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

Thursday, 17. Sep 2026

0.8GENERAL LECTURE 5 ISABE and the next generation of aircraft propulsion (by Frank Haselbach ISABE president)
Chair:
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
15 - Guest lectures (by personal invitation only)
17. Sep 26 09:15 09:40 1.10.1 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 APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY OF A PILOT DIGITAL ASSISTANT
A. Mayima, Penrose Business Centre, Ireland
17. Sep 26 10:05 10:30 1.10.3 OFFLINE MULTIMODAL LARGE LANGUAGE MODELS FOR DECISION SUPPORT IN AIR OPERATIONS
J. Dantas, Instituto de Estudos Avançados, Brazil
17. Sep 26 10:30 10:55 1.10.4 AI IN THE COCKPIT, A 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
2.10Failures
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.10Military
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 09:15 09:40 3.10.1 AERODYNAMIC SHAPE OPTIMISATION USING A STRUCTURAL MODAL PARAMETERISATION METHOD
A. R. Wang, Boeing Aerostructures Australia, Australia
17. Sep 26 09:40 10:05 3.10.2 MODELLING COUPLED ON-BOARD SYSTEMS AND THEIR TOP-LEVEL IMPACT ON FIGHTER AIRCRAFT DESIGN
E. Espinosa-Juárez, Linköping University, Sweden
17. Sep 26 10:05 10:30 3.10.3 MULTI-FIDELITY BAYESIAN NEURAL NETWORKS FOR STEALTH/AERODYNAMIC DATA FUSION METHOD
J. He, China
17. Sep 26 10:30 10:55 3.10.4 FAST INTEGRATED EVALUATION AND OPTIMIZATION DESIGN METHOD FOR AERODYNAMIC AND STEALTH PERFORMANCE OF INLETS WITH ENTRANCE GRIDS
J.-W. He, Northwestern Polytechnical University, China
Reserve Paper 3.10.R CONCEPTUAL DESIGN AND AERODYNAMIC ANALYSIS OF A GENERIC FUTURE FIGHTER AIRCRAFT
P.-D. Bravo-Mosquera, EESC-USP, Brazil
4.10Configuration/Aero/Aerothermal/Flight-Performance
Chair(s): ,
Track 4
15 - Guest lectures (by personal invitation only)
5.10Propeller Aerodynamics and Rotor Flows
Chair(s): Rana, Z., Kiszkowiak, L.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 09:15 09:40 5.10.1 AERODYNAMICS OF OPEN FAN INTEGRATION FOR THE DLR-25 CONCEPT
I.J. Pawlikow, DLR, Germany
17. Sep 26 09:40 10:05 5.10.2 STUDY OF THE AERODYNAMIC INTERFERENCE OF STRUT-BRACED WINGS WITH DISTRIBUTED PROPELLERS
n/a Fossati, Unniversity of Strathclyde, United Kingdom
17. Sep 26 10:05 10:30 5.10.3 UNSTEADY EXERGY ANALYSIS OF A HIGHLY LOADED HIGH-SPEED ROTOR UNDER ROTATING STALL
C Paillard, ISAE-SUPAERO, France
17. Sep 26 10:30 10:55 5.10.4 COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM
Jiawen He¹, Yue Zhao¹, Xinyuan Wei¹, Tieren Chen¹, Yong Yang¹; ¹Northwestern Polytechnical University, China
Reserve Paper 5.10.R INVESTIGATION AND ONE-DIMENSIONAL MODELING OF THE DUAL-ROTOR GEROTOR PUMP AT HIGH ALTITUDES
Z.C. Su, China; P.F. Zhu, China; G.L. Li, China; C.H. Zhong, China; Y.G. Lyu, China
6.10Advanced measurement technique
Chair(s): Moreau, D., Allen, N.
Track 6
03.2 - Experimental Aerodynamics
17. Sep 26 09:15 09:40 6.10.1 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 09:40 10:05 6.10.2 CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS
C.W Marshall, Defence Science and Technology Group, Australia
17. Sep 26 10:05 10:30 6.10.3 FFECT OF THE FST ON THE BOUNDARY LAYER, THE WALL-PRESSURE FLUCTUATIONS, AND THE TRAILING-EDGE NOISE OF AIRFOILS
L Botero-Bolivar, Universidad Industrial de Santander, Colombia
additional information (interactive) 6.10.R ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM
D.-T Rajeepan, School of Aerospace, Mechanical and Mechatronics Engineering, Australia
7.10Flight Dynamics and Control
Chair(s): , , Grabowski, T.
Track 7
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 09:15 09:40 7.10.1 SIMULATION-BASED AUTOPILOT TUNING FOR FIXED-WING UAVS
C.-V. Boruga, Linkoping University, Sweden
17. Sep 26 09:40 10:05 7.10.2 A 3D-PRINTED TESTBED FOR FLIGHT CONTROL SYSTEM RESEARCH.
D Lundström, Sweden
17. Sep 26 10:05 10:30 7.10.3 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 RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAVS WINGTIP-LINKED FLIGHT
R. Wang, Northwestern Polytechnical University, P.R.China, China
Reserve Paper 7.10.R EXPERIMENTAL FLIGHT DYNAMICS AND CONTROL OF AN AGILE FIXED-WING UAV USING HYBRID ONBOARD & OFFBOARD CONTROL
Y. Huang, the University of Sydney, Australia
Reserve Paper 7.10.R MODEL-PREDICTIVE-CONTROL-BASED TRAJECTORY GENERATION ENHANCED WITH REINFORCEMENT LEARNING FOR FORMATION MANEUVERING
A. Rossi, Airbus Defence and Space GmbH, Germany
8.10Material Properties & Certifications
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
17. Sep 26 09:15 09:40 8.10.1 STRENGTH DESIGN AND TEST VERIFICATION OF AIRCRAFT SUSPENSION TRACK CONNECTION ZONE
K. Yin, China
17. Sep 26 09:40 10:05 8.10.2 INTERNATIONAL RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION
R. Degenhardt, DLR, Germany
17. Sep 26 10:05 10:30 8.10.3 DIGITAL-PHYSICAL SYNERGY: FEM-DRIVEN CERTIFICATION OF AT-5 AND AT-6 AIRCRAFT
M. Kowalski, Warsaw University of Technology, Poland
9.10Aeroelastic Analysis & Design 2
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
17. Sep 26 09:15 09:40 9.10.1 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 ENABLING FORWARD SWEPT WING DESIGNS
J E Cooper, University of Bristol, United Kingdom
17. Sep 26 10:05 10:30 9.10.3 DEVELOPMENT OF CONTROL LAWS FOR ENHANCED PERFORMANCE AND AEROELASTIC STABILITY OF EVTOL AIRCRAFT
P. Kantzidis, RMIT University, Australia
17. Sep 26 10:30 10:55 9.10.4 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
Reserve Paper 9.10.R AEROELASTIC TAILORING OF A SBW USING AFP TOW STEERED COMPOSITES
Tianqiang Huang¹, Touraj Farsadi, Adana Alparslan Turkes Science and Technology University, Turkey; Wesley Cantwell¹, Rafic Ajaj¹; ¹Khalifa University, China
10.10Hydrogen Propulsion Concepts
Chair(s): ,
Track 10
05 - Propulsion and Energy
17. Sep 26 09:15 09:40 10.10.1 ADVANCING CRYOGENIC COOLING AND ELECTRICAL DISTRIBUTION SYSTEMS FOR FUTURE HYDROGEN-POWERED AVIATION
D. Kierbel, AIRBUS NL, Netherlands
17. Sep 26 09:40 10:05 10.10.2 EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS
F. Thilker, FH JOANNEUM GesmbH, Austria
17. Sep 26 10:05 10:30 10.10.3 REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION
G. Marinaro¹, C. Serpico¹, L. Garbarino¹, M. Inverno¹, A. Bono¹, G. Malaponte¹, A. Pagano¹; ¹Italian Research Centre - CIRA, Italy
17. Sep 26 10:30 10:55 10.10.4 HEAT EXCHANGER MODELLING METHODS FOR HYDROGEN POWERED AERO ENGINES DURING THERMODYNAMIC CYCLE DESIGN
F.-H. Görtz, German Aerospace Center, Germany
Reserve Paper 10.10.R AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES
F. Pak, Eindhoven University of Technology, Netherlands
11.10Flight testing
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 09:15 09:40 11.10.1 PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA
J.-W. Wang, Beihang University, China
17. Sep 26 09:40 10:05 11.10.2 AERO–PROPULSIVE MODELING AND PRELIMINARY FLIGHT TESTING OF INDIVIDUAL THRUST CONTROL FOR A DISTRIBUTED ELECTRIC PROPULSION DEMONSTRATOR
G.F. Filippoli, Politecnico di Milano, Italy
17. Sep 26 10:05 10:30 11.10.3 PHYSICS-INFORMED MACHINE LEARNING FOR FLIGHT DYNAMICS IDENTIFICATION OF THE SAAB 340 USING FLIGHT TEST DATA
M Alam, Cranfield University, United Kingdom
17. Sep 26 10:30 10:55 11.10.4 EVALUATION OF STALL BEHAVIOUR OF T-TAIL AIRCRAFT: MODELING AND FLIGHT TEST
MH Lowenberg, University of Bristol, United Kingdom
12.10Advanced Aircraft Design and Manufacturing
Chair(s): ,
Track 12
08 - Manufacturing and Supply Chain Management
17. Sep 26 09:15 09:40 12.10.1 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 RESEARCH ON A DIGITAL-DRIVEN LIFE-CYCLE SUPPLY CHAIN MANAGEMENT SYSTEM FOR COLLABORATIVE AIRCRAFT DEVELOPMENT
J. Chai, AVIC The First Aircraft Institute, , China
17. Sep 26 10:05 10:30 12.10.3 RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING
TJH Mahr, University of Melbourne, Australia
17. Sep 26 10:30 10:55 12.10.4 A FORMALLY VERIFIED, EVENT-DRIVEN ROS SCADA SUPERVISORY SYSTEM ARCHITECTURE FOR SAFETY-CRITICAL ROBOTIC CELLS IN AEROSPACE MANUFACTURING
F. S. Braga, Aeronautics Institute of Technology (ITA), Brazil
13.10Global Airport and Network Operations
Chair(s): Mori, R.
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
17. Sep 26 09:15 09:40 13.10.1 FEASIBILITY STUDY ON LANDING CAPACITY ENHANCEMENT AT CONGESTED AIRPORTS VIA ARRIVAL TRAJECTORY ANALYSIS
R. Kajikawa, Graduate School of Systems Design, Tokyo Metropolitan University, Japan
17. Sep 26 09:40 10:05 13.10.2 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 10:05 10:30 13.10.3 A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION
G Enea, MIT Lincoln Laboratory, United States
17. Sep 26 10:30 10:55 13.10.4 AVIATION NETWORK MODELLING IN THE CONTEXT OF SMALL ISLAND DEVELOPING STATES: CONSTRAINTS, LIMITATIONS AND OPPORTUNITIES FOR AVIATION IN FIJI
P.F.D. Bowes, Australia
Reserve Paper 13.10.R ATTRIBUTION OF ATFM DELAY AS A RESULT OF A GROUND DELAY PROGRAM (GDP)
C.A. Tait, Airservices Australia, Australia
14.10MBSE - Model based Systems Engineering
Chair(s): , , Wiels, V.
Track 14
02 - Systems Engineering and Integration
17. Sep 26 09:15 09:40 14.10.1 PROPAGATING SAFETY ASSESSMENT RESULTS FOR SYSTEM ARCHITECTURE CANDIDATES IN MBSE
S. Lübbe¹, M. Schäfer¹, O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 09:40 10:05 14.10.2 MODEL-BASED FUNCTIONAL HAZARD ASSESSMENT BASED ON ARP4761A USING SYSML V1 AND SYSML V2
M. Schäfer¹, S. M. Lübbe¹, O. Bertram¹, A. Bierig¹; ¹DLR, Germany
17. Sep 26 10:05 10:30 14.10.3 ARCADIA VIEWPOINTS FOR ENTERPRISE ARCHITECTING COMPARISON WITH UAF VIEWS THROUGH AN EVTOL COMPANY OPERATION MODELING
R.M. Machado Cezar, Technological Institute of Aeronautics (ITA), Brazil
17. Sep 26 10:30 10:55 14.10.4 MANEUVER- AND DELAY-ROBUST DISTRIBUTED SATELLITE SSA VIA SPATIO-TEMPORAL GRAPH FORECASTING
Hamada Rizk¹, Hirozumi Yamaguchi¹, Sumio Morioka², Takahiro Inagawa²; ¹Osaka University, Japan ;²Interstellar Technologies Inc., Japan
Reserve Paper 14.10.R MODEL-BASED SYSTEMS ENGINEERING APPLICATION USING FLIGHT-TEST DATA FROM THE ACS-100 SORA AIRCRAFT
L. H. J. Machado, UFMG, Brazil
15.10Maintenance technologies
Chair(s): Anderson, K.
Track 15
11 - Operations and Sustainment
17. Sep 26 08:50 09:15 15.10.1 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 09:15 09:40 15.10.2 ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA
C. Klein, Deutsches Zentrum für Luft- und Raumfahrt, Germany
17. Sep 26 09:40 10:05 15.10.3 ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085
J. P Rogers, RMIT University, Australia
17. Sep 26 10:30 10:55 15.10.4 INFRARED AND GREEN FEMTOSECOND LASER PAINT STRIPPING ON AIRCRAFT COATINGS: EXPERIMENTAL AND NUMERICAL ASSESSMENT
S. Zhu¹, J. Panta¹, R. Yang¹, S. Zhang, Univeristy of Technology Sydney , Australia; ¹Western Sydney University, Australia
additional information (interactive) 15.10.R LIGHTWEIGHT AND ROBUST REAL-TIME DETECTION SYSTEM FOR AIRCRAFT SKIN DEFECTS UNDER COMPLEX UAV INSPECTION CONDITIONS
Wenqing Yang¹, Jianlin Xuan¹; ¹Northwestern Polytechnical University, China

10:55 - 11:00CHANGEOVER BREAK

1.11Air transport resilience to climate change and weather hazards
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
17. Sep 26 11:00 11:25 1.11.1 COMBINED IMPACT OF JET STREAM AND TURBULENCE ON LONG-TERM TRANS-OCEANIC FLIGHT ROUTES
J.-H. Kim, Seoul National University, South Korea
17. Sep 26 11:25 11:50 1.11.2 PROGRESS IN AIRCRAFT-BASED METEOROLOGICAL OBSERVATIONS
T.F. Rahmes, The Boeing Company, United States
2.11Sharing the Air (Airspace)
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
17. Sep 26 11:00 11:25 2.11.1 A HOLISTIC APPROACH TO ENABLE ADVANCED AIR MOBILITY FOR REGIONAL, RURAL AND REMOTE AUSTRALIA
P Burka, Swinburne University of Technology, Australia
17. Sep 26 11:25 11:50 2.11.2 THE ROLE OF COMMUNITY ENGAGEMENT IN INTRODUCING UNMANNED AERIAL VEHICLE TECHNOLOGY: A RAPID SCOPING REVIEW
J. Porter, Australia
3.11Aerostructures
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 11:00 11:25 3.11.1 ROBUST HIGH-FIDELITY DATASET-BASED AEROELASTIC 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 LARGE-SCALE AEROSTRUCTURAL OPTIMISATION WITH MODAL AND NONLINEAR BUCKLING CONSTRAINTS ASSISTED BY ALGORITHMIC DIFFERENTIATION
L Scalia, Universidad Carlos III de Madrid, Spain
17. Sep 26 11:50 12:15 3.11.3 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 12:15 12:40 3.11.4 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
Reserve Paper 3.11.R COMPARISON OF CONFIGRATIONS FOR FLEXIBLE AIRCRAFT USING AEROELASTIC ANALYSIS
N.O. Okubo, The University of Tokyo, Japan
4.11CFD Needs and Progress Towards Vision 2030 & Beyond
Chair(s): Cary, A., Azevedo, J.
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 11:00 11:25 4.11.1 CFD VISION 2030 PROGRESS AND NEXT STEPS
J. P. Slotnick, United States
17. Sep 26 11:25 11:50 4.11.2 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 THE ROLE OF NEXT-GENERATION HPC AND MACHINE LEARNING IN ACHIEVING THE 2030 VISION GOALS
N. Ashton, NVIDIA, United States
17. Sep 26 12:15 12:40 4.11.4 CFD VISION 2030 LOOKING FORWARD: PANEL DISCUSSION
A. W. Cary, United States
5.11UAS and AAM Design Applications
Chair(s): Pezzella, G., Lawson, N.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 11:00 11:25 5.11.1 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 11:25 11:50 5.11.2 PREDICTION OF PROPELLER NOISE IN LOW REYNOLDS NUMBER OPERATION USING MACHINE LEARNING MODELS
M. de Rosa Jacinto¹, D. Skrna¹, J. Haegemans, Katholieke Universiteit Leuven, Belgium; M. Berens¹; ¹Technische Universität Wien, Austria
17. Sep 26 11:50 12:15 5.11.3 A COMPARATIVE STUDY OF THE AERODYNAMIC CHARACTERISTICS OF TWO CONFIGURATIONS
K. You, Northwestern Polytechnical University, China
Presenter: Kai You
17. Sep 26 12:15 12:40 5.11.4 INTEGRATION OF ACOUSTIC LINERS AND INTERNAL BYPASS CHANNELS INTO AAM PROPELLERS FOR NOISE REDUCTION
D. Skrna¹, M. de Rosa Jacinto¹, Martin Berens¹; ¹Technische Universität Wien, Austria
Reserve Paper 5.11.R RESEARCH ON AN AERODYNAMIC LOAD METHODOLOGY FOR FLAPPING WINGS BASED ON EXPERIMENTALLY ACQUIRED DEFORMATION
K.-Y. Yang, Northwestern Polytechnical University, China
additional information (interactive) 5.11.R ARODYNAMIC COUPLING OF TYPICAL FORMATION CONFIGURATION
JY.-Z. Zhao, Northwestern Polytechnical University, China
6.11Flow seperation and control
Chair(s): Atkin, C., Gowree, E.
Track 6
03.2 - Experimental Aerodynamics
17. Sep 26 11:00 11:25 6.11.1 WIND-TUNNEL STATIC AND DYNAMIC TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES
D. Farcy, ONERA, France
17. Sep 26 11:25 11:50 6.11.2 SIDE JET-CROSSFLOW INTERACTION: PRESSURE DISTRIBUTION AND FLOW FIELD ANALYSIS IN SUBSONIC, TRANSONIC AND SUPERSONIC FLOW
B. Ilic, Military Technical Institute, Serbia
17. Sep 26 11:50 12:15 6.11.3 WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS
?. P. Malicki, Wroc?aw University of Science and Technology , Poland
17. Sep 26 12:15 12:40 6.11.4 EXPERIMENTAL ASSESSMENT OF SIDE JET EFFECTS ON AERODYNAMIC FORCES AND MISSILE CONTROL IN SUBSONIC, TRANSONIC, AND SUPERSONIC FLOWS
M.-Dj Samardzic, Military Technical Institute (VTI), Serbia
Reserve Paper 6.11.R 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
additional information (interactive) 6.11.R DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE.
Estela Barroso Barderas, instituto Nacional de Técnica Aeroespacial (INTA),, Spain; Rafael Bardera Mora¹, Juan Carlos Matías García¹, Jaime Fernández Antón¹, Ángel A. Rodríguez Sevillano, Universidad Politécnica de Madrid, Spain; ¹Instituto Nacional de Técnica Aeroespacial (INTA),, Spain
7.11Flight Simulation and Testing
Chair(s): , , Krus, P.
Track 7
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 11:00 11:25 7.11.1 FLIGHT TRIALS OF DRONES CONTROLLED BY AI LARGE LANGUAGE MODELS
S Crase, Australia
17. Sep 26 11:25 11:50 7.11.2 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 INFORMATIVE PATH PLANNING BASED ON REDUCED-RANK GAUSSIAN PROCESS FOR HAZARDOUS SUBSTANCE MONITORING
C.M lee, South Korea
17. Sep 26 12:15 12:40 7.11.4 SENSOR-DRIVEN CONTROL OF UAS UTILISING AI IN SIMULATION
S. R. Pywell, Australia
Reserve Paper 7.11.R ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES
K. Thomessen¹, S. Schopferer¹, P. Nagarajan¹; ¹German Aerospace Center (DLR), Germany
8.11High-Temperature Materials/Structures
Chair(s): ,
Track 8
15 - Guest lectures (by personal invitation only)
9.11Student Final
Chair(s): Rein Weston, K.
Track 9
10.11Propulsion optimization 1
Chair(s): ,
Track 10
05 - Propulsion and Energy
17. Sep 26 11:00 11:25 10.11.1 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 11:25 11:50 10.11.2 RUBBER ENGINE INTEGRATED OPTIMIZATION STRATEGY FOR OVERALL AIRCRAFT DESIGN
J. Häßy, DLR, Germany
17. Sep 26 11:50 12:15 10.11.3 ON THE ACCURACY AND ROBUSTNESS OF TRANSIENT PNEUMATIC TRAVERSES: AN EXPERIMENTAL STUDY ON SYSTEM PARAMETERS
S. Eilers, University of the Bundeswehr Munich, Germany
17. Sep 26 12:15 12:40 10.11.4 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
11.11Performances
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 11:00 11:25 11.11.1 STUDY ON FLIGHT PERFORMANCE DEGRADATION CHARACTERISTICS OF ABLATION-INDUCED DAMAGE IN LOITERING MUNITIONS
MX-Z zhang, China
17. Sep 26 11:25 11:50 11.11.2 GAIN OPTIMIZATION FOR CASCADED INDI CONTROL WITH INTEGRATED PERFORMANCE AND ROBUSTNESS REQUIREMENTS
D. Surmann, University of the Bundeswehr Munich, Germany
17. Sep 26 11:50 12:15 11.11.3 LATERAL-DIRECTIONAL HANDLING AND FLYING QUALITIES ASSESSMENT OF A BLENDED WING BODY (BWB) ACFA 2020 CONFIGURATION
M Alam, Cranfield University, United Kingdom
17. Sep 26 12:15 12:40 11.11.4 FLIGHT PERFORMANCE ANALYSIS OF ELECTRIC AIRCRAFT UNDER MOTOR FAILURE CONDITIONS USING REDUCED-ORDER MODELING
L. Hein¹, S. Myschik¹; ¹University of the Bundeswehr Munich, Germany
Reserve Paper 11.11.R ACHIEVING ACCURATE AND CONSISTENT AIRSPEED MEASUREMENT FOR AIRCRAFT DEVELOPMENT AND CERTIFICATION
J. Luo, The Boeing Company, United States
additional information (interactive) 11.11.R AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE
R. Wang, China
12.11Additive Manufacturing and Intelligent Manufacturing
Chair(s): van Manen, R.
Track 12
08 - Manufacturing and Supply Chain Management
17. Sep 26 11:00 11:25 12.11.1 BALANCING STRENGTH AND THERMAL CONDUCTIVITY IN LPBF-PROCESSED ALUMINUM-BASED MATERIALS
H. Z Zhang, Nanjing University of Aeronautics and Astronautics, China
17. Sep 26 11:25 11:50 12.11.2 3D ANALYSIS AND PREDICTION OF ASSEMBLY STEP DEVIATIONS IN 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 A NOVEL MULTI-TASK LEARNING METHOD FOR DEFECT SUPPRESSION IN AERONAUTICAL PARTS DURING LASER POWDER BED FUSION
Y.S. Chen, Nanjing University of Aeronautics and Astronautics, China
17. Sep 26 12:15 12:40 12.11.4 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): ,
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
17. Sep 26 11:00 11:25 13.11.1 THREE-DIMENSIONAL ADAPTIVE TRAJECTORY OPTIMIZATION FOR RPAS-BASED ATMOSPHERIC MEASUREMENTS
K.-A. Buchtal, German Aerospace Center, Germany
17. Sep 26 11:25 11:50 13.11.2 A FIELD-THEORETIC FRAMEWORK FOR AUTONOMOUS COLLISION AVOIDANCE IN URBAN AIR MOBILITY
F. Y. Wu, Hong Kong SAR of China
17. Sep 26 11:50 12:15 13.11.3 EXPLORING DETROIT METROPOLITAN WAYNE COUNTY AIRPORT AS A TESTBED FOR RESOLVING EVTOL INTEGRATION CHALLENGES FOR AIR TAXI OPERATIONS
S.M. Abdulhak, United States
17. Sep 26 12:15 12:40 13.11.4 STANDARDIZED TAKE-OFF AND LANDING PROCEDURES FOR AIR TAXIS: URBAN AIR MOBILITY
FN Naeem, TUHH, Germany
Reserve Paper 13.11.R DETERMINATION OF SAFE SEPARATION FOR UAVS: CONSIDERING AIRSPACE STRUCTURE AND MANEUVERING STRATEGIES
K.H. Low, Civil Aviation University of China, China
14.11AI & SE
Chair(s): , , Stoufflet, B.
Track 14
02 - Systems Engineering and Integration
17. Sep 26 11:00 11:25 14.11.1 LLM-ASSISTED GENERATION OF SYSML V2 MODELS FROM HETEROGENEOUS SYSTEM REPORTS
V. Voth¹, J. Wade, UCSD, United States; O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 11:25 11:50 14.11.2 INTEGRATED SYSTEMS ARCHITECTURE FOR AEROSPACE DIGITAL THREAD ECOSYSTEM: A HUB-N-SPOKE TO MODELLING AND SIMULATION
K Dang, Boeing, United States
17. Sep 26 11:50 12:15 14.11.3 COMMON ONTOLOGY FOR PROPULSION ARCHITECTURES - COPA
S. Reitenbach, German Aerospace Center (DLR), Germany
17. Sep 26 12:15 12:40 14.11.4 AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS
Y.-L. Ren¹, L.-F. You¹, X.-H. Gao¹, C.-Y. Chang¹, Z.-Q. Wang¹, Z.-Q. Guo¹; ¹Beihang University, China
Reserve Paper 14.11.R BEYOND THE HARDWARE: REGULATION AND CERTIFICATION AS THE CRITICAL PATH TO ADF AUTONOMOUS CAPABILITY
K.J. Joyce, RAAF / UNSW, Australia
15.11Operations optimisation
Chair(s): Stamoulis, K.
Track 15
11 - Operations and Sustainment
17. Sep 26 11:00 11:25 15.11.1 FLIGHT MISSION MODELLING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION
Z. 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 15.11.2 PROVIDING SENSOR INFORMATION FOR BORDING TIME PREDICTION
M. Schultz, Unibw M, Germany
17. Sep 26 11:50 12:15 15.11.3 INVESTIGATION OF DECARBONISATION PATHWAYS FOR SHORT HAUL AVIATION USING A DISCRETE OPTIMISATION DECISION-MAKING ALGORITHM
N Barry, Trinity College Dublin, The University of Dublin, Ireland
17. Sep 26 12:15 12:40 15.11.4 ASSESSING AIRLINE PURCHASE MOTIVATION FOR HYDROGEN AIRCRAFT UNDER FUTURE CORSIA
Hiroko Nakamura, The University of Tokyo, Japan
Reserve Paper 15.11.R LIMITED-HORIZON LOOK-AHEAD SCHEDULING FOR DEMAND-RESPONSIVE OVERNIGHT CARGO AIRLINE OPERATIONS
Palak Singh¹, Rajkumar.S Pant¹, Geetika Kapil, Independent Researcher, United States; ¹IIT Bombay, India
Presenter: Rajkumar S. Pant, Indian Institute of Technology (IIT) Bombay
additional information (interactive) 15.11.R LOSS OF RELIABILITY OF NEW GENERATION ENGINES IN COMMERCIAL AVIATION: THE BUSINESS IMPACT OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION
A Sanchez Mata, SANMATC Consulting, Mexico

12:40 - 13:40LUNCH BREAK

1.12tbd1
Chair(s): ,
Track 1
2.12DPI workshop results
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.12Aero Optimization
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 13:40 14:05 3.12.1 INVERSE AIRFOIL DESIGN USING CONDITIONAL VARIATIONAL AUTOENCODERS
K. Swannet, Delft University of Technology, Netherlands
17. Sep 26 14:05 14:30 3.12.2 DATA-DRIVEN SHAPE PARAMETERIZATION FOR EFFECTIVE AERODYNAMIC DESIGN OPTIMIZATION OF PROPELLERS
J. L. Li, Northwestern Polytechnical University, China
17. Sep 26 14:30 14:55 3.12.3 AN INVESTIGATION OF KRIGING MODELS USING CORRELATED INDEPENDENT VARIABLES FOR AERODYNAMIC DESIGN
T. Kanno, Purdue University, United States
17. Sep 26 14:55 15:20 3.12.4 META-ENHANCED MULTI-OBJECTIVE REINFORCEMENT LEARNING FOR WIDE-SPEED-RANGE AIRFOIL OPTIMIZATION
Z. Li, Northwestern Polytechnical University, China
Reserve Paper 3.12.R AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS
J.-W Wu, Northwestern Polytechnical University, China
Reserve Paper 3.12.R RESEARCH ON GENERALIZED REPRESENTATION OF FLYING-WING CONFIGURATIONS BASED ON DEEP LEARNING
Xiaomeng Zhang, China
4.12Propulsion/Propulsion-Integration
Chair(s): ,
Track 4
15 - Guest lectures (by personal invitation only)
5.12Applied CFD Approaches
Chair(s): Bura, R., Imamura, T.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 13:40 14:05 5.12.1 EFFECTS OF FLAPPING–PITCHING PHASE DIFFERENCE ON THE AERODYNAMIC PERFORMANCE OF HOVERING DRAGONFLY WINGS
Haozhe Wang¹, Jialong Wang¹, Zhantao Li¹, Wenqing Yang¹, Xiaojun Yang¹; ¹Northwestern Polytechnical University, China
17. Sep 26 14:05 14:30 5.12.2 UNCERTAINTY QUANTIFICATION AND CROSS-CORRELATION EFFECTS IN AERODYNAMIC COEFFICIENTS DERIVED QUANTITIES
L. Pirillo, Italy
17. Sep 26 14:30 14:55 5.12.3 A STALL EXTENSION TO LIFTING-LINE THEORY: IMPLEMENTATION AND VALIDATION IN ASWING
L. Avoni, ISAE-Supaero, France
17. Sep 26 14:55 15:20 5.12.4 FALCON: FRAMEWORK FOR AIRFOIL CFD AND ANALYSIS OPTIMIZATION
P. Desai, Manipal Institute of Technology, India
6.12Challenges in wind tunnel testing
Chair(s): Jagadeesh, C., Allen, N.
Track 6
03.2 - Experimental Aerodynamics
17. Sep 26 13:40 14:05 6.12.1 PROPOSAL FOR DISTINGUISHING USALE DATA UNDER HIGH WIND TUNNEL BLOCKAGE USING AN RAE2822 TEST CASE
M.H. Mohsin, Cranfield University, United Kingdom
17. Sep 26 14:05 14:30 6.12.2 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 FORCE RECONSTRUCTION TECHNIQUES FOR DYNAMIC LOAD ESTIMATION ON A HEMISPHERE IN LOW-SPEED WIND TUNNEL TESTING
C.J.K Brown, RMIT University , Australia
17. Sep 26 14:55 15:20 6.12.4 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
Reserve Paper 6.12.R GROUND EFFECT EXPERIMENTAL ANALYSIS IN A NAVAL TESTING TANK AS AN ALTERNATIVE TO WIND TUNNEL
L.G. Souza, Instituto Tecnológico de Aeronáutica, Brazil
7.12Guidance and Path Planning
Chair(s): , , Hristozov, S.
Track 7
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 13:40 14:05 7.12.1 ONLINE TRAJECTORY PLANNING FOR FIXED-WING UAVS BASED ON PSEUDO-SPECTRAL CONVEX PROGRAMMING
Y. Peng, National University of Defense Technology, China
17. Sep 26 14:05 14:30 7.12.2 THREE-DIMENSIONAL PATH PLANNING OF UAV IN WIND FIELD ENVIRONMENT OF PLATEAU MOUNTAINOUS AREA
F. H.-F. Fan, Northwestern Polytechnical University, China
17. Sep 26 14:30 14:55 7.12.3 VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A TEMPORAL RESIDUAL NETWORK APPROACH WITH CHANNEL ATTENTION
Ziyang Zhang¹, Shaokun Li¹, XiaoPing Xu¹, Zhou Zhou¹; ¹Northwestern Polytechnical University, China
17. Sep 26 14:55 15:20 7.12.4 TRAJECTORY FEASIBILITY AND CONTROL FOR DYNAMIC SOARING IN 6-DOF FLIGHT
Y. Zhu, Northwestern Polytechnical University, China
Reserve Paper 7.12.R MPPI-BASED COMPUTATIONAL GUIDANCE FOR MOTION PLANNING OF A MULTIROTOR UAV USING DEPTH-CAMERA-BASED OBSTACLE REPRESENTATION
K.W Jang¹, Yangjae Jeong¹, G.G Kim¹; ¹Electronics and Telecommunications Research Institute, South Korea
8.12 Aircraft Electrification, Systems and Certification
Chair(s): ,
Track 8
12 - Host Nation (by personal invitation only)
9.12Aircraft Design
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
17. Sep 26 13:40 14:05 9.12.1 EFFECT OF UNCERTAINTY ON ROBUST JIG SHAPE DESIGN OF A HIGH ASPECT RATIO WING
G. Yang, University of Bristol, United Kingdom
17. Sep 26 14:05 14:30 9.12.2 METHODOLOGY FOR CRITICAL LOAD-CASE AND CONSTRAINT IDENTIFICATION IN PRELIMINARY COMPOSITE WING SIZING USING RAPID DESIGN TOOLS
M Alam, Cranfield University, United Kingdom
17. Sep 26 14:30 14:55 9.12.3 NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL
V. N. Mueller, Technical University of Munich, Germany
17. Sep 26 14:55 15:20 9.12.4 AIRCRAFT MASS EVALUATION MODEL: FROM TUBE-AND-WING TO BLENDED WING BODY USING WHALE.
V Priasso¹, A Lannoo¹; ¹DMAS, ONERA, 59000, Lille, France, France
additional information (interactive) 9.12.R A STOCHASTIC GRADIENT ONLINE LEARNING AND PREDICTION METHOD FOR ACCELERATING TOPOLOGY OPTIMIZATION AND ITS APPLICATION IN THE DESIGN OF MORPHING WING
Y. Xing, The University of Sydney, Australia
10.12Propulsion optimization 2
Chair(s): ,
Track 10
05 - Propulsion and Energy
17. Sep 26 13:40 14:05 10.12.1 INLET OPTIMIZATION DESIGN OF A BOUNDARY LAYER INGESTION PROPULSION SYSTEM
X.K. Ma, Northwestern Polytechnical University , China
17. Sep 26 14:05 14:30 10.12.2 PD-STGNN: A PHYSICS-INFORMED DYNAMIC SPATIO-TEMPORAL GRAPH NEURAL NETWORK FOR AERO-ENGINE THRUST PREDICTION
C. Song, Northwestern Polytechnical University, China
17. Sep 26 14:30 14:55 10.12.3 PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES
T.-D Dinh, Vietnam
17. Sep 26 14:55 15:20 10.12.4 GPU-ENABLED SURROGATE MODEL-BASED AEROACOUSTIC OPTIMISATION FOR JET FLOWS
G. Yang, University of Bristol, United Kingdom
11.12Flight dynamics
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 13:40 14:05 11.12.1 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 AIRCRAFT BUFFET QUANTIFICATION
Jia Luo, The Boeing Company, United States
17. Sep 26 14:30 14:55 11.12.3 METHODOLOGY FOR VERIFYING DYNAMIC PARAMETERS OF A STEWART PLATFORM FOR FLIGHT SIMULATION
M. D. Dutra Turazza, University of São Paulo, Brazil
17. Sep 26 14:55 15:20 11.12.4 A NEW APPROACH TO MODELLING THE FLIGHT DYNAMICS OF A TAILLESS AIRCRAFT
A. Kwiek, Warsaw University of Technology, Poland
Reserve Paper 11.12.R EFFECTS OF LIFT DISTRIBUTION AND WING POSTURE ON THE STABILITY AND CONTROL OF TAILLESS AIRCRAFT
MR de Kock, University of Pretoria, South Africa
Presenter: Barbara Huyssen, University of Pretoria
12.12Advanced Forming Technology for Aviation
Chair(s): Gu, D.
Track 12
08 - Manufacturing and Supply Chain Management
17. Sep 26 13:40 14:05 12.12.1 ACHIEVING HIGH-PERFORMANCE MAGNESIUM MATRIX COMPOSITES BY LASER POWDER BED FUSION
L.X.XI Xi, China
17. Sep 26 14:05 14:30 12.12.2 HIGH-RATE AUTOMATED STAMP FORMING OF CF/LM-PAEK COMPOSITES FOR NEXT-GENERATION UAV AEROSTRUCTURES
M. Ravandi, Aerostructures Innovation Research (AIR) Hub, Swinburne Universi, Australia
17. Sep 26 14:30 14:55 12.12.3 THE MAKING OF LUCHTVAART IN TRANSITIE (LIT) – AND THE REMAKING OF A STRONG GLOBALLY CONNECTED NATIONAL AERONAUTICS INDUSTRY
Ron Van Manen¹, Kjelt Van Rijswijk¹, Laura Veldenz¹; ¹Stichting Luchtvaart in Transitie, Netherlands
17. Sep 26 14:55 15:20 12.12.4 A MULTI-STAGE FORMING APPROACH FOR MANUFACTURING TITANIUM BIPOLAR PLATES FOR FUEL CELLS
J.-H. Hong, Korea Institute of Materials Science, South Korea
13.12CRM-HL 2
Chair(s): Rivers, M.
Track 13
03.2 - Experimental Aerodynamics
17. Sep 26 13:40 14:05 13.12.1 AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT
M. Murayama, Japan Aerospace Exploration Agency, Japan
17. Sep 26 14:05 14:30 13.12.2 CROSS-TEST COMPARISONS AND REYNOLDS NUMBER EFFECTS IN THE CRM-HL ECOSYSTEM
S.M. Rivers, NASA Langley Research Center, United States
Presenter: Courtney Winski
17. Sep 26 14:30 14:55 13.12.3 ICING EXPERIMENTAL DATABASE USING THE COMMON RESEARCH MODEL(ICED CRM)
D.D.P. Di Pasquale, Cranfield University, United Kingdom
17. Sep 26 14:55 15:20 13.12.4 ICING EXPERIMENTAL DATA ON THE NASA HIGH-LIFT CRM MODEL
D.D.P. Di Pasquale, Cranfield University, United Kingdom
14.12Aeronautical R&D in Australia
Chair(s): ,
Track 14
15 - Guest lectures (by personal invitation only)
17. Sep 26 13:40 14:05 14.12.1 EVTOL AND PROPULSION R&D IN THE SYDNEY PROPULSION LAB
D. Verstraete, Australia
15.12Through-Life support
Chair(s): Kelly, M.
Track 15
11 - Operations and Sustainment
17. Sep 26 13:40 14:05 15.12.1 INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES
A.F. Filippatos, Department of Mechanical Engineering & Aeronautics, University o, Greece
17. Sep 26 14:05 14:30 15.12.2 FROM DATA TO DECISIONS: A CONCEPTUAL FRAMEWORK FOR DATA-DRIVEN AIRLINE OPERATIONS AND SUSTAINMENT
A. Apostolidis, KLM Royal Dutch Airlines, Netherlands
17. Sep 26 14:30 14:55 15.12.3 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 15.12.4 PERFORMANCE DEGRADATION ASSESSMENT METHOD FOR AERO-ENGINES ACROSS THE FULL-LIFE-CYCLE BASED ON DIGITAL TWIN
D. Xiao, China
Reserve Paper 15.12.R ENGINEERING COMMERCIAL AIRCRAFT FOR SUSTAINABLE THROUGH-LIFE SUPPORT
RG Ramachandran, Boeing, India
additional information (interactive) 15.12.R KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH
I. Hallstedt, Chalmers University of Technology, Sweden

15:20 - 15:25CHANGEOVER BREAK

0.9ICAS VON KARMAN LECTURE Swedish – Brazilian Partnership
Chair:
17. Sep 26 15:25 16:15

0.10CLOSING CEREMONY
Chair:
17. Sep 26 15:15 17:00