35th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

Please use your browser's search function (Ctrl+F) to look up a specific author or title.

Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.

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

Tuesday, 15. Sep 2026

0.3ICAS 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 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 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 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 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 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 PROGRESS IN AIRCRAFT-BASED METEOROLOGICAL OBSERVATIONS
J. Hileman, The Boeing Company, United States
15. Sep 26 09:45 10:10 2.4.3 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 DISCRIMINATORY AUTONOMY: OPERATING FASTER, SMARTER, AND WITH PURPOSE
James Garth, BAE SYSTEMS Australia, Australia
15. Sep 26 09:20 09:45 14.4.2 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 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 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 FACTORS AFFECTING COMMUNICATION IN AVIATION
B. Molesworth¹, D. Estival¹, L. Chow¹; ¹UNSW, Australia
15. Sep 26 09:20 09:45 15.4.2 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 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 ECONOMIC, ENVIRONMENTALLY SUSTAINABLE AVIATION ENERGY
J.I. Hileman, Boeing, United States
15. Sep 26 11:25 11:50 1.5.2 AIRBUS' PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES
F Haselbach, Airbus, France
15. Sep 26 11:50 12:15 1.5.3 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 SYSTEM IDENTIFICATION USING FLIGHT TEST DATA AND MACHINE LEARNING
R Larsson, Saab Aeronautics, Sweden
15. Sep 26 11:25 11:50 11.5.2 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION
C. Galinski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland
Reserve Paper 14.5.R 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 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 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 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 AEROSPACE ELECTRIFICATION - DEVELOPMENT AND TEST FOR MORE ELECTRIFIED AIRCRAFT
G. Bezos OConnor, United States
15. Sep 26 14:05 14:30 1.6.2 BUILDING A TECHNOLOGY PLATFORM FOR THE ELECTRIC AGE
B. Loxton, United States
15. Sep 26 14:30 14:55 1.6.3 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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

0.4GENERAL 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 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 JET ZERO: ATJ SAF PROJECT DEVELOPER
J Mason, Jet Zero Australia, Australia
15. Sep 26 17:30 17:55 1.7.3 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 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 GARTEUR: FRAMEWORK, ORGANIZATION AND COLLABORATIVE RESEARCH
B. Hammer, Germany
15. Sep 26 17:05 17:30 2.7.2 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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