAV related)
08. Sep 22 13:30 14:00 14.2.1 DEVELOPMENT OF MULTI-CANARD UAV FOR ACTIVE AEROELASTIC CONTROL TOWARD PSEUDO-SMALL SATELLITES
N Morita¹, N Nakasuka¹, T Tsuchiya¹, K Takashima¹, Y Taguchi¹, K Suzuki¹, T Koyama¹, R Eto¹, I Baba¹; ¹the University of Tokyo, Japan
08. Sep 22 14:00 14:30 14.2.2 OVERALL LAYOUT DESIGN OF NEW TYPE TILTROTOR VEHICLES
H Kitaba¹, M Bando¹, S Hokamoto¹; ¹Kyushu Univ., Japan
Presenter: Shinji Hokamoto, Kyushu University
08. Sep 22 14:30 15:00 14.2.3 INFLUENCE OF OVERALL LAYOUT DESIGN OF COMPOUND MULTI-ROTOR VEHICLES ON FLIGHT PERFORMANCE
Y HUANG¹, M BANDO¹, S HOKAMOTO¹; ¹Kyushu University, Japan
08. Sep 22 15:00 15:30 14.2.4 USE OF MULTIPLE LOW COST AUTONOMOUS DRONES FOR HIGH VOLTAGE LINE INSPECTION
L D Jesus¹, A J D Filho¹, M. A. Almeida¹, W. M. Martins¹, T. C. Pimenta¹, A. C. B. Ramos¹, P. Funk, Mälardalen University, Sweden; ¹Federal University of Itajubá, Brazil

15:30 - 16:00Break

0.216:00-17:00 ICAS von Karman Lecture: “Clean Sky Programme Achievements and Clean Aviation Outlook” S.Klauke CTO Airbus , E. Dalbies CTO SAFRAN, M. Protti Head of Advanced Research Leonardo Aircraft
Chair: A. Krein Head of Clean Sky GER, J.L. Azevedo, ICAS President Brazil
08. Sep 22 16:00 17:00

17:00 - 17:30Closing Ceremony