35th 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, 14. Sep 2026

07:00 - 08:00Registration

0.1OPENING CEREMONY
Chair: C. Atkin ICAS President
14. Sep 26 08:00 08:30

0.2ICAS Daniel & Florence Guggenheim Memorial Lecture Adnan Raghdo –The Boeing’s MQ-28 Ghost Bat to Australian Aerospace Industry & MQ-28 Development
Chair: F. Haselbach ICAS EC Member
14. Sep 26 08:30 09:30

09:30 - 09:55COFFEE BREAK

1.1GSA2: Global Sustainable Aviation – Setting the Stage with Global Airlines
Chair(s): Wahls, R., Krein, A.
Track 1 Pyrmont Theatre
15 - Guest lectures
14. Sep 26 09:55 10:20 1.1.1
1020		 SETTING THE STAGE FOR THE GLOBAL SUSTAINABLE AVIATION TRACK WITH GLOBAL AIRLINES
A Krein, Clean Aviation, Germany
14. Sep 26 10:20 10:45 1.1.2
0986		 JAL’ CHALLENGE TO THE NET-ZERO GH GAS EMISSION
MS Suzuki, JAL, Japan
14. Sep 26 10:45 11:10 1.1.3
1019		 THE WHOLE JOURNEY: PEOPLE, PLANET AND PROGRESS AT QANTAS
Hudson, Qantas Group, Australia
14. Sep 26 11:10 11:35 1.1.4
1028		 PANEL DISCUSSION Q&A WITH THE AIRLINES
P Panel,
2.1Progress in Certification by Analysis
Chair(s): Slotnick, J., Aponso, B.L.
Track 2 C4.1
15 - Guest lectures
14. Sep 26 09:55 10:20 2.1.1
1051		 TOWARDS CERTIFICATION BY ANALYSIS: A MILITARY AIRWORTHINESS PERSPECTIVE
S. Geisbauer, DLR, Germany; S. Shaw, MBDA, United Kingdom
Presenter: Andreas Goerttler, DLR,
14. Sep 26 10:20 10:45 2.1.2
1052		 EXPLORING AIRWORTHINESS CBA: A STALL SPEED CASE STUDY BASED ON AERO-STRUCTURAL COUPLED ANALYSIS
M. Amano, Japan
14. Sep 26 10:45 11:10 2.1.3
1053		 PROGRESS TOWARDS AIRCRAFT CERTIFICATION BY ANALYSIS WITHIN THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTIC
J. Schaefer, United States
14. Sep 26 11:10 11:35 2.1.4
1054		 AN EFFORT TOWARD PROCESS DEVELOPMENT OF CBA FOR FLIGHT CHARACTERISTICS
T. Ishida, Japan
3.1Cabin
Chair(s): Hesse, C.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
14. Sep 26 09:55 10:20 3.1.1
0899		 AURAL DIGITAL TWIN FOR AIRCRAFT CABIN DESIGN
M.C. Moruzzi¹, T. Fadda¹, E. Caligari¹, S. Bagassi¹; ¹Università di Bologna, Italy
14. Sep 26 10:20 10:45 3.1.2
0214		 AUTOMATED KNOWLEDGE-BASED CABIN DESIGN AND EVALUATION WITHIN A PRELIMINARY AIRCRAFT DESIGN LOOP
S. Hellbrück¹, P. Zemke¹, C. Hesse¹, M. Fuchs¹, J. Biedermann¹, B. Nagel¹; ¹DLR e.V., Germany
14. Sep 26 10:45 11:10 3.1.3
0406		 ASSESSING THE POTENTIAL OF MULTI-MODEL TOPOLOGY OPTIMIZATION FOR MODULAR LIGHTWEIGHT DESIGN OF AIRCRAFT CABIN STRUCTURES
P. Inselmann¹, F.D. Bischop¹, F.H. Christiansen¹, M. Höhner¹, T. Schüppstuhl¹, D. Krause¹; ¹Hamburg University of Technology, Germany
14. Sep 26 11:10 11:35 3.1.4
0348		 A FRAMEWORK FOR AUTOMATED SYSTEM COMPONENT PLACEMENT IN AIRCRAFT CONCEPTUAL DESIGN
J. Vézina¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada
Reserve Paper 3.1.R
0604		 MULTI-STATE FLIGHT DECK DISPLAY LAYOUT OPTIMIZATION UNDER FAILURE AND REVERSION CONDITIONS
Y. Yamai¹, M. Itoh¹, M.-P. Pacaux-Lemoine, Université Polytechnique Hauts-de-France, France; ¹University of Tsukuba, Japan
4.1Application of Aerodynamics in Design
Chair(s): Schmollgruber, P.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 09:55 10:20 4.1.1
0187		 A LAMINAR TAILORED WING WITH CATNLF AND HLFC FOR EXTRA LONG RANGE
J. Ruberte Bailo¹, T. Streit¹, A. Seitz¹; ¹DLR, Germany
14. Sep 26 10:20 10:45 4.1.2
0817		 EVALUATION OF PERCEIVED X-15 FLYING QUALITIES BASED ON RAPID AERODYNAMIC PREDICTIONS
H.B. Rogers¹, T.T. Takahashi¹, J.A. Camberos¹, R.V. Grandhi¹; ¹AFIT, United States
14. Sep 26 10:45 11:10 4.1.3
0371		 MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE
E. Riccio¹, R. Bombardieri¹, A. Ceresa¹, V.R. Baraniello¹, F. Tufano¹, G. Persechino¹, D. Coiro, University Federico II of Naples, Italy; ¹Italian Aerospace Research Centre, Italy
14. Sep 26 11:10 11:35 4.1.4
0482		 RESEARCH ON OVERALL AERODYNAMIC DESIGN OF GRID-DUCT INTEGRATED VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING AIRCRAFT
B. Li¹, B. Mi¹; ¹Northwestern Polytechnical University, China
5.1Scale Resolving Simulations
Chair(s): Coder, J., Zingg, D.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 09:55 10:20 5.1.1
0368		 LAMINAR SEPARATION ON AN AIRFOIL WITH PERTURBATION OF OUTER AND INNER BOUNDARY CONDITIONS
E. Tangermann¹, A. Jagadeesha¹, M. Klein¹; ¹Universität der Bundeswehr München, Germany
14. Sep 26 10:20 10:45 5.1.2
0267		 LARGE EDDY SIMULATIONS OF LOW-REYNOLDS NUMBER FLOWS IN THE COMPRESSIBLE REGIME
P. Catalano¹, F.A. D'Aniello¹; ¹C.I.R.A., Italy
14. Sep 26 10:45 11:10 5.1.3
0168		 REYNOLDS NUMBER EFFECTS OF A BIRD-FEATHER-INSPIRED POROUS-MEDIUM AIRFOIL
Z.P. Zhang¹, Z.Y. Ye¹; ¹Northwestern Polytechnical University, China
14. Sep 26 11:10 11:35 5.1.4
0480		 NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION
H. Wang¹, T. Lin¹, G. Wang¹, L. Xu¹; ¹Northwestern Polytechnical University, China
Presenter: Huiyue Wang, Northwestern Polytechnical University
additional information (interactive) 5.1.R
0939		 ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS
T.A. Missato¹, R.G. Annes da Silva¹, A.F. de Castro da Silva¹, T. Wainwright, Zenotech, United Kingdom; ¹Instituto Tecnológico de Aeronáutica, Brazil
6.1Aerodynamic Response and Wake Characteristics
Chair(s): Vijgen, P.
Track 6 C4.5
03.3 - Basic Fluid Dynamics and Flow Control
14. Sep 26 09:55 10:20 6.1.1
0194		 RESPONSE CHARACTERISTICS OF WINGTIP VORTEX INSTABILITY TO EXTERNAL DISTURBANCES
Y. Wu¹, Z. Xiao¹, Y. Xiang¹, Z.Y. Zhu¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 10:20 10:45 6.1.2
0228		 NON-LINEAR PARAMETRIC MODEL FOR THE 3DOF MOTION OF A BOX IN WAVES USING SPARSE REGRESSION
Z. Hoffman¹, S. Vahaji¹, A. Das¹, M. Candon¹, N. Jayarathne, Navantia Australia, Australia; P. Marzocca¹; ¹RMIT, Australia
14. Sep 26 10:45 11:10 6.1.3
0637		 THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW
J. Mourad¹, V. Ferrand¹, E. Gowree¹; ¹ISAE-Supaero, France
14. Sep 26 11:10 11:35 6.1.4
0655		 INTERACTION OF COUNTER-PLUNGING BIPLANE AIRFOILS WITH A FLAT PLATE BOUNDARY LAYER AND WAKE
B. Anilir¹, D.F. Kurtulus¹, M.F. Platzer, University of California, Davis, United States; ¹Middle East Technical University, Turkey
7.1Distributed Propulsion and Aerodynamic Interaction
Chair(s): Lacy, D.
Track 7 C4.6
03.4 - Applied Aerodynamics
14. Sep 26 09:55 10:20 7.1.1
0108		 INVESTIGATION OF DISTRIBUTED PROPELLER PROPULSIVE CHARACTERISTICS UNDER NON-AXIAL INFLOW
B.-M. Xu¹, K.-L. Wang¹, Z. Zhou¹, S.-K. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Presenter: Shao-Kun LI
14. Sep 26 10:20 10:45 7.1.2
0200		 EFFECT OF LIP/NOZZLE DEFLECTION ANGLE ON THE AERODYNAMIC AND PROPULSIVE CHARACTERISTICS OF PROPULSIVE WING UNIT
M. Li¹, Z. Zhou¹, K. Wang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 10:45 11:10 7.1.3
0444		 PROPELLER AERODYNAMICS UNDER NON-UNIFORM INFLOWS
S. Montagner¹, J. Serpieri¹, G. Cafiero¹; ¹Politecnico di Torino, Italy
Presenter: Sara Montagner, Politecnico di Torino
14. Sep 26 11:10 11:35 7.1.4
0516		 EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT ENHANCEMENT OF A HIGH-LIFT CONFIGURATION
H.-X. He¹, W.-P. Song¹, Y. Wang¹, Y.-H. Wang¹, Y.-J. Shi, China Ship Scientific Research Center, China; ¹Northwestern Polytechnical University, China
8.1Advanced Aerostructures
Chair(s): Bayandor, J.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 09:55 10:20 8.1.1
0181		 INTERNATIONAL AND EUROPEAN RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION
R. Degenhardt, DLR, Italy; F. Ferrigno, CIRA, Italy; A. Gliszczynski, Lodz University of Technology, Poland; A.-L. Delot, ONERA, France
Presenter: Adrian Gliszczynski, Lodz University of Technology
14. Sep 26 10:20 10:45 8.1.2
0493		 MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK
Z. Li¹, D. Wei¹, W. Zeng, Chinese Academy of Sciences, China; K.K. Alynur¹, X. Liu¹, B. Zhao¹, S. Li¹, L. Ma, KUCH ENERGY Technology Co., Ltd., China; S. Yang¹; ¹Beihang University, China
14. Sep 26 10:45 11:10 8.1.3
0940		 A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED REPAIR OF ALUMINUM PARTS
J. Lua¹, M.R. Rajanna¹, H. Yu, Virginia Tech, United States; A. Timmons², G. Murray², N. Phan²; ¹Global Engineering and Materials, Inc., United States ;²Naval Air Systems Command, United States
14. Sep 26 11:10 11:35 8.1.4
0083		 MULTIPHYSICS COUPLING EFFECT ON INTERFACIAL PROPERTIES OF CNT/GFRP/CFRP COMPOSITES FOR ELECTROTHERMAL ANTI-/DE-ICING APPLICATIONS
X. Yao¹, Y. Wang¹, H. Wang¹, Y. Wang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 8.1.R
0172		 FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING
X. Liu¹, D.S. Wei¹, S.Z. Jin, AVIC Manufacturing Technology Institute, China; S. Yang¹, D.X. Yin², B. Niakate², D. Lasne²; ¹Beihang university, China ;²BSS Turbotech Ltd., China
9.1System of Systems 1
Chair(s): Amadori, K., Prakasha, P.
Track 9 C4.8
02 - Systems Engineering and Integration
14. Sep 26 09:55 10:20 9.1.1
0046		 ONTOLOGY-BASED EXPLORATION OF SYSTEM-OF-SYSTEMS ARCHITECTURES USING A FEDERATED STRUCTURE
L. Knöös Franzén, Linköping University, Sweden; C. Jouannet, Saab Aeronautics, Sweden
14. Sep 26 10:20 10:45 9.1.2
0076		 DIGITAL TWIN FOR AIR DEFENSE: LIVE-VIRTUAL-CONSTRUCTIVE INTEGRATION AND DECISION SUPPORT
S. Malka¹, M. Ben Simon¹, O. Yakimenko¹; ¹Naval Postgraduate Shcool, United States
14. Sep 26 10:45 11:10 9.1.3
0671		 COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER
P.F. Li¹, W.Z. Liu¹, B.L. Shang¹, Y.Z. Wang¹, R.X. Lin¹; ¹Northwestern Polytechnical University, China
14. Sep 26 11:10 11:35 9.1.4
0675		 INTERFACING MISSION SIMULATION WITH INTELLIGENT AGENTIC SYSTEMS FOR OPERATIONAL AND ETHICAL EVALUATION
H. Budig¹, E. Zegarra Berodt¹, N.G. Wood¹, V. Gollnick¹; ¹Hamburg University of Technology, Germany
10.1AI Applications in Flight Control, Simulation and Modeling
Chair(s): Kiszkowiak, L.
Track 10 C4.9
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 09:55 10:20 10.1.1
0872		 NEURAL NETWORK BASED SLIDING MODE CONTROL FOR HYPERSONIC LONGITUDINAL CONTROL
H.J. Kim¹, J.H. Shin¹; ¹Chungbuk national University, South Korea
14. Sep 26 10:20 10:45 10.1.2
0648		 SUPPORTING PILOT SITUATIONAL AWARENESS BY EXTRACTING INSIGHTS FROM AN AI EXPERT
C. Koopman¹, D. Zammit Mangion¹; ¹University of Malta, Malta
14. Sep 26 10:45 11:10 10.1.3
1033		 MULTI-SENSOR BASED ADAPTIVE FUSION SCHEME FOR POSITION ESTIMATION OF MULTIROTOR UAV SYSTEMS IN GPS-DENIED ENVIRONMENTS
L. Busse¹, M. Kumar¹; ¹University of Cincinnati, United States
11.1Flight Control 1
Chair(s): Shaferman, V., Rogalski, T.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 09:55 10:20 11.1.1
0011		 ADAPTIVE FLIGHT CONTROL LAWS APPLIED TO AIR REFUELING WITH RECEIVERS EQUIPPED WITH RECEPTACLE OUT OF THE PLANE OF SYMMETRY
V. Martinez Jimenez¹, F. Asensio Nieto¹, I. Romo Martinez¹, A. Sanz De Blas¹, D. Lodares Gomez¹; ¹AIRBUS, Spain
14. Sep 26 10:20 10:45 11.1.2
0647		 BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL
Y.L. Niu¹, L.X. Wang¹, J.X. Li², Y.N. Gao², S.H. Xu, COMAC Beijing Aircraft Technology Research Institute, China; T. Yue¹, S. Tai¹, H.L. Liu¹; ¹Beihang University, China ;²The First Aircraft Institute AVIC, China
14. Sep 26 10:45 11:10 11.1.3
0843		 AIRBRAKES CONTROL SYSTEM FOR PRECISE APOGEE CONTROL OF A SOUNDING ROCKET
N. Gee-Landman¹, J.L. Palmer¹; ¹RMIT University, Australia
14. Sep 26 11:10 11:35 11.1.4
0425		 FIXED-WING AIRCRAFT PORT-HAMILTONIAN DYNAMICS AND CONTROL
J.E.M. Fernandes¹, F.L. Cardoso-Ribeiro¹, M.A.V. Morales¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
12.1UAV Component
Chair(s): Alexander, M.
Track 12 C2.3
07 - Systems, Subsystems and Equipment
14. Sep 26 09:55 10:20 12.1.1
0335		 IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL
G. Schmitz¹, I. Pruter¹, H. Duda¹, M. Laubner¹, S. Lorenz¹; ¹DLR e.V., Germany
14. Sep 26 10:20 10:45 12.1.2
0684		 RECONFIGURABLE MULTILEVEL BATTERY ARCHITECTURE FOR SMALL UAV PROPULSION SYSTEMS
N. Sorokina¹, W. Bliemetsrieder¹, P. Panchal¹, L. Hein¹, T. Weyh¹; ¹Universität der Bundeswehr München, Germany
14. Sep 26 10:45 11:10 12.1.3
0833		 STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS
A.A.J. Oliveira¹, L.H.J. Machado¹, M.S. Ferreira¹, J.P.B. Souza¹, E.J.T. Santos¹, J.V.N. Oliveira¹, P.H.C. Picanço¹; ¹Universidade Federal de Minas Gerais, Brazil
14. Sep 26 11:10 11:35 12.1.4
0590		 A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING
J.B. Cheng¹, J. Li, AVIC Chengdu Aircraft Design and Research Institute, China; B.X. Wang¹, C. Chen, Information Center of the National Administration of Defense Sci, China; P. He, AVIC Luoyang Institute of Electro-Optical Equipment, China; K. Zhang¹; ¹Northwestern Polytechnical University, China
13.1Safety and Efficiency in Aviation
Chair(s): Maroney, D.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
14. Sep 26 09:55 10:20 13.1.1
0247		 DESIGN AND FEASIBILITY ASSESSMENT OF TRANSPORT OPERATIONS FOR DELIVERING TYPHOON CONTROL SUBSTANCES
H. Akiyama¹, S. Ueno¹, T. Higuchi¹, T. Sakurai¹; ¹Yokohama National University, Japan
14. Sep 26 10:20 10:45 13.1.2
0332		 A PEAKS-OVER-THRESHOLD APPROACH TO RUNWAY COLLISION RISK ESTIMATION FOR EFFICIENT ARRIVAL OPERATIONS
N.K. Wickramasinghe, Electronic Navigation Research Institute, Japan; R. Mori, Kobe University, Japan
14. Sep 26 10:45 11:10 13.1.3
0216		 NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT
R. Sáez¹, R. Pitarque¹, B. Heesbeen, Royal Netherlands Aerospace Centre (NLR), Netherlands; Y.J. Hasan², J. Kurz², D. Vechtel², M. Gerber, Swiss Skylab Foundation (Skylab), Switzerland; ¹Technical University of Catalonia (UPC), Spain ;²German Aerospace Centre (DLR), Germany
14. Sep 26 11:10 11:35 13.1.4
0302		 EVALUATING HUMAN-MACHINE-TEAMING CONCEPTS FOR A HIGHLY AUTOMATED GROUND CONTROLLER WORKING POSITION
L. Nöhren¹, A. Simon¹, M. Schaper¹; ¹DLR, Germany
14.1Vision & Control
Chair(s): , , Grabowski, T.
Track 14 C2.5
06.2 - Flight Dynamics and Control (UAV related)
14. Sep 26 09:55 10:20 14.1.1
0143		 MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS
R. Perz, WUT, Institute of Aeronautics and Applied Mechanics, Poland; P. Wozniak¹, R. Chalupczynski¹, K. Barys², J. Konowalski², A. Abratanski², J. Swierk¹, I. Dabrowski²; ¹Uavionics Ltd Poland, Poland ;²Rafal Perz Scientific Network, Poland
14. Sep 26 10:20 10:45 14.1.2
0163		 ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW
M. Yanagisawa¹, R. Okabayashi¹, T. Yamaguchi², M. Takamoto², M. Bando¹, S. Hokamoto¹; ¹Kyushu University, Japan ;²Mitsubishi Electric Corporation, Japan
14. Sep 26 10:45 11:10 14.1.3
0737		 FLIGHT TEST VALIDATION OF A VISION-GUIDED MULTIROTOR TERMINAL INTERCEPTION SYSTEM
Y.R. Kim¹, J.H. Hong¹, Y.J. Jang¹, J.H. Moon¹; ¹Cheongju University, South Korea
14. Sep 26 11:10 11:35 14.1.4
0096		 A SYSTEMATIC, TUNING-FREE ATTITUDE CONTROL METHOD FOR VTOL UAVS
K. Okamoto¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan
Presenter: Kazuki Okamoto, The University of Tokyo
Reserve Paper 14.1.R
0288		 DEEP LEARNING VS. TRADITIONAL COMPUTER VISION FOR UAV LANDING SITE DETECTION IN ADVERSE WEATHER
R. Schmidt¹, J. Rüter¹; ¹German Aerospace Center (DLR), Germany
additional information (interactive) 14.1.R
0649		 AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION FOR JUNGLE RECONNAISSANCE UAVS
S.K. Li¹, N.H. Zhu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China
15.1AI Safety, Verification, and Trust
Chair(s): Würfel, J.
Track 15 C2.6
10 - Safety and Security
14. Sep 26 09:55 10:20 15.1.1
0210		 ON THE APPLICABILITY OF SAFETY NETS: A SAFETY-BY-DESIGN SOLUTION FOR CERTIFYING NEURAL NETWORKS
J.M. Christensen¹, T. Stefani¹, E. Hoemann¹, F. Köster¹, S. Hallerbach¹; ¹German Aerospace Center, Germany
14. Sep 26 10:20 10:45 15.1.2
0536		 COVERAGE-DRIVEN VERIFICATION FOR SAFETY-BY-DESIGN IN AI-BASED COLLISION AVOIDANCE SYSTEMS
T. Stefani¹, J.M. Christensen¹, E. Hoemann¹, F. Koester¹, S. Hallerbach¹; ¹DLR, Germany
14. Sep 26 10:45 11:10 15.1.3
0782		 RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING
J. Gao¹, T. Wang, Taiyuan University of Technology, China; H. Gao¹, Y. Ding¹, Z. Wang¹; ¹ University of Sydney, Australia

11:35 - 11:40CHANGEOVER BREAK

0.3GENERAL LECTURE 1 The Time Has Come for an All-Wing Airplane by Florentina Viscotchi, Jet Zero
Chair: F. Collier ICAS PPSC Chair
14. Sep 26 11:40 12:30

12:30 - 13:30LUNCH BREAK

1.2GSA2: Perspectives and Progress towards NextGen Airliners
Chair(s): Krein, A., Vijgen, P.
Track 1 Pyrmont Theatre
15 - Guest lectures
14. Sep 26 13:30 13:55 1.2.1
0987		 BOEING PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY
M L Drake, The Boeing Company, United States
14. Sep 26 13:55 14:20 1.2.2
1023		 AIRBUS PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY
V Roca, Airbus SAS, France
14. Sep 26 14:20 14:45 1.2.3
1026		 EMBRAER'S PERSPECTIVES & PROGRESS TOWARDS NEXTGEN AIRLINERS
V di Nucci, Embraer, Brazil
14. Sep 26 14:45 15:10 1.2.4
1029		 PANEL DISCUSSION Q&A WITH THE AIRCRAFT OEMS
P Panel,
2.2High-Speed Flight: Progress and Prospects
Chair(s): Bowcutt, K., Neely, A.
Track 2 C4.1
15 - Guest lectures
14. Sep 26 13:30 13:55 2.2.1
1064		 RECENT DEVELOPMENTS IN HYPERSONIC INNOVATION, SCIENCE & TECHNOLOGY IN AUSTRALIA
A. Neely, UNSW, Australia
14. Sep 26 13:55 14:20 2.2.2
1065		 EUROPEAN HYPERSONICS OVERVIEW
N. Viola, Politecnico di Torino, Italy
14. Sep 26 14:20 14:45 2.2.3
1066		 HYPERSONIC RESEARCH AND DEVELOPMENT IN THE REPUBLIC OF KOREA: FROM FUNDAMENTAL AEROTHERMODYNAMICS TO FLIGHT DEMONSTRATION
B.J. Lee, Seoul National University, South Korea
14. Sep 26 14:45 15:10 2.2.4
1067		 AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION
J. Akatsuka¹, S. Takahashi¹, Y. Makino¹, S. Tomioka¹, M. Takegoshi¹, M. Koga¹, T. Isono¹; ¹JAXA, Japan
3.2Conceptual Design 1
Chair(s): Alexander, M., Nagel, B.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
14. Sep 26 13:30 13:55 3.2.1
0528		 POINT-CLOUD-BASED INTELLIGENT DESIGN OF FLYING-WING CONFIGURATIONS WITH CONDITIONAL GENERATION AND PRESSURE PREDICTION
J.-Z, Zhang¹, Z.-H. Han¹, W.-P. Song¹, K.-S. Zhang¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 13:55 14:20 3.2.2
0285		 ASSESSMENT OF LIQUID HYDROGEN-POWERED AIRCRAFT RANGE: A NOVEL BREGUET FORMULATION
G. Palaia, Polytechnic of Turin, Italy; K. Abu Salem, University of Trento, Italy; A.A. Quarta, University of Pisa, Italy; P.D. Bravo-Mosquera, University of São Paulo, Brazil
Presenter: Karim Abu Salem, University of Trento
14. Sep 26 14:20 14:45 3.2.3
0229		 INTEGRATING SYSTEM ARCHITECTURE OPTIMIZATION INTO MODEL-BASED SYSTEMS ENGINEERING METHODS
S. Valencia-Ibáñez¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada
additional information (interactive) 3.2.R
0455		 CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT
X. Lu¹, S. Chen¹, X. Wang¹, J. Yu¹, D. Li¹; ¹Northwestern Polytechnical University, China
4.2Conceptual Design Studies - 1
Chair(s): Lott, M.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 13:30 13:55 4.2.1
0447		 PERFORMANCE COMPARISON BETWEEN PASSENGER AIRCRAFT WITH NOVEL PROPULSION SYSTEMS AT CONCEPTUAL DESIGN LEVEL
J.L.C Chan¹, H Smith¹; ¹Cranfield University, United Kingdom
14. Sep 26 13:55 14:20 4.2.2
0888		 FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION
P. Schmollgruber¹, S. Defoort¹, E. Nguyen-Van¹, J. Gauvrit-Ledogar¹, J. Chan², C. Lawson², L. Kugler³, T. Zill³, J. Kos, NLR, Netherlands; ¹ONERA, France ;²Cranfield University, United Kingdom ;³DLR, Germany
14. Sep 26 14:20 14:45 4.2.3
0926		 SUPPORTING THE REGULATORY COMMUNITY SHAPING THE FUTURE OF SUSTAINABLE HIGH-SPEED CIVIL AVIATION: THE ESATTO FRAMEWORK
N. Viola¹, R. Fusaro¹, D. Feretto¹; ¹Politecnico di Torino, Italy
14. Sep 26 14:45 15:10 4.2.4
0688		 PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS
S. Trivedi¹, A.K. Munshi¹, R.S. Pant¹; ¹Indian Institute Technology Bombay, India
5.2Transition Predictions
Chair(s): , , Halila, G.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 13:30 13:55 5.2.1
0936		 OVERVIEW OF VERIFICATION AND VALIDATION EFFORTS FOR PDE-BASED LAMINAR-TURBULENT TRANSITION MODELS
J.G. Coder, Penn State University, United States
14. Sep 26 13:55 14:20 5.2.2
0226		 ACCURACY AND EFFICIENCY OF TRANSITION–TURBULENCE MODELS IN PREDICTING HIGH AND LOW REYNOLDS NUMBER PROPELLER PERFORMANCE
F. Parra¹, D. Domínguez¹, A. Delgado¹, J. Gonzalo¹; ¹Universidad de León, Spain
14. Sep 26 14:20 14:45 5.2.3
0463		 A ROTOR TRANSITION PREDICTION METHOD BASED ON GALILEAN INVARIANCE AND THE C1 CROSSFLOW TRANSITION CRITERION
K.Y. Zhou¹, W.P. Song¹, J.H. Xu¹; ¹Northwestern Polytechnical University, China
14. Sep 26 14:45 15:10 5.2.4
0653		 HYPERSONIC RECEPTIVITY TO FREESTREAM DISTURBANCES OVER A BLUNT WEDGE: A LINEARIZED NAVIER-STOKES APPROACH
Z. Zhu¹, Y. Xi¹, S. Fu¹; ¹Tsinghua University, China
6.2Aircraft Flow Control Applications
Chair(s): Moreau, D.
Track 6 C4.5
03.3 - Basic Fluid Dynamics and Flow Control
14. Sep 26 13:30 13:55 6.2.1
0185		 PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS
Y. Mou¹, Y. Wu¹, T. Liu², D. Li², Y. Xiang¹, H. Liu¹; ¹School of Aero. & Astro., Shanghai Jiao Tong Univ., China ;²COMAC Shanghai Aircraft Design and Research Institute, China
14. Sep 26 13:55 14:20 6.2.2
0255		 ACTIVE FLOW CONTROL AND THERMAL PROTECTION FOR A WING-BODY CONFIGURATION BASED ON LATERAL JET
L. He¹, F. Chen¹, Y. Wei¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 14:20 14:45 6.2.3
0374		 REDUCED-ORDER MODELLING OF MINI-TAB SPOILER DYNAMICS FOR GUST LOAD ALLEVIATION
A. Jürisson¹, P.H.L. Blom¹; ¹Royal Netherlands Aerospace Centre, Netherlands
7.2Aero-Thermal Effects, Icing and Propulsion System Integration
Chair(s): Herbert, L.
Track 7 C4.6
03.4 - Applied Aerodynamics
14. Sep 26 13:30 13:55 7.2.1
0242		 NUMERICAL SIMULATION OF SUPERCOOLED LARGE DROPLET IMPINGEMENT ON ROTATING FAN BLADES
H. Yan¹, H. Zheng¹, Z. Dong¹, W. Dong¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 13:55 14:20 7.2.2
0339		 JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM
Z.Y. Dong, China; H.R. Zheng, China; H. Yan, China; P.Y. Wang, China; W. Dong, China
14. Sep 26 14:20 14:45 7.2.3
0501		 AIRFRAME-INLET INTEGRATION DESIGN FOR AN OVER-WING-MOUNTED SUPERSONIC TRANSPORT CONFIGURATION
Q. Chen¹, Z.-H. Han¹, K.-S. Zhang¹, K. Song¹; ¹Northwestern Polytechnical University, China
14. Sep 26 14:45 15:10 7.2.4
0297		 DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING
B. Li, China; X. Zhu, China; Z. Zhou, China; M. Li, China; R. Wang, China
8.2Damage Tolerance
Chair(s): Bayandor, J.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 13:30 13:55 8.2.1
0357		 IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITES
A.M. Caporale¹, G. Janszen¹, A.S. Jambhulkar¹, M. Ursic², A. Tasca², R. Passoni², A. Airoldi¹; ¹Politecnico di Milano, Italy ;²Brembo N.V., Italy
14. Sep 26 13:55 14:20 8.2.2
0160		 EFFICIENT SIMULATION AND UNCERTAINTY QUANTIFICATION OF PROGRESSIVE CRUSHING IN COMPOSITE LAMINATES
J. Reiner, Deakin University, Australia; R. Vaziri, The University of British Columbia, Canada
14. Sep 26 14:20 14:45 8.2.3
1100		 PROGRESSIVE FAILURE TIMELINE RECOUNT OF AN ATMOSPHERIC REENTRY TRAGEDY - IN MEMORY OF STS-107 CREW, AND DR. FRANK ABDI
J. Bayandor, United States
9.2System of Systems 2
Chair(s): Crossley, W., Jouannet, C.
Track 9 C4.8
02 - Systems Engineering and Integration
14. Sep 26 13:30 13:55 9.2.1
0607		 THE CONFERENCE LOCATIONS: A QUANTITATIVE APPROACH TO REDUCING IMPACT GLOBAL TRAVEL
C. Jouannet¹, K. Amadori¹, R. Perez, Royal Military College of Canada, Canada; E. Moerland, DLR, Germany; ¹Saab Aeronautics an Linköpings University, Sweden
Presenter: christopher Jouannet
14. Sep 26 13:55 14:20 9.2.2
0910		 MODELING, SIMULATION AND EVALUATION OF LARGE FOREST FIRE EXTINGUISHING AND RESCUE BASED ON AVIATION MATERIEL
W. Cheng¹, S. Chen¹, G. Wang¹, H. Cao¹, Y. Wu¹; ¹Aviation Industry Development Research Center of China (ADR), China
14. Sep 26 14:20 14:45 9.2.3
0918		 FEATURE MODEL CREATION THROUGH MISSION ANALYSIS IN THE CONTEXT OF VEHICLE FAMILIES
A.M. Zarate Villazon¹, M. Balchanos¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
10.2Hydrogen Propulsion Concepts
Chair(s): Bezos O Connor, G.
Track 10 C4.9
05 - Propulsion and Energy
14. Sep 26 13:30 13:55 10.2.1
0299		 EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS
F. Thilker¹, R. Krewinkel, Graz University of Technology , Austria; A. Tramposch¹; ¹University of Applied Sciences JOANNEUM GmbH, Austria
14. Sep 26 13:55 14:20 10.2.2
0574		 HEAT EXCHANGER MODELING METHODS FOR HYDROGEN POWERED AERO ENGINES DURING THERMODYNAMIC CYCLE DESIGN
A. Görtz¹, J. Häßy¹, M. Baier Schmelcher¹, M. El-Soueidan¹, F. Herbst¹; ¹German Aerospace Center, Germany
14. Sep 26 14:20 14:45 10.2.3
0338		 REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION
G. Marinaro¹, C. Serpico¹, L. Garbarino¹, M. Inverno¹, G. Malaponte¹, A. Bono¹, A. Pagano¹; ¹Italian Research Centre - CIRA, Italy
11.2Flight Control 2
Chair(s): Rogalski, T., Woszidlo, R.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 13:30 13:55 11.2.1
0123		 ROBUST ESTIMATION-AWARE GUIDANCE FOR STOCHASTIC INTERCEPTION WITH PARAMETRIC UNCERTAINTY
L. Mudrik, Naval Postgraduate School, United States; Y. Oshman, Technion---Israel Institute of Technology, Israel
Presenter: Yaakov Oshman, Technion---Israel Institute of Technology
14. Sep 26 13:55 14:20 11.2.2
0166		 DISTURBANCE OBSERVER-BASED ADAPTIVE NONSINGULAR TERMINAL SLIDING MODE CONTROL FOR FAULT-TOLERANT CONTROL OF QUAD-TILTROTOR EVTOL
S.W. Kim¹, T.W Yun¹, D.H. Seo¹, J.Y. Suk¹, S.K. Kim¹; ¹Chungnam National University, South Korea
14. Sep 26 14:20 14:45 11.2.3
0441		 FLIGHT ENVELOPE PROTECTION FOR HIGH ALTITUDE LONG ENDURANCE AIRCRAFT
C. Weiser, German Aerospace Center (DLR), Germany
14. Sep 26 14:45 15:10 11.2.4
0725		 CONTROL ALLOCATION AND SIZING FOR OVER-ACTUATED AIRCRAFT
C. Doll, ONERA, France
12.2De-icing
Chair(s): Stumpf, E.
Track 12 C2.3
07 - Systems, Subsystems and Equipment
14. Sep 26 13:30 13:55 12.2.1
0025		 A THERMO-MECHANICAL PHASE FIELD MODEL CONSIDERING SOLID-LIQUID TRANSITION: APPLICATION TO ELECTROTHERMAL DE-ICING
Y. Ying, Northwestern Polytechnical University , China; X. Yao¹, Y. Feng¹, W. Huang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 13:55 14:20 12.2.2
0186		 ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL
L. Mangiacrapa¹, T. Klaas², N. Rehfeld², F. Amoroso, Eurotech s.r.l., Italy; G. Mingione¹, S. Ameduri¹; ¹Italian Aerospace Research Centre, Italy ;²Fraunhofer IFAM , Germany
Presenter: Luigi Mangiacrapa, Italian Aerospace Research Centre
14. Sep 26 14:20 14:45 12.2.3
0660		 A MPC–MHE STRATEGY FOR FREQUENCY TRACKING AND PARAMETERS ESTIMATION OF RESONANT DE-ICING SYSTEMS
A. Suti¹, J. Pothin², M. Budinger¹, V. Pommier-Budinger², A. Reysset¹; ¹INSA Toulouse, France ;²Isae Supaero, France
Presenter: Aleksander SUTI
13.2Air Traffic Sequencing and Flows
Chair(s): Brown, M.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
14. Sep 26 13:30 13:55 13.2.1
0048		 REDUCING AIR TRAFFIC COMPLEXITY IN JAPANESE AIRSPACE THROUGH MINOR LATERAL TRAJECTORY ADJUSTMENTS
S.B. Goeppel¹, E. Asadi¹, E. Itoh, he University of Tokyo, Japan; M. Schultz, University of the Bundeswehr, Germany; ¹University of the Bundeswehr Munich, Germany
Presenter: Simon Goeppel, University of the Bundeswehr Munich
14. Sep 26 13:55 14:20 13.2.2
0408		 RUNWAY-AWARE CAPACITY ENVELOPES FOR LONG-RANGE ARRIVAL METERING UNDER OPERATING-DIRECTION CHANGES AT SINGAPORE CHANGI
E. Asadi¹, G. Enea, MIT Lincoln Laboratory, United States; M. Schultz¹; ¹University of the Bundeswehr Munich, Germany
14. Sep 26 14:20 14:45 13.2.3
0446		 AIRCRAFT SEQUENCING UNDER UNCERTAINTY: GAME-THEORETIC OPTIMIZATION AND A COMPARATIVE ASSESSMENT OF GLOBAL AND INTRA-AIRLINE COOPERATIVE DECISION FRAMEWORKS
S. Tsuru¹, A. Andreeva-Mori¹; ¹Osaka Metropolitan University, Japan
14. Sep 26 14:45 15:10 13.2.4
0591		 IMPACT OF DYNAMIC METERING OPERATIONS UNDER ADVERSE WEATHER AND MITIGATION THROUGH OPTIMAL SEQUENCING
Y. Matsuno¹, H. Matsuda¹; ¹Japan Aerospace Exploration Agency, Japan
14.2Mission Planning and Navigation
Chair(s): , , Hristozov, S.
Track 14 C2.5
06.2 - Flight Dynamics and Control (UAV related)
14. Sep 26 13:30 13:55 14.2.1
0217		 DYNAMIC RECONFIGURABLE PATH PLANNING FOR FIRE-FIGHTING UAVS
Z. Lin¹, D. Geraghty¹, S.F. Armanini¹, L. Mainini¹; ¹Imperial College London, United Kingdom
14. Sep 26 13:55 14:20 14.2.2
0709		 COOPERATIVE TRACKING ALGORITHM OF MULTIPLE UAVS USING PSO FOR AERIAL SURVEILLANCE
D.Y. Yoon¹, J.Y. Ka¹, D.J. Lee¹, Z. Wang², K.C. Wong²; ¹Hanseo University, South Korea ;²The University of Sydney, Australia
14. Sep 26 14:20 14:45 14.2.3
0695		 MODELING OF CRITICAL WEATHER FLIGHT PERFORMANCE OF MULTICOPTER UAVS FOR RESILIENT CONTROLLER DESIGN.
A. Fallast¹, S. Lesak¹; ¹FH JOANNEUM University of Applied Sciences, Austria
Presenter: Samuel Lesak, FH JOANNEUM University of Applied Sciences
14. Sep 26 14:45 15:10 14.2.4
0079		 SIMULATION-BASED ANALYSIS OF REDUNDANT UAV NAVIGATION UNDER GNSS OUTAGES
M. Ben Simon¹, S. Malka¹, D. Chudnovsky¹, O. Yakimenko¹; ¹Naval Postgraduate School, United States
15.2 Aircraft Systems, Operations, and Certification
Chair(s): Finck, T.
Track 15 C2.6
10 - Safety and Security
14. Sep 26 13:30 13:55 15.2.1
0154		 WHO SHOULD SIT AT THE EXIT ROW? A HUMAN FACTORS APPROACH TO EMERGENCY EVACUATION PASSENGER SELECTION IN COMMERCIAL AVIATION
A. Reis¹, C. Lessa¹, P. Kurka¹, R. Santos Alencar, ITA , Brazil; M. Machado Cardoso Júnior ¹; ¹ITA, Brazil
14. Sep 26 13:55 14:20 15.2.2
0307		 CONCEPT OF OPERATIONS FOR A HYDROGEN-ELECTRIC POWERED MODIFIED DASH 8-300 REGIONAL AIRCRAFT: PERFORMANCE, OPERATIONAL, AND REGULATORY IMPACTS
B. Rietdijk¹, B. Sulejmanovic¹, R. Coertze¹; ¹Conscious Aerospace BV, Netherlands
14. Sep 26 14:20 14:45 15.2.3
0363		 TOWARDS THE INTEGRATION OF NEUROPHYSIOLOGICAL SIGNALS AND HUMAN BODY DYNAMICS FOR ADAPTIVE CONTROL ALLOCATION
T. Treichl, German Aerospace Center, Germany; T.S. Paul, Thales France, France
14. Sep 26 14:45 15:10 15.2.4
0701		 VLSEC: A CONCEPT FOR SECURING VIRTUAL LINKS IN AVIONICS NETWORKS THROUGH CENTRALIZED GROUP KEY MANAGEMENT
C.A. Dautel¹, M. Werthwein¹, M. Homolya¹, M. Lehmann¹, S. Queiroz¹, B. Annighoefer¹; ¹University of Stuttgart, Institute of Aircraft Systems (ILS), Germany

15:10 - 15:15CHANGEOVER BREAK

0.4GENERAL LECTURE 2 Airbus 400M by Francisco Hernandez
Chair: G. Holmberg ICAS PC Chair
14. Sep 26 15:15 16:05

16:05 - 16:30AFTERNOON BREAK

1.3GSA2: Perspectives and Progress on NextGen Propulsion for Future Airliners
Chair(s): Haselbach, F., Drake, M.
Track 1 Pyrmont Theatre
15 - Guest lectures
14. Sep 26 16:30 16:55 1.3.1
1008		 PRATT & WHITNEY: MEETING THE FUTURE PROPULSION NEEDS OF COMMERCIAL AVIATION
A.M. Murphy, Pratt & Whitney, United States
14. Sep 26 16:55 17:20 1.3.2
1037		 RR PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS
T Newby, Rolls-Royce plc, United Kingdom
14. Sep 26 17:20 17:45 1.3.3
1010		 CFM INTERNATIONAL'S RISE PROGRAM: A STEP-CHANGE FOR DURABILITY AND EFFICIENCY
C.-A. Andrews, GE Aerospace, United States
14. Sep 26 17:45 18:10 1.3.4
1099		 PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS FROM SAFRAN’S STANDPOINT
E. Dalbies, SAFRAN, France
2.3Digital Thread and Integration
Chair(s): Jouannet, C.
Track 2 C4.1
15 - Guest lectures
14. Sep 26 16:30 16:55 2.3.1
1081		 COMPUTATIONAL AVENUES TO ADVANCE DIGITAL CAPABILITIES AND EMPOWER SYNERGIES FOR THE BLUE SKIES
L. Mainini, please select...
14. Sep 26 16:55 17:20 2.3.2
1087		 MBSE AS A KEY ENABLER IN AEROSPACE DIGITAL ENGINEERING
A. Habibi Husain, please select...
14. Sep 26 17:20 17:45 2.3.3
1088		 DIGITAL ENGINEERING FOR TRANSFORMATIVE AEROSPACE
O. Pinon-Fischer, United States
3.3Conceptual Design 2
Chair(s): Alexander, M., Bagassi, S.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
14. Sep 26 16:30 16:55 3.3.1
0400		 AN INTEGRATED CONCEPTUAL DESIGN WORKFLOW FOR LIQUID HYDROGEN-POWERED BOX-WING AIRCRAFT
G. Palaia, Politecnico di Torino, Italy; K. Abu Salem, University of Trento, Italy; A.A. Quarta, University of Pisa, Italy; P.D. Bravo-Mosquera, São Carlos School of Engineering, University of São Paulo, Brazil
14. Sep 26 16:55 17:20 3.3.2
0575		 AGENTIC AI FOR AIRCRAFT PRELIMINARY DESIGN: PROOF OF CONCEPT
A. Kirste¹, L. Faltum¹, E. Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany
14. Sep 26 17:20 17:45 3.3.3
0668		 AI-SUPPORTED AIRCRAFT SYSTEM ARCHITECTURE SYNTHESIS
P. Krus, Linköping University, Sweden
14. Sep 26 17:45 18:10 3.3.4
0130		 DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+
J. Song¹, S. Park², D. Lee², Y.-E. Kang¹, Y. Kim¹, W.I. Choi¹, S. Lee¹; ¹Manufacturing AI Research Center, KITECH, South Korea ;²Department of Unmanned Aircraft Systems, Hanseo University, South Korea
Presenter: Juhun Song, Korea Institute of Industrial Technology/Sungkyunkwan University
4.3Conceptual Design Studies - 2
Chair(s): Nicolosi, f.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 16:30 16:55 4.3.1
0296		 FLIGHT TESTING OF A HIGH-ALTITUDE UNCREWED AND SOLAR POWERED PLATFORM HEAVIER THAN AIR
F. Nikodem¹, C. Weiser¹; ¹DLR e.V., Germany
Presenter: Christian Weiser, DLR e.V.
14. Sep 26 16:55 17:20 4.3.2
0420		 CONCEPTUAL DESIGN OF A MIDDLE-OF-THE-MARKET AIRCRAFT FOR EDUCATIONAL PURPOSES
A.S.J. van Heerden¹, N.M. Ahamad¹, J.F. Castiblanco Aponte¹, J. Gibbs¹, I.J. Taylor¹; ¹University of Glasgow, United Kingdom
14. Sep 26 17:20 17:45 4.3.3
0931		 INVESTIGATING A STABLE LIFTING FUSELAGE FOR A TWO SEAT SAILPLANE OF THE GULL WING CONFIGURATION
B.-B. Huyssen¹, D. Fenthum¹, J. Huyssen, CSIR, South Africa; ¹University of Pretoria, South Africa
14. Sep 26 17:45 18:10 4.3.4
0960		 PROPOSING A STABLE LIFTING FUSELAGE FOR AN AIRLINER OF THE IDEAL AIRCRAFT CONFIGURATION
Joachim Huyssen, CSIR, South Africa; Eduard van Heerden, University of Pretoria, South Africa
5.3Buffeting and Other Aeroelastic Analyses
Chair(s): Slotnick, J., Azevedo, J.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 16:30 16:55 5.3.1
0183		 TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT
M. Candon¹, T. Gerner¹, A. Das¹, Z. Hoffman¹, P. Marzocca¹, L. Munholand², V. Viti², E. H. Dowell, Duke University, United States; ¹RMIT University, Australia ;²ANSYS, United States
14. Sep 26 16:55 17:20 5.3.2
0927		 HIGH-FIDELITY ANALYSIS OF AIRCRAFT TAIL BUFFETING UNDER DYNAMIC MANEUVERING
M.R. Rajanna¹, J. Lua¹, N. Phan, Naval Air System Command, United States; M.-C. Hsu, Iowa State University, United States; ¹Global Engineering and Materials, Inc., United States
14. Sep 26 17:20 17:45 5.3.3
0282		 BUFFETING SCALE EFFECTS ON A LAUNCH VEHICLE: HYBRID RANS-LES ANALYSIS
D. Palma¹, L. Pirillo¹, M. Bernardini¹, F. Stella¹; ¹Sapienza university of Rome, Italy
14. Sep 26 17:45 18:10 5.3.4
0796		 AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING
Y. Zhao¹, J. He¹, X. Wei¹, T. Chen¹, Y. Yang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 5.3.R
0953		 COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT
G.C. Ribolla¹, L.J.F. Meirelles¹, L.F.S. Gomes¹, M.B. Stergiou¹, R.M. Granzoto, Embraer, Brazil; P. Bufacchi¹; ¹Insper, Brazil
6.3Hypersonics Boundary Layer and Flow Features
Chair(s): , , Vijgen, P.
Track 6 C4.5
03.3 - Basic Fluid Dynamics and Flow Control
14. Sep 26 16:30 16:55 6.3.1
0070		 RECEPTIVITY OF NON-MODAL STREAKS IN HYPERSONIC BLUNT BOUNDARY LAYERS: FROM NUMERICS TO ASYMPTOTICS
M. Dong, Institute of Mechanics, Chinese Academy of Sciences, China; L. Zhao, Departiment of Mechanics, Tianjin University, China
14. Sep 26 16:55 17:20 6.3.2
0094		 ORIGIN OF TRANSIENT TURBULENT SPOTS IN HYPERSONIC SWEPT BOUNDARY LAYERS WITH MORPHING SWEEP ANGLES
G. Jiang¹, M. Dong¹; ¹Institute of Mechanics, Chinese Academy of Sciences, China
14. Sep 26 17:20 17:45 6.3.3
0311		 NUMERICAL SIMULATION OF HYPERSONIC PLASMA FLOW BASED ON NONLINEAR COUPLED CONSTITUTIVE RELATIONS
H. Shi¹, C. Song¹, H. Xiao¹; ¹Northwestern Polytechnical University, China
14. Sep 26 17:45 18:10 6.3.4
0781		 AFTERBODY CURVATURE EFFECTS ON FLOW LOSS CHARACTERISTICS BASED ON ENTROPY PRODUCTION
X.W. Chen¹, M.S. He¹, B. Yu¹, W. Wang¹, H. Liu¹; ¹Shanghai Jiao Tong University, China
7.3High-Performance and Laminar Flow Wing Design
Chair(s): Rivers, M.
Track 7 C4.6
03.4 - Applied Aerodynamics
14. Sep 26 16:30 16:55 7.3.1
0066		 SWEEP ANGLE STUDY OF A STRUT-BRACED-WING REGIONAL JET WITH NATURAL LAMINAR FLOW
N. Saadeh¹, D.W. Zingg¹; ¹University of Toronto, Canada
14. Sep 26 16:55 17:20 7.3.2
0087		 AERODYNAMIC SHAPE OPTIMIZATION OF INFINITE SWEPT WINGS FOR NATURAL LAMINAR FLOW AT TRANSONIC CRUISE CONDITIONS
F. Husain¹, D.W. Zingg¹; ¹University of Toronto Institute for Aerospace Studies, Canada
14. Sep 26 17:20 17:45 7.3.3
0934		 MULTIPOINT INVERSE DESIGN FOR TRANSONIC, SLOTTED, NATURAL-LAMINAR-FLOW WINGS
A. Heletkanycz¹, C.J. Axten¹, J.G. Coder¹; ¹Penn State University, United States
14. Sep 26 17:45 18:10 7.3.4
0162		 VORTEX TOPOLOGY AND CORE-UNWINDING MECHANISM IN SPIROID WINGTIP DEVICES USING LAGRANGIAN PARTICLE TRACKING
M.A. Mwasandube¹, M. Marino¹, J.L. Palmer¹; ¹RMIT University, Australia
8.3Aerospace-Grade Composites
Chair(s): Bayandor, J., Denquin, A.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 16:30 16:55 8.3.1
0036		 DEVELOPMENT OF CONDUCTIVE COMPOSITE MATERIALS FOR HIGH VOLTAGE APPLICATIONS
S.A. Brown¹, P. Sangkarat¹, Z. Sha, Western Sydney University, Australia; C.-H. Wang¹; ¹University of New South Wales, Australia
14. Sep 26 16:55 17:20 8.3.2
0082		 COMPRESSIVE PERFORMANCE OF VARIABLE-STIFFNESS COMPOSITE HYPERBOLIC STIFFENED PANELS BASED ON GEOMETRIC PATH MAPPING
R.B. Ma¹, C.Y. Wang¹, X.M. Chen, Aircraft Strength Research Institute of China, China; W.Z. Wang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 17:20 17:45 8.3.3
0868		 ENHANCEMENT AND DEGRADATION: THE DUAL ROLE OF GRAPHENE NANOPLATELETS ON THE STRUCTURAL PERFORMANCE OF COMPOSITE T-JOINTS AND MECHANISTIC INSIGHTS
M. Bhasin¹, A.P. Mouritz¹; ¹RMIT University, Australia
Presenter: Mukesh Bhasin, RMIT University
14. Sep 26 17:45 18:10 8.3.4
0276		 NUMERICAL SIMULATION OF STRESS-OXIDATION DAMAGE IN C/SIC COMPOSITES AT HIGH TEMPERATURES
G. Chen¹, L. Yao¹, B. Li¹, X. Tong¹; ¹Northwestern Polytechnical University, China
9.3Health Monitoring
Chair(s): Alaimo, A., Coppotelli, G.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
14. Sep 26 16:30 16:55 9.3.1
0032		 KEY PARAMETER IDENTIFICATION IN AIRCRAFT STRAIN PREDICTION MODELS
K. Niessen¹, D. Franke¹; ¹Defence Science and Technology Group, Australia
14. Sep 26 16:55 17:20 9.3.2
0706		 AIRFRAME HEALTH MONITORING ON THE BAE SYSTEMS HAWK T1A JET TRAINER
G. Dessena¹, M. Civera², E.P. Mottola², O.E. Bonilla-Manrique¹; ¹Universidad Carlos III de Madrid, Spain ;²Politecnico di Torino, Italy
14. Sep 26 17:20 17:45 9.3.3
0072		 SEMI-SUPERVISED MULTI-TASK CONSISTENCY LEARNING FOR DEFECT DETECTION AND DEPTH ESTIMATION
S. Miao¹, Y. Ge¹, Y. Pei¹; ¹Northwestern Polytechnical University, China
14. Sep 26 17:45 18:10 9.3.4
0379		 IMPACT LOAD IDENTIFICATION METHOD FOR AIRCRAFT RUDDER PLANES BASED ON NARX NEURAL NETWORK
S.Y. Liang¹, T. Yang¹, Z.C. Yang¹; ¹Northwestern Polytechnical University, China
10.3Hybrid Electric Fuel Cell Concepts
Chair(s): Bezos O Connor, G.
Track 10 C4.9
05 - Propulsion and Energy
14. Sep 26 16:30 16:55 10.3.1
0139		 IMPACT ASSESSMENT OF COMPONENT FAILURES IN A PEM-FUEL CELL BASED PROPULSION SYSTEM FOR AIRCRAFT APPLICATIONS FOCUSING ON WATER MANAGEMENT
S. Bäumler, Chair of Electrified Aero Engines, BTU Cottbus-Senftenberg, Germany; S. Kazula¹, A. Zwingler, Department of Mechanical Engineering, TU Munich, Germany; L. Enghardt¹; ¹DLR Institute of Electrified Aero Engines, Germany
14. Sep 26 16:55 17:20 10.3.2
0652		 NUMERICAL AND EXPERIMENTAL EVALUATION OF COMPACT TPMS AND OFFSET-STRIP-FIN HEAT EXCHANGERS FOR FUEL CELL SYSTEM COOLING IN AN ELECTRIC AIRCRAFT
C.K. Sain¹, S. Bhapkar¹, M. Kober¹, S. Kazula¹; ¹German Aerospace Center (DLR), Germany
14. Sep 26 17:20 17:45 10.3.3
0826		 THERMAL–HYDRAULIC OPTIMIZATION OF AXIALLY GRADED OFFSET STRIP-FIN HEAT EXCHANGERS FOR MEGAWATT-CLASS FUEL CELL ELECTRIC AIRCRAFT
S. Bhapkar¹, C. Sain¹, M. Kober¹, S. Kazula¹; ¹German Aerospace Center, Germany
Presenter: Chetan Sain, German Aerospace Center
11.3Flight Control 3
Chair(s): Kim, S., Kiszkowiak, L.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 16:30 16:55 11.3.1
0891		 DATA-DRIVEN SYNTHESIS OF AIRCRAFT FEEDBACK CONTROL LAWS FOR NEW COMMERCIAL FLIGHT SCENARIOS
M. Szymanski¹, V. Gollnick¹; ¹Hamburg University of Technology, Germany
14. Sep 26 16:55 17:20 11.3.2
0791		 AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL
M.T. Morales¹, M.A. Rempel, Embraer, Brazil; M.A.V. Morales¹, J.E.M. Fernandes¹; ¹ITA, Brazil
14. Sep 26 17:20 17:45 11.3.3
0152		 KNOW YOUR LIMITS: ESTIMATING THE TILT-WING TRANSITION CORRIDOR UNDER FAILURE CONDITIONS
M. May¹, D. Milz¹, S.F. Armanini, Imperial College London, Germany; ¹German Aerospace Center (DLR), Germany
14. Sep 26 17:45 18:10 11.3.4
0506		 ROBUST ATTITUDE RECOVERY CONTROL FOR AIR-LAUNCHED FOLDING-WING UAVS VIA DISTURBANCE-COMPENSATED SUPER-TWISTING SLIDING MODE
S.W. Han¹, T.L. Ma¹, J.C. Fu¹, X.O. Zhang¹, Q.L. Zhang¹, L.Z. Wang¹; ¹Beihang University, China
12.3Actuation Fault and Optimization
Chair(s): Viola, N.
Track 12 C2.3
07 - Systems, Subsystems and Equipment
14. Sep 26 16:30 16:55 12.3.1
0623		 MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II
Z. Zhu¹, Y. Lyu¹, L. Jiang¹, Z. Liu¹, S. Li¹, F. Liu¹; ¹Northwestern Polytechnical University, China
Presenter: Fulin Liu, Northwestern Polytechnical University
14. Sep 26 16:55 17:20 12.3.2
0683		 OSCILLATORY FAILURE DETECTION IN AIRCRAFT ACTUATION SYSTEMS USING WAVELET TRANSFORM
I.O. Skusa, ITA/Embraer, Brazil; R.N. Calvo, Embraer, Brazil; A.A. Filho, ITA, Brazil
Presenter: Isabella Ono Skusa
14. Sep 26 17:20 17:45 12.3.3
0784		 PERFORMANCE DEGRADATION ANALYSIS OF RESOLVER FAULTS IN ELECTRO-MECHANICAL ACTUATOR
S. Guan¹, J. Fu¹, T.Q. Yang¹, Z.H. Ge¹, T.Y. Zhang², Z.Y. Zhao²; ¹Beihang University, China ;²AVIC Shenyang Aircraft Design Institute, China
Presenter: Taoqing YANG, Beihang University,
14. Sep 26 17:45 18:10 12.3.4
0961		 MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEMS
T.Q. Yang¹, J. Fu¹, S. Guan¹, J. Pan², C.F. Yao², H.L. Qu²; ¹Beihang University, China ;²AVIC Xi'an Flight Automatic Control Research Institute, China
additional information (interactive) 12.3.R
0621		 INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE HIGH-ENERGY SYSTEMS
S. Bai¹, Y. Li¹, L. Jiang¹, Z. Li¹, K. He¹, Z. Jiao¹; ¹Beihang University, China
13.3Pathways for Sustainable Aviation
Chair(s): Andreeva-Mori, A.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
14. Sep 26 16:30 16:55 13.3.1
1003		 FLIGHT PLANNING, THE FORGOTTEN ASSET
A. Dickinson, Qantas Airways Limited, Australia
14. Sep 26 16:55 17:20 13.3.2
0666		 GLOBAL EMISSION MONITOR FOR 2023
M. Clococeanu¹, C.M. Weder¹, H. Bruder¹, Z.L. Zengerling¹; ¹German Aerospace Center, Germany
Presenter: Maximilian Clococeanu, Deutsches Zentrum für Luft- und Raumfahrt e.V.
14. Sep 26 17:20 17:45 13.3.3
0212		 JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION
T. Ehlers¹, A. Lau¹, M. Mendiguchia Meuser¹, A. Kuenz¹, S. Dietmüller¹, S. Matthes¹; ¹DLR, Germany
14. Sep 26 17:45 18:10 13.3.4
0870		 CLIMATE HAZARD TIMING AND FLIGHT DEMAND COOCCURRENCE: A DEMAND-WEIGHTED EXPOSURE FRAMEWORK
K. Sumaja¹, T.-R.T. Koo¹, S. Mooney, School of Biological, Earth and Environmental Sciences, UNSW, Australia; T.H. Rashidi¹; ¹School of Civil and Environmental Engineering, UNSW, Australia
14.3Launch and Recovery
Chair(s): Gerner, T., Palmer, J.
Track 14 C2.5
06.2 - Flight Dynamics and Control (UAV related)
14. Sep 26 16:30 16:55 14.3.1
0937		 A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH
A.G.P. Sarmento¹, C.C. Duarte da Silva¹, G.V. Ferreira¹, E. Villani¹, D. Rade¹; ¹Aeronautics Institute of Technology (ITA), Brazil
Presenter: Caroline Cristine Duarte da Silva, Aeronautics Institute of Technology (ITA)
14. Sep 26 16:55 17:20 14.3.2
0248		 AUTONOMOUS PATH PLANNING ALGORITHM FOR EMERGENCY LANDING OF AAM CONSIDERING WIND DISTURBANCES
H. Iwamoto¹, N. Yokoyama, Japan Aerospace Exploration Agency, Japan; T. Higuchi¹; ¹Yokohama National University, Japan
14. Sep 26 17:20 17:45 14.3.3
0208		 ASSESSMENT OF THE LANDING CAPABILITIES OF A FLEXIBLE HIGH-ALTITUDE PLATFORM AT LONGITUDINAL AND LATERAL-DIRECTIONAL WIND DISTURBANCES
Y.J. Hasan, DLR Institute of Flight Systems, Germany
14. Sep 26 17:45 18:10 14.3.4
0867		 DECOUPLED DEEP REINFORCEMENT LEARNING FOR AUTONOMOUS LANDING OF UAVS ON SHIPS
T. Gerner¹, M. Candon¹, A.K. Gostar¹, N. Jayarathne, Navantia Australia, Australia; J. Venning, University of Tasmania, Australia; M. Saska, Czech Technical University in Prague, Czech Republic; P. Marzocca¹; ¹RMIT University, Australia
15.3Human Factors, Workload, and Cognition
Chair(s): Fadda, T.
Track 15 C2.6
10 - Safety and Security
14. Sep 26 16:30 16:55 15.3.1
0056		 QUANTIFYING THE EFFECT OF IN-CABIN AIRCRAFT NOISE ON COGNITION.
Brett R.C. Molesworth, UNSW Sydney, School of Aviation, Australia; Marion Burgess, UNSW Sydney, School of Built Environment, Australia
14. Sep 26 16:55 17:20 15.3.2
0091		 PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE
W.D. Xiao¹, C.L. Zhao, Shanghai Aircraft Design and Research Institute, China; Y. Gao¹, Y.Y. Lu¹, S. Fu¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 17:20 17:45 15.3.3
0118		 UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION
A. Lemetti¹, L. Meyer², M. Peukert², T. Polishchuk¹, C. Schmidt¹, H. Alpfjord Wylde²; ¹Linköping University (LiU), Sweden ;²Air Navigation Services of Sweden (LFV), Research & Innovation, Sweden
14. Sep 26 17:45 18:10 15.3.4
0422		 HRV BASED PILOTS WORKLOAD PREDICTION FOR AN INTELLIGENT COCKPIT WARNING SYSTEM
C.R. Vindigni¹, A. Esposito¹, C. Orlando¹, A. Alaimo¹; ¹University of Enna Kore, Italy

Tuesday, 15. Sep 2026

0.5ICAS IFAR LECTURE Quiet aviation research for a sustainable tomorrow
Chair: I. Yimer ICAS and IFAR EC Member
15. Sep 26 08:00 08:50

08:50 - 08:55CHANGEOVER BREAK

1.4IFAR Follow Up Session: Innovations in Noise Reduction for Emerging and Conventional Air Transport
Chair(s): Fischer, M., Simon, F.
Track 1 Pyrmont Theatre
15 - Guest lectures
15. Sep 26 08:55 09:20 1.4.1
0912		 IFAR 2025 PERSPECTIVES ON NOISE REDUCTION FOR EMERGING AND CONVENTIONAL AIR TRANSPORT
K. Benameur¹, M. Jacinto, TU Wien, Austria; F. Simon¹, L. Bertsch², B. Schuchardt²; ¹ONERA, France ;²DLR, Germany
Presenter: Kaouthar Benameur, ONERA
15. Sep 26 09:20 09:45 1.4.2
0345		 CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION
B.I. Schuchardt¹, A.J. Torija, University of Salford, United Kingdom; I. Legriffon, Office National d’Études et de Recherches Aérospatiales (ONERA), France; D. Casalino, Delft University of Technology, Netherlands; L. Bertsch¹, R. Aalmoes, Netherlands Aerospace Centre (NLR), Netherlands; ¹German Aerospace Center (DLR), Germany
15. Sep 26 09:45 10:10 1.4.3
0964		 RECENT ADVANCES IN AEROACOUSTIC DESIGN OF ADVANCED AIR MOBILITY VEHICLES
W. Klimczyk¹, P. Kekus-Kumor¹, M. Rajek¹, A. Sieradzki¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland
Presenter: Witold Klimczyk, Lukasiewicz Research Network - Institute of Aviation
15. Sep 26 10:10 10:35 1.4.4
1048		 PANEL DISCUSSION AND Q&A
&A Q,
2.4Air Transport Resilience to Climate Change and Weather Hazards
Chair(s): Schmollgruber, P., Viola, N.
Track 2 C4.1
15 - Guest lectures
15. Sep 26 08:55 09:20 2.4.1
0994		 COMBINED IMPACT OF JET STREAM AND TURBULENCE ON LONG-TERM TRANS-OCEANIC FLIGHT ROUTES
J.-H. Kim, Seoul National University, South Korea
15. Sep 26 09:20 09:45 2.4.2
0997		 PROGRESS IN AIRCRAFT-BASED METEOROLOGICAL OBSERVATIONS
J. Hileman, The Boeing Company, United States
15. Sep 26 09:45 10:10 2.4.3
1035		 ADAPTING AVIATION TO A CHANGING CLIMATE: A GLOBAL AND REGIONAL PERSPECTIVE
R. Burbidge, EUROCONTROL, Belgium
15. Sep 26 10:10 10:35 2.4.4
1038		 PANEL DISCUSSION
1 Panel,
3.4Propulsion 1
Chair(s): Bagassi, S., Young, T.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 08:55 09:20 3.4.1
0915		 IMPLEMENTATION OF PROPELLER-WING INTERFERENCE MODEL AND HORIZONTAL TAIL ANALYSIS INTO A VISCOUS FULL POTENTIAL FLOW SOLVER FRAMEWORK FOR AIRCRAFT DESIGN
T.A. Ramprakash¹, D. Di Pasquale¹, S. Kumar¹; ¹Cranfield University, United Kingdom
15. Sep 26 09:20 09:45 3.4.2
0837		 IMPACT OF DIFFERENT PROPELLER CONFIGURATIONS ON THE FLIGHT DYNAMICS AND STABILITY OF A SMALL REGIONAL ELECTRIC AIRCRAFT
G. Babunaidu¹, A. Hammad¹; ¹Technical University of Munich, Germany
15. Sep 26 09:45 10:10 3.4.3
0484		 RESONANT ELASTIC SHAFT THRUST VECTORING: IMPLICATIONS FOR UAV DESIGNS
H. Guan, Australia; K.C. Wong, Australia
15. Sep 26 10:10 10:35 3.4.4
1112		 PROPULSIVE EFFICIENCY AND ENERGY ANALYSIS OF AIRCRAFT CONCEPTS WITH AFT-FUSELAGE BOUNDARY-LAYER-INGESTION
C. Zhou, Northwestern Polytechnical University, China
4.4Hydrogen in Design
Chair(s): Verstraete, D.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 08:55 09:20 4.4.1
0073		 DESIGN AND INVESTIGATION OF A SHORT-TO-MEDIUM-RANGE AIRCRAFT WITH LIQUID HYDROGEN AND SAF MULTI-FUEL PROPULSION
B. Türkyilmaz¹, M.G. Kolb¹, X. Zhao, Chalmers University of Technology, Sweden; M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
15. Sep 26 09:20 09:45 4.4.2
0213		 CHALLENGES AND SOLUTIONS FOR LIQUID HYDROGEN-POWERED UAVS: REGULATIONS AND CASE STUDY INSIGHTS
B. Legrand¹, N. Gavrilovic¹; ¹Département Aérodynamique, Energie et Propulsion, ISAE-SUPAERO, France
15. Sep 26 09:45 10:10 4.4.3
0333		 ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035
M. Kotzem¹, J. Häßy¹, V. Kriewall Peters, Hamburg University of Technology (TUHH), Germany; P. Schatrow¹, S. Wöhler¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 10:10 10:35 4.4.4
0316		 AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN
A. Tramposch¹, F. Thilker¹, S. Pfeifer¹, P. Kirschnek¹; ¹University of Applied Sciences FH Joanneum GesmbH, Austria
5.4Supersonic and Hypersonic Flows
Chair(s): , , Kiszkowiak, L.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 08:55 09:20 5.4.1
0241		 AN ADAPTIVE AND PARAMETER-FREE SLOPE LIMITER FOR UNSTRUCTURED COMPRESSIBLE FLOW SOLVER
G. Wang¹, Z.-K. Liu¹, T.-Y. Lin¹, H.-Y. Wang¹; ¹Northwestern Polytechnical University, China
15. Sep 26 09:20 09:45 5.4.2
0065		 A STUDY ON THE CELL REYNOLDS NUMBER AS A PARAMETER FOR MESH QUALITY ON HYPERSONIC FLOWS
G.M. Poltronieri¹, F.C. Moreira¹, J.L.F. Azevedo¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
Presenter: Joao Azevedo, Instituto Tecnologico de Aeronautica
15. Sep 26 09:45 10:10 5.4.3
0043		 INVESTIGATION OF PLUME NON-EQUILIBRIUM INFRARED RADIATION CHARACTERISTICS AT DIFFERENT MACH NUMBERS
J. Xu, China; L. Zhou, China; J. Shi, China; Z. Wang, China; H. Shi, China
15. Sep 26 10:10 10:35 5.4.4
0550		 NUMERICAL INVESTIGATION OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH 2.5 OVER A COMPRESSION RAMP
S. Gunasekaran, Cranfield Univeristy, United Kingdom; Z.A. Rana, Prince Mohammad Bin Fahd University, Saudi Arabia; S. Prince, Cranfield University, United Kingdom
6.4Complex Flow Phenomena
Chair(s): Coder, J.
Track 6 C4.5
03.2 - Experimental Aerodynamics
15. Sep 26 08:55 09:20 6.4.1
0362		 REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMICS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK
A. Goerttler¹, S. Koch¹, M. Werner¹, F. Tocci¹, F. Mayer, Airbus Defence and Space GmbH, Germany; A. Wagner¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 09:20 09:45 6.4.2
0472		 EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL
K.J. Groot, University of Wyoming, United States; N.J. Porfido¹, H.L. Reed¹, J.G. Coder, Penn State University, United States; D.M. Somers, Airfoils, Incorporated, United States; ¹Texas A&M University, United States
15. Sep 26 09:45 10:10 6.4.3
0748		 INTERMITTENT LOW FREQUENCY EXPERIMENTAL CAVITY DYNAMICS
J. McCarthy¹, C. Marshall¹, C. Brown, RMIT University, Australia; M. Jones¹; ¹Defence Science and Technology Group, Australia
Presenter: Connor Marshall, Defence Science and Technology Group
15. Sep 26 10:10 10:35 6.4.4
0545		 EFFECTS OF SLOT LOCATION ON FLOW AND HEAT TRANSFER IN A LATTICEWORK COOLING CHANNEL: AN MRV EXPERIMENT AND NUMERICAL STUDY
Y.X. Jia¹, H.R. Shen¹, J.M. Wu¹; ¹Xian Jiaotong University, China
7.4Boundary Layer Control and Stall Mitigation
Chair(s): Winski, C.
Track 7 C4.6
03.4 - Applied Aerodynamics
15. Sep 26 08:55 09:20 7.4.1
0047		 VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, CRANKED SWEPT WING
N. van Luijk¹, A. van Meenen¹, R. Vos¹; ¹Delft University of Technology, Netherlands
15. Sep 26 09:20 09:45 7.4.2
0221		 INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBER
M. Avirovic¹, C. Brunelli¹, B.G. Marinus¹, J. Degroote, University of Ghent, Belgium; J. van Beeck, von Karman Insititute for Fluid Dynamics , Belgium; E. Van Vaerenbergh¹; ¹Royal Military Academy, Belgium
15. Sep 26 09:45 10:10 7.4.3
0378		 EXERGY AND INTEGRAL BOUNDARY LAYER PARAMETERS CHARACTERISTIC CURVES FOR AERODYNAMIC DESIGN AND OPTIMIZATION
G. Bourreau-Tirel¹, S. Duplaa, ISAE-SUPAERO, France; J.P. Ruscio¹; ¹Aura Aero, France
15. Sep 26 10:10 10:35 7.4.4
0723		 PARAMETRIC AERODYNAMIC STUDY OF LEADING-EDGE SERRATIONS ON WING SECTIONS ACROSS REYNOLDS NUMBERS
J.J. Whittaker, University of New South Wales, Australia
8.4High Speed Flight: Configuration/Aero/Aerothermal/Flight-Performance
Chair(s): Bowcutt, K., Neely, A.
Track 8 C4.7
15 - Guest lectures
15. Sep 26 08:55 09:20 8.4.1
1068		 TOWARDS MULTI-DISCIPLINARY OPTIMIZATION OF A GENERIC HYPERSONIC VEHICLE – AN OVERVIEW OF RESEARCH AT LHSR, IISC
S. Rao, Indian Institute of Science, India
15. Sep 26 09:20 09:45 8.4.2
1069		 AERO-THERMO-STRUCTURAL OPTIMIZATION OF INTEGRATED THERMAL PROTECTION SYSTEMS
M. Santer, Imperial College London, United Kingdom
15. Sep 26 09:45 10:10 8.4.3
1070		 SDF-BASED GEOMETRY BLENDING OF HYPERSONIC VEHICLE CONCEPTS
S. Takahashi¹, T. Nagata, Nagoya University, Japan; M. Koga¹, T. Isono¹, M. Takegoshi¹; ¹JAXA, Japan
15. Sep 26 10:10 10:35 8.4.4
1071		 THE TREATMENT OF NON-IDEAL SURFACE TOPOLOGIES RELATED TO HIGH-SPEED VEHICLE DESIGN
J. Merrifield, Fluid Gravity Engr Ltd., United Kingdom
9.4Impact & Vibration 1
Chair(s): Alaimo, A., Dessena, G.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 08:30 08:55 9.4.1
0290		 ENERGY DISSIPATION OF THIN-WALLED RIBBED SPHERES FOR CARGO AIRDROP
A. Lloyd¹, K.C. Wong¹; ¹University of Sydney, Australia
15. Sep 26 08:55 09:20 9.4.2
0153		 GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL
A. Das¹, J. Yao¹, G. Coppotelli, University of Rome, La Sapienza, Italy; M. Candon¹, M. Fard¹, P. Marzocca¹; ¹RMIT University, Australia
15. Sep 26 09:20 09:45 9.4.3
0364		 NUMERICAL PREDICTION OF CABIN NOISE FOR FUTURE SHORT-HAUL AIRCRAFT IN EARLY AIRCRAFT DESIGN
C. Hesse¹, P. Allebrodt¹, S. Proskurov¹, B. Nagel¹; ¹DLR, Germany
10.4Advanced Vehicle Concepts
Chair(s): Hebert, L.
Track 10 C4.9
05 - Propulsion and Energy
15. Sep 26 08:55 09:20 10.4.1
0551		 EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY
P. Kirschnek¹, A. Görtz², M. Schmelcher², F. Thilker¹, J. Häßy²; ¹FH JOANNEUM, Austria ;²Deutsches Zentrum für Luft- und Raumfahrt, Germany
15. Sep 26 09:20 09:45 10.4.2
0487		 ASSESSMENT OF ENGINE-OUT ATMOSPHERIC EMISSIONS FROM COCONUT-OIL-DERIVED BIOJET FUEL
S. Ogawa¹, T. Hongo¹, Y. Maeda¹, H.P.U. Nguyen¹, K. Mori¹; ¹Osaka Metropolitan University, Japan
15. Sep 26 09:45 10:10 10.4.3
0739		 MAGNETOPLASMAIONIC (MPI) ENGINE
N.K. Chaudhary, Australia
11.4Guidance and Flight Trajectory Control 1
Chair(s): Drupka, G., Kim, S.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 08:55 09:20 11.4.1
0164		 TRAJECTORY OPTIMIZATION FOR TAKEOFF/LANDING BASED ON FLAP-AND-GLIDE FOR FLAPPING-WING UNMANNED AERIAL VEHICLE
W.S. Lee¹, S.J. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea
15. Sep 26 09:20 09:45 11.4.2
0821		 SENSITIVITY-BASED REFERENCE TRAJECTORY UPDATES FOR AIRCRAFT PATH-FOLLOWING MODEL PREDICTIVE CONTROL
S. Fuchsgruber¹, M. Gerdts, University of the Bundeswehr Munich, Germany; F. Holzapfel¹; ¹Technical University of Munich, Germany
15. Sep 26 09:45 10:10 11.4.3
0563		 OPTIMAL ZEM-BASED MIDCOURSE GUIDANCE FOR INTERCEPTORS USING TRAJECTORY PREDICTION
S. Kim¹, K.-W. Jung¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea
15. Sep 26 10:10 10:35 11.4.4
0246		 FLIGHT DYNAMICS AND GUIDANCE CONTROL FOR AIRCRAFT IN TYPHOON ENVIRONMENTS FOR DELIVERY OF TYPHOON CONTROL SUBSTANCE
T. Sakurai¹, S. Ueno¹, T. Higuchi¹, H. Akiyama¹; ¹Yokohama National University, Japan
additional information (interactive) 11.4.R
0532		 CONVEX OPTIMIZATION-BASED EMERGENCY LANDING TRAJECTORY GENERATION FOR UAM VEHICLES
Y. Jung, Korea Aerospace Research Institute, South Korea; S. Cho, Cheongju University, South Korea
12.4Concept Design/MBSE
Chair(s): Stumpf, E.
Track 12 C2.3
07 - Systems, Subsystems and Equipment
15. Sep 26 08:55 09:20 12.4.1
0265		 DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE
P. Thöne¹, F. Abdelmoula¹, M. Gerber², M. Hornby³, N.A. Epps³, A. Winhard², F. Schwerzmann², C. Deiler¹; ¹German Aerospace Center - DLR, Germany ;²Swiss Skylab Foundation, Switzerland ;³NATS, United Kingdom
15. Sep 26 09:20 09:45 12.4.2
0438		 WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH
Z. Milani¹, L. Nichman², E. Matida¹, M. Wolde², A. Brown², A. Benmeddour², M. Mamou², R.S. Martins, ONERA, France; D. Orchard²; ¹Carleton University, Canada ;²National Research Council of Canada, Canada
15. Sep 26 09:45 10:10 12.4.3
0809		 AUTOMATING SYSTEM MODELING USING LARGE LANGUAGE MODELS
I. de Souza Rehder¹, P. Krus, LIU, Brazil; E. Villani¹; ¹ITA, Brazil
Presenter: Emilia Villani, ITA
15. Sep 26 10:10 10:35 12.4.4
0170		 A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-HDBK-1763-COMPLIANT STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES
Q.-V. Pham, Viettel Aeropsace, Vietnam; N.-V. Nguyen¹, V.-T. Nguyen¹, T.-.B. Nguyen¹, P.-M. Nguyen¹; ¹Viettel Aerospace, Vietnam
additional information (interactive) 12.4.R
0322		 SYSTEM EFFECTIVENESS EVALUATION OF CHINA'S AVIATION EMERGENCY COMMUNICATION SYSTEM
L. Zhao¹, W. Cheng¹, G. Wang¹; ¹Aviation Industry Development Research Center of China, China
13.4Architecting , Production and Supply chain
Chair(s): , , Prakasha, P.
Track 13 C2.4
02 - Systems Engineering and Integration
15. Sep 26 08:55 09:20 13.4.1
0336		 VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS
G. Donelli¹, P. Pantelas¹, H. Niemann², C. Özkan², C. Christen ², L. Boggero¹, B. Nagel¹; ¹DLR, Germany ;²Airbus Operation, Germany
15. Sep 26 09:20 09:45 13.4.2
0966		 ENABLING HIGH RATE COMPOSITE MANUFACTURING THROUGH A ROBUST MANUFACTURING DIGITAL ECOSYSTEM
M. Rabiega¹, C. Reynolds¹; ¹The Boeing Company, United States
15. Sep 26 09:45 10:10 13.4.3
0337		 AIRCRAFT AND INDUSTRIAL SYSTEMS CO-ARCHITECTING BASED ON VALUE-DRIVEN MBPLE APPROACH
G. Donelli¹, L. Boggero¹, M. Forlingieri, PTL, Germany; ¹DLR, Germany
14.4UAV Design
Chair(s): Chakraborty, I., Bil, C.
Track 14 C2.5
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 26 08:55 09:20 14.4.1
1012		 DISCRIMINATORY AUTONOMY: OPERATING FASTER, SMARTER, AND WITH PURPOSE
James Garth, BAE SYSTEMS Australia, Australia
15. Sep 26 09:20 09:45 14.4.2
0237		 QUASI-STEADY AERODYNAMIC AND MBD COUPLED FLIGHT SIMULATION OF FOLDING MORPHING UAV
Y.K. Bu¹, L. Qiao¹, L. Li, Chang’an University, China; H.J. Feng¹, J.Q. Bai¹; ¹Northwestern Polytechnical University, China
Presenter: Yikai Bu, Northwestern Polytechnical University
15. Sep 26 09:45 10:10 14.4.3
0845		 A WORKFLOW FOR RAPID DESIGN, SIMULATION, FABRICATION, AND SUBSCALE FLIGHT-TESTING OF NOVEL AIRCRAFT CONCEPTS
I. Chakraborty¹, B. Kunwar¹, S. Putra¹, R. Bhandari¹, C. McCormick¹; ¹Department of Aerospace Engineering, Auburn University, United States
15. Sep 26 10:10 10:35 14.4.4
0929		 SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION
B. Kunwar¹, S. Putra¹, R. Bhandari¹, C. McCormick¹, I. Chakraborty¹; ¹Auburn University, United States
Presenter: Imon Chakraborty, Auburn University
15.4Human Performance, Training, and Communication
Chair(s): Corsi, M.
Track 15 C2.6
10 - Safety and Security
15. Sep 26 08:55 09:20 15.4.1
0059		 FACTORS AFFECTING COMMUNICATION IN AVIATION
B. Molesworth¹, D. Estival¹, L. Chow¹; ¹UNSW, Australia
15. Sep 26 09:20 09:45 15.4.2
0086		 A HUMAN-CENTRIC APPROACH TO UNDERSTANDING THE CONTRIBUTING FACTORS OF PILOT-RELATED RUNWAY INCURSIONS
Y. Yan¹, S. Boufous¹, B.R.C. Molesworth¹; ¹School of Aviation, University of New South Wales, Australia
Presenter: Yan Yan
15. Sep 26 09:45 10:10 15.4.3
0685		 SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES
A. Chappell¹, S. Karunathilake¹, A. Comer¹, P. Saravanan¹; ¹Oklahoma State University, United States
Presenter: Antonio Chappell, Oklahoma State University

10:35 - 11:00COFFEE BREAK

1.5GSA2: Perspectives and Progress on Airliners for 2050+ Energy Landscapes
Chair(s): Mavris, D., Nagel, B.
Track 1 Pyrmont Theatre
15 - Guest lectures
15. Sep 26 11:00 11:25 1.5.1
0992		 ECONOMIC, ENVIRONMENTALLY SUSTAINABLE AVIATION ENERGY
J.I. Hileman, Boeing, United States
15. Sep 26 11:25 11:50 1.5.2
1024		 AIRBUS' PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES
F Haselbach, Airbus, France
15. Sep 26 11:50 12:15 1.5.3
0983		 NASA RESEARCH FOR AIRLINERS OF 2050 AND BEYOND / DLR'S PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES
N. Madavan, NASA, United States; M. Fischer, DLR, Germany
15. Sep 26 12:15 12:40 1.5.4
1031		 PANEL DISCUSSION Q&A WITH THE SPEAKERS
P Panel,
2.5EASN Response to Emerging Challenges in Sustainable and Competitive Aviation
Chair(s): Filippatos, A.
Track 2 C4.1
15 - Guest lectures
15. Sep 26 11:00 11:25 2.5.1
0975		 AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES
A. Filippatos¹, T. Kyriazis¹, S. Pantelakis¹, D. Markatos¹; ¹Department of Mechanical Engineering and Aeronautics, University, Greece
15. Sep 26 11:25 11:50 2.5.2
0976		 CHALLENGES AND BREAKTHROUGHS IN AIR TRANSPORT SYSTEM: VISION FROM EUROPE
G. Alonso-Rodrigo, Universidad Politecnica de Madrid, Spain
15. Sep 26 11:50 12:15 2.5.3
0981		 CURRENT AND ALTERNATIVE PROPULSION SYSTEMS IN EUROPE; TECHNOLOGIES AND THEIR INTEGRATION
O. Isaksson¹, T. Grönstedt¹, S.I. Hallstedt¹, A. Brahma¹, R. Avellan, GKN Aerospace, Sweden; T. Kipouros, Cambridge University, United Kingdom; ¹Chalmers University of Technology, Sweden
15. Sep 26 12:15 12:40 2.5.4
0984		 OVERVIEW OF CRITICAL ISSUES AND OPPORTUNITIES FOR NEW A/C WITH HYBRID AND FULL-ELECTRIC POWERTRAIN
F. Nicolosi¹, M. Di Stasio¹; ¹UNINA, Italy
3.5Propulsion 2
Chair(s): Donelli, P.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 11:00 11:25 3.5.1
0687		 A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION
T.X.Q. Hoang¹, T.A. Pham¹, X.H. Vu¹, H.H. Nguyen¹, C.A. Pham¹, D.L. Chu¹; ¹Viettel Aerospace Institute, Vietnam
15. Sep 26 11:25 11:50 3.5.2
0353		 TOWARDS AN ONTOLOGY-BASED APPROACH FOR DISCIPLINE-SPECIFIC ENGINEERING VIEWS IN ENGINE DESIGN
K. Becker¹, J.P. Haug¹, M. Schuff¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 11:50 12:15 3.5.3
0836		 MIXED-FIDELITY, NONLINEAR AIRCRAFT MISSION MODELING FOR HYBRID REGIONAL AIRCRAFT DESIGN VERIFICATION
D. Ciliberti¹, A. De Marco¹, F. Nicolosi¹; ¹University of Naples Federico II, Italy
15. Sep 26 12:15 12:40 3.5.4
0293		 EFFECT OF ENGINE RESPONSE TIME IN AIRCRAFT CONCEPTUAL DESIGN
A.P.S. Inderawan¹, M. Hoogreef¹; ¹Delft University of Technology, Netherlands
4.5Application of Advanced Propulsion Concepts
Chair(s): ,
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 11:00 11:25 4.5.1
0319		 INTEGRATION OF A SOLID OXIDE FUEL CELL PROPULSION SYSTEM: A TECHNOLOGY DEVELOPMENT GOAL FOR REGIONAL AIRCRAFT
N. Schneiders¹, D. Keller¹, A. Link¹, T. Burschyk¹, G. Atanasov¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 11:25 11:50 4.5.2
0360		 MULTIDISCIPLINARY DESIGN EXPLORATION OF HYBRID-ELECTRIC REGIONAL AIRCRAFT
S. Trepiccione¹, G. Melone¹, F. Nicolosi¹, G. Piscopo, Leonardo, Italy; M. Di Stasio¹; ¹UNINA, Italy
15. Sep 26 11:50 12:15 4.5.3
0673		 EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION
M. Bouchard¹, M. Bashir², D. Rancourt¹, S. Liscouët-Hanke², F. Sirois, Polytechnique Montréal, Canada; S. Lloyd², A. Tfaily³, M. Mark³, R. Freer, Pratt & Whitney Canada, Canada; J. Moriot, Calogy Solutions, Canada; ¹Université de Sherbrooke, Canada ;²Concordia University, Canada ;³Bombardier, Canada
Presenter: David Rancourt, Université de Sherbrooke
15. Sep 26 12:15 12:40 4.5.4
0062		 AERODYNAMIC EFFECTS OF DISTRIBUTED PROPULSION WING CONFIGURATION PARAMETERS
K. Wang¹, Z. Zhou¹, J. Wang¹; ¹Northwestern Polytechnical University, China
Presenter: Jiaxu Wang, Northwestern Polytechnical University
5.5CFD Applications
Chair(s): Marzocca, P., Imamura, T.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 11:00 11:25 5.5.1
0572		 NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE
N. Montella¹, D. Quagliarella¹, L. Iuspa², A. Aprovitola², G. Pezzella², A. Viviani ²; ¹CIRA (Centro Italiano Ricerche Aerospaziali), Italy ;²University of Campania , Italy
15. Sep 26 11:25 11:50 5.5.2
0283		 NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING
H. Mohsin¹, S.A. Prince¹, D. Di Pasquale¹; ¹Cranfield University, United Kingdom
Presenter: Davide Di Pasquale, Cranfield University
15. Sep 26 11:50 12:15 5.5.3
0119		 SIMULATION OF FIFTH-GENERATION HIGH-PERFORMANCE AIRCRAFT USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S. Shahjahan¹, E. Sirak¹, V. Ahuja¹; ¹Siemens Digital Software Industries, United States
15. Sep 26 12:15 12:40 5.5.4
0373		 EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT
H.C. Yang¹, X.K. Ma¹, R.B. Zhu¹, K. You¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China
Presenter: Rongbo Zhu, Northwestern Polytechnical University
additional information (interactive) 5.5.R
0263		 EFFECTS OF FLYING WING CONFIGURATION PARAMETERS ON AERODYNAMICS AND STABILITY
Y. Gao¹, H. Zhao¹, K. Gan¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 5.5.R
0849		 STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS
P.-F. Zhu¹, T.-S. Xie¹, R.-S. Feng¹, S. Zhang¹, C. Zhang¹; ¹Northwestern Polytechnical University, China
6.5Rotor Aerodynamics and Acoustics
Chair(s): Azarpeyvand, M., Jagadeesh, C.
Track 6 C4.5
03.2 - Experimental Aerodynamics
15. Sep 26 11:00 11:25 6.5.1
0828		 PHASE-SPECIFIC SEMI-EMPIRICAL AEROACOUSTIC NOISE MODELING OF A CARGO EVTOL UAV WITH CONSIDERATION OF A SIMPLIFIED URBAN FLYOVER CASE
I. Peleshok¹, M. Hornung¹; ¹Technical University of Munich, Germany
15. Sep 26 11:25 11:50 6.5.2
0743		 STUDY OF THE FEASIBILITY OF ACOUSTIC LINERS INSIDE THE BEAM THAT INTERACTS WITH A UAV DRONE ROTOR
S. Montoya-Ospina¹, R. Gojon¹, H. Parisot-Dupuis¹, F. Simon, DMPE-ONERA, France; ¹ISAE-SUPAERO, France
15. Sep 26 11:50 12:15 6.5.3
0033		 EXPERIMENTAL INVESTIGATION ON THE INNER DUCT SURFACE UNSTEADY PRESSURE OF A DUCTED PROPELLER
J. Li¹, Y. Yendrew¹, D. Moreau¹, C. Doolan¹; ¹University of New South Wales, Australia
7.5Transonic and Supersonic Aerodynamics for Advanced Configurations
Chair(s): Gregg, R.
Track 7 C4.6
03.4 - Applied Aerodynamics
15. Sep 26 11:00 11:25 7.5.1
0223		 AERODYNAMIC TRANSONIC DESIGN OF A STRUT-BRACED WING
D. Losada Costoso¹, O. Atinault¹, M. Meheut¹, G. Starck¹, E. Stragiotti¹, E. Nguyen Van¹; ¹ONERA, France
15. Sep 26 11:25 11:50 7.5.2
0235		 SPARSE POLYNOMIAL CHAOS-BASED ROBUST OPTIMIZATION DESIGN OF AERODYNAMIC AND SONIC BOOM
S.K. Wang¹, H. Zhao¹; ¹Northwestern Polytechnical University, China
15. Sep 26 11:50 12:15 7.5.3
0598		 SUPERSONIC GROUND EFFECT AERODYNAMICS OF A SLENDER BODY
Y.Y. Xun¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China
15. Sep 26 12:15 12:40 7.5.4
0632		 FLOW SOLUTIONS AROUND VON KÁRMÁN OGIVES AT SUPERSONIC SPEEDS USING PHYSICS-INFORMED NEURAL NETWORKS AND PSP
M.A. Escudero¹, B.G. Marinus, Royal Military Academy, Belgium; K. Depuru-Mohan¹; ¹Cranfield University, United Kingdom
8.5Fatigue & Progressive Damage
Chair(s): Marklund, P.O., Denquin, A.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 11:00 11:25 8.5.1
0365		 FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS
H Park¹, D Lee¹, M Seok¹, H Choi¹, Y Kwon¹; ¹Korea Institute of Materials Science, South Korea
15. Sep 26 11:25 11:50 8.5.2
0234		 NEW INSIGHTS INTO AA7085 ENVIRONMENTALLY ASSISTED CRACKING THROUGH HIGH RESOLUTION FRACTOGRAPHY
I. Field¹, J. Rogers, RMIT, Australia; N. Tugwell¹; ¹DSTG, Australia
15. Sep 26 11:50 12:15 8.5.3
0253		 LABORATORY METHOD FOR REPLICATING FASTENER HOLE CORROSION IN AA7085
N. Tugwell¹, M. Salagaras¹, J. Rogers, RMIT, Australia; ¹DSTG, Australia
15. Sep 26 12:15 12:40 8.5.4
1111		 CYCLOSTATIONARY ANALYSIS AND UNSUPERVISED CLUSTERING FOR DETECTING CRACKS IN HELICOPTER GEARBOX CASING
N. Sawalhi, Platforms Division, Defence Science and Technology Group (DSTG),, Australia
9.5Impact & Vibration 2
Chair(s): Ikeda, T., Han, J.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 11:00 11:25 9.5.1
0885		 IMPACT RESISTANCE ENHANCEMENT IN FIBER-REINFORCED COMPOSITES USING CARBON/BASALT HYBRIDIZATION APPROACHES
Z. Sajid¹, T. Rehman¹, A.H. Baluch¹; ¹King Fahd University of Petroleum & Minerals, Saudi Arabia
Presenter: Abrar Ul Haq Khan Baluch, King Fahd University of Petroleum & Minerals
15. Sep 26 11:25 11:50 9.5.2
0724		 VALIDATION OF A LOW-COST DATA ACQUISITION SYSTEM FOR AIRCRAFT VIBRATION TESTING
G. Dessena¹, A. Dell'Edera, Politecnico di Bari, Italy; F.M.A. Mitrotta, University of Bristol, United Kingdom; O.E. Bonilla-Manrique¹; ¹Universidad Carlos III de Madrid, Spain
15. Sep 26 11:50 12:15 9.5.3
1080		 EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROLLED CAVITY FLOW FOR PIEZOELECTRIC ENERGY HARVESTING APPLICATIONS
J. Kirkness¹, N.J. Lawson¹, G. Vio, 2Defence Science and Technology, Australia; ¹University of Sydney, Australia
10.5Hybrid Electric UAVs
Chair(s): Bezos O Connor, G.
Track 10 C4.9
05 - Propulsion and Energy
15. Sep 26 11:00 11:25 10.5.1
0619		 POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS
A. Suti¹, M. Budinger¹, G. Di Rito, Università di Pisa, Italy; A. Reysset¹, I. Hazyuk¹; ¹INSA Toulouse, France
15. Sep 26 11:25 11:50 10.5.2
0882		 TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS
B Van Magill¹, D Verstraete¹; ¹The University of Sydney, Australia
15. Sep 26 11:50 12:15 10.5.3
0597		 IN-FLIGHT LOW-COST THRUST MEASUREMENT SYSTEM FOR SMALL UNMANNED AERIAL VEHICLES
C. Rieger¹, M. Hornung¹; ¹Chair of Aircraft Design, Technical University of Munich, Germany
15. Sep 26 12:15 12:40 10.5.4
0678		 HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION
Hussain Ali Abid¹, Igor SOLNTSEV, GPU Prime LTD, United Kingdom; Andrea RAPISARDA¹, Hassan Ali Abid, King Fahd University of Petroleum and Minerals, Saudi Arabia; Sergey A. Karabasov¹; ¹Queen Mary University of London, United Kingdom
Reserve Paper 10.5.R
0613		 A MODEL PREDICTIVE CONTROL STRATEGY FOR THE ENERGY MANAGEMENT OF HYBRID ELECTRIC PROPULSION SYSTEMS IN FIXED-WING UAVS
A. Suti¹, M. Budinger¹, G. Di Rito, Università di Pisa, Italy; A. Reysset¹, I. Hazyuk¹; ¹INSA Toulouse, France
11.5Machine Learning in Flight Control, Simulation and Modeling
Chair(s): Lee, C.H., Brown, M.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 11:00 11:25 11.5.1
0622		 SYSTEM IDENTIFICATION USING FLIGHT TEST DATA AND MACHINE LEARNING
R Larsson, Saab Aeronautics, Sweden
15. Sep 26 11:25 11:50 11.5.2
0865		 PHYSICS-INFORMED LEARNING-BASED RECOVERY TRAJECTORY PREDICTION FOR AUTOMATIC GROUND COLLISION AVOIDANCE
J. Han¹, S. Kim¹, M. Jung¹, J. Woo¹, H.-S. Kim, APPIA Engineering Co., Ltd., South Korea; H. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea
15. Sep 26 11:50 12:15 11.5.3
0567		 LEARNING-BASED CONTROL ALLOCATION FOR OVER-ACTUATED VTOL AIRCRAFT WITH NONLINEAR DYNAMICS
D. Kim¹, J.D. Lee¹, H. Lee¹, Y. Kim¹, H. Bang¹; ¹KAIST, South Korea
15. Sep 26 12:15 12:40 11.5.4
0664		 RESIDUAL LEARNING FRAMEWORK FOR NONLINEAR AEROELASTIC–FLIGHT-DYNAMICS CONTROL-ORIENTED MODELING OF VERY FLEXIBLE AIRCRAFT
D. Sanghi, United States; C.E.S. Cesnik, United States
additional information (interactive) 11.5.R
0109		 PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE
Z. Wu¹, S. Yang¹, Z. Zhang¹, Y. Qu¹, B. Xiao¹; ¹Northwestern Polytechnical University, China
12.5Electric Aircraft
Chair(s): Viola, N.
Track 12 C2.3
07 - Systems, Subsystems and Equipment
15. Sep 26 11:00 11:25 12.5.1
0093		 A MULTIDIMENSIONAL FRAMEWORK FOR DEMONSTRATION AND V&V CAPABILITIES FOR NEXT-GENERATION FLIGHT CONTROL SYSTEMS
O. Bertram¹, H. Schumann¹, R. Kowalski¹, A. Bagdahn¹; ¹DLR (German Aerospace Center), Germany
15. Sep 26 11:25 11:50 12.5.2
0303		 EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN
A. Testera¹, G. Ferrara¹, F. Di Fede¹, S. Caggese¹, V. Barba¹, G. Accardo¹, R. Pennino¹; ¹Leonardo SpA, Italy
15. Sep 26 11:50 12:15 12.5.3
0557		 HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL RECONFIGURABLE BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT
P. Panchal¹, W. Bliemetsrieder¹, N. Sorokina¹, S. Myschik¹; ¹University of the Bundeswehr Munich, Germany
15. Sep 26 12:15 12:40 12.5.4
0715		 AN EMBEDDED PHYSICS-INFORMED NEURAL NETWORK (PINN) FRAMEWORK FOR HIGH-FIDELITY REAL-TIME SIMULATION OF A FLIGHT CONTROL SURFACE ACTUATION SYSTEM
D.C. Lyu¹, J. Fu¹, S.J. Zhao, Beijing Institute of Precision Mechatronics and Controls, China; Y.Y. Wang¹; ¹Beihang University, China
additional information (interactive) 12.5.R
0561		 POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH
L. Jiang¹, Y. Li¹, S. Bai¹, Z. Li¹, K. Jia¹, Y. Shang¹; ¹Beihang University, China
13.5Aviation & Energy
Chair(s): , , Jouannet, C.
Track 13 C2.4
02 - Systems Engineering and Integration
15. Sep 26 11:00 11:25 13.5.1
0016		 MODEL PREDICTIVE CONTROL OF HYDROGEN–ELECTRIC AIRPORT ENERGY SYSTEMS FOR SUSTAINABLE GROUND OPERATIONS
Y. Chen, University of New South Wales, Australia
15. Sep 26 11:25 11:50 13.5.2
0722		 TOWARDS A SYSTEM-OF-SYSTEMS ENGINEERING ROADMAP FOR INTEGRATING SUSTAINABLE AVIATION FUEL INTO MEXICO’S AIRPORT FUEL INFRASTRUCTURE
L. Gómez Falcón¹, V. Montiel Viruel¹, E. Espinosa-Juárez, Linköping University, Sweden; ¹Universidad Autonoma de Baja California, Mexico
Presenter: Erick Espinoza Juárez, Linköping University
15. Sep 26 11:50 12:15 13.5.3
0957		 ANALYSIS OF SOFTWARE DEVELOPMENT METHODS FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT
W. Bliemetsrieder¹, P. Panchal¹, N. Sorokina¹, S. Diecke, Ingenieurbüro Stephan Diecke, Germany; T. Weyh¹; ¹University of the Bundeswehr Munich, Germany
14.5Propulsion & Control
Chair(s): Yakimenko, O., Bil, C.
Track 14 C2.5
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 26 11:00 11:25 14.5.1
0689		 EXPERIMENTAL CHARACTERIZATION OF PROPELLER-WING INTERACTIONS FOR A SUBSCALE LIFT + CRUISE VTOL UAV
P. Bhandari¹, Z. Atkinson¹, A. Comer¹; ¹Oklahoma State University, United States
15. Sep 26 11:25 11:50 14.5.2
0874		 RAPID FLIGHT DYNAMICS EVALUATION OF STRONGLY COUPLED DISTRIBUTED PROPULSION
Y. Zhu¹, R. Wang¹, Y.H. Xie¹, Z. Zhou¹; ¹Northwestern Polytechnical University, School of Aeronautics, China
Presenter: Yuhang Xie, Northwestern Polytechnical University
15. Sep 26 11:50 12:15 14.5.3
0529		 ENSEMBLE MACHINE LEARNING FOR UAV PROPELLER PERFORMANCE PREDICTION WITH UNCERTAINTY QUANTIFICATION
M.I. Alam¹, A.H. Baluch¹, S.H. Vattathurvalappil¹; ¹King Fahd University of Petroleum and Minerals, Saudi Arabia
15. Sep 26 12:15 12:40 14.5.4
0219		 STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION
C. Galinski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland
Reserve Paper 14.5.R
0404		 TETHERED HOVER FLIGHT TESTS OF BASELINE CONTROL LAWS FOR A TANDEM TILT-WING SUB-SCALE DEMONSTRATOR
D. Milz¹, L. Ott¹, M. May¹; ¹German Aerospace Center (DLR), Germany
15.5Operational Safety Monitoring and Data Analytics
Chair(s): Brito, W.
Track 15 C2.6
10 - Safety and Security
15. Sep 26 11:00 11:25 15.5.1
0038		 ACCELERATING THE LEARNING CURVE: GENERATIVE AI FOR WORKED EXAMPLES IN HUMAN FACTORS ANALYSIS
A. Reisier¹, M.M. Cardoso-Junior¹; ¹Technological Institute of Aeronautics, Brazil
Presenter: Moacyr Cardoso-Junior, Technological Institute of Aeronautics
15. Sep 26 11:25 11:50 15.5.2
0192		 ASSESSING AN ALTERNATE AIRPORT ASSISTANT
J.I. González Cabeza¹, S. Petersen¹, J.-P. Buch¹, D. Niedermeier¹, M. Wies¹, A. Papenfuß¹; ¹DLR e.V., Germany
15. Sep 26 11:50 12:15 15.5.3
0291		 EVALUATION OF METHODS FOR ANOMALY DETECTION IN THE APPROACH PHASE OF OPERATIONAL FLIGHT DATA
R. Hähnel, German Aerospace Centre (DLR), Germany

12:40 - 13:40LUNCH BREAK

1.6GSA2: Regional Airliners: Electrified/H2 Prospects and Demonstrations
Chair(s): Bezos O Connor, G., Schlickenmaier, H.
Track 1 Pyrmont Theatre
15 - Guest lectures
15. Sep 26 13:40 14:05 1.6.1
0993		 AEROSPACE ELECTRIFICATION - DEVELOPMENT AND TEST FOR MORE ELECTRIFIED AIRCRAFT
G. Bezos OConnor, United States
15. Sep 26 14:05 14:30 1.6.2
1102		 BUILDING A TECHNOLOGY PLATFORM FOR THE ELECTRIC AGE
B. Loxton, United States
15. Sep 26 14:30 14:55 1.6.3
1103		 BEYOND 30,000 FEET: GE AEROSPACE AND THE FUTURE OF ELECTRIC FLIGHT
C. Andrews, GE Aerospace, United States
15. Sep 26 14:55 15:20 1.6.4
1104		 PANEL DISCUSSION
P.D. Panel,
2.6X-59 The first Chapter in the QUESST for Quiet Commercial Supersonic Flight
Chair(s): Bahm, C..M., Coen, P.G.
Track 2 C4.1
15 - Guest lectures
15. Sep 26 13:40 14:05 2.6.1
0758		 X-59: THE FIRST CHAPTER IN THE QUESST FOR QUIET COMMERICAL SUPERSONIC FLIGHT
C.M Bahm, NASA, United States
15. Sep 26 14:05 14:30 2.6.2
1007		 X-59: PART 2 BY C.M.BAHM AND P.G.COEN
C. Bahm, United States
15. Sep 26 14:30 14:55 2.6.3
0769		 X-59 EXTERNAL VISION SYSTEM FLIGHT TESTING
R.E. Bailey¹, S.P. Williams¹, J.J. (Trey) Arthur¹, K.S. Kibler¹; ¹NASA, United States
15. Sep 26 14:55 15:20 2.6.4
0839		 X-59 FLIGHT DYNAMICS AND CONTROL
M.J. Boucher, NASA, United States
3.6MDO 1
Chair(s): Nagel, B.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 13:40 14:05 3.6.1
0524		 A SINGLE-LOOP BAYESIAN OPTIMIZATION FRAMEWORK FOR MULTIDISCIPLINARY DESIGN OPTIMIZATION UNDER UNCERTAINTY
B. Wang, The University of Sydney, Australia; D. Lee¹, G. Lee¹; ¹Hanyang University, South Korea
15. Sep 26 14:05 14:30 3.6.2
0088		 MULTIDISCIPLINARY PHYSICS-CONSTRAINED GENERATIVE DESIGN OF DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
W. Wei¹, Y. Ma¹, Z. Han¹; ¹ School of Aeronautics, Northwestern Polytechnical University, China
15. Sep 26 14:30 14:55 3.6.3
0469		 A MIXED-FIDELITY VISCOUS-INVISCID INTERACTION APPROACH FOR WING AERODYNAMIC DESIGN OPTIMIZATION
S.A. Bakhshi¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States
15. Sep 26 14:55 15:20 3.6.4
0747		 RESEARCH ON AN AERODYNAMIC LOAD METHODOLOGY FOR FLAPPING WINGS BASED ON EXPERIMENTALLY ACQUIRED DEFORMATION
K.R. Yang¹, B.F. Song¹, D. Xue¹; ¹Northwestern Polytechnical University, China
4.6UAVs and Advanced Air Mobility
Chair(s): Kanazaki, M.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 13:40 14:05 4.6.1
0636		 ENDURANCE EVALUATION OF DIFFERENT UAV CONFIGURATIONS AND POWERTRAIN ARCHITECTURES
A. Orgiu, ISAE-SUPAERO, Concordia University, Canada; S. Delbecq, ISAE-SUPAERO, France; J. Liscouët, Concordia University, Canada
15. Sep 26 14:05 14:30 4.6.2
0801		 COMMON RESEARCH MODELS FOR SMALL UNCREWED AERIAL VEHICLES
J. Rasines Mazo¹, B. Van Magill¹, D. Verstraete¹; ¹The University of Sydney, Australia
Presenter: Dries Verstraete, The University of Sydney
15. Sep 26 14:30 14:55 4.6.3
0594		 DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE
P.P. Kapoor¹, R.S. Pant, IIT Bombay, India; M. Abdelrahman¹, D. Mohd-Nasir, University of Sheffield, United Kingdom; M.S. Ismail¹; ¹University of Hull, United Kingdom
15. Sep 26 14:55 15:20 4.6.4
0331		 FLIGHT OPERATIONS AND TESTING OF A 450 KG EXPERIMENTAL GYROPLANE UAV
I. Pruter¹, G. Schmitz¹, H. Duda¹, M. Laubner¹, S. Lorenz¹; ¹DLR e.V., Germany
Presenter: Gregor Schmitz, DLR e.V.
5.6Turbulence Modeling
Chair(s): Coder, J., Viviani, A.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 13:40 14:05 5.6.1
0112		 DATA-DRIVEN TURBULENCE MODELING FOR MULTI-MECHANISM SEPARATED FLOWS OVER ICED AIRFOILS
Z.Z. He¹, Y.F. Zhang¹; ¹Tsinghua University, China
15. Sep 26 14:05 14:30 5.6.2
0785		 NUMERICAL INVESTIGATION OF GUST LOAD ALLEVIATION FOR WINGS WITH PASSIVELY RELEASED FFWT
T. Chen¹, Z. Zeng¹, Y. Zhao¹, J. He¹, Y. Yang¹; ¹NorthWestern Polytechnical University, China
15. Sep 26 14:30 14:55 5.6.3
0054		 CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER
J. Fernández¹, R. Bardera¹, J.C. Matías¹, E. Barroso¹, A.A. Rodríguez-Sevillano, Universidad Politécnica de Madrid, Spain; ¹Instituto Nacional de Técnica Aeroespacial, Spain
additional information (interactive) 5.6.R
0634		 MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELING
P. Kovar, Czech Technical University in Prague, Czech Republic; J. Fürst, Czech Technical University,, Czech Republic; G. Frulla¹, G.M. Di Cicca¹, E. Cestino¹; ¹Polytechnic University of Turin, Italy
6.6Flow interactions and integration
Chair(s): , , Lawson, N.
Track 6 C4.5
03.2 - Experimental Aerodynamics
15. Sep 26 13:40 14:05 6.6.1
0705		 MIDAS: A MODULAR SOFTWARE FOR INTAKE FLOW DISTORTION ANALYSIS
T. Piovesan¹, A. Giannouloudis¹, J. Hueso Rebassa¹, M. Migliorini¹, P. Zachos¹, D. MacManus¹; ¹Cranfield University, United Kingdom
Presenter: Josep Hueso Rebassa, Cranfield University
15. Sep 26 14:05 14:30 6.6.2
0970		 EXPERIMENTAL STUDY OF GROUND EFFECT ON A HEAVING NACA0012 AEROFOIL
M. Li¹, M.A. Legovich, Cranfield University, United Kingdom; N.J. Lawson¹; ¹The University of Sydney, Australia
15. Sep 26 14:30 14:55 6.6.3
0218		 LOW-SPEED EXPERIMENTAL INVESTIGATION OF PODDED ENGINE INTEGRATION OF FLYING V AIRCRAFT
A. Kumar¹, R. Vos¹; ¹Delft University of Technology, Netherlands
15. Sep 26 14:55 15:20 6.6.4
0804		 TOROIDAL RECIRCULATION, SADDLE-POINT TOPOLOGY, AND WALL-JET OUTWASH IN A TWIN-ROTOR SYSTEM IN GROUND EFFECT
N. Pradyumna¹, M. Li¹, D. Verstraete¹; ¹The University of Sydney, Australia
7.6Unsteady and Bio-Inspired Aerodynamics
Chair(s): Jagadeesh, C.
Track 7 C4.6
03.4 - Applied Aerodynamics
15. Sep 26 13:40 14:05 7.6.1
0542		 AERODYNAMIC EFFECT OF PITCHING MOTION FOR FLAPPING AIRFOIL ACROSS DIFFERENT SWEEPING TRAJECTORIES
Y.C. Liu, China; B. Song, China; L. Zhou, China
15. Sep 26 14:05 14:30 7.6.2
0665		 AERODYNAMIC OPTIMISATION OF BIOINSPIRED CORRUGATED WINGS FOR HIGH-EFFICIENCY MAV GLIDING
M. Krasniqi¹, S.F. Armanini¹; ¹Imperial College London, United Kingdom
15. Sep 26 14:30 14:55 7.6.3
0777		 AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK
H.-H. Yang¹, S.-G. Lee¹, E.-H. Lee¹, H.-S. Ko¹, J.-H. Han¹; ¹Korea Advanced Institude of Science and Technology, South Korea
Presenter: Jae-Hung Han, Korea Advanced Institude of Science and Technology
15. Sep 26 14:55 15:20 7.6.4
0916		 THREE-DIMENSIONAL FLOW STRUCTURES OVER A LOW-ASPECT-RATIO PLUNGING WING
B. Anilir¹, D.F. Kurtulus¹, M.F. Platzer, University of California, Davis, United States; ¹Middle East Technical University, Turkey
Reserve Paper 7.6.R
0184		 AERODYNAMIC PERFORMANCE ANALYSIS OF A NOVEL LIFT-THRUST INTEGRATED ROTARY FLAPPING AERIAL VEHICLE
J. Liu¹, W. Yang¹, Y. Guo¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 7.6.R
0147		 STUDY ON AERODYNAMICS OF THE WING WITH FLAP INSPIRED FROM BIRD COVERTS
X. Xu¹, W. Yang¹, J. Xuan¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 7.6.R
0182		 INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATIONS
S.S. Cao¹, W.Q. Yang¹, Y.G. Zhang¹, X.L. Xu¹; ¹Northwestern Polytechnical University, China
8.6Fuselage Structures
Chair(s): Marklund, P.O.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 13:40 14:05 8.6.1
0115		 COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT
Y.C. Roth, Airtbus Operations GmbH, Germany; P. Joern, Airbus Operations GmbH, Germany; A. Sadelfeld, Airbus Aerostructures GmbH, Germany; C. Rowedder, CTC GmbH, Germany; J. Buck, CTC GmbH, Germany; B. Demel, Airbus Helicopters Deutschland GmbH, Germany
15. Sep 26 14:05 14:30 8.6.2
0830		 FIVE DEACADES OF T-38 WING TEARDOWNS: DATA, INSIGHT, AND IMPACT
T. Moran¹, I. Grothe¹, C. King, United States Air Force, United States; L. Hunt¹, P. Clark¹; ¹Southwest Research Institute, United States
15. Sep 26 14:30 14:55 8.6.3
0071		 GEOMETRICALLY EXACT MODEL OF CANTILEVER BEAM UNDERGOING LARGE DEFLECTION AND LINEARIZED DYNAMICS CHARACTERIZATION
C.Y. Yang¹, R. Zhao¹, Y.S. Gu¹, Z.C. Yang¹; ¹Northwestern Polytechnical University School of Aeronautics, China
Presenter: Changyun Yang, School of Aeronautics, Northwestern Polytechnical University
15. Sep 26 14:55 15:20 8.6.4
0640		 TRACING MATERIAL PROPERTIES TO SYSTEM-LEVEL PERFORMANCE: A NORMALISED SENSITIVITY ANALYSIS FOR A BOEING 737-CLASS AIRCRAFT
S. Stekovic¹, P. Krus¹; ¹Linköping University, Sweden
9.6Testing & Demonstrator
Chair(s): Tsushima, N., Priasso, V.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 13:40 14:05 9.6.1
0157		 A FULL-SCALE DEMONSTRATOR FOR RAPID TESTING OF HELICOPTER AIRFRAMES USING ADVANCED CONTROL SYSTEM METHODOLOGIES
G. Swanton¹, A. Manning¹, B. Evans¹, M. Chipper, RMIT University, Australia; ¹Defence Science and Technology Group, Australia
15. Sep 26 14:05 14:30 9.6.2
0014		 WIND TUNNEL TESTING OF WHIRL FLUTTER AEROELASTIC DEMONSTRATOR
J. Cecrdle¹, O. Vich¹, P. Malinek¹, R. Kulhanek¹; ¹VZLU AEROSPACE, Czech Republic
15. Sep 26 14:30 14:55 9.6.3
0852		 EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL
N. Kishimoto¹, R. Sakata¹, Y. Iwami², N. Tomita², M. Tamayama, JAXA, Japan; Y. Tanahashi³, T. Ikeda³; ¹Kwansei Gakuin University, Japan ;²Yamashina Institute for Ornithology, Japan ;³Chubu University, Japan
15. Sep 26 14:55 15:20 9.6.4
0680		 AN INVESTIGATION OF SAFETY-CRITICAL GROUND INTERFACE (TAKEOFF, LANDING) REGIME RECOGNITION FOR AUTOMATED AND AUTONOMOUS VERTICAL LIFT AIRCRAFT MISSION TASK DESIGN
M. Alexander, National Research Council of Canada/Flight Research Laboratory , Canada
10.6Supersonic
Chair(s): Lee, B.
Track 10 C4.9
05 - Propulsion and Energy
15. Sep 26 13:40 14:05 10.6.1
0788		 NUMERICAL INVESTIGATION OF GEOMETRIC EFFECTS ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES
Y. Wu¹, L. Zhou¹, J. Shi¹, Y. Meng¹, Z. Wang¹; ¹Northwestern Polytechnical University, China
15. Sep 26 14:05 14:30 10.6.2
0207		 COMPARATIVE ASSESSMENT OF PROPULSION SYSTEM ARCHITECTURES TAILORED FOR SUPERSONIC APPLICATIONS
L. Carrea¹, K. Kyprianidis¹; ¹Mälardalen University, Sweden
15. Sep 26 14:30 14:55 10.6.3
0418		 SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET
H. Miki¹, J. Akatsuka¹, R. Nimura, Tokyo University of Agriculture and Technology, Japan; ¹JAXA, Japan
15. Sep 26 14:55 15:20 10.6.4
0510		 NUMERICAL STUDY OF UNSTEADY DISTORTION IN AN S-DUCT INTAKE SUBJECTED TO BLAST SHOCK WAVES
L.L. Shi¹, Y. Fan¹, B.G. Mi¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 10.6.R
0341		 STRUCTURAL DESIGN AND PERFORMANCE STUDY OF A TWO-STAGE DYNAMIC PRESSURE OIL-AIR SEPARATOR
S. Li¹, J.P. Hu¹, J. Wang¹, Y.P. Li¹, Y.B. Wang, China; ¹Northwestern Polytechnical University School of Power and Energy, China
11.6Optimization
Chair(s): Matsuno, Y., Alaimo, A.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 13:40 14:05 11.6.1
0099		 A HYBRID CNN-LSTM AND PSEUDOSPECTRAL METHOD FOR RAPID SPACECRAFT REENTRY OPTIMIZATION
Y.-X. Yang¹, Z. Xu¹; ¹Northwestern Polytechnical University, China
15. Sep 26 14:05 14:30 11.6.2
0505		 OPTIMAL GUIDANCE ALGORITHM FOR BOOST-BACK OF REUSABLE LAUNCH VEHICLES
J. Shim¹, J.-I. Jang¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea
15. Sep 26 14:30 14:55 11.6.3
0224		 AIRSPACE CAPACITY IMPLICATIONS OF CONTRAIL-AWARE TRAJECTORY OPTIMIZATION
A. Lemetti¹, T. Polishchuk¹, L. Smetanova¹; ¹LiU, Sweden
15. Sep 26 14:55 15:20 11.6.4
0377		 TRIM PERFORMANCE EXPLORATION FOR AN AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION AND A TAIL THRUST UNIT
G. Fernandes Lourenço¹, C. Varriale¹; ¹Delft University of Technology, Netherlands
12.6Thermal
Chair(s): Stumpf, E.
Track 12 C2.3
07 - Systems, Subsystems and Equipment
15. Sep 26 13:40 14:05 12.6.1
0030		 DESIGN AND OPERATION OF LOW-COST MULTI-SCALE TEST BEDS FOR BATTERY THERMAL RUNAWAY INITIATION AND PROPAGATION
W. Mooney¹, M. Gendron, Calogy Solutions, Canada; X. Arcand¹, D. Francoeur¹, D. Rancourt¹; ¹Université de Sherbrooke, Canada
15. Sep 26 14:05 14:30 12.6.2
0663		 MODAL-BASED FUEL LEVEL ESTIMATION OF CRYOGENIC PROPELLANT TANKS
S. Pfeifer¹, F. Thilker¹, A. Tramposch¹, A. Buchroithner, University of Technology, Austria; ¹FH JOANNEUM, Austria
15. Sep 26 14:30 14:55 12.6.3
0807		 SIZING OF LINEAR ACTUATORS FOR SPAN EXTENSION OF HALE UAV
T. Prakash, Larsen and Toubro, India; R.S. Pant, Indian Institute of Technology Bombay, India
Presenter: Tanvi Prakash, Larsen and Toubro
15. Sep 26 14:55 15:20 12.6.4
0593		 PREDICTION OF MINIMUM STARTING PRESSURE FOR HYDROSTATIC HELICAL ROTARY ACTUATOR USING PHYSICS-INFORMED NEURAL NETWORKS
S.Y. Chen¹, J. Fu¹, K. Ci¹, H.Z. Song, Beijing Institute of Precision Mechatronics and Controls, China; Z.L. Li¹, D.C. Lyu¹; ¹Beihang University, China
additional information (interactive) 12.6.R
0483		 HIGH-PRECISION EDDY-CURRENT TIP CLEARANCE SENSOR WITHEXCEPTIONALHEAT RESISTANCE
F.L. Liu¹, L.Q. Zhao¹, Y.G. Lyu¹, B.S. Chang¹, Z.X. Liu¹; ¹Northwestern Polytechnical University, China
Presenter: Fulin Liu
13.6Air Traffic Operational Safety
Chair(s): New Tze How, D.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
15. Sep 26 13:40 14:05 13.6.1
0863		 APPROPRIATE ATC GO-AROUND INSTRUCTION TIMING TO PREVENT RUNWAY COLLISIONS
S. Kontani¹, R. Mori¹; ¹Kobe University, Japan
15. Sep 26 14:05 14:30 13.6.2
0568		 VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS
J. Meier¹, M.-M. Temme¹, R. Hunger¹, S. Shetty¹, M. Hagl¹, O. Ohneiser¹, M. Finke¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 14:30 14:55 13.6.3
0178		 FLIGHT CENTRIC ATC – HOW TO SOLVE CONFLICTS WITHOUT COMMUNICATION AND COORDINATION OVERLOADS?
T. Finck¹, V. Bottino¹, M. Weber¹, B. Korn¹; ¹German Aerospace Center, Germany
15. Sep 26 14:55 15:20 13.6.4
0811		 AUGMENTED REALITY SAFETY NETS FOR INCREASED AIRPORT SAFETY
S. Bagassi¹, T. Fadda¹; ¹University of Bologna, Italy
14.6Swarm Control
Chair(s): Mwasandube, M., Palmer, J.
Track 14 C2.5
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 26 13:40 14:05 14.6.1
0670		 AN AUTONOMY ARCHITECTURE FOR COLLABORATIVE UAV SWARMS - A BOTTOM-UP PERSPECTIVE
P. Nagarajan¹, S. Schopferer¹, K. Thomessen¹; ¹German Aerospace Center (DLR), Germany
Presenter: Karolin Thomessen, German Aerospace Center (DLR)
15. Sep 26 14:05 14:30 14.6.2
0167		 SOFTWARE-IN-THE-LOOP SIMULATION OF DISTRIBUTED 3D INTEGRATED SWARM GUIDANCE FOR FIXED-WING UAVS
Y.C. Yang¹, J.H. Jeong, Hanseo University, South Korea; S.K. Kim¹, J.Y. Suk¹; ¹Chungnam National University, South Korea
Presenter: Yechan Yang, Chungnam National University
15. Sep 26 14:30 14:55 14.6.3
0765		 REINFORCEMENT LEARNING-BASED ADAPTIVE WEIGHTING OF SWARM GUIDANCE LAWS FOR SMALL FIXED-WING UAVS
C. Kang¹, J. Jeong¹; ¹Hanseo University, South Korea
15. Sep 26 14:55 15:20 14.6.4
0735		 2D AND 3D TRAJECTORY PLANNING FOR UAVS FORMATION SYSTEM USING DYNAMIC WINDOW APPROACH
R.B. Zhu¹, K. You¹, H.C. Yang¹, X.K. Ma¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 14.6.R
0037		 ADAPTIVE PRACTICAL PRESCRIBED-TIME FAULT-TOLERANT CONTROL FOR SMALL TANDEM-ROTOR UAV FORMATIONS
X.L. Li¹, C.Q. Wang¹, Y. Guo¹, A.J. Li¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 14.6.R
0098		 PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION
J. Fang¹, Y. Guo¹, A. Li¹, C. Wang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 14.6.R
0531		 RESEARCH ON OFFENSIVE AUTONOMOUS VEHICLE TRAJECTORY PREDICTION METHOD BASED ON IMPROVED INVERSE REINFORCEMENT LEARNING IN AIRCRAFT ACTIVE DEFENSE MODE
H. Zhang¹, J.N Liu¹, Z. Xu¹, Y.X. Yang¹; ¹School of Astronautics, Northwestern Polytechnical University, China
15.6Safety, Environment, and Hazard Mitigation
Chair(s): Schuchard, B.
Track 15 C2.6
10 - Safety and Security
15. Sep 26 13:40 14:05 15.6.1
0041		 A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC AND CANADIAN NRC COLLABORATION.
J. Armstrong¹, O.M. Ozcakir¹, L.L. Waite¹, T. Austin¹, C.A. Pepper¹, A. Tvaryanas², H. Uyhelji², S. Gearhart, US CDC, United States; P. Lebbin, Canadian NRC, Canada; I.S. Koolhof¹; ¹Boeing, Australia ;²FAA, United States
15. Sep 26 14:05 14:30 15.6.2
0439		 EARLY WARNING FOR POTENTIAL BIRD STRIKES: STRATEGIC OPTIMIZATION OF PAN-TILT-ZOOM SENSOR NETWORKS FOR BIRD HAZARD DECREASE IN AIRPORT ENVIRONMENT
Y.H. Mei¹, Z.H. Wang¹; ¹The university of Sydney, Australia
15. Sep 26 14:30 14:55 15.6.3
0457		 TEMPORAL INJECTION FOR REAL-TIME FLYING-BIRD DETECTION WITH RT-DETR
J. Gao¹, T.Q. Wang, Taiyuan University of Technology, China; H. Gao¹, Y. Ding¹, Z. Wan¹; ¹ University of Sydney, Australia

15:20 - 15:25CHANGEOVER BREAK

0.6GENERAL LECTURE 3 X59 Low Boom Demonstrator by Walt Silva
Chair: C. Bil ICAS EC Member
15. Sep 26 15:25 16:15

16:15 - 16:40AFTERNOON BREAK

1.7GSA2: Future Sustainable Aviation Infrastructure: Prospects and Challenges
Chair(s): Gerhards, R., Hileman, J.
Track 1 Pyrmont Theatre
15 - Guest lectures
15. Sep 26 16:40 17:05 1.7.1
1089		 MODERNISING AT SCALE: DELIVERING AUSTRALIA’S NEXT-GENERATION AIR TRAFFIC SYSTEM
R. Sharp, Airservices Australia, Australia; J. Connolly, THALES, Australia
15. Sep 26 17:05 17:30 1.7.2
0985		 JET ZERO: ATJ SAF PROJECT DEVELOPER
J Mason, Jet Zero Australia, Australia
15. Sep 26 17:30 17:55 1.7.3
1027		 FUTURE SUSTAINABLE AVIATION INFRASTRUCTURE: PROSPECTS & CHALLENGES FROM CHRISTCHURCH AIRPORT'S PERSPECTIVE
C Waghorn, Christchurch International Airport, New Zealand
15. Sep 26 17:55 18:20 1.7.4
1032		 PANEL DISCUSSION Q&A WITH THE SPEAKERS
P Panel,
2.7GARTEUR 1
Chair(s): Hammer, B.
Track 2 C4.1
15 - Guest lectures
15. Sep 26 16:40 17:05 2.7.1
1101		 GARTEUR: FRAMEWORK, ORGANIZATION AND COLLABORATIVE RESEARCH
B. Hammer, Germany
15. Sep 26 17:05 17:30 2.7.2
0989		 THE GARTEUR GROUP OF RESPONSABLES IN AERODYNAMICS (GOR AD) AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES
M. Tormalm, Sweden
15. Sep 26 17:30 17:55 2.7.3
0996		 GARTEUR AG59 IMOLA: IMPROVING THE MODELLING OF LAMINAR SEPARATION BUBBLES
P. Catalano, C.I.R.A., Italy
15. Sep 26 17:55 18:20 2.7.4
1011		 GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION
E. Andrés Pérez¹, D. Quagliarella, CIRA, Italy; D. Hines Chaves², P. Bekemeyer², T. Taddei, Sapienza University of Rome, Italy; J. Peter, Onera, France; O. Amoignon, FOI, Sweden; A. Alaia³, A. Scardigli³, R. Castellanos, UC3M, Spain; J. Nieto-Centenero¹; ¹INTA, Spain ;²DLR, Germany ;³OPTIMAD/ESTECO, Italy
3.7MDO 2
Chair(s): Bagassi, S., Abu Salem, K.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 16:40 17:05 3.7.1
0305		 LINKING PRODUCT FAMILY ARCHITECTURE ANALYSIS AND COMPONENT-LEVEL OPTIMISATION USING SYSTEM MODELS
F.H. Christiansen¹, M.C. Berschik¹, S. Wehrend¹, D. Krause¹; ¹Hamburg Univeristy of Technology, TUHH, Germany
15. Sep 26 17:05 17:30 3.7.2
0445		 COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS
J.L.C. Chan¹, D. Pasquale¹, W. Widjaja¹, S. Lyu¹, J. Rispin¹, H. Smith¹; ¹Cranfield University, United Kingdom
15. Sep 26 17:30 17:55 3.7.3
0278		 DEEP LEARNING-BASED INVERSION OF NEAR-FIELD OVERPRESSURE SIGNATURES FOR LOW-BOOM SUPERSONIC TRANSPORT
Y.-H. Peng¹, K.-S. Zhang¹, Q. Chen¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China
Presenter: Yuhuan Peng, Northwestern Polytechnical University
15. Sep 26 17:55 18:20 3.7.4
0876		 AN INCREMENTAL MODULAR MDO FRAMEWORK FOR HYDROGEN-ELECTRIC POWERTRAIN SIZING AND INTEGRATION IN GENERAL AVIATION AIRCRAFT
P. Moreno-Escolastico¹, M. Raiola¹, R. Castellanos¹, A. Cini¹; ¹Universidad Carlos III de Madrid, Spain
4.7Optimization in Design
Chair(s): Melkert, J.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 16:40 17:05 4.7.1
0416		 A MULTI-SCALE COMPUTATIONAL FRAMEWORK FOR EVALUATING TECHNOLOGY IMPACTS ON FUTURE AIRCRAFT FLEETS
E. Cassidy¹, A. Garcia, Collins Aerospace, France; G. Cinar¹; ¹University of Michigan, United States
15. Sep 26 17:05 17:30 4.7.2
0783		 COST-DRIVER MULTIDISCIPLINARY FRAMEWORK FOR WINGLET DESIGN: A REGIONAL AIRCRAFT CASE STUDY
L. Falcone¹, S. Corcione¹, F. Nicolosi¹, S. Trepiccione¹; ¹University of Naples Federico II, Italy
15. Sep 26 17:30 17:55 4.7.3
0703		 TOP-LEVEL AIRCRAFT REQUIREMENT TRADE STUDIES FOR HYDROGEN FUEL CELL REGIONAL AIRCRAFT
M. Di Stasio¹, F. Nicolosi¹; ¹UNINA, Italy
15. Sep 26 17:55 18:20 4.7.4
0696		 MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY
G. Shen¹, X. Zhang¹, W. Hao¹, Z. Wang¹; ¹Northwestern Polytechnical University, China
5.7Aeroacoustics and Noise Predictions
Chair(s): Thomber, B., Lawson, N.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 16:40 17:05 5.7.1
0488		 THE NUMERICAL SIMULATIONS OF THE ACOUSTIC SHIELDING EFFECTS ON THE BLADE-VORTEX INTERACTION NOISE OF THE HART-II MODEL
T. Ikeda¹, K. Yasue¹, M. Kanayama, Ryoyu Systems, Japan; ¹JAXA, Japan
15. Sep 26 17:05 17:30 5.7.2
0569		 NOISE-OPTIMIZED HOVER PROPELLER DESIGN FOR VTOL CARGO DRONES IN TRANSIENT FLIGHT CONDITIONS
T. Moses¹, M. Hornung¹; ¹Technical University of Munich, Germany
15. Sep 26 17:30 17:55 5.7.3
0693		 HIGH-FIDELITY AEROACOUSTIC AND UNSTEADY FLOW ANALYSIS OF WIND TURBINE BLADES
Hassan Ali Abid, King Fahd University of Petroleum and Minerals, Saudi Arabia
15. Sep 26 17:55 18:20 5.7.4
0923		 PRACTICAL ASPECTS OF ROTOR AERODYNAMIC AND AEROACOUSTIC DESIGN OPTIMIZATION
W. Klimczyk, Lukasiewicz Research Network - Institute of Aviation, Poland
6.7Morphing and Shape Adaptation
Chair(s): Imamura, T., Allen, N.
Track 6 C4.5
03.2 - Experimental Aerodynamics
15. Sep 26 16:40 17:05 6.7.1
0730		 EXPERIMENTAL STUDY OF LOAD ALLEVIATION WITH PASSIVE ADAPTIVE CAMBER AIRFOILS
A. Sumi¹, S. Otomo¹, H. Nishida¹; ¹Tokyo University of Agriculture and Technology, Japan
15. Sep 26 17:05 17:30 6.7.2
0789		 EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY
M. Marciniuk¹, M. Szumski², Z. Szczerba², L. Kiszkowiak³, L. Malicki¹, P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; K. Sibilski, Air Force Institute of Technology, Poland; S. Kachel³; ¹Wroclaw University of Science and Technology, Poland ;²Rzeszow University of Technology, Poland ;³Military University of Technology, Poland
Presenter: Łukasz Kiszkowiak, Military University of Technology
15. Sep 26 17:30 17:55 6.7.3
0347		 AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC
X. Delon¹, J. Abou Khalil, ONERA - Toulouse, France; N. Maynard², A. Marouf¹, R. El Akoury³, Y. Hoarau¹, C. Doll, Onera - Toulouse, France; J.-F. Rouchon², M. Braza³; ¹ICUBE - Strasbourg, France ;²LAPLACE - Toulouse, France ;³IMFT - Toulouse, France
15. Sep 26 17:55 18:20 6.7.4
0517		 EFFECT OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS
Y. Tanhashi¹, F. Sakai¹, S. Nishizuka¹, T. Ikeda¹, N. Kishimoto, Kwansei Gakuin University, Japan; M. Tamayama, Japan Aerospace Exploration Agency, Japan; Y. Iwami², N. Tomita²; ¹Chubu University, Japan ;²Yamashina Institute for Ornithology, Japan
7.7Data-Driven Design, Optimization and Reduced-Order Modeling
Chair(s): Gregg, R.
Track 7 C4.6
03.4 - Applied Aerodynamics
15. Sep 26 16:40 17:05 7.7.1
0358		 A GRAPH NEURAL NETWORK SIMULATOR FOR TRANSONIC VORTEX-DOMINATED FLOWS ON THE DLR-F23 CONFIGURATION
A. Goerttler¹, D. Hines¹, A. Wagner¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 17:05 17:30 7.7.2
0502		 SUPERVISED DIMENSIONALITY-REDUCED MULTI-FIDELITY SURROGATE MODEL ASSISTED HIGH-DIMENSIONAL NATURAL LAMINAR FLOW OPTIMIZATION
Y. Gan¹, H. Zhao¹, S. Wang¹; ¹Northwestern Polytechnical University, China
Presenter: Shekun Wang, Northwestern Polytechnical University
15. Sep 26 17:30 17:55 7.7.3
0546		 AIRFOIL DESIGN OPTIMIZATION FOR HIGH-LIFT AND HIGH-EFFICIENCY APPLICATIONS USING DEEP REINFORCEMENT LEARNING
P. Scavella¹, G. Paolillo¹, C.S. Greco¹; ¹University Of Naples Federico II, Italy
Presenter: Gerardo Paolillo, UNIVERSITY OF NAPLES FEDERICO II
15. Sep 26 17:55 18:20 7.7.4
0767		 UNSTEADY AERODYNAMIC OPTIMIZATION OF A THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH THE LEVEL SET METHOD
D. Sasaki¹, C. Yuma¹, Y. Kawamoto¹, M. Okamoto, Kanazawa Institute of Technology, Japan; H. Nagai, Institute of Fluid Science, Tohoku University, Japan; ¹Osaka Metropolitan University, Japan
Reserve Paper 7.7.R
0473		 MULTI-SCALE LINEAR FEATURE MODULATION DEEP NEURAL OPERATOR FOR RAPID PRESSURE COEFFICIENT PREDICTION
W.-F. Zhang¹, H. Zhao¹, S.-K. Wang¹; ¹Northwestern Polytechnical University, China
Presenter: She-Kun Wang, Northwestern Polytechnical University
8.7Non Destructive Testing [NDT] & Structural Trials
Chair(s): Marklund, P.O.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 16:40 17:05 8.7.1
0313		 ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS
A. Gliszczynski, Lodz University of Technology, Poland; R. Degenhardt¹, F. Franzoni¹, T.D. Baciu, PFH, Germany; ¹DLR, Germany
Presenter: Adrian Gliszczynski, Lodz University of Technology
15. Sep 26 17:05 17:30 8.7.2
0861		 ULTRASONIC NON-DESTRUCTIVE TESTING: SYSTEM SELECTION FOR CHARACTERISATION AND DETECTION OF DEFECTS IN REPAIRED COMPOSITE MATERIALS
H.R. Spratling¹, M.E. Ibrahim¹; ¹Defence Science and Technology Group, Australia
15. Sep 26 17:30 17:55 8.7.3
0127		 EXPERIMENTAL INVESTIGATION OF FRETTING WEAR IN TI-6AL-4V DOVETAIL ASSEMBLIES UNDER RESONANT VIBRATION
X. Zhang¹, D. Wei¹, S. Yang¹; ¹Beihang University School of Energy and Power Engineering, China
15. Sep 26 17:55 18:20 8.7.4
0776		 EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA
J. Heo¹, J. Lee¹, A.-A. Reynolds¹, J. Cho¹, J.-H. Han¹; ¹KAIST, South Korea
9.7Composite Structure
Chair(s): Ikeda, T., Falzon, B.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 16:40 17:05 9.7.1
0355		 COMBINED TOPOLOGY AND COMPOSITE LAMINATE OPTIMIZATION OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT
L. Vertonghen¹, C. Mollet, DAAA, ONERA, Institut Polytechnique de Paris, France; C. Julien¹, F.-X. Irisarri¹; ¹DMAS, ONERA, Université Paris-Saclay, France
15. Sep 26 17:05 17:30 9.7.2
0614		 OPTIMIZATION APPROACHES FOR THE SHEAR-POSTBUCKLING DESIGN OF THERMOPLASTIC THIN-PLY COMPOSITE SHELLS IN HELICOPTERS
M. Mauersberger¹, J. Rehfeldt¹, F. Hähnel¹, J. Markmiller¹; ¹Dresden University of Technology (TUD), Germany
15. Sep 26 17:30 17:55 9.7.3
0948		 AN AUTOMATED PARAMETRIC FRAMEWORK FOR EARLY-STAGE STRUCTURAL DESIGN AND OPTIMIZATION OF COMPOSITE AIRFRAMES
N. Ziakos, Spain; A. Cini, Spain
15. Sep 26 17:55 18:20 9.7.4
0853		 CURVATURE-CONTROLLED MORPHING OF FOLDING WINGTIPS USING HONEYCOMB PLATES
R. Yang¹, S. Li¹, S. Sun ¹; ¹School of Mechanical Engineering Dalian University of Technology, China
10.7Hypersonic
Chair(s): Lee, B.
Track 10 C4.9
05 - Propulsion and Energy
15. Sep 26 16:40 17:05 10.7.1
0370		 PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN
K. Tsukuda¹, H. Kato¹, D. Sasaki¹, C. Fujio², S. Takahashi², T. Isono², M. Koga², M. Takegoshi²; ¹Osaka Metropolitan University, Japan ;²Japan Aerospace Exploration Agency, Japan
15. Sep 26 17:05 17:30 10.7.2
0504		 NUMERICAL PREDICTION AND EXPERIMENTAL VALIDATION ON THRUST PERFORMANCE OF SCRAMJET EXTERNAL NOZZLES
T. Isono, Japan Aerospace Exploration Agency, Japan
15. Sep 26 17:30 17:55 10.7.3
0508		 HYBRID ROCKET HOT-GAS DRIVER FOR DIRECT-CONNECT SCRAMJET THERMO-STRUCTURAL SCREENING
A. Roco¹, H. Chisholm, Advanced Composite Structures Australia, Australia; D. Hartley¹; ¹Defence Science and Technology Group, Australia
Presenter: Alison Roco
11.7Flight Control System Simulation
Chair(s): Rogalski, T., Che, J.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 16:40 17:05 11.7.1
0125		 PILOT-IN-THE-LOOP SIMULATION OF OPTIMAL DEEP-STALL RECOVERY FOR T-TAIL AIRLINER
K. Yoshioka¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan
15. Sep 26 17:05 17:30 11.7.2
0662		 A SIMULATION STUDY ON THE EFFECT OF EXTENDED ROTATIONAL KINEMATICS IN HEXAPOD MOTION SIMULATORS
T. Bernhofer¹, A. Seefried¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 17:30 17:55 11.7.3
0869		 HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS
S. Joshin¹, F. Tanaka, RIKEN R-CCS, Japan; T. Amano¹, A. Hiromori¹, A. Uchiyama¹, H. Yamaguchi¹, S. Morioka², T. Inagawa²; ¹The University of Osaka, Japan ;²Interstellar Technologies Inc., Japan
15. Sep 26 17:55 18:20 11.7.4
0174		 HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL
H.S. Choi¹, S. Shin¹, H.M. Lee¹, I. Yang¹, C.-H. Lee, KAIST, South Korea; ¹KARI, South Korea
12.7Digital Modeling, Autonomous Systems and Operability
Chair(s): Viola, N.
Track 12 C2.3
07 - Systems, Subsystems and Equipment
15. Sep 26 16:40 17:05 12.7.1
0028		 ANOMALY B-VALUE DETECTION AND EXCLUSION OF GBAS BASED ON WAVELET MULTI-RESOLUTION ANALYSIS
R.X. Gong, Airbus (Tianjin) Final Assembly Company Limited, China; S.G. Sun¹, M. Xu¹, Y. Zheng, Northeast Air Traffic Management Bureau of Civil Aviation of Chi, China; ¹civil aviation university of China, China
15. Sep 26 17:05 17:30 12.7.2
0460		 MODELING OF AIRCRAFT COMPONENT PLACEMENTS WITH BIN PACKING
J. Chang, McGill University, Canada; M. Kokkolaras, Clemson University, United States
15. Sep 26 17:30 17:55 12.7.3
0831		 NEUROMORPHIC ASCENT: REVOLUTIONISING AIRCRAFT STORES COMPATIBILITY AND INTELLIGENT & AUTONOMOUS SYSTEMS
M.G. Tutty¹, S. McKee¹, A. Cenko¹; ¹JAIME AMERICA LLC, Australia
13.7Dynamic Modeling of Aviation Systems
Chair(s): Pinon-Fischer, O., Saez, R.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
15. Sep 26 16:40 17:05 13.7.1
0838		 WEATHER-DRIVEN DEEP LEARNING FOR AIRPORT RUNWAY DIRECTION FORECASTING
H.W. Kim¹, Y.J. Eun¹, D.K. Jeon¹; ¹Korea Aerospace Research Institute, South Korea
15. Sep 26 17:05 17:30 13.7.2
0697		 A PRELIMINARY STUDY ON DYNAMIC AIRSPACE CONFIGURATION USING FLEXIBLE VERTICAL BOUNDARIES IN DOUBLE-LAYER AIRSPACE
H. Suizu¹, H. Hirabayashi¹, N. Takeichi, Tokyo Metropolitan University, Japan; ¹Electronic Navigation Research Institute, Japan
15. Sep 26 17:30 17:55 13.7.3
0779		 EVALUATING IMPACT OF INTERNATIONAL DEPARTURE TIME CONTROL ON DOMESTIC ARRIVAL DELAYS IN JAPAN USING MULTI-OBJECTIVE SIMULATION-BASED OPTIMIZATION
K. Sekine¹, T. Tatsukawa, Tokyo University of Science, Japan; Y. Kawagoe, Tohoku University, Japan; E. Itoh¹; ¹The University of Tokyo, Japan
15. Sep 26 17:55 18:20 13.7.4
0521		 UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS
Y. Cho¹, J. Lee¹, Y. Kim¹, C. Jung², S. Kang², J. Kim¹; ¹Sejong University, South Korea ;²TOFF Mobility, South Korea
additional information (interactive) 13.7.R
0298		 QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY
G. Wang¹, W. Cheng¹, Y. Wu¹, L. Zhao¹; ¹Aerial Industry Development Research Center of China, China
Presenter: Luodi Zhao, Aerial Industry Development Research Center of China
14.7MBSE - Model Based Systems Engineering
Chair(s): , , Wiels, V.
Track 14 C2.5
02 - Systems Engineering and Integration
15. Sep 26 16:40 17:05 14.7.1
0399		 PROPAGATING SAFETY ASSESSMENT RESULTS FOR SYSTEM ARCHITECTURE CANDIDATES IN MBSE
S.M. Lübbe¹, M. Schäfer¹, O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 17:05 17:30 14.7.2
0674		 MODEL-BASED FUNCTIONAL HAZARD ASSESSMENT BASED ON ARP4761A USING SYSML V1 AND SYSML V2
M. Schäfer¹, S. Lübbe¹, O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany
Presenter: Sascha Lübbe, German Aerospace Center (DLR)
15. Sep 26 17:30 17:55 14.7.3
0959		 MANEUVER- AND DELAY-ROBUST DISTRIBUTED SATELLITE SSA VIA SPATIO-TEMPORAL GRAPH FORECASTING
H. Rizk¹, H. Yamaguchi¹, S. Morioka², T. Inagawa²; ¹Osaka University, Japan ;²Interstellar Technologies Inc., Japan
15. Sep 26 17:55 18:20 14.7.4
0917		 MODEL-BASED INTEGRATION OF FLIGHT-TEST EVIDENCE AND SEMI-EMPIRICAL PERFORMANCE MODELS: THE ACS-100 SORA LIGHT AIRCRAFT CASE STUDY
L.H.J. Machado¹, J.L.C. Reis¹, A. Zaramella, ACS Aviation / MOYA Aero, Brazil; L.G.M. Soltz¹; ¹Universidade Federal de Minas Gerais, Brazil
15.7Design Challenges and Training Enablers
Chair(s): Corsi, M.
Track 15 C2.6
14 - Education and Training
15. Sep 26 16:40 17:05 15.7.1
0827		 DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY
B. Sebastiani¹, M. Stefanetti¹, F.D. Fabozzi¹, A. Bitelli¹, N. Cognolato¹, L. Linguerri¹, T. Fadda¹, S. Bagassi¹; ¹University of Bologna, Italy
15. Sep 26 17:05 17:30 15.7.2
0464		 A MIXED REALITY FRAMEWORK FOR EVALUATING AIRCRAFT PRE-FLIGHT WALK-AROUND TRAINING
M.A. Higinio¹, M.J. Scott¹, W.J.C. Verhagen¹; ¹RMIT University, Australia
15. Sep 26 17:30 17:55 15.7.3
0692		 FROM DATA TO DEBRIEF: A FRAMEWORK FOR PILOT PERFORMANCE ASSESSMENT
P.B. Kurka¹, E. Villani¹; ¹Aeronautics Institute of Technology, Brazil
Presenter: Emilia Villani, Aeronautics Institute of Technology
15. Sep 26 17:55 18:20 15.7.4
0639		 TOWARDS AN ECOSYSTEM FOR AERONAUTICAL RESEARCH IN MEXICO
A.M. Zarate Villazon¹, E. Espinosa-Juarez, Linköping Universitet, Sweden; F. Perez Fuentes, Consejo Mexicano de Educacion Aeroespacial, Mexico; D.N. Mavris¹; ¹Georgia Institute of Technology, United States

Wednesday, 16. Sep 2026

0.7ICAS LECTURE FOR INNOVATION IN AERONAUTICS Veronique Roca – Airbus Beluga X
Chair: A. Andreeva-Mori ICAS EC Member
16. Sep 26 08:00 08:50

08:50 - 09:15COFFEE BREAK

0.8INTERACTIVE PRESENTATIONS
Chair:
16. Sep 26 09:15 10:45

10:45 - 10:50CHANGEOVER BREAK

1.8GSA2: Super Panel: Pathways to Global Sustainable Aviation
Chair(s): Madavan, N., Fischer, M.
Track 1 Pyrmont Theatre
15 - Guest lectures
16. Sep 26 10:50 11:15 1.8.1
0982		 GLOBAL SUSTAINABLE AVIATION PANEL DISCUSSION WITH VERONIQUE ROCA, ALAN NEWBY, JIM HILEMAN, CHRISTINE ANDREWS, RICH WAHLS AND CLAIRE WAGHORN (DURATION 100 MINUTES)
R.A. Wahls, NASA, Retired, United States
2.8GARTEUR 2
Chair(s): Hammer, B.
Track 2 C4.1
15 - Guest lectures
16. Sep 26 10:50 11:15 2.8.1
1006		 MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS
F.J. San Millán¹, J. Garcia-Martinez¹, P. Pflueger Tejero¹, I. Martinez Teres¹, U. Dincer², M. Misol, Germany; P. Wierach², A. Riccio³, A. Garofano³, M. Battaglia³, J. Berthe*, R. Ortiz*, J. Germain*, F. Roudolff*, W.W. Witsº, B. Noordmanº, O. Erartsinº, J. de Kruijk, Netherlands; ¹INTA, Spain ;²DLR, Germany ;³University of Campania, Italy ;*ONERA, France ;ºNLR, Netherlands
Presenter: Francisco Javier San Millan Fiel, INTA- Spanish National Institute for Aerospace Research
16. Sep 26 11:15 11:40 2.8.2
1005		 ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS
M.L. Montero-Sistiaga¹, M. de Smit¹, A. Pastor Muro², N. Redondo Torrico², M. Thomas³, A. Morel³, S. Drawin³, F. Palm, Airbus, Central Research & Technology (CRT), Germany; ¹Royal NLR-Netherlands Aerospace Centre, Netherlands ;²National Institute of Aerospace Technology (INTA), Spain ;³DMAS, ONERA, France
Presenter: Francisco Javier San Millan Fiel, INTA- Spanish National Institute for Aerospace Research
16. Sep 26 11:40 12:05 2.8.3
1004		 CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING
F. Laurin¹, Y. Delgado González, NLR, Netherlands; S. Reh, DLR, Germany; A. Russo, 4Università degli Studi della Campania , Italy; C. Footer, QINETIQ, United Kingdom; F. Roudolff¹; ¹ONERA, France
16. Sep 26 12:05 12:30 2.8.4
1009		 AI IN AVIATION CYBERSECURITY RISK ASSESSMENT: OPPORTUNITIES AND CHALLENGES
R. Elia, Univesity of Campania Luigi Vanvitelli, Italy; P. Bieber¹, D. Pascarella, CIRA, Italy; M. Rak, University of Naples Federico II, Italy; C. Döll¹; ¹ONERA, France
3.8Case Studies 1
Chair(s): Gibson, T.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
16. Sep 26 10:50 11:15 3.8.1
0602		 SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT
E. Stragiotti¹, E. Nguyen Van¹, R. Parello¹, S. Defoort¹, D. Losada Costoso², C. Mollet², M. Méheut², O. Atinault², F. Moëns², L. Vertonghen³, C. Julien³, A. Lannoo*, V. Priasso*; ¹DTIS, ONERA, Université de Toulouse, France ;²DAAA, ONERA, Institut Polytechnique de Paris, France ;³DMAS, ONERA, Université Paris-Saclay, France ;*DMAS, ONERA, France
16. Sep 26 11:15 11:40 3.8.2
0596		 RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT
W.Z. Liu, China; B.L. Shang, China; P.F. Li, China; R.X. Ling, China; Y.Z. Wang, China; K.A. Xing, China; H.X. Li, China; M.Z. Hou, China
16. Sep 26 11:40 12:05 3.8.3
0209		 A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION
L. Liu¹, Y. Wu¹, M.A. Hariansyah¹, R.P. Liem, ICL, Department of Aeronautics, United Kingdom; ¹HKUST, Department of Mechanical and Aerospace Engineering, Hong Kong SAR of China
Presenter: Yiran Wu, HKUST,Department of Mechanical and Aerospace Engineering
16. Sep 26 12:05 12:30 3.8.4
0631		 OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES
M.A. Hariansyah¹, C. Reyner¹, R.P. Liem, Imperial College London, United Kingdom; P.S. Palar, Institut Teknologi Bandung, Indonesia; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China
Reserve Paper 3.8.R
0873		 THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV
S. Choi¹, Y. Lee¹, H. Choi¹, B. Cho¹, Y. Kim¹, D. Jung¹; ¹Korea Aerospace University, South Korea
Presenter: Byeonggeun Cho, Korea Aerospace University
4.8Unconventional Configurations - 1
Chair(s): Gerhards, R.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
16. Sep 26 10:50 11:15 4.8.1
0625		 A MULTI-RANGE HYBRID-ELECTRIC OPEN-ROTOR AIRCRAFT CONCEPT FOR THE WIDE-BODY PASSENGER CLASS
G. Atanasov¹, D. Silberhorn¹, V. Nugnes¹; ¹German Aerospace Center (DLR), Germany
16. Sep 26 11:15 11:40 4.8.2
0078		 COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS
L. Li¹, M. Chao¹, L. Wang, AVIC (CHENGDU) UAS CO., LTD., China; J. Zhong, School of Aeronautics, Northwestern Polytechnical University, China; F. Li, Xinjiang Institute of Intelligent Equipment, China; ¹School of Future Transportation, Chang’an University, China
16. Sep 26 11:40 12:05 4.8.3
0576		 RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS
H. Reindle¹, J. Hoffelner¹, N. Sekyra¹, N. Schlautmann¹, M. Weber¹, V. Sittel¹, C. Mishra¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany
16. Sep 26 12:05 12:30 4.8.4
0401		 PROPULSION SYSTEM MODELING AND OPTIMIZATION FOR CONCEPTUAL DESIGN OF HYBRID-ELECTRIC VTOL AIRCRAFT
D.E. Lampl, Technical University of Munich, Germany; S.F. Armanini, Imperial College London, United Kingdom
5.8Machine Learning Applications
Chair(s): , , Halila, G.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 10:50 11:15 5.8.1
0492		 EFFICIENT ROTOR AERODYNAMIC SHAPE DESIGN USING A MULTI-FIDELITY NEURAL NETWORK-BASED GLOBAL OPTIMIZATION METHOD
S. Li¹, W.P. Song¹, Z.Q. Shen¹; ¹ Northwestern Polytechnical University, China
16. Sep 26 11:15 11:40 5.8.2
0530		 MACHINE LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION OF NACA AIRFOILS UNDER GEOMETRIC DESIGN CONSTRAINTS
M.S. Abulela¹, M.I. Alam¹; ¹King Fahd University of Petroleum and Minerals, Saudi Arabia
16. Sep 26 11:40 12:05 5.8.3
0051		 PHYSICS-INFORMED NEURAL OPERATORS FOR DISTURBANCE FIELD PREDICTION IN NONPARALLEL BOUNDARY-LAYER STABILITY ANALYSIS
G. Dalinajara Abreu Smith Borges¹, V. Silva Figueredo¹, G.L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J.L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
16. Sep 26 12:05 12:30 5.8.4
0490		 EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN
Y. Fan¹, Y. Sun¹, J. Xue¹, Y. Wang¹, B. Mi¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
6.8High Speed Flight: High-Temperature Materials/Structures
Chair(s): Bowcutt, K., Neely, A.
Track 6 C4.5
15 - Guest lectures
16. Sep 26 10:50 11:15 6.8.1
1093		 PREDICTING THE RESPONSE OF HIGH-TEMPERATURE STRUCTURE FOR HIGH-SPEED VEHICLES THROUGH SIMULATION AND MEASUREMENT
A. Neely, UNSW, Australia
16. Sep 26 11:15 11:40 6.8.2
1076		 FROM HIGH-TEMPERATURE MATERIALS TO HIGH-RATE PRODUCTION: OVERVIEW OF EXISTING RESEARCH EFFORTS AND OUTLOOK
M. Heitzmann, University of Queeensland, Australia
16. Sep 26 11:40 12:05 6.8.3
1077		 PANEL DISCUSSION (TIL END OF THE BLOCK)
P. Panel
7.8Configuration Aerodynamics and Coupled Flight Behaviour
Chair(s): Lawson, N.
Track 7 C4.6
03.4 - Applied Aerodynamics
16. Sep 26 10:50 11:15 7.8.1
0269		 FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH
Z. Zhang¹, H. Zhao¹, W. Zhang¹, J. He¹, Z. Gao¹; ¹Northwestern Polytechnical University, China
16. Sep 26 11:15 11:40 7.8.2
0284		 MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLOW REGIMES
A. Petrillo¹, D. Palma¹, L. Pirillo¹, P.P. Ciottoli¹, M. Bernardini¹, F. Stella¹; ¹Sapienza university of Rome, Italy
16. Sep 26 11:40 12:05 7.8.3
0330		 STUDY ON THE IMPACT OF TRIM CONDITION ON LATERAL AND DIRECTIONAL STABILITY FOR A TAILLESS AIRCRAFT
K. Kania, Warsaw University of Technology, Poland
Presenter: Agnieszka Kwiek, Warsaw University of Technology
16. Sep 26 12:05 12:30 7.8.4
0456		 GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY
F. Kuci¹, N. Railean¹, P. Kantzidis², P. Marzocca², V. Muscarello²; ¹Polytechnic University of Turin, Italy ;²Royal Melbourne Institute of Technology, Australia
Reserve Paper 7.8.R
0759		 NUMERICAL CHARACTERISATION OF SHIP-AIRWAKE EFFECTS ON MEDIUM-WEIGHT UAV APPROACH AND GO-AROUND OPERATIONS TO CANBERRA-CLASS LHDS
M.J. Ericksen¹, N.J. Lawson¹; ¹The University of Sydney, Australia
8.8Additive Manufacturing
Chair(s): Denquin, A, Gliszcynski, A.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
16. Sep 26 10:50 11:15 8.8.1
0351		 ELECTROMAGNETISM FOR SMART MANUFACTURING OF POLYMER COMPOSITES
S.H. Vattathurvalappil, King Fahd University of Petroleum and Minerals, Saudi Arabia
16. Sep 26 11:15 11:40 8.8.2
0250		 DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS
J. Rodrigues¹, M. Pelosi², W. Foster², S. Barter¹, R. Das¹; ¹RMIT University, Australia ;²DSTG, Australia
16. Sep 26 11:40 12:05 8.8.3
0507		 LASER SCANNING STRATEGIES TO INVESTIGATE THE EFFECTS OF OXIDATION IN PURE TANTALUM
M. Davids, HH Industries, University of Cape Town, South Africa; J. Strauss¹, D. Hagedorn-Hansen¹, T.H. Becker, University of Cape Town, South Africa; ¹HH Industries, South Africa
16. Sep 26 12:05 12:30 8.8.4
0499		 FLYING BY THE THREAD OF MY PANTS: USING HOUSEHOLD TEXTILES COMPOSITES FOR ACCESSIBLE UAV AIRFRAMES
C. Koutsambasis¹, M. Marino¹, N.J. Brown¹, W. Wu¹; ¹RMIT University, Australia
9.8Flutter
Chair(s): Tsushima, N., Candon, M.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
16. Sep 26 10:50 11:15 9.8.1
0627		 A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY
W. Qian¹, J. Liu¹, X. Hu¹, C. Han¹, X. He¹, X. Ran¹, X. Ai¹; ¹Dalian University of Technology, China
16. Sep 26 11:15 11:40 9.8.2
0566		 MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY
X. Ai¹, Z. Chen¹, Z. Liang¹, Z. An¹, X. Xu¹, Y. Lu¹, W. Qian¹; ¹Dalian University of Technology, China
16. Sep 26 11:40 12:05 9.8.3
0620		 TIME-VARYING AEROELASTIC MODELING AND FLUTTER ANALYSIS OF TELESCOPIC WINGS
C.-Y. Li¹, S. He¹, Z.-C. Yang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 9.8.R
0179		 FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING
Z.Y. Xi¹, Y.T. Dai¹, C. Yang¹; ¹Beihang University, China
additional information (interactive) 9.8.R
0494		 MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION
C.Y. Zhao, China; B.G. Mi, China; X. Bai, China
10.8Propellers, Compressors and Turbines 1
Chair(s): Haselbach, F.
Track 10 C4.9
05 - Propulsion and Energy
16. Sep 26 10:50 11:15 10.8.1
0261		 CONCEPTUAL PERFORMANCE AND MASS ASSESSMENT OF AN OPEN FAN ENGINE FOR THE DLR-F25 AIRCRAFT
P. Wehrel¹, J. Häßy¹, R. Schnell¹, S. Wöhler¹; ¹German Aerospace Center (DLR)), Germany
16. Sep 26 11:15 11:40 10.8.2
0712		 SURROGATE-BASED OPTIMIZATION OF AIRCRAFT PROPELLER PERFORMANCE USING A HIGH-FIDELITY AND EFFICIENT RANS FRAMEWORK
A. Stuermer¹, M. Hepperle¹, P. Wegener¹; ¹DLR, Germany
16. Sep 26 11:40 12:05 10.8.3
0084		 FEASIBILITY OF ELECTRIC DUCTED FANS TO REPLACE OPEN PROPELLERS ON AN ELECTRIFIED TRAINING AIRCRAFT
G. Braggett¹, K.F. Joiner¹, A. Somerville¹, D. Hill, Altavia Aerospace, Australia; ¹University of New South Wales, Australia
Presenter: Georgia Braggett, University of New South Wales
16. Sep 26 12:05 12:30 10.8.4
0690		 FLIGHT-DATA-DRIVEN PHYSICS-INFORMED COMPONENT MAP DERIVATION WITH STRUCTURAL COMPLIANCE
Y. Liu¹, L. Gou¹, Y. Huang, Shenzhen Research Institute of Northwestern Polytechnical Univer, China; ¹School of Power and Energy, Northwestern Polytechnical Universit, China
additional information (interactive) 10.8.R
0461		 STUDY ON OIL CAVITATION AND PUMPING CHARACTERISTICS OF SURFACE MICROTOPOGRAPHY GRAPHITE SEALS
Y.P. Li, China; J.P. Hu, China; G.L. Li, China; H.L. Zhao, China; S. Li, China
Presenter: Shu Li
11.8System Identification
Chair(s): Kim, S., Wan, T.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 26 10:50 11:15 11.8.1
0176		 SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION
E.J. Kim¹, B. Seo¹, S.K. Kim¹, J.Y. Suk¹; ¹Chungnam National University, South Korea
16. Sep 26 11:15 11:40 11.8.2
0361		 ATTITUDE CONTROL TECHNIQUES FOR A MICRO-SCALE FLAP-BASED AERODYNAMIC DECELERATOR SYSTEM
J. Clarendon¹, T. Fields¹, J. Nguyen¹, A. Chance¹, O. Yakimenko, Naval Postgraduate School, United States; ¹University of Missouri-Kansas City, United States
16. Sep 26 11:40 12:05 11.8.3
0633		 GUST ERROR METHOD (GEM): PARAMETER IDENTIFICATION FOR AIRCRAFT SUBJECT TO VON KÁRMÁN PROCESS NOISE
J. Cox¹, K.C. Wong¹, G. Chamitoff, Texas A&M University College of Engineering, United States; ¹The University of Sydney, Australia
16. Sep 26 12:05 12:30 11.8.4
0742		 WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING
Y.L. He, China; X.P. Xu, China; Z. Zhou, China; S. Song, China
Presenter: Shiqi Song
Reserve Paper 11.8.R
0344		 AFFINE-INVARIANT ELLIPTICAL STATE ESTIMATION FOR ROBUST EXTENDED OBJECT TRACKING
I.H. Lee, Korea Institute of Industrial Technology, South Korea
Presenter: inho lee
12.8CRM-HL 1
Chair(s): , , Imamura, T.
Track 12 C2.3
03.2 - Experimental Aerodynamics
16. Sep 26 10:50 11:15 12.8.1
1046		 ECOSYSTEM UPDATES AND PLANS
M. Rivers, NASA, United States
16. Sep 26 11:15 11:40 12.8.2
0256		 AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL
M. Kohzai¹, M. Murayama¹, A. Sansica¹, D. Lusher¹, T. Takaishi¹, H. Abe¹; ¹Japan Aerospace Exploration Agency, Japan
16. Sep 26 11:40 12:05 12.8.3
0756		 AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT
M. Murayama¹, Y. Murata¹, M. Kohzai¹, K. Yamamoto¹, Y. Ito¹, H. Ura¹, T. Takaishi¹; ¹Japan Aerospace Exploration Agency, Japan
16. Sep 26 12:05 12:30 12.8.4
0328		 NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL
T. Hashioka¹, Y. Murahashi¹, H. Yasuda¹, Y. Sawaki¹, S. Suzuki¹, W. Suzuki¹, T. Kawamura¹; ¹KHI, Japan
13.8Optimizing AAM Networks
Chair(s): Wickramasinghe, N.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
16. Sep 26 10:50 11:15 13.8.1
0587		 RECIPROCITY-GUIDED JOINT BASE STATION PLACEMENT AND FLIGHT CORRIDOR PLANNING FOR URBAN AIR MOBILITY
Y. He¹, Y. Wang¹, F. Wu¹, J. Guo¹, Z. Gao¹; ¹HKUST, Hong Kong SAR of China
16. Sep 26 11:15 11:40 13.8.2
0325		 SIMULATION-BASED EVALUATION OF SIGNALISED INTERSECTIONS FOR EMERGENCY SAFETY LANDINGS IN URBAN AIR MOBILITY
P. Sathya Kumar¹, M. Schultz¹, E. Asadi¹; ¹Universität der Bundeswehr München, Germany
16. Sep 26 11:40 12:05 13.8.3
0103		 SCHEDULING AND ROUTING FOR TIMETABLE-BOUND URBAN AIR MOBILITY OPERATIONS
A. Edsel¹, W.A. Crossley¹, D.A. DeLaurentis¹; ¹Purdue University, United States
16. Sep 26 12:05 12:30 13.8.4
0802		 ESTIMATION AND ANALYSIS OF RNP REQUIREMENTS FOR HETEROGENEOUS UAM CONFIGURATIONS: INSIGHTS FROM OPPAV DEMONSTRATION
J.S. Lee¹, K.R. Oh¹; ¹Korea Aerospace Research Institute, South Korea
additional information (interactive) 13.8.R
0900		 OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES
A. Tiwari¹, R.S. Pant¹; ¹Indian Institute of Technology Bombay, India
14.8Multidisciplinary Advances in Aerodynamics, Aeroacoustics, and Aeroelasticity (by IFAR)
Chair(s): Schuchardt, B.
Track 14 C2.5
15 - Guest lectures
16. Sep 26 10:50 11:15 14.8.1
0195		 AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS
D. Skrna¹, M. de Rosa Jacinto¹, L. Frei¹, B. Mittenecker¹, J. Nagl¹, H. Mad¹, M. Berens¹; ¹Technische Universität Wien, Austria
16. Sep 26 11:15 11:40 14.8.2
1001		 ON THE GROUND AND IN FLIGHT: AERODYNAMIC AND AEROELASTIC TESTING SUPPORTING INNOVATION IN AERONAUTICS
C. Mertens, Royal Netherlands Aerospace Centre, Netherlands
Presenter: Christoph Mertens, Royal Netherlands Aerospace Centre
16. Sep 26 11:40 12:05 14.8.3
1002		 UNDERSTANDING HYPERSONIC BOUNDARY LAYER LAMINAR TO TURBULENT TRANSITION IN WIND TUNNEL ENVIRONMENT
M. Lugrin, ONERA, France
Presenter: Mathieu Lugrin, ONERA
16. Sep 26 12:05 12:30 14.8.4
1047		 PANEL DISCUSSION AND Q&A
1 Q,
15.8Education Enablers
Chair(s): Corsi, M.
Track 15 C2.6
14 - Education and Training
16. Sep 26 10:50 11:15 15.8.1
0453		 PREPARING AERONAUTICAL ENGINEERING UNDERGRADUATES FOR WORKING IN GLOBAL TEAMS
J. Abulawi, HAW Hamburg, Germany; P. Raj, Virginia Tech, United States
16. Sep 26 11:15 11:40 15.8.2
0549		 REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR
K. Ramotsabi¹, L. Strydom¹, L. Zwane¹; ¹CSIR, South Africa
16. Sep 26 11:40 12:05 15.8.3
0718		 AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME
N. Moser¹, N. Singer¹, V. N. Mueller¹, T. Siemer¹, F. Daoud¹; ¹TU Munich, Germany
Presenter: Valentin Müller
16. Sep 26 12:05 12:30 15.8.4
0933		 AN MBSE-ORIENTED FRAMEWORK FOR AEROSPACE SYSTEMS EDUCATION: THE CEA-UFMG LIGHT-AIRCRAFT DESIGN-BUILD-TEST TRADITION
L.H.J. Machado¹, J.L.C. Reis¹, M. Lott², R. Carlana²; ¹Universidade Federal de Minas Gerais, Brazil ;²Boeing, Brazil
additional information (interactive) 15.8.R
0380		 INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION
C. Varriale¹, F. Angioni¹; ¹Delft University of Technology, Netherlands

12:30 - 13:30LUNCH BREAK

0.9GENERAL LECTURE 4 Aeronautics Outlook - Directors Cut (Michael Edwards, Boeing, Veronique Roca, Airbus, Dimitri Mavris, Georgia Tech, Alan Newby, Rolls-Royce, Per Olof Marklund, SAAB. Markus Fischer, DLR
Chair: S.Bagassi/A.Krein ICAS EC Members
16. Sep 26 13:30 15:15

15:15 - 15:40AFTERNOON BREAK

1.9ECSC Pitch Session (10 Minute Talks with Q&A afterwards)
Chair(s): Citron, T.
Track 1 Pyrmont Theatre
15 - Guest lectures
16. Sep 26 15:40 16:05 1.9.1
1094		 DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS (PITCH SESSION)
J. Rodrigues, RMIT, Australia
16. Sep 26 16:05 16:30 1.9.2
1095		 AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES (PITCH SESSION)
P. Faezeh, Eindhoven University of Technology, Netherlands
16. Sep 26 16:30 16:55 1.9.3
1096		 ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES (PITCH SESSION)
K. Thomessen, DLR, Germany
16. Sep 26 16:55 17:20 1.9.4
1097		 NONLINEAR FRICTION MODELING OF HELIX SWING HYDRAULIC CYLINDERS FOR MORPHING AIRCRAFT USING PHYSICS-INFORMED NEURAL NETWORKS (PITCH SESSION)
S. Chen, Beihang University, China
Reserve Paper 1.9.R
1098		 SENSITIVITY STUDY OF DEPARTURE TIME ACCURACY FOR AIRPORT COLLABORATIVE DECISION MAKING USING FAST-TIME SIMULATION (PITCH SESSION)
Y. Iwatsuki, Mitsubishi Research Institute, Inc., Japan
2.9Shaping Aviation for Society ETF with Introduction and Panel Discussion at the End
Chair(s): Holmberg, G., Collier, F.
Track 2 C4.1
15 - Guest lectures
16. Sep 26 15:40 16:05 2.9.1
1092		 THE COLLABORATIVE NATURE OF AVIATION INDUSTRY
B. Stoufflet, France
16. Sep 26 16:05 16:30 2.9.2
1013		 PRACTICAL INNOVATION IN AEROSPACE
William Dean Donovan, DiamondStream Partners, United States
16. Sep 26 16:30 16:55 2.9.3
1015		 AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH
X.S. Zheng, United States; J. Mukhopadhaya, United States; J. Benoit, United States; S.N. Kumar, United States; D. Rutherford, United States; D. Rhode, Germany; D. Sitompul, United States
16. Sep 26 16:55 17:20 2.9.4
1016		 A MULTI-FUEL PROPULSION SYSTEM STRATEGY FOR AVIATION TRANSPORT RESILIENCE
A. Murphy, United States
3.9Case Studies 2
Chair(s): Gibson, T.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
16. Sep 26 15:40 16:05 3.9.1
0346		 DYNAMIC ANALYSES AND FLIGHT TESTING FOR THE DESIGN OF FLOATING CANARD AIRCRAFT
N. Morita¹, N. Okubo¹, T. Ogawa¹, Y. Sasaki¹; ¹Velcity Aeroworks .Inc, Japan
16. Sep 26 16:05 16:30 3.9.2
0552		 LOW BOOM DESIGN AND ANALYSIS OF A BLENDED-WING-BODY CONFIGURATION FOR LARGE-SIZED SUPERSONIC TRANSPORT
Y. Lin¹, K.S. Zhang¹, Z.H. Han¹, Q. Chen¹; ¹Northwestern Polytechnical University, China
16. Sep 26 16:30 16:55 3.9.3
0466		 STUDY ON INDUCED DRAG CALCULATION FOR BIRD-LIKE WINGTIP SLOTS USING WAKE-PLANE INTEGRATION
X. Liu, China; T. Yu, China; B. Song, China; D. Xue, China
16. Sep 26 16:55 17:20 3.9.4
0610		 MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY: INTRODUCING AN ARCHITECTURE-AWARE OPTIMIZATION STRATEGY
B. Blaxall¹, F. Di Fiore¹, D. Venetsanos¹, L. Mainini¹; ¹Imperial College London, United Kingdom
4.9Unconventional Configurations - 2
Chair(s): Melkert, J.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
16. Sep 26 15:40 16:05 4.9.1
0055		 MODELING & PRELIMINARY ANALYSIS OF AN ECOFRIENDLY AIRBORNE GLOBAL LUXURY EKRANOPLAN
M. Sankrithi, RIC Enterprises, United States; D. Mavris¹, R. Sundar¹; ¹Georgia Institute of Technology, United States
16. Sep 26 16:05 16:30 4.9.2
0643		 LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY
A. Frediani¹, E. Rizzo¹, G. Palaia, Politecnico di Torino, Italy; K. Abu Salem, University of Trento, Italy; M. Martini¹; ¹SkyBox Engineering, Italy
16. Sep 26 16:30 16:55 4.9.3
0274		 EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT
E.M. Künstler¹, S. Roscher², A. Bardenhagen², A. Strohmayer¹; ¹University of Stuttgart, Germany ;²Technische Universität Berlin, Germany
16. Sep 26 16:55 17:20 4.9.4
0924		 EFFECTS OF LIFT DISTRIBUTION AND WING POSTURE ON THE STABILITY AND CONTROL OF TAILLESS AIRCRAFT
M.R. de Kock¹, B.B. Huyssen¹, R.J. Huyssen, Council for Scientific and Industrial Research, South Africa; ¹University of Pretoria, South Africa
Presenter: Barbara Huyssen, University of Pretoria
5.9Aerodynamic Optimization
Chair(s): , , Zingg, D.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 15:40 16:05 5.9.1
0052		 HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINES USING A DISCRETE ADJOINT APPROACH
L. Rodrigues Arnaud¹, F. Maia Nunes Celestino¹, G.L. Olichevis Halila¹, J.L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
16. Sep 26 16:05 16:30 5.9.2
0105		 CONTINUOUS UNSTEADY ADJOINT VARIATIONAL MULTISCALE METHOD FOR AIRFOILS SHAPE OPTIMIZATION
C. Brunelli¹, M. Avirovic¹, B. Janssens¹, B.G. Marinus¹; ¹Royal Military Academy, Belgium
16. Sep 26 16:30 16:55 5.9.3
0120		 SIMULATION OF AERODYNAMIC GROUND EFFECT FOR TILTED PROPELLERS USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S. Shahjahan¹, V. Ahuja¹; ¹Siemens Digital Software Industries, United States
Presenter: Shahfiq Shahjahan, Siemens Digital Software Industries Software Inc.
16. Sep 26 16:55 17:20 5.9.4
0061		 A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS
G. Dessio Junior¹, G.L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J.L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
additional information (interactive) 5.9.R
0862		 LEAKAGE PREDICTION AND GEOMETRIC PARAMETER OPTIMIZATION OF STEPPED LABYRINTH SEALS BASED ON DATA-DRIVEN SURROGATE MODELS
X. Li¹, L. Yang¹, Y. Wei¹; ¹Beijing Jiaotong University, China
6.9Certification by Analysis - Accelerating Momentum and Impact
Chair(s): Slotnick, J., van Dam, C.P.
Track 6 C4.5
15 - Guest lectures
16. Sep 26 15:40 16:05 6.9.1
1055		 PANEL DISCUSSION WITH J. SLOTNICK, B.APONSO, D.PETERSON, T.ISHIDA, H.SCKLICKENMAIER (DURATION 100 MINUTES)
J. Slotnick, United States
7.9Aerodynamics of Unconventional Aircraft Configurations
Chair(s): Jagadeesh, C.
Track 7 C4.6
03.4 - Applied Aerodynamics
16. Sep 26 15:40 16:05 7.9.1
0122		 AERODYNAMIC OPTIMIZATION DESIGN OF FULL-WING SOLAR-POWERED UAV FOR FLOW SEPARATION CONTROL
J. Wang¹, Z. Zhou¹, K. Wang¹, M. Li¹; ¹Northwestern Polytechnical University, China
16. Sep 26 16:05 16:30 7.9.2
0295		 STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS
C. Zheng¹, Q. Qu¹, P. Liu¹, T. Hu¹; ¹Beihang University, China
16. Sep 26 16:30 16:55 7.9.3
0318		 AERODYNAMIC AND STABILITY-DRIVEN PRE-DESIGN OF A FUEL-CELL POWERED FLYING WING AIRCRAFT
P. Kirschnek¹, S. Lesak¹, A. Tramposch¹; ¹FH JOANNEUM, Austria
16. Sep 26 16:55 17:20 7.9.4
0866		 AERODYNAMIC FEASIBILITY OF A NOVEL SWIVEL ROTOR ARCHITECTURE
B.I. Soemarwoto, Royal Netherlands Aerospace Centre NLR, Netherlands
Reserve Paper 7.9.R
0841		 DEVELOPMENT OF HYDROPHILIC COATINGS FOR PRACTICAL APPLICATION OF LAMINAR FLOW WINGS
H. Iijima¹, Y. Iijima¹, N. Tokugawa¹; ¹JAXA, Japan
additional information (interactive) 7.9.R
0171		 FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES
K. Qiao, China; D. Wei, China; L. Han, China; Z. Chen, China; Z. Yan, China; Y. Qin, China; G. Xu, China; H. Tang, China
additional information (interactive) 7.9.R
0392		 UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND FLIGHT DURATION ANALYSIS
J. Guo¹, Y. Sun¹; ¹Cranfield University, United Kingdom
8.9Structural Optimization
Chair(s): Gliszcynski, A.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
16. Sep 26 15:40 16:05 8.9.1
0930		 HIERARCHICAL HIGH-ORDER BEAM MODELS FOR OPTIMISATION-ORIENTED ANALYSIS OF COMPOSITE WING-LIKE STRUCTURES
D. Cardone¹, R. Cavallaro, Barcelona Supercomputing Center, Spain; A. Cini¹; ¹Universidad Carlos III de Madrid, Spain
16. Sep 26 16:05 16:30 8.9.2
0225		 DESIGN ASSESSMENT OF A HELICOPTER BLADE
C. Pagwiwoko¹, K. Warnakula¹, M. Silla¹, C. Barber¹, T. Hallwright¹, O. Kaleagasi¹, D. Schoemaker, Gyro Technic Inc., United States; ¹SYOS Aerospace, New Zealand
Presenter: Cosmas Pagwiwoko, SYOS Aerospace
16. Sep 26 16:30 16:55 8.9.3
0053		 ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS
G.C. Cristea¹, M. Pop¹, A. Stefan¹, M. Botan¹, A. Dragomirescu¹; ¹INCAS, Romania
16. Sep 26 16:55 17:20 8.9.4
0943		 OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR UAVS
C.D. Scott¹, A.M. Comer¹, J.C. Hanan¹, A. Nunley¹; ¹Oklahoma State University, United States
9.9Aeroelastic Analysis & Design 1
Chair(s): Han, J., Muscarello, V.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
16. Sep 26 15:40 16:05 9.9.1
0448		 AEROELASTIC TAILORING FOR COMPOSITE ADAPTIVE WINGLETS
N. Tsushima, Kyushu University, Japan; R. Higuchi¹, T. Yokozeki¹; ¹The University of Tokyo, Japan
16. Sep 26 16:05 16:30 9.9.2
0326		 PARAMETRIC AEROELASTIC STUDY OF WINGLET GEOMETRY USING VORTEX LATTICE METHOD FOR FUTURE PASSIVE MORPHING APPLICATIONS
M. Kouchlef¹, N. Tsushima¹, T. Yokozeki¹; ¹The University of Tokyo, Japan
16. Sep 26 16:30 16:55 9.9.3
0342		 AEROELASTIC DESIGN OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT IN AN MDO FRAMEWORK
C. Mollet¹, L. Vertonghen¹, C. Julien¹; ¹ONERA, France
16. Sep 26 16:55 17:20 9.9.4
0277		 MANEUVER LOAD ALLEVIATION OF THE DRY WING FOR HYDROGEN AIRCRAFT
F. Yu¹, M. Hornung¹; ¹Technical University of Munich, Germany
10.9Propellers, Compressors and Turbines 2
Chair(s): Haselbach, F
Track 10 C4.9
05 - Propulsion and Energy
16. Sep 26 15:40 16:05 10.9.1
0813		 MODULAR JET AND PROPELLER ENGINE – PART I: INITIAL STUDIES
T. Otten¹, T. Matuschek¹, J. Häßy¹, J. Frank¹, R.G. Brakmann¹; ¹German Aerospace Center (DLR), Germany
16. Sep 26 16:05 16:30 10.9.2
0829		 MODULAR JET AND PROPELLER ENGINE – PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT
T. Matuschek¹, T. Otten¹, J. Häßy¹, R. Brakmann¹, J. Frank¹, P. Wehrel¹; ¹German Aerospace Center (DLR), Germany
16. Sep 26 16:30 16:55 10.9.3
0334		 INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY
L. Oberthür¹, M. Stößel¹, D. Kozulovic¹, M. Krummenauer, Bundeswehr Technical Center for Aircraft and Aeronautical Equipm, Germany; ¹University of the Bundeswehr Munich, Germany
16. Sep 26 16:55 17:20 10.9.4
0768		 INITIAL GEOMETRIC UNCERTAINTY ASSESSMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD
K. Omoto¹, D. Sasaki¹, K. Matsui², M. Yamagami²; ¹Osaka Metropolitan University, Japan ;²IHI Corporation, Japan
11.9Guidance and Flight Trajectory Control 2
Chair(s): Drupka, G., Rohacs, D.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 26 15:40 16:05 11.9.1
0534		 TRAJECTORY OPTIMIZATION OF HIT-TO-KILL INTERCEPTORS VIA SEQUENTIAL CONVEX PROGRAMMING APPROACH
S.-J. Im¹, C.-H. Lee¹, J.-H. Jin, Sunchon National University, South Korea; H.-C. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea
16. Sep 26 16:05 16:30 11.9.2
0805		 DUAL BEZIER SPACE-TIME OPTIMIZATION UNDER HARD OBSERVATION-WINDOW CONSTRAINTS: A FEASIBILITY-ORIENTED JERK-CAP COMPARISON
H. Kim¹, S. Lee¹; ¹Kookmin University, South Korea
16. Sep 26 16:30 16:55 11.9.3
0858		 OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL
S. Kim¹, J. Shin¹, H.-G. Kim, Konkuk University, South Korea; ¹Chungbuk National University, South Korea
12.9Robot Manufacturing and Assembly Technology
Chair(s): Guevara, E., Zhang, H.
Track 12 C2.3
08 - Manufacturing and Supply Chain Management
16. Sep 26 15:40 16:05 12.9.1
0058		 GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY
M. Tatar¹, L. Branko¹, R.W. Grube¹, R. Noll¹, G.M. Buckus¹, O. Wagner¹; ¹Boeing, United States
16. Sep 26 16:05 16:30 12.9.2
0080		 EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY
I. Ali¹, C. Silva², E. Villani², J.M. Mello¹, W. Oliveira²; ¹Embraer, Brazil ;²ITA, Brazil
16. Sep 26 16:30 16:55 12.9.3
0198		 VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL
A.T. Ferraz¹, C.C.D. Silva¹, J.M.G. Mello, EMBRAER, Brazil; E. Villani¹; ¹ITA, Brazil
Presenter: Emilia Villani, ITA
16. Sep 26 16:55 17:20 12.9.4
0991		 LIGHTWEIGHT BIMETALLIC GEARS FOR AEROSPACE TRANSMISSIONS ENABLED BY OPEN-AIR DIFFUSION BONDING
Z.C. Xu¹, E. Tang¹, N. Teyssier¹, M.F. Humphreys¹, J. Jiang¹; ¹Imperial College London, United Kingdom
13.9Strategic Planning for AAM
Chair(s): Enea, G.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
16. Sep 26 15:40 16:05 13.9.1
0150		 VERTIPORT FINAL APPROACH AND TAKEOFF AREA ORIENTATION IDENTIFICATION USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS
D.S. Nithya¹, F. Monteleone¹, V. Muscarello, RMIT University, Australia; G. Quaranta¹; ¹Politecnico di Milano, Italy
16. Sep 26 16:05 16:30 13.9.2
0580		 LOW-NOISE VERTIPORT PROCEDURE PLANNING USING DEEP REINFORCEMENT LEARNING
Y. Wang¹, J. Guo¹, Y. He¹, F. Wu¹, Z. Gao¹; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China
16. Sep 26 16:30 16:55 13.9.3
0672		 IMPACT OF BOOKING LEAD TIME ON FLEET AND INFRASTRUCTURE IN URBAN AIR MOBILITY
M. Swaid, German Aerospace Center (DLR), Germany
16. Sep 26 16:55 17:20 13.9.4
0897		 ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT
M. Corsi, DLR German Aerospace Center, Institute of Flight Guidance, Germany; K. Schweiger¹, C. Bettremieux¹, C. Nava Gaxiola², A. Mangas Pita², M. Hardt³, A. Tutku Altun³, S. McNamee Freire, URBANV S.p.A., Italy; G. Riccardi, ENAV S.p.A., Italy; E. Fornaciari, D-Flight S.p.A., Italy; ¹EUROCONTROL Innovation Hub, France ;²AENA S.M.E., Spain ;³Boeing Aerospace Spain, Spain
additional information (interactive) 13.9.R
0538		 A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS
M. Xu¹, L. Wang, School of Reliability and Systems Engineering, Beihang universi, China; T. Ma¹, X. Wang, School of Reliability and Systems Engineering, Beihang universit, China; J. Fu¹; ¹Institute of Unmanned System, Beihang University, China
14.9Emerging Technologies for Future Air Operations (by IFAR)
Chair(s): Kramar, V., Kopardakar, P.
Track 14 C2.5
15 - Guest lectures
16. Sep 26 15:40 16:05 14.9.1
0871		 ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES
V. Kramar, VTT Technical Research Centre of Finland (VTT) , Finland; L. Asmer¹, B. Schuchardt¹, A. Badea², J. Teutsch², J. Vreeken², E. Sunil², B. Gungen², J. Kok², M. Murça, Technological Institute of Aeronautics (ITA), Brazil; I. Borshchova³, J. Keillor³, L. Pinjala*, A. Hebbar*, G. Madhuranath*, D.M. Manindrakumar*, N. Yokoyama, Japan Aerospace Exploration Agency (JAXA), Japan; H.U. Park, Korea Aerospace Administration (KASA), South Korea; P.H. Kopardekar, National Aeronautics and Space Administration (NASA), United States; ¹German Aerospace Center (DLR) , Germany ;²Royal Netherlands Aerospace Centre (NLR), Netherlands ;³National Research Council Canada (NRC) , Canada ;*Council of Scientific & Industrial Research (CSIR), India
16. Sep 26 16:05 16:30 14.9.2
0901		 PREDICTION OF STRUCTURAL VIBRATIONS INDUCED BY MASS-UNBALANCED ELECTRIC PROPULSION SYSTEMS
G.R. Dias¹, D.V.R. Silva¹, A.G. Heck¹, D.A. Rade¹; ¹Aeronautics Institute of Technology, Brazil
16. Sep 26 16:30 16:55 14.9.3
0932		 METHODOLOGY AND V1 PROTOTYPE OF AN ADAPTIVE/ADAPTABLE MULTI-UAV GCS HMI IN A FLOOD SAR CO-SIMULATION TESTBED
A.G.P. Sarmento¹, P. Krus, Linköping University (LiU), Sweden; E. Villani¹; ¹Aeronautics Institute of Technology (ITA), Brazil
Presenter: Petter Krus, Linköping University
16. Sep 26 16:55 17:20 14.9.4
0947		 A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS
R. Fernandes Viana¹, C. Rutili de Lima¹, V. Abrão S. Marques, Federal University of Triângulo Mineiro, Brazil; M. Condé Rocha Murça¹, M. R. O. A. Maximo¹, Q.F. Carlos Henrique¹; ¹Aeronautics Institute of Technology, Brazil
Presenter: Vinicius Abrão da Silva Marques, Federal University Of Triângulo Mineiro
15.9Condition Based Maintenance
Chair(s): Koschlik, A.K., Scott, M.
Track 15 C2.6
11 - Operations and Sustainment
16. Sep 26 15:40 16:05 15.9.1
0738		 EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION
V. Kekoc, Defence Science and Technology Group, Australia; M. Scott¹, W.J.C. Verhagen¹, P. Marzocca¹; ¹RMIT University, Australia
16. Sep 26 16:05 16:30 15.9.2
0770		 AI-BASED MAINTENANCE CODE CORRECTION FOR RELIABLE MTBF ANALYSIS
M. Kim¹, S.-H. Jeong¹, I. Lee¹, B. Shim¹; ¹Korea Aerospace Industries, LTD, South Korea
16. Sep 26 16:30 16:55 15.9.3
0573		 PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING
L. Jilke¹, M. Schubert¹, N. Hosters², F. Raddatz¹, M. Behr², G. Wende¹; ¹German Aerospace Center (DLR), Germany ;²RWTH Aachen University, Germany
16. Sep 26 16:55 17:20 15.9.4
1034		 DATA-DRIVEN TECHNOLOGY INTELLIGENCE: AN APPLICATION TO AIRCRAFT ENGINE MAINTENANCE
A. Dadashi, DLR, Germany
additional information (interactive) 15.9.R
0010		 REBUILDING AGRICULTURAL STATISTICS IN POST-WAR SUDAN: A STRATEGIC FRAMEWORK FOR RECOVERY AND RESILIENCE
N. Ahmed, Sudan
additional information (interactive) 15.9.R
0264		 PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE ? -PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE
L.Y. Hou¹, J.T. Liu¹, Y.L. Song¹, H. Xiao¹; ¹Nanjing University of Aeronautics and Astronautics, China

0.10SPEED MENTORING
Chair: The Speed Mentoring initiative aims to create meaningful interactions between students, early-career researchers, and experienced professionals from academia, industry, and government sectors through structured discussions and networking opportunities
16. Sep 26 17:20 19:00

Thursday, 17. Sep 2026

0.11GENERAL LECTURE 5 ISABE and the next generation of aircraft propulsion (by Frank Haselbach ISABE president)
Chair: R. Gerhards ICAS Treasurer
17. Sep 26 08:00 08:50

08:50 - 09:15COFFEE BREAK

1.10Explainable and Human-Centered AI in Aviation
Chair(s): Toebben, H.
Track 1 Pyrmont Theatre
15 - Guest lectures
17. Sep 26 09:15 09:40 1.10.1
0177		 EXPLAINABILITY AT ALL LEVELS OF SYSTEM DEVELOPMENT: INSIGHTS FROM THE DESIGN OF INTELLIGENT SYSTEMS IN AVIATION
J. Würfel¹, B. Djartov¹, M. Friedrich¹, S. Schog¹, A. Papenfuss¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 09:40 10:05 1.10.2
0359		 APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY DEVELOPING AN AI-BASED DIGITAL ASSISTANT FOR PILOTS
A. Mayima¹, C. Bejarano Espada¹, A. Gampe², A. Hamann², R. De Masellis¹, A. Fuchs¹, M. Athanasiadou¹, H. Palop¹, D. Watkins¹; ¹Collins Aerospace, Applied Research & Technology, Ireland ;²German Aerospace Center, Institute of Flight Guidance, Germany
17. Sep 26 10:05 10:30 1.10.3
0450		 OFFLINE MULTIMODAL LARGE LANGUAGE MODELS FOR DECISION SUPPORT IN AIR OPERATIONS
J.P.A. Dantas¹, J.A. Cunha¹, G. Dietzsch¹; ¹Instituto de Estudos Avançados, Brazil
17. Sep 26 10:30 10:55 1.10.4
0547		 AI IN THE COCKPIT: THE JARVIS STORY
R. De Masellis¹, A. Fuchs¹, A. Mayima¹, C. Bejarano Espada¹, M. Athanasiadou¹, H. Palop¹, D. Watkins¹; ¹Collins Aerospace, Applied Research & Technology, Italy
Presenter: Riccardo De Masellis, Collins Aerospace
2.10Aircraft Electrification: Certification Perspectives & Challenges
Chair(s): Schlickenmaier, H., van Dam, C.P.
Track 2 C4.1
15 - Guest lectures
17. Sep 26 09:15 09:40 2.10.1
0398		 ENTRY INTO SERVICE REQUIRES CERTIFICATION FOR NOVEL TECHNOLOGY
H. Schlickenmaier, HS Advanced Concepts LLC, United States; V. Schultz, Revolutionary Concepts LLC, United States; C. Baczynski, BAC Aerospace Inc, Canada; J, Maris, Flight Test Centre of Excellence d.b.a. Cert Center Canada, Canada; M. Cummings, Certification Engineering Services, LLC, United States; M. Traskos, Lectromec, United States
17. Sep 26 09:40 10:05 2.10.2
1106		 EXPERIENCES CERTIFYING INNOVATIVE VEHICLES IN AUSTRALIA
D. Peterson, Civil Aviation Safety Agency, Australia
17. Sep 26 10:05 10:30 2.10.3
1063		 PANEL DISCUSSION WITH H. SCHLICKENMAIER (MODERATOR), D. PETERSON, M. CUMMINGS, C. BACZYNSKI, J. MARIS AND M. TRASKOS (DURATION TIL END OF THE BLOCK)
P. Discussion,
3.10Military
Chair(s): Nagel, B.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 09:15 09:40 3.10.1
0155		 GEOMETRY PARAMETERISATION VIA A STRUCTURAL MODAL BASIS FOR AERODYNAMIC SHAPE OPTIMISATION
A. Wang¹, R. Carrese¹, L. Brown¹, J. Collins¹, P. Marzocca, RMIT University, Australia; ¹Boeing Aerostructures Australia, Australia
17. Sep 26 09:40 10:05 3.10.2
0201		 MODELLING COUPLED ON-BOARD SYSTEMS IN AIRCRAFT DESIGN
E. Espinosa-Juárez¹, A. Dell'Amico¹; ¹Linköping University, Sweden
17. Sep 26 10:05 10:30 3.10.3
0485		 MULTI-FIDELITY BAYESIAN NEURAL NETWORKS FOR STEALTH/AERODYNAMIC DATA FUSION METHOD
J.Y. He¹, H. Zhao¹; ¹Northwestern Polytechnical University, China
17. Sep 26 10:30 10:55 3.10.4
0515		 A UNIFIED PARAMETRIC MODELING METHOD FOR CONVENTIONAL, SEMI-BURIED, AND EMBEDDED INLETS
J.W. He¹, B.G. Mi¹, J.Y. Zhang¹; ¹School of Aeronautics of Northwestern Polytechnical University, China
additional information (interactive) 3.10.R
0578		 A RAPID AERODYNAMIC ASSESSMENT METHOD FOR BATTLE-DAMAGED CRUISE MISSILES
Zhengdong LUO¹, Baigang MI¹; ¹School of Aeronautics of Northwestern Polytechnical University, China
4.10High Speed Flight: Propulsion/Propulsion-Integration
Chair(s): Bowcutt, K., Neely, A.
Track 4 C4.3
15 - Guest lectures
17. Sep 26 09:15 09:40 4.10.1
1072		 THE DART HYPERSONIC VEHICLE: FROM CONCEPT TO LAUNCH
J. Sandral, Hypersonix, Australia
17. Sep 26 09:40 10:05 4.10.2
1073		 FROM FIRST ROTATING DETONATION ROCKET ENGINE (RDRE) FLIGHT TO HYPERSONIC RDRE FLIGHT
A. Duggleby, Venus Aerospace, United States
17. Sep 26 10:05 10:30 4.10.3
1074		 MACH 5 WIND TUNNEL TEST OF HIGH-MACH INTEGRATED CONTROL EXPERIMENT AIRCRAFT (HIMICO)
H. Taguchi, Tokio University of Science, Japan; T. Sato¹, C. Fujio¹, M. Tsue², T. Tsuchiya², S. Nakaya², K. Takizawa², A. Matsuo, Keio University, Japan; T. Hirotani³, H. Takahashi³, M. Hongoh³, A. Tezuka¹; ¹Waseda University, Japan ;²University of Tokyo, Japan ;³JAXA, Japan
17. Sep 26 10:30 10:55 4.10.4
1075		 PHYSICAL AND NUMERICAL MODELING OF SUPERSONIC COMBUSTION FOR HYPERSONIC FLIGHT
C. Fureby, Lund University, Sweden
5.10Propeller Aerodynamics and Rotor Flows
Chair(s): Rana, Z., Kiszkowiak, L.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 09:15 09:40 5.10.1
0654		 EPSILON V4: AN OPEN-SOURCE TOOL FOR EXTENDED AERODYNAMICS EXERGY ANALYSIS
C. Paillard¹, G. Bourreau-Tirel, Aura Aero and ISAE-SUPAERO, University of Toulouse, France; S. Duplaa¹, M. Fiore¹; ¹ISAE-SUPAERO, University of Toulouse, France
17. Sep 26 09:40 10:05 5.10.2
0795		 COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM
J. He¹, Y. Zhao¹, X. Wei¹, T. Chen¹, Y. Yang¹; ¹Northwestern Polytechnical University, China
17. Sep 26 10:05 10:30 5.10.3
0352		 HIGH-ALTITUDE PERFORMANCE AND ONE-DIMENSIONAL MODELING OF A DUAL-ROTOR GEROTOR PUMP FOR AEROENGINE LUBRICATION SYSTEMS
Z.C. Su, China; P.F. Zhu, China; G.L. Li, China; C.H. Zhong, China; Y.G. Lyu, China; T.S. Xie, China
17. Sep 26 10:30 10:55 5.10.4
0089		 OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT
D. Xue¹, Y. Gao¹, T. Wu¹, B. Song¹, W. Song¹; ¹Northwestern Polytechnical University, China
Presenter: Gao Yating, Northwestern Polytechnical University
6.10Advanced Measurement Technique
Chair(s): , , Allen, N.
Track 6 C4.5
03.2 - Experimental Aerodynamics
17. Sep 26 09:15 09:40 6.10.1
0749		 CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS
C. Marshall¹, N. Heath², D. Handford², J. Smith², P. Manovski¹, T. Avadiar¹, M. Jones¹, A. Neely²; ¹Defence Science and Technology Group, Australia ;²University of New South Wales, Australia
17. Sep 26 09:40 10:05 6.10.2
0133		 COMPARATIVE ATMOSPHERIC MEASUREMENTS USING UAV-MOUNTED ULTRASONIC ANEMOMETER AND DOPPLER LIDAR
N. Gavrilovic¹, D. Lanot¹, M. Bronz, ENAC, France; ¹ISAE-SUPAERO, France
Presenter: Nikola Gavrilovic, ISAE-SUPAERO
17. Sep 26 10:05 10:30 6.10.3
0775		 ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM
D.T. Rajeepan¹, N.J. Lawson¹, A. Galffy, Turbulence Solutions, Austria; ¹University of Sydney, Australia
17. Sep 26 10:30 10:55 6.10.4
0049		 WIND TUNNEL INVESTIGATION OF HELICOPTER LOADS DURING URBAN OPERATIONS ON A BUILDING WITH COLUMNAR VORTEX GENERATORS
J.C. Matias¹, R. Bardera¹, E. Barroso¹, J. Fernández¹; ¹INTA, Spain
7.10Flight Dynamics and Control
Chair(s): , , Grabowski, T.
Track 7 C4.6
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 09:15 09:40 7.10.1
0435		 SIMULATION-BASED AUTOPILOT TUNING FOR FIXED-WING UAVS
C.-V. Boruga¹, N. Zalewska¹, D. Lundström¹, P. Krus¹; ¹Linköping University, Sweden
17. Sep 26 09:40 10:05 7.10.2
0713		 A 3D-PRINTED TESTBED FOR FLIGHT CONTROL SYSTEM RESEARCH.
D. Lundström¹, C.-V. Boruga¹, S. Riethausen¹, R. Larsson¹; ¹Linköping University, Sweden
17. Sep 26 10:05 10:30 7.10.3
0138		 SLIPSTREAM MODELING AND CONTROL ALLOCATION OF A DISTRIBUTED HETEROGENEOUS ELECTRIC PROPULSION TANDEM-WING UAV
Y. Xie, School of Aeronautics, Northwestern Polytechnical University Cit, China; Z. Zhou, Northwestern Polytechnical University, China
17. Sep 26 10:30 10:55 7.10.4
0815		 RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAV WINGTIP-LINKED FLIGHT
R. Wang¹, Y. Wu¹, Z. Zhou¹, S. Yao¹, Z. Zhang¹; ¹Northwestern Polytechnical University, China
8.10Aeronautical R&D in Australia (4x15 Min Presentations then Panel Discussion)
Chair(s): Lawson, N.
Track 8 C4.7
15 - Guest lectures
17. Sep 26 09:15 09:40 8.10.1
1021		 EVTOL AND PROPULSION R&D IN THE SYDNEY PROPULSION LAB
D. Verstraete, Australia
17. Sep 26 09:40 10:05 8.10.2
1044		 LOW MACH NUMBER AEROACOUSTICS R&D AT UNSW SYDNEY
D. Moreau, UNSW, Australia
17. Sep 26 10:05 10:30 8.10.3
1045		 DRONE TECHNOLOGIES IN AUSTRALIA: FROM AIR-VEHICLE DEVELOPMENT TO AUTONOMOUS FLIGHT SYSTEMS
K.C. Wong, Australia
17. Sep 26 10:30 10:55 8.10.4
1050		 EXPERIMENTAL DEVELOPMENT OF HIGH-SPEED AEROSPACE SYSTEMS: CHALLENGES & OPPORTUNITIES
A. Neely, Australia
9.10Aeroelastic Analysis & Design 2
Chair(s): Ikeda, T., Muscarello, V.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
17. Sep 26 09:15 09:40 9.10.1
0141		 AN AEROELASTIC DYNAMICS MODELING METHOD FOR INSECT-INSPIRED FLEXIBLE FLAPPING-WING UAV
Y. Guo¹, W. Yang¹, X. Xu¹, Z. Li¹, J. Liu¹, S. Cao¹; ¹Northwestern Polytechnical University, China
17. Sep 26 09:40 10:05 9.10.2
0381		 ENABLING FORWARD SWEPT WING DESIGNS
F. Saachi¹, F. Healy¹, D. Rezgui¹, J. Cooper¹; ¹University of Bristol, United Kingdom
17. Sep 26 10:05 10:30 9.10.3
0452		 DEVELOPMENT OF CONTROL LAWS FOR ENHANCED PERFORMANCE AND AEROELASTIC STABILITY OF EVTOL AIRCRAFT
N. Demant, FH Aachen University of Applied Sciences, Germany; P. Kantzidis¹, G. Lazzaro, Polytechnic University of Milan, Italy; V. Muscarello¹; ¹Royal Melbourne Institute of Technology, Australia
17. Sep 26 10:30 10:55 9.10.4
0262		 AEROSERVOELASTIC MODELING AND ANALYSIS OF THRUST VECTORING LAUNCH VEHICLE CONSIDERING RIGID-ELASTIC INTERACTION
W.L. Lei, China; Y.S. Gu, China; Z.C. Yang, China
10.10Propulsion Optimization 1
Chair(s): , , Stephens, J.
Track 10 C4.9
05 - Propulsion and Energy
17. Sep 26 09:15 09:40 10.10.1
0110		 NOVEL METHODS FOR THE CHARACTERISATION OF INTAKE FLOW DISTORTION
J. Hueso-Rebassa¹, D. MacManus¹, R. Christie¹, J. Matesanz-Garcia¹, Y. Frey², C. Sheaf²; ¹Cranfield University, United Kingdom ;²Rolls-Royce plc., United Kingdom
17. Sep 26 09:40 10:05 10.10.2
0612		 RUBBER ENGINE INTEGRATED OPTIMIZATION STRATEGY FOR OVERALL AIRCRAFT DESIGN
J. Häßy¹, J. Schmeink¹, B. Fröhler¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 10:05 10:30 10.10.3
0111		 EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION
J. Hueso-Rebassa¹, D. MacManus¹, F. Tejero¹, T. Williams, Cambridge University, United Kingdom; Y. Frey², G. Thorne²; ¹Cranfield University, United Kingdom ;²Rolls-Royce plc., United Kingdom
17. Sep 26 10:30 10:55 10.10.4
0954		 AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES
F. Pak¹, U. Perra¹, F. Willems¹, T. Hofman¹, M. Salazar¹; ¹Eindhoven University of Technology, Netherlands
additional information (interactive) 10.10.R
0024		 ACTIVE THRUST BALANCING CONTROL OF A TURBOPUMP WITH A SWIRL BREAKER
S.M. Jeon, Korea Aerospace Research Institute, South Korea
additional information (interactive) 10.10.R
0426		 IGNIT3: AN INTEGRATED COMPUTATIONAL FRAMEWORK FOR NON-IDEAL THERMODYNAMIC ANALYSIS AND OPTIMIZATION OF TURBOJET AND TURBOFAN ENGINES
P. Gonzales-DeGreiff, New Granada Military University (UMNG), Colombia; J. Gonzalez-Mitte¹, G. Palaia², K. Salem², P. Bravo-Mosquera¹; ¹São Carlos School of Engineering, University of São Paulo (EESC , Brazil ;²Department of Mechanical and Aerospace Engineering, Politecnico , Italy
Presenter: Karim Abu Salem, Department of Mechanical and Aerospace Engineering
additional information (interactive) 10.10.R
0584		 INTELLIGENT FULL-ENVELOPE OPTIMIZATION OF TRANSIENT CONTROL LAWS FOR ADAPTIVE CYCLE ENGINES VIA TRANSFER LEARNING-ENHANCED DEEP REINFORCEMENT LEARNING
M. Qiao¹, Y.Z. Huang, Shenzhen Research Institute of NPU , China; L.F. Gou¹; ¹Northwestern Polytechnical University, China
11.10Flight Testing
Chair(s): Lee, C.H., Drupka, G.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 09:15 09:40 11.10.1
0624		 PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA
J.H. Wang¹, L.X. Wang¹, R. Zhao², Z. Wu², Y.F. Xu¹, H.L. Liu¹, S. Tai¹, T. Yue¹; ¹Beihang University, China ;²COMAC Shanghai Aircraft Customer Service Co. Ltd., China
17. Sep 26 09:40 10:05 11.10.2
0686		 PHYSICS-INFORMED MACHINE LEARNING FOR FLIGHT DYNAMICS IDENTIFICATION OF THE SAAB 340B USING FLIGHT TEST DATA
A. Navarro¹, M. Alam¹, A. Elliott¹, E. Jinks, Siemens Digital Industries Software, United Kingdom; ¹Cranfield University, United Kingdom
17. Sep 26 10:05 10:30 11.10.3
0518		 EVALUATION OF STALL BEHAVIOUR OF T-TAIL AIRCRAFT: MODELLING AND FLIGHT TEST
M. Lowenberg¹, D. Pusztai¹; ¹University of Bristol, United Kingdom
12.10Advanced Aircraft Design and Manufacturing
Chair(s): Jiang, L., Xi, L.
Track 12 C2.3
08 - Manufacturing and Supply Chain Management
17. Sep 26 09:15 09:40 12.10.1
0260		 MATERIAL-STRUCTURE INTEGRATED LASER ADDITIVE MANUFACTURING OF HIGH-PERFORMANCE PARTS FOR AERONAUTICAL APPLICATIONS
D.-D. Gu, Nanjing University of Aeronautics and Astronautics, China
17. Sep 26 09:40 10:05 12.10.2
0945		 A FORMALLY VERIFIED, EVENT-DRIVEN ROS SCADA SUPERVISORY SYSTEM ARCHITECTURE FOR SAFETY-CRITICAL ROBOTIC CELLS IN AEROSPACE MANUFACTURING
F. S. Braga¹, E. B. S. de Andrade¹, W. R. de Oliveira¹; ¹ITA, Brazil
Presenter: Wesley Oliveira, Aeronautics Institute of Technology (ITA)
17. Sep 26 10:05 10:30 12.10.3
0840		 RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING
T. Mahr¹, L. Whiteman¹, A. Daley¹, S. Hewa Witharange¹, J. Prpic¹, K. Holtta-Otto¹, M. Das¹; ¹University of Melbourne, Australia
Presenter: Lily Whiteman, University of Melbourne
13.10Global Airport and Network Operations
Chair(s): Mori, R.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
17. Sep 26 09:15 09:40 13.10.1
0995		 INNOVATION & TRANSFORMATION AT SINGAPORE CHANGI AIRPORT AND A CASE STUDY ON AI-ENABLED LINE MAINTENANCE OPERATIONS
T.L. Teck, Changi Airport Group, Singapore; D.S. Man Fung, Institutions of Engineers, Singapore
17. Sep 26 09:40 10:05 13.10.2
0329		 FEASIBILITY STUDY ON IMPROVING ARRIVAL-SEPARATION STABILITY THROUGH ARRIVAL TRAJECTORY ANALYSIS AT CONGESTED AIRPORTS
R. Kajikawa¹, N. Takeichi¹; ¹Tokyo Metropolitan University, Japan
17. Sep 26 10:05 10:30 13.10.3
0272		 AN AUGMENTED AIRPORT MODEL FOR GROUND OPERATIONS ANALYSIS: A CASE STUDY OF NARITA INTERNATIONAL AIRPORT
C.S.X. Ng¹, M. Schultz, University of Bundeswehr Munich, Germany; E. Itoh¹; ¹The University of Tokyo, Japan
17. Sep 26 10:30 10:55 13.10.4
0412		 A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN THE UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION
G. Enea¹, V. Mollwitz², T. Finck², T. Reynolds¹, B. Korn²; ¹MIT Lincoln Laboratory, United States ;²DLR Institute of Flight Guidance, Germany
14.10Maintenance Technologies
Chair(s): Jones, M,, Anderson, K.
Track 14 C2.5
11 - Operations and Sustainment
17. Sep 26 09:15 09:40 14.10.1
0803		 ON THE FEASIBILITY OF MACHINE LEARNING-BASED DETECTION OF AIRCRAFT LIGHTNING STRIKE RISK AREAS
E. Yoshikawa¹, S. Horishita², Y. Hamada², T. Ushio¹, V. Chandrasekar, Colorado State University, United States; ¹The University of Osaka, Japan ;²Japan Aerospace Exploration Agency, Japan
17. Sep 26 09:40 10:05 14.10.2
0716		 ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA
C. Klein¹, E. Arts¹, B. Atanasoaie¹, H. Meyer¹, F. Raddatz¹, Z. Daw, University of Stuttgart, Institute of Aircraft Systems, Germany; ¹German Aerospace Center (DLR), Germany
17. Sep 26 10:05 10:30 14.10.3
0244		 ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085
J. Rogers, RMIT University, Australia; I. Field¹, N. Tugwell¹, M. Salagaras¹, B. Dixon¹; ¹DSTG, Australia
17. Sep 26 10:30 10:55 14.10.4
0159		 FEMTOSECOND LASER PAINT STRIPPING ON AIRCRAFT COATINGS: EXPERIMENTAL AND NUMERICAL ASSESSMENT
S. Zhu¹, J. Panta¹, R. Yang¹, Y.X. Zhang, Univeristy of Technology Sydney , Australia; ¹Western Sydney University, Australia
additional information (interactive) 14.10.R
0134		 LIGHTWEIGHT AND ROBUST REAL-TIME DETECTION SYSTEM FOR AIRCRAFT SKIN DEFECTS UNDER COMPLEX UAV INSPECTION CONDITIONS
D. Tang¹, W. Yang¹, J. Xuan¹; ¹Northwestern Polytechnical University, China
15.10tbd1
Chair(s): ,
Track 15 C2.6

10:55 - 11:00CHANGEOVER BREAK

1.11AI in Aero Science 1
Chair(s): Citron, T., Prakasha, P.
Track 1 Pyrmont Theatre
15 - Guest lectures
17. Sep 26 11:00 11:25 1.11.1
0279		 LLM-ASSISTED GENERATION OF SYSML V2 MODELS FROM STRUCTURED ENGINEERING REPORTS
V. Voth¹, J. Wade, UCSD, United States; O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 11:25 11:50 1.11.2
1042		 DESIGN AND DEVELOPMENT OF A BLENDED WING BODY CONCEPT USING AUGMENTED INTELLIGENCE FOR SYSTEMS ENGINEERING
S. Pate, United States
17. Sep 26 11:50 12:15 1.11.3
0252		 BEYOND THE HARDWARE: REGULATION AND CERTIFICATION AS THE CRITICAL PATH TO ADF AUTONOMOUS CAPABILITY
K. Joyce¹, K. Joiner¹, V. Daria, Royal Australian Air Force, Australia; J. Young¹; ¹University of New South Wales, Australia
17. Sep 26 12:15 12:40 1.11.4
1049		 A CASE STUDY OF CONTEXT OPERATIONS WITH LARGE LANGUAGE MODELS FOR THE SYSTEMS ARCHITECTURE DESIGN OF A HEAVY SAR UAV
P. Krus, Sweden; V. Kaster Marini, Sweden
2.11Australian Air Mobility
Chair(s): Palmer, J.
Track 2 C4.1
15 - Guest lectures
17. Sep 26 11:00 11:25 2.11.1
1083		 IMPLICATIONS OF AAM OPERATIONS FOR FUTURE SHARED AIRSPACE IN VICTORIA, AUSTRALIA
J.L. Palmer¹, C. Zhang¹, Y. Xie¹, M. Alidadi¹, A. Bubb¹, M.J. Hasan¹, N. Kumar¹, D. Notman¹; ¹RMIT University, Australia
17. Sep 26 11:25 11:50 2.11.2
0988		 A HOLISTIC APPROACH TO ENABLE ADVANCED AIR MOBILITY FOR REGIONAL, RURAL AND REMOTE AUSTRALIA
P. Burka¹, P. Smith¹; ¹Swinburne University of Technology, Australia
17. Sep 26 11:50 12:15 2.11.3
1017		 THE ROLE OF COMMUNITY ENGAGEMENT IN INTRODUCING UNMANNED AERIAL VEHICLE TECHNOLOGY: A RAPID SCOPING REVIEW
J. Porter, Australia
17. Sep 26 12:15 12:40 2.11.4
1084		 OPTIMISING THE HUMAN FACTORS IN ADVANCED AIR MOBILITY
K. Stevens, please select...
3.11Aerostructures
Chair(s): Gibson, T.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 11:00 11:25 3.11.1
0042		 HIGH-FIDELITY DATASET-BASED SHAPE AND STRUCTURE OPTIMIZATION FOR AIRCRAFT DESIGN
M. Maier¹, K. Sørensen-Libik², Ö. Petersson², C. Breitsamter¹; ¹Technical University of Munich (TUM), Germany ;²Airbus Defence and Space GmbH, Germany
17. Sep 26 11:25 11:50 3.11.2
0034		 MULTI-OBJECTIVE OPTIMISATION OF AERIAL VEHICLES USING REINFORCEMENT LEARNING
T. Batty, Defence Science and Technology Group, Department of Defence, Australia
Presenter: Trevor Batty, Defence Science And Technology Group
17. Sep 26 11:50 12:15 3.11.3
0100		 INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING
Y.Y. Ma, China; W.Y. Wei, China; Y.Q. Du, China; M. Abouhamzeh, Netherlands; Z.H. Han, China
17. Sep 26 12:15 12:40 3.11.4
0609		 COMPARISON OF FLEXIBLE AIRCRAFT CONFIGURATIONS USING AEROELASTIC ANALYSIS
N. Okubo¹, N. Morita, Velocity Aeroworks .Inc, Japan; T. Tuchiya¹; ¹The University of Tokyo, Japan
4.11CFD Needs and Progress Towards Vision 2030 & Beyond
Chair(s): Coder, J., Azevedo, J.
Track 4 C4.3
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 11:00 11:25 4.11.1
0998		 CFD VISION 2030 PROGRESS AND NEXT STEPS
J. P. Slotnick, United States
17. Sep 26 11:25 11:50 4.11.2
1000		 GEOMETRY AND MESHING ADVANCEMENTS TOWARD CFD VISION 2030
N. J. Wyman, Cadence Design Systems, Inc., United States
17. Sep 26 11:50 12:15 4.11.3
1022		 THE ROLE OF NEXT-GENERATION HPC AND MACHINE LEARNING IN ACHIEVING THE 2030 VISION GOALS
N.J. Wyman, Cadence Design Systems, Inc., United States; N. Ashton, NVIDIA, United States
17. Sep 26 12:15 12:40 4.11.4
0999		 CFD VISION 2030 LOOKING FORWARD: PANEL DISCUSSION WITH J.CODER, J.P.SLOTNICK, N.J.WYMAN, C.WINKLER
J. Coder, United States
5.11Applied CFD Approaches
Chair(s): , , Imamura, T.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 11:00 11:25 5.11.1
0193		 EFFECTS OF FLAPPING–PITCHING PHASE DIFFERENCE ON THE AERODYNAMIC PERFORMANCE OF HOVERING DRAGONFLY WINGS
H. Wang¹, J. Wang¹, Z. Li¹, W. Yang¹, X. Yang¹; ¹Northwestern Polytechnical University, China
17. Sep 26 11:25 11:50 5.11.2
0281		 UNCERTAINTY QUANTIFICATION AND CROSS-CORRELATION EFFECTS IN AERODYNAMIC COEFFICIENTS DERIVED QUANTITIES
L. Pirillo¹, R. Bianchini¹, D. Palma¹, F. Stella¹; ¹Sapienza University of Rome, Italy
17. Sep 26 11:50 12:15 5.11.3
0720		 A STALL EXTENSION TO LIFTING-LINE THEORY: IMPLEMENTATION AND VALIDATION IN ASWING
L. Avoni¹, M. Bronz¹, J.-M. Moschetta¹, J.-P. Condomines¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France
17. Sep 26 12:15 12:40 5.11.4
0462		 RESEARCH ON AERODYNAMIC-STEALTH INTEGRATED DESIGN METHODOLOGY BASED ON MPPO ALGORITHM
K. Gan¹, H. Zhao¹, S. Wang¹; ¹Northwestern Polytechnical University, China
Presenter: Zhengang Zhang, Northwestern Polytechnical University
6.11Flow Separation and Control
Chair(s): Jagadeesh, C.
Track 6 C4.5
03.2 - Experimental Aerodynamics
17. Sep 26 11:00 11:25 6.11.1
0203		 STATIC AND DYNAMIC WIND-TUNNEL TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES
D. Farcy¹, S. Prince², M. Alam², G. Tanguy¹, N. Vauchel¹, A. Proenca²; ¹ONERA, France ;²Cranfield University, United Kingdom
17. Sep 26 11:25 11:50 6.11.2
0232		 EXPERIMENTAL INVESTIGATION OF WISHBONE VORTEX GENERATOR EFFECTS ON THE NACA 4412 AIRFOIL AT LOW REYNOLDS NUMBERS
D. Domínguez¹, F. Parra¹, D. López¹, A. García-Gutiérrez¹; ¹Universidad de León, Spain
17. Sep 26 11:50 12:15 6.11.3
0763		 WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS
L. Malicki¹, M. Marciniuk¹, L. Kiszkowiak², P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; S. Kachel²; ¹Wroclaw University of Science and Technology, Poland ;²Military University of Technology, Poland
Presenter: Łukasz Kiszkowiak, Military University of Technology
17. Sep 26 12:15 12:40 6.11.4
0427		 DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE.
E. Barroso, instituto Nacional de Técnica Aeroespacial (INTA),, Spain; R. Bardera¹, J.C. Matías¹, J. Fernández¹, A.A. Rodríguez Sevillano, Universidad Politécnica de Madrid, Spain; ¹Instituto Nacional de Técnica Aeroespacial (INTA),, Spain
7.11Flight Simulation and Testing
Chair(s): , , Stekovic, S.
Track 7 C4.6
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 11:00 11:25 7.11.1
0156		 FLIGHT TRIALS OF DRONES CONTROLLED BY AI LARGE LANGUAGE MODELS
S. Crase¹, S. Pywell¹, K. Rosser¹; ¹Defence Science and Technology Group, Australia
17. Sep 26 11:25 11:50 7.11.2
0204		 FAMILIARIZATION, OPERATION, AND DEBRIEFING: AN ADAPTIVE AUGMENTED REALITY SUPPORT SYSTEM FOR UAV FLIGHT TESTING
M. Zintl¹, F. Holzapfel¹; ¹Technical University of Munich, Germany
17. Sep 26 11:50 12:15 7.11.3
0289		 ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES
K. Thomessen¹, S. Schopferer¹, P. Nagarajan¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 12:15 12:40 7.11.4
0513		 INFORMATIVE PATH PLANNING BASED ON REDUCED-RANK GAUSSIAN PROCESS FOR HAZARDOUS SUBSTANCE MONITORING
M. Lee¹, M. Park¹; ¹Changwon National Unviersity, South Korea
8.11Monash University Aero Research
Chair(s): Mazharmanesh, S.
Track 8 C4.7
15 - Guest lectures
17. Sep 26 11:00 11:25 8.11.1
1085		 PASSIVE FLOW CONTROL OF A TURBULENT BOUNDARY LAYER AT THE VERGE OF SEPARATION USING SURFACE ROUGHNESS
C. Meglio¹, Z. Chen¹, B. Sun¹, C.S. Greco, University of Naples, Italy; C. Atkinson¹, J. Soria¹; ¹Monash University, Australia
17. Sep 26 11:25 11:50 8.11.2
1082		 MECHANISMS OF SCREECH MODE STAGING IN UNDEREXPANDED SUPERSONIC JETS
S. Mazharmanesh¹, J. Weightman¹, P.A.S. Nogueira¹, D. Edgington-Mitchell¹; ¹Monash University, Australia
17. Sep 26 11:50 12:15 8.11.3
1091		 SOME OBSERVATIONS ON DEEP STALL LANDING, WITH APPLICATION TO SMALL UNMANNED AIRCRAFT
P. Gupta, Monash University, Australia
17. Sep 26 12:15 12:40 8.11.4
1105		 LOWERING THE BARRIER TO AEROACOUSTIC PREDICTION: GPU-COMPUTED SBES FOR FAR-FIELD LANDING GEAR NOISE PREDICTION
B. Edmonds¹, A. Romesh¹, L. Clark¹; ¹LEAP, Australia
9.11Student Final
Chair(s): Rein Weston, K.
Track 9 C4.8
17. Sep 26 11:00 11:25 9.11.1
1116		 EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY
I. Frascareli Ali, Brazil
17. Sep 26 11:25 11:50 9.11.2
1115		 A MIXED REALITY FRAMEWORK FOR EVALUATING AIRCRAFT PRE-FLIGHT WALK-AROUND TRAINING
M. Higinio, Australia
17. Sep 26 11:50 12:15 9.11.3
1113		 TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS
B. van Magill, Australia
17. Sep 26 12:15 12:40 9.11.4
1114		 VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, CRANKED SWEPT WING
N. van Luijk, Netherlands
10.11Propulsion Optimization 2
Chair(s): Bezos O Connor, G.
Track 10 C4.9
05 - Propulsion and Energy
17. Sep 26 11:00 11:25 10.11.1
0906		 INLET OPTIMIZATION DESIGN OF A BOUNDARY LAYER INGESTION PROPULSION SYSTEM
X.K. Ma¹, H.C. Yang¹, K. You¹, R.B. Zhu¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China
Presenter: Rongbo Zhu, Northwestern Polytechnical University
17. Sep 26 11:25 11:50 10.11.2
0314		 PD-STGNN: A PHYSICS-INFORMED DYNAMIC SPATIO-TEMPORAL GRAPH NEURAL NETWORK FOR AERO-ENGINE THRUST PREDICTION
C. Song¹, H. Shi¹, Z. Huang¹, H. Xiao¹; ¹Northwestern Polytechnical University, China
17. Sep 26 11:50 12:15 10.11.3
0579		 PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES
T.Q. Dinh¹, H.X. Vu¹, A.C. Pham¹, L.D. Chu¹; ¹Viettel Aerospace Institute, Vietnam
additional information (interactive) 10.11.R
0148		 ADAPTIVE PREDICTION HORIZON-BASED MODEL PREDICTIVE CONTROL FOR AERO ENGINE
G.A. Liang¹, L.F. Gou¹, L.J. Lu¹; ¹School of Power and Energy,Northwestern Polytechnical University, China
additional information (interactive) 10.11.R
0149		 ROBUST FAULT DIAGNOSIS FOR AERO-ENGINE NETWORKED CONTROL SYSTEMS UNDER TRANSMISSION UNCERTAINTIES
L.J. Lu¹, Y.Z. Chen¹, G.A. Liang¹, L.F. Gou¹; ¹School of Power and Energy,Northwestern Polytechnical University, China
11.11Performances
Chair(s): Kwiek, A., Matsuno, Y.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 11:00 11:25 11.11.1
0306		 STUDY ON DAMAGE SEVERITY ASSESSMENT METHODS FOR ASYMMETRICALLY DAMAGED LOITERING MUNITIONS
M.X. Zhang¹, Y.S. Zhang, Chinese Flight Test Establishment, China; B.G. Mi¹, Y. Liu¹, R.Q. Wang¹; ¹Northwestern Polytechnical University, China
17. Sep 26 11:25 11:50 11.11.2
0372		 GAIN OPTIMIZATION FOR CASCADED INDI CONTROL WITH INTEGRATED PERFORMANCE AND ROBUSTNESS REQUIREMENTS
D. Surmann¹, S. Myschik¹; ¹University of the Bundeswehr Munich, Germany
17. Sep 26 11:50 12:15 11.11.3
0630		 LATERAL-DIRECTIONAL HANDLING AND FLYING QUALITIES ASSESSMENT OF A BLENDED WING BODY (BWB) ACFA 2020 CONFIGURATION
M. Alam¹, J. Renault¹, M. Hromcik², T. Hanis²; ¹Cranfield University, United Kingdom ;²Czech Technical University, Czech Republic
17. Sep 26 12:15 12:40 11.11.4
0539		 FLIGHT PERFORMANCE ANALYSIS OF ELECTRIC AIRCRAFT UNDER MOTOR FAILURE CONDITIONS USING REDUCED-ORDER MODELING
L. Hein¹, S. Myschik¹; ¹University of the Bundeswehr Munich, Germany
additional information (interactive) 11.11.R
0106		 AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE
R. Wang¹, Y. Liu¹, M. Zhang¹; ¹Northwestern Polytechnical University, China
12.11Additive Manufacturing and Intelligent Manufacturing
Chair(s): van Manen, R., Xi, L.
Track 12 C2.3
08 - Manufacturing and Supply Chain Management
17. Sep 26 11:00 11:25 12.11.1
0124		 BALANCING STRENGTH AND THERMAL CONDUCTIVITY IN LPBF-PROCESSED ALUMINUM-BASED MATERIALS
H. Zhang¹, L. Wang¹, D.D. Gu¹; ¹Nanjing University of Aeronautics and Astronautics, China
17. Sep 26 11:25 11:50 12.11.2
0140		 3D ANALYSIS AND PREDICTION FOR ASSEMBLY STEP DEVIATIONS OF FOUR-BAR LINKAGE BAY DOORS
R. Yang¹, L.K. Yang¹, L. Wei¹, S.Y. Sun¹; ¹Dalian University of Technology, China
17. Sep 26 11:50 12:15 12.11.3
0270		 A NOVEL DUAL-PHASE BAYESIAN ESTIMATION AND MULTI-TASK LEARNING METHOD FOR PROCESS OPTIMIZATION FOR REDUCING LACK-OF-FUSION DEFECTS DURING LASER POWDER BED FUSION
Y.S. Chen¹, D.D. Gu¹; ¹Nanjing University of Aeronautics and Astronautics, China
17. Sep 26 12:15 12:40 12.11.4
0766		 A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING
Y.A.D. Martins¹, C.C.D. Silva¹, D.A. Rade¹, J.M.G. Mello², A.V.S. Silva², A.P.C. Cuco²; ¹Aeronautics Institute of Technology, Brazil ;²Embraer S. A., Brazil
Presenter: Caroline Silva, Aeronautics Institute of Technology
13.11AAM Trajectory and Integration
Chair(s): Li, M.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
17. Sep 26 11:00 11:25 13.11.1
0292		 THREE-DIMENSIONAL ADAPTIVE TRAJECTORY OPTIMIZATION FOR RPAS-BASED ATMOSPHERIC MEASUREMENTS
K.A. Buchtal¹, A. Lau¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 11:25 11:50 13.11.2
0605		 GEOMETRY-DRIVEN AIR TRAFFIC CONFLICT RESOLUTION VIA CAUCHY-STOKES RANDERS METRIC
F. Wu, China; Y. He, China; J. Guo, China; Y. Wang, China; Z. Gao, China
17. Sep 26 11:50 12:15 13.11.3
0682		 EXPLORING DETROIT METROPOLITAN WAYNE COUNTY AIRPORT AS A TESTBED FOR RESOLVING INTEGRATION CHALLENGES FOR AIR TAXI OPERATIONS
S. Abdulhak, University of Michigan, Industrial and Operations Engineering, United States; B. Donaldson¹, A. Kamat¹, K. Hu¹, Z. Huang¹, M.Z. Li, University of Michigan, United States; ¹University of Michigan, Aerospace Engineering, United States
17. Sep 26 12:15 12:40 13.11.4
0946		 STANDARDIZED TAKE-OFF AND LANDING PROCEDURES FOR AIR TAXIS: URBAN AIR MOBILITY
F. Naeem¹, V. Gollnick¹; ¹Hamburg University of Technology, Germany
14.11Operations Optimisation
Chair(s): Verhagen, W., Stamoulis, K.
Track 14 C2.5
11 - Operations and Sustainment
17. Sep 26 11:00 11:25 14.11.1
0315		 FLIGHT MISSION MODELING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION
Z.L. Zengerling¹, A. Lau¹, M. Clococeanu¹, R. Kanitz¹, J. Schwengler², A. Vogel², K. Abu-Taa²; ¹German Aerospace Center (DLR), Germany ;²Rolls-Royce Deutschland, Germany
17. Sep 26 11:25 11:50 14.11.2
0611		 PROVIDING SENSOR INFORMATION FOR BOARDING TIME PREDICTION
M. Schultz¹, S. Göppel¹, S. Reitmann, University of Technology Chemnitz, Germany; ¹University of the Bundeswehr Munich, Germany
17. Sep 26 11:50 12:15 14.11.3
0396		 INVESTIGATION OF DECARBONISATION PATHWAYS FOR SHORT HAUL AVIATION USING A DISCRETE OPTIMISATION DECISION-MAKING ALGORITHM
N. Barry¹, C. Gallagher¹, C. Stuart¹; ¹Trinity College Dublin, Ireland
17. Sep 26 12:15 12:40 14.11.4
0031		 ASSESSING AIRLINE PURCHASE MOTIVATION FOR HYDROGEN AIRCRAFT UNDER FUTURE CORSIA
Hiroko Nakamura, The University of Tokyo, Japan
additional information (interactive) 14.11.R
0822		 LOSS OF RELIABILITY OF NEW GENERATION ENGINES: THE CASE STUDY OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION AS A SYSTEM OF SYSTEMS
A. Sanchez Mata, SANMATC Aircraft Technical & Financial Consulting, Mexico; E. Espinosa Juarez¹, A.M. Zarate Villazon², B. Ravikanti², H. Szöke-Erös³, P. Shiva Prakasha³, L. Knöös Franzén¹; ¹Linköping University, Sweden ;²Georgia Institute of Technology, United States ;³German Aerospace Center (DLR), Germany
15.11tbd2
Chair(s): ,
Track 15 C2.6

12:40 - 13:40LUNCH BREAK

1.12AI in Aero Science 2
Chair(s): Prakasha, P., Citron, T.
Track 1 Pyrmont Theatre
15 - Guest lectures
17. Sep 26 13:40 14:05 1.12.1
1018		 HYBRID AI-SIMULATION FOR AERODYNAMICS APPLICATIONS
D. Gueyffier, ONERA, France
17. Sep 26 14:05 14:30 1.12.2
1043		 BEYOND AI HYPE: TRUST, EVALUATION, AND HUMAN JUDGEMENT IN AEROSPACE ENGINEERING
J. Pinon Fischer, Georgia Institute of Technology, United States
17. Sep 26 14:30 14:55 1.12.3
0990		 APPLICATION OF AI IN AEROSPACE AND IMPLICATIONS FOR AEROSPACE ENGINEERS
T. Citron, United States
17. Sep 26 14:55 15:20 1.12.4
0479		 AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS
Y.L. Ren¹, L.F. You¹, X.H. Gao¹, Z.Q. Wang¹, C.Y. Chang¹, Z.Q. Guo¹; ¹Beihang University, China
2.12ICAS Digital Pioneering Initiative
Chair(s): Nagel, B., Crossley, W.
Track 2 C4.1
15 - Guest lectures
17. Sep 26 13:40 14:05 2.12.1
1107		 PIONEERING THE EXCHANGE OF KNOWLEDGE IN AIRCRAFT DESIGN
B. Nagel, DLR, Germany; P. Schmollgruber, ONERA, France
17. Sep 26 14:05 14:30 2.12.2
1108		 DIGITAL ENGINEERING IN THE AGE OF AI AS BASIS FOR SYSTEM OF SYSTEMS ENGINEERING
J. Abulawi¹, C. Jouannet, SAAB, Sweden; P. Prakasha¹; ¹DLR, Germany
17. Sep 26 14:30 14:55 2.12.3
1109		 VR FOR CABIN DESIGN AND CERTIFYING DIGITAL MRO MEASURES
T. Fadda, Uni Bologna, Italy; A.K. Koschlik, DLR, Germany; M. Scott, RMIT, Australia
17. Sep 26 14:55 15:20 2.12.4
1110		 HYPERSONIC TRANSPORT AND WAY FORWARDS WITH THE ICAS DIGITAL PIONEERING INITIATIVE
N. Viola,
3.12Aero Optimization
Chair(s): Gibson, T.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 13:40 14:05 3.12.1
0894		 INVERSE AIRFOIL DESIGN USING AERODYNAMICALLY CONDITIONED VARIATIONAL AUTOENCODERS
K. Swannet¹, N.A.K. Doan, Imperial College London, United Kingdom; C. Varriale¹; ¹Delft University of Technology, Netherlands
17. Sep 26 14:05 14:30 3.12.2
0393		 ADAPTIVE-PREFERENCE MULTI-OBJECTIVE REINFORCEMENT LEARNING FOR WIDE-SPEED-REGIME AIRFOIL OPTIMIZATION
Z.X Li¹, Z.H Han¹, K. Song¹, K.S Zhang¹; ¹Northwestern Polytechnical University, China
17. Sep 26 14:30 14:55 3.12.3
0254		 AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS
J. Wu, China; W. Song, China; H. Nie, China; C. Liu, China
17. Sep 26 14:55 15:20 3.12.4
0476		 DATA-DRIVEN SHAPE PARAMETERIZATION FOR EFFECTIVE AERODYNAMIC DESIGN OPTIMIZATION OF PROPELLERS
W. Lin¹, C.C. Nian¹, J.C. Li¹; ¹Northwestern Polytechnical University, China
Reserve Paper 3.12.R
0458		 RESEARCH ON GENERALIZED REPRESENTATION OF FLYING-WING CONFIGURATIONS BASED ON DEEP LEARNING
X.M. zhang, China; H. Zhao, China; Z. Gong, China
Presenter: He He
additional information (interactive) 3.12.R
0273		 DATA-DRIVEN FAST NOISE PREDICTION OF AN UNCONVENTIONAL AIRCRAFT USING HIGH-FIDELITY SIMULATION DATA
D. Eisenhut, Germany; A. Strohmayer, Germany
additional information (interactive) 3.12.R
0577		 RESEARCH ON AERODYNAMIC-STRUCTURAL RAPID EVALUATION AND OPTIMIZATION METHODS FOR JOINED-WING CONFIGURATIONS
X. Tang¹, B.G. Mi¹; ¹Northwestern Polytechnical University, China
4.12Propulsion/Airframe and BLI Integration
Chair(s): van Dam, C.P., Vijgen, P.
Track 4 C4.3
15 - Guest lectures
17. Sep 26 13:40 14:05 4.12.1
1059		 OVERVIEW OF PROPULSION-AIRFRAME INTEGRATION RESEARCH AT NASA (PART I)
J. Stevens, NASA, United States
17. Sep 26 14:05 14:30 4.12.2
1060		 OVERVIEW OF PROPULSION-AIRFRAME INTEGRATION RESEARCH AT NASA (PART II)
J. Stephens, United States
17. Sep 26 14:30 14:55 4.12.3
1061		 BLI/PROPULSION STUDIES AT TU DELFT (PART I)
J. Melkert¹, G. Rao¹; ¹TU Delft, Netherlands
17. Sep 26 14:55 15:20 4.12.4
1062		 BLI/PROPULSION STUDIES AT TU DELFT (PART II)
J. Melkert¹, G. Rao¹; ¹TU Delft, Netherlands
5.12UAS and AAM Design Applications
Chair(s): , , Huyssen, J.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 13:40 14:05 5.12.1
0238		 SUPERIOR CRUISE EFFICIENCY OF A NOVEL EVTOL CONFIGURATION FEATURING INCLINED PROPELLERS AND A PARASOL WING
E. Shima¹, K. Yonezawa, CRIEPI, Japan; M. Sato, Kogakuin Univ., Japan; A. Oyama¹; ¹JAXA, Japan
Presenter: Eiji Shima
17. Sep 26 14:05 14:30 5.12.2
0196		 PREDICTION OF PROPELLER NOISE IN LOW REYNOLDS NUMBER OPERATION USING MACHINE LEARNING MODELS
M. de Rosa Jacinto¹, D. Skrna¹, M. Berens¹; ¹Technische Universität Wien, Austria
17. Sep 26 14:30 14:55 5.12.3
0197		 INTEGRATION OF ACOUSTIC LINERS AND INTERNAL BYPASS CHANNELS INTO AAM PROPELLERS FOR NOISE REDUCTION
D. Skrna¹, M. de Rosa Jacinto¹, M. Berens¹; ¹Technische Universität Wien, Austria
17. Sep 26 14:55 15:20 5.12.4
0280		 A COMPARATIVE STUDY OF THE AERODYNAMIC CHARACTERISTICS OF FOUR CONFIGURATIONS
K. You, China; R. Zhu, China; Z. Chen, China
Presenter: Rongbo Zhu
6.12Challenges in Wind Tunnel Testing
Chair(s): Jagadeesh, C., Allen, N.
Track 6 C4.5
03.2 - Experimental Aerodynamics
17. Sep 26 13:40 14:05 6.12.1
0592		 PROPOSAL FOR DISTINGUISHING USABLE DATA UNDER HIGH WIND TUNNEL BLOCKAGE USING AN RAE2822 TEST CASE
H. Mohsin¹, S.A. Prince¹, D. Di Pasquale¹; ¹Cranfield University, United Kingdom
Presenter: Davide Di Pasquale, Cranfield University
17. Sep 26 14:05 14:30 6.12.2
0151		 EXPERIMENTAL VALIDATION OF A COANDA-BASED FLUIDIC THRUST VECTORING NOZZLE USING A HIGH-SPEED WIND TUNNEL
N. Schwagerus¹, M. Stößel¹, D. Kozulovic¹; ¹University of the Bundeswehr Munich, Germany
17. Sep 26 14:30 14:55 6.12.3
0790		 FORCE RECONSTRUCTION TECHNIQUES FOR DYNAMIC LOAD ESTIMATION ON GENERIC GEOMETRIES IN LOW-SPEED WIND TUNNEL TESTING
C. Brown, RMIT university, Australia; J. McCarthy¹, C. Marshall¹, M. Jones¹, I. Maatz, Air Force Research Laboratory (AFRL), United States; ¹Defence Science and Technology Group (DSTG), Australia
17. Sep 26 14:55 15:20 6.12.4
0428		 METROLOGY METHODS FOR ISOLATING PROFILE FORM, WAVINESS, STEPS, AND TWIST FROM SCANS OF SMALL-SCALE LAMINAR FLOW WIND TUNNEL MODELS
C. Hiemcke¹, R. Buth¹, C. Schneider¹, C.J. Jones¹; ¹General Atomics Aeronautical Systems, Inc., United States
7.12Guidance and Path Planning
Chair(s): , , Hristozov, S.
Track 7 C4.6
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 13:40 14:05 7.12.1
0859		 VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A PHYSICS-AUGMENTED TEMPORAL RESIDUAL NETWORK APPROACH
Z. Zhang¹, S. Li¹, X.P. Xu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China
17. Sep 26 14:05 14:30 7.12.2
0128		 CASCADE ADRC FOR TRAJECTORY TRACKING OF A FLYING-WING SOLAR AIRCRAFT UNDER WIND DISTURBANCES
S. Song¹, X. Zhu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China
17. Sep 26 14:30 14:55 7.12.3
0259		 EXPERIMENTAL FLIGHT DYNAMICS AND CONTROL OF AN AGILE FIXED-WING UAV USING HYBRID ONBOARD AND OFFBOARD CONTROL
Y. Huang, Australia; K.C. Wong, Australia
17. Sep 26 14:55 15:20 7.12.4
0771		 IMPLEMENTATION OF DISTRIBUTED SWARM GUIDANCE ALGORITHMS ON LOW-COST UAVS
J. McGuire¹, B. McIvor¹, S. Crase¹; ¹DSTG, Australia
8.12tbd5
Chair(s): ,
Track 8 C4.7
9.12Aircraft Design
Chair(s): Han, J., Kantzidis, P.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
17. Sep 26 13:40 14:05 9.12.1
0628		 CRITICAL LOAD-CASE AND CONSTRAINT IDENTIFICATION FOR PRELIMINARY COMPOSITE WING SIZING USING RAPID DESIGN TOOLS
Y. Pan¹, M. Alam¹; ¹Cranfield University, United Kingdom
17. Sep 26 14:05 14:30 9.12.2
0230		 NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL
V.N. Mueller¹, N. Singer¹, N. Moser¹, T. Siemer¹, F. Daoud¹; ¹Technical University of Munich, Germany
17. Sep 26 14:30 14:55 9.12.3
0211		 AIRCRAFT MASS EVALUATION MODEL: FROM TUBE-AND-WING TO BLENDED WING BODY USING WHALE.
V. Priasso¹, A. Lannoo¹; ¹DMAS, ONERA, 59000, Lille, France, France
10.12CRM-HL 2
Chair(s): Rivers, M.
Track 10 C4.9
03.2 - Experimental Aerodynamics
17. Sep 26 13:40 14:05 10.12.1
0793		 A COMPARATIVE WMLES STUDY OF THE CRM-HL IN FREE-AIR AND IN THE NTF FACILITY
V.C.B. Sousa¹, E. Sozer², K. Ravikumar¹, S.S. Hosseini², J. Duensing²; ¹Analytical Mechanics Associates, United States ;²NASA, United States
17. Sep 26 14:05 14:30 10.12.2
0896		 MODELLING SENSITIVITIES IN THREE-DIMENSIONAL FZRA-SPECTRUM ICE-SHAPE PREDICTION FOR THE CRM-HL STOWED CONFIGURATION
S. Min¹, D. Di Pasquale¹, H. Moshin¹, A. Vincent¹, S. Prince¹, D. MacManus¹; ¹Cranfield University, United Kingdom
17. Sep 26 14:30 14:55 10.12.3
0977		 ICING EFFECT EXPERIMENTS ON THE NASA HIGH-LIFT COMMON RESEARCH MODEL
S. Prince¹, D. MacManus¹, D. Di Pasquale¹, A. Vincent¹, A. Sharma¹, S. Daniels¹, K.K. Hood, The Boeing Company, United States; M.B. Rivers², C.S. Winski², T.A. Ozoroski, NASA Glenn Research Center, United States; P. White³, J. Brown³, S. Gates*, M. Schulz*, C. Jux*, H. Quix*, G. Dietz*; ¹Cranfield University, United Kingdom ;²NASA Langley Research Center, United States ;³Airbus, United Kingdom ;*European Transonic Windtunnel, Germany
17. Sep 26 14:55 15:20 10.12.4
0844		 CROSS-TEST COMPARISONS AND REYNOLDS NUMBER EFFECTS IN THE CRM-HL ECOSYSTEM
C.S. Winski¹, M. Rivers¹, S.S. Hosseini¹; ¹NASA, United States
Presenter: Courtney Winski
11.12Flight Dynamics
Chair(s): , , Jouannet, C.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 13:40 14:05 11.12.1
0191		 MULTI-BODY DYNAMIC MODELING OF A BIRD-LIKE FLAPPING-WING VEHICLE: ANALYSIS OF FLAPPING-AERODYNAMIC COUPLING EFFECTS
L.B. Zhou¹, B.F. Song¹, Y.C. Liu¹, M.X. Chen, COMAC Shanghai Aircraft Manufacturing Co., Ltd., China; Q. Fu¹; ¹Northwestern Polytechnical University, China
17. Sep 26 14:05 14:30 11.12.2
0206		 AIRCRAFT BUFFET QUANTIFICATION
J. Luo, The Boeing Company, United States
17. Sep 26 14:30 14:55 11.12.3
0658		 A NEW APPROACH TO MODELLING THE FLIGHT DYNAMICS OF A TAILLESS AIRCRAFT
A. Kwiek¹, K. Kania¹; ¹Warsaw University of Technology, Poland
12.12Advanced Forming Technology for Aviation
Chair(s): Gu, D.
Track 12 C2.3
08 - Manufacturing and Supply Chain Management
17. Sep 26 13:40 14:05 12.12.1
0126		 PROCESS OPTIMIZATION, MANUFACTURING QUALITY AND MECHANICAL PROPERTIES OF HIGH-VOLUME-FRACTION TIB2 REINFORCED AL-BASED COMPOSITES PREPARED BY SELECTIVE LASER MELTING
L. Xi, China; Z. Wang, China; D.D. Gu, China
17. Sep 26 14:05 14:30 12.12.2
0286		 HIGH-RATE AUTOMATED STAMP FORMING OF CF/LM-PAEK COMPOSITES FOR NEXT-GENERATION UAV AEROSTRUCTURES
M. Ravandi¹, G. Miris¹, P. Burka¹; ¹AIR Hub, Swinburne University Of Technology, Australia
17. Sep 26 14:30 14:55 12.12.3
0651		 THE MAKING OF LUCHTVAART IN TRANSITIE (LIT) AND THE REMAKING OF A STRONG GLOBALLY CONNECTED NATIONAL AERONAUTICS INDUSTRY
R. Van Manen¹, K. Van Rijswijk¹, L. Veldenz¹; ¹Stichting Luchtvaart in Transitie, Netherlands
17. Sep 26 14:55 15:20 12.12.4
0825		 A MULTI-STAGE FORMING APPROACH FOR MANUFACTURING TITANIUM BIPOLAR PLATES FOR FUEL CELLS
J.-H. Hong, Korea Institute of Materials Science, South Korea
13.12Air Traffic Management and Trajectory Analytics
Chair(s): Andreeva-Mori, A.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
17. Sep 26 13:40 14:05 13.12.1
0554		 UNIFIED SEPARATION ASSURANCE FOR MULTI-UAV OPERATIONS: RISK-CALIBRATED BASELINES AND FAULT-AWARE ADAPTIVE RESOLUTION
Z. Chen¹, Y. Zhao¹, X. Wang¹, W. Dai¹, K.H. Low¹; ¹Civil Aviation University of China, China
17. Sep 26 14:05 14:30 13.12.2
0860		 SENSITIVITY STUDY OF DEPARTURE TIME ACCURACY FOR AIRPORT COLLABORATIVE DECISION MAKING USING FAST-TIME SIMULATION
Y. Iwatsuki, Mitsubishi Research Institute, Inc./ Kyushu University, Japan; A. Harada¹, S. Higashino¹; ¹Kyushu University, Japan
17. Sep 26 14:30 14:55 13.12.3
0893		 AIRCRAFT CLIMB PROFILE PREDICTION VIA MACHINE LEARNING-BASED FRAMEWORK
H. Seon¹, K. Lee¹, M. Brown², H. Hirabayashi²; ¹Korea Aerospace University, South Korea ;²Electronic Navigation Research Institute, Japan
17. Sep 26 14:55 15:20 13.12.4
0816		 LIMITED HORIZON AIRLINE SCHEDULING USING GREY THEORY AND GRASP FRAMEWORK
P. Singh¹, R.S. Pant¹; ¹IIT Bombay, India
14.12Through-Life Support
Chair(s): Kekoc, V., Kelly, M.
Track 14 C2.5
11 - Operations and Sustainment
17. Sep 26 13:40 14:05 14.12.1
0914		 TOWARDS INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES: INSPECTABILITY ASSESSMENT OF HAT-STIFFENED PANELS
A. Filippatos¹, D. Markatos¹, T. Kalampoukas¹, N. Raptis¹, M. Abouhamzeh², K. Stamoulis², S. Pantelakis¹; ¹Department of Mechanical Engineering & Aeronautics, University o, Greece ;²Faculty of Technology, Amsterdam University of Applied Sciences, Netherlands
17. Sep 26 14:05 14:30 14.12.2
0710		 FROM DATA TO DECISIONS: A CONCEPTUAL FRAMEWORK FOR DATA-DRIVEN AIRLINE OPERATIONS AND SUSTAINMENT
A. Apostolidis, KLM Royal Dutch Airlines, Netherlands; K.P. Stamoulis, Amsterdam University of Applied Sciences, Netherlands
17. Sep 26 14:30 14:55 14.12.3
0451		 LIFE CYCLE ANALYSIS OF EMISSIONS IN AVIATION: IDENTIFIYING AND ADJUSTING FACTORS TO REDUCE CARBON EMISSIONS
J. Roesing, RWTH Aachen University, Germany
17. Sep 26 14:55 15:20 14.12.4
0856		 PERFORMANCE DEGRADATION ASSESSMENT METHOD FOR AERO-ENGINES ACROSS THE FULL-LIFE-CYCLE BASED ON DIGITAL TWIN
Z. Huang¹, D. Xiao¹, X. Guo¹, L. Zhao¹, C. Song¹; ¹Northwestern Polytechnical University, China
Presenter: Zilang Huang, Northwestern Polytechnical University
additional information (interactive) 14.12.R
0222		 KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH
S.I. Hallstedt¹, P.L.Y. Léonard¹, M. Aldèn¹, G. Dokter¹, O. Isaksson¹; ¹Chalmers University of Technology, Sweden
15.12tbd4
Chair(s): ,
Track 15 C2.6

15:20 - 15:25CHANGEOVER BREAK

0.12ICAS VON KARMAN LECTURE Swedish – Brazilian Partnership
Chair: D. Mavris past ICAS President
17. Sep 26 15:25 16:15

0.13Closing Ceremony
Chair: G. Holmberg incoming ICAS President
17. Sep 26 16:15 17:00