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

Wednesday, 16. Sep 2026

0.6ICAS LECTURE FOR INNOVATION IN AERONAUTICS Veronique Roca – Airbus Beluga X
Chair:
16. Sep 26 08:00 08:50

08:50 - 09:15COFFEE BREAK

0.7INTERACTIVE PRESENTATIONS
Chair:
16. Sep 26 09:15 10:45

10:45 - 10:50CHANGEOVER BREAK

1.7GSA2: Super Panel: Pathways to Global Sustainable Aviation
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
16. Sep 26 10:50 11:15 1.7.1 GLOBAL SUSTAINABLE AVIATION PANEL DISCUSSION WITH SELECTED SPEAKERS
R.A. Wahls, NASA, Retired, United States
2.7GARTEUR 2
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
16. Sep 26 10:50 11:15 2.7.1 MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS
F. J. San Millan, INTA, Spain
16. Sep 26 11:15 11:40 2.7.2 ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS
M.L. Montero-Sistiaga¹, M. de Smit¹, A. Pastor Muro², N. Redondo Torrico², M. Thomas³, A Morel³, S Drawin³, F. Palm, Airbus, Central Research & Technology (CRT), Germany; ¹Royal NLR-Netherlands Aerospace Centre, Netherlands ;²National Institute of Aerospace Technology (INTA), Spain ;³ONERA-The French Aerospace Lab, France
Presenter: Francisco Javier San Millan Fiel, INTA- Spanish National Institute for Aerospace Research
16. Sep 26 11:40 12:05 2.7.3 CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING
F Roudolff, ONERA, France
16. Sep 26 12:05 12:30 2.7.4 GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION
P. Catalano, Italy
3.7Case Studies 1
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
16. Sep 26 10:50 11:15 3.7.1 ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING CONCEPTUAL DESIGN FOR HYDROGEN-POWERED AIRCRAFT
ES Stragiotti, ONERA, France
16. Sep 26 11:15 11:40 3.7.2 RESEARCH ON EFFECTIVENESS-DRIVEN INTELLIGENT OPTIMIZATION METHOD FOR CONCEPTUAL LAYOUT OF AIRCRAFT
W. Liu, School of Aeronautics, Northwestern Polytechnical University, China
16. Sep 26 11:40 12:05 3.7.3 A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION
L. LIU¹, Y. WU¹, M.A. Hariansyah¹, R.-P. LIEM, ICL, Department of Aeronautics, United Kingdom; ¹HKUST, Department of Mechanical and Aerospace Engineering, Hong Kong SAR of China
Presenter: Yiran Wu, HKUST,Department of Mechanical and Aerospace Engineering
16. Sep 26 12:05 12:30 3.7.4 OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES
M. A. Hariansyah¹, C. Reyner¹, R. P. Liem, Imperial College London, United Kingdom; P. S. Palar, Institut Teknologi Bandung, Indonesia; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China
Reserve Paper 3.7.R MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY
L Mainini, Imperial College London, United Kingdom
Reserve Paper 3.7.R THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WINGUAV
S. Choi¹, B. Cho¹, D. Jung¹; ¹Korea Aerospace University, South Korea
Presenter: Byeonggeun Cho, Korea Aerospace University
4.7Unconventional configurations - 1
Chair(s): Melkert, J.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
16. Sep 26 10:50 11:15 4.7.1 A HYBRID-ELECTRIC OPEN-ROTOR AIRCRAFT FOR HIGHLY EFFICIENT LONG-RANGE AND PEOPLE-MOVER OPERATIONS
G. Atanasov, DLR, Germany
16. Sep 26 11:15 11:40 4.7.2 BUZZ-E: A BIOINSPIRED HIGH-PAYLOAD CARRYING FLAPPING WING ROBOT
A. H Hammad, Technical University Munich, Germany, Germany
16. Sep 26 11:40 12:05 4.7.3 COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS
L. Li, Chang’an University, China
16. Sep 26 12:05 12:30 4.7.4 RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS
H. Reindle, Technical University of Munich, Germany
Reserve Paper 4.7.R EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT
E. M. Künstler, University of Stuttgart, Germany
additional information (interactive) 4.7.R EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT
E. M. Künstler, University of Stuttgart, Germany
5.7Machine Learning Applications
Chair(s): Ashton, N., Halila, G.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 10:50 11:15 5.7.1 AERODYNAMIC OPTIMIZATION DESIGN METHOD FOR ROTORS USING A MULTI-FIDELITY NEURAL NETWORK MODEL
Z.-Q. Shen, Northwestern Polytechnical University, China
16. Sep 26 11:15 11:40 5.7.2 MACHINE LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION OF NACA AIRFOILS UNDER GEOMETRIC DESIGN CONSTRAINTS
M. I. Alam, King Fahd University of Petroleum and Minerals (KFUPM), Saudi Arabia
16. Sep 26 11:40 12:05 5.7.3 A COMPARATIVE STUDY OF PHYSICS-INFORMED NEURAL NETWORK FORMULATIONS FOR PARABOLIZED STABILITY EQUATIONS
G. Dalinajara Abreu Smith Borges¹, V. Silva Figueredo¹, G. L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J. L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
16. Sep 26 12:05 12:30 5.7.4 EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN
Y. Fan, NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
Reserve Paper 5.7.R RESEARCH ON AERODYNAMIC-STEALTH INTEGRATED DESIGN METHODOLOGY BASED ON MPPO ALGORITHM
Keyao Gan¹, Huan Zhao¹, Shekun Wang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 5.7.R PHYSICS-CONSTRAINED INVERTIBLE NEURAL NETWORKS FOR AIRFOIL OPTIMIZATION MODEL AT LOW REYNOLDS NUMBER
Z. Peng Peng, Nanjing University of Aeronautics and Astronautics, China
additional information (interactive) 5.7.R A HYBRID MACHINE LEARNING PIPELINE FOR AIRFOIL AERODYNAMICS: COMPARING UNIVERSAL AND CLUSTER-SPECIFIC PREDICTION STRATEGIES
R. M. Coelho, Universidade Federal de Uberlândia, Brazil
6.7AI 1
Chair(s): ,
Track 6
15 - Guest lectures (by personal invitation only)
16. Sep 26 10:50 11:15 6.7.1 TOWARDS A FOUNDATIONAL AI MODEL FOR AIRCRAFT DESIGN: FROM HIGH-FIDELITY DATASETS TO SCALING LAWS
n. Ashton, United States
7.7Configuration Aerodynamics and Coupled Flight Behaviour
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
16. Sep 26 10:50 11:15 7.7.1 FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH
Z.G. Zhang, Northwestern Polytechnical University, China
16. Sep 26 11:15 11:40 7.7.2 MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLIGHT REGIMES
D. Palma, Sapienza university of Rome, Italy
16. Sep 26 11:40 12:05 7.7.3 STUDY ON THE IMPACT OF TRIM CONDITION ON LATERAL AND DIRECTIONAL STABILITY FOR A TAILLESS AIRCRAFT
K. Kania, Warsaw University of Technology, Poland
16. Sep 26 12:05 12:30 7.7.4 GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY
P. Kantzidis, RMIT University, Australia
Reserve Paper 7.7.R NUMERICAL STUDY OF MEDIUM-WEIGHT UAV AERODYNAMIC CHARACTERISTICS DURING APPROACH AND RECOVERY TO JUAN CARLOS/CANBERRA CLASS LHDS
M. J. Ericksen¹, N. J. Lawson¹; ¹The University of Sydney, Australia
8.7Non Destructive Testing [NDT] & Structural Trials
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
16. Sep 26 10:50 11:15 8.7.1 FROM MICROCRACKING TO CRACK-NETWORK INDUCED GAS LEAKAGE IN CARBON FIBRE COMPOSITES: A MULTISCALE MODELLING FRAMEWORK
W. Chang, University of New South Wales, Australia
16. Sep 26 11:15 11:40 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
16. Sep 26 11:40 12:05 8.7.3 EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON THE FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA
J. Heo¹, J. Lee¹, A.-A. Reynolds¹, J. Cho¹, J.-H. Han¹; ¹KAIST, South Korea
16. Sep 26 12:05 12:30 8.7.4 EXPERIMENTAL INVESTIGATION OF FRETTING WEAR IN TI6-AL-4V DOVETAIL ASSEMBLIES UNDER RESONANT VIBRATION
Xiyuan Zhang¹, Dasheng Wei¹, Shun Yang¹; ¹Beihang University School of Energy and Power Engineering, China
Reserve Paper 8.7.R ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS
R. Degenhardt, DLR, Germany
Reserve Paper 8.7.R ALUMINA ENHANCED CARBON/PHENOLIC NOZZLE LINER COMPOSITE: MULTISTAGE MIXING, DSC GUIDED CURING, AND MICROSTRUCTURAL VALIDATION
Kalid-Abebe: K.- Kassa, King Fahd University of Petroleum and Minerals, Saudi Arabia
9.7Flutter
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
16. Sep 26 10:50 11:15 9.7.1 A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY
W. Qian, Dalian University of Technology, China
16. Sep 26 11:15 11:40 9.7.2 FLUTTER RESPONSE OF NOZZLE AFT DECK IN UNSTEADY ACCELERATING FLOW CONDITIONS
Haibo Zheng, Northwestern Polytechnical University, China
16. Sep 26 11:40 12:05 9.7.3 MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY
X.-Y. Ai, Dalian University of Technology, China
16. Sep 26 12:05 12:30 9.7.4 TIME-VARYING AEROELASTIC MODELING AND FLUTTER ANALYSIS OF TELESCOPIC WINGS
C.-Y. Li¹, S. He¹, Z.-C. Yang¹; ¹Northwestern Polytechnical University, China
Reserve Paper 9.7.R AEROELASTIC STABILITY AND FLUTTER PREDICTION OF A FLEXIBLE WING USING PHYSICS-BASED MODELS AND LIGHTWEIGHT AI-AIDED SURROGATE MODELS
M.V. Mehta, VIT Bhopal University, India
additional information (interactive) 9.7.R FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING
Z.-Y. Xi, Beihang University, China
additional information (interactive) 9.7.R MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION
C. -Z. Zhao, Northwestern Polytechnical University, China
10.7Propellers, Compressors and Turbines 1
Chair(s): ,
Track 10
05 - Propulsion and Energy
16. Sep 26 10:50 11:15 10.7.1 CONCEPTUAL PERFORMANCE AND MASS ASSESSMENT OF AN OPEN FAN ENGINE FOR A SHORT-MEDIUM RANGE AIRCRAFT
P. Wehrel¹, J. Häßy¹, R. Schnell¹, S. Wöhler¹; ¹German Aerospace Center (DLR)), Germany
16. Sep 26 11:15 11:40 10.7.2 SURROGATE-BASED OPTIMIZATION OF AIRCRAFT PROPELLER PERFORMANCE USING A HIGH-FIDELITY AND EFFICIENT RANS FRAMEWORK
A W Stuermer, DLR, Germany
16. Sep 26 11:40 12:05 10.7.3 FEASIBILITY OF ELECTRIC DUCTED FANS TO REPLACE OPEN PROPELLERS ON AN ELECTRIFIED TRAINING AIRCRAFT
G Braggett¹, K. F. Joiner¹, A. Somerville¹, D. Hill, Altavia Aerospace, Australia; ¹University of New South Wales, Australia
Presenter: Georgia Braggett, University of New South Wales
16. Sep 26 12:05 12:30 10.7.4 FLIGHT-DATA-DRIVEN PHYSICS-INFORMED COMPONENT MAP DERIVATION WITH STRUCTURAL COMPLIANCE
Y. Liu¹, L. Gou¹, Y. Huang, Shenzhen Research Institute of Northwestern Polytechnical Univer, China; ¹School of Power and Energy, Northwestern Polytechnical Universit, China
Reserve Paper 10.7.R ENHANCED T-MATS MODELING OF COMPRESSOR SURGE AND STALL DYNAMICS USING THE MOORE-GREITZER FRAMEWORK
Huy Nguyen, Viettel Aerospace Institute, Vietnam
11.7System identification
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 26 10:50 11:15 11.7.1 SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION
E Kim, Chungnam National University, South Korea
16. Sep 26 11:15 11:40 11.7.2 REAL TIME MODEL IDENTIFICATION OF A MICRO FLAP-BASED DELIVERY VEHICLE
T. D. Fields, University of Missouri-Kansas City, United States
16. Sep 26 11:40 12:05 11.7.3 GUST ERROR METHOD (GEM): PARAMETER IDENTIFICATION FOR AIRCRAFT SUBJECT TO VON KÁRMÁN PROCESS NOISE
P Cox, The University of Sydney, Australia
16. Sep 26 12:05 12:30 11.7.4 WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING
Yinglong He, China; Xiaoping Xu, China; Zhou Zhou, China; Shiqi Song, China
Reserve Paper 11.7.R AFFINE-INVARIANT ELLIPTICAL STATE ESTIMATION FOR ROBUST EXTENDED OBJECT TRACKING
In-Ho:I.-H. Lee, Korea Institute of Industrial Technology, South Korea
Presenter: inho lee
Reserve Paper 11.7.R INVESTIGATION OF SAFETY-CRITICAL GROUND INTERFACE (TAKEOFF, LANDING) REGIME RECOGNITION FOR AUTOMATED/AUTONOMOUS VERTICAL LIFT MISSION TASK DESIGN
M.-D. Alexander, National Research Council of Canada/Flight Research Laboratory, Canada
12.7CRM-HL 1
Chair(s): , , Imamura, T.
Track 12
03.2 - Experimental Aerodynamics
16. Sep 26 10:50 11:15 12.7.1 A COMPARATIVE WMLES STUDY OF THE CRM-HL IN FREE-AIR AND IN THE NTF FACILITY
V Sousa¹, E Sozer², K Ravikumar¹, S Hosseini², J Duensing²; ¹Analytical Mechanics Associates, United States ;²NASA, United States
16. Sep 26 11:15 11:40 12.7.2 AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMISPAN CRM-HL AT THE JAXA 6.5M X 6.5M LOW SPEED WIND TUNNEL
M. Kohzai¹, M. Murayama¹, A. Sansica¹, D. Lusher¹, T. Takaishi¹, H. Abe¹; ¹Japan Aerospace Exploration Agency, Japan
16. Sep 26 11:40 12:05 12.7.3 NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL
T.H. Hashioka, Kawasaki Heavy Industries,Ltd., Japan
13.7Optimizing AAM Networks
Chair(s): ,
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
16. Sep 26 10:50 11:15 13.7.1 THE JOINT OPTIMIZATION OF COMMUNICATION INFRASTRUCTURE AND FLIGHT CORRIDOR IN LOW-ALTITUDE URBAN AIRSPACE
Y. He, Hong Kong SAR of China
16. Sep 26 11:15 11:40 13.7.2 SIMULATION-BASED EVALUATION OF MULTIMODAL TRAFFIC COORDINATION AT SIGNALISED INTERSECTIONS FOR EMERGENCY SAFETY LANDINGS IN URBAN AIR MOBILITY
S K Sathya Kumar, Universität der Bundeswehr München, Germany
16. Sep 26 11:40 12:05 13.7.3 SCHEDULING AND ROUTING FOR TIMETABLE-BOUND URBAN AIR MOBILITY OPERATIONS
A. Edsel, Purdue University, United States
16. Sep 26 12:05 12:30 13.7.4 ESTIMATION AND ANALYSIS OF RNP REQUIREMENTS FOR HETEROGENEOUS UAM CONFIGURATIONS: INSIGHTS FROM K-UAM GRAND CHALLENGE OPPAV DEMONSTRATION
J.S. Lee¹, K. R. Oh¹; ¹Korea Aerospace Research Institute, South Korea
Reserve Paper 13.7.R WHAT UAM CNS NEEDS AND WHAT IT COSTS: AN EXPERT SURVEY
FN Naeem, TUHH, Germany
additional information (interactive) 13.7.R OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES
A. Tiwari, Indian Institute of Technology Bombay, India
14.7Multidisciplinary Advances in Aerodynamics, Aeroacoustics, and Aeroelasticity (by IFAR)
Chair(s): ,
Track 14
12 - Host Nation (by personal invitation only)
16. Sep 26 10:50 11:15 14.7.1 AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS
D. Skrna¹, M. de Rosa Jacinto¹, L. Frei¹, B. Mittenecker¹, J. Nagl¹, H. Mad¹, M. Berens¹; ¹Technische Universität Wien, Austria
16. Sep 26 11:15 11:40 14.7.2 PREDICTION OF BOUNDARY LAYER TRANSITION FOR SUPERSONIC CIVIL AIRCRAFT BASED ON NEURAL NETWORK
S.H. Yu, China
16. Sep 26 11:40 12:05 14.7.3 ON THE GROUND AND IN FLIGHT: AERODYNAMIC AND AEROELASTIC TESTING SUPPORTING INNOVATION IN AERONAUTICS
C. Mertens, Royal Netherlands Aerospace Centre, Netherlands
Presenter: Christoph Mertens, Royal Netherlands Aerospace Centre
16. Sep 26 12:05 12:30 14.7.4 UNDERSTANDING HYPERSONIC BOUNDARY LAYER LAMINAR TO TURBULENT TRANSITION IN WIND TUNNEL ENVIRONMENT
M. Lugrin, France
15.7Education enablers
Chair(s): ,
Track 15
14 - Education and Training
16. Sep 26 10:50 11:15 15.7.1 PREPARING AERONAUTICAL ENGINEERING UNDERGRADUATES FOR WORKING IN GLOBAL TEAMS
J. Abulawi, HAW Hamburg, Germany
16. Sep 26 11:15 11:40 15.7.2 REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR
K Ramotsabi, CSIR, South Africa
16. Sep 26 11:40 12:05 15.7.3 AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME
N. Moser, Germany
16. Sep 26 12:05 12:30 15.7.4 EDUCATION-ORIENTED MODEL-BASED SYSTEMS ENGINEERING FOR AERONAUTICAL ENGINEERING TRAINING AND INNOVATION
L. H. J. Machado, UFMG, Brazil
Reserve Paper 15.7.R DESIGNING AND DELIVERING A NEW PROJECT-BASED CAPSTONE AIRCRAFT DEVELOPMENT COURSE
S.J. van Heerden, University of Glasgow, United Kingdom
additional information (interactive) 15.7.R INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION
C. Varriale¹, F. Angioni¹; ¹Delft University of Technology, Netherlands

12:30 - 13:30LUNCH BREAK

0.8GENERAL LECTURE 4 Aeronautics Outlook - Directors Cut (Lane Ballard, Boeing, Veronique Roca, Airbus, Dimitri Mavris, Georgia Tech, Alan Newby, Rolls-Royce, Per Olof Marklund, SAAB. Markus Fischer, DLR
Chair:
16. Sep 26 13:30 15:15

15:15 - 15:40AFTERNOON BREAK

1.8ECSC pitch session
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
2.8Shaping aviation for society ETF
Chair(s): Holmberg, G., Collier, F.
Track 2
15 - Guest lectures (by personal invitation only)
16. Sep 26 15:40 16:05 2.8.1 ETF 2025 INTRO FOLLOWED BY INDIVIDUAL PRESENTATIONS AND A PANEL DISCUSSION AT THE END
Fayette Collier, NASA, United States; Gunnar Holmberg, Saab AB, Sweden
Presenter: Fayette Collier, NASA
16. Sep 26 16:05 16:30 2.8.2 PRACTICAL INNOVATION IN AEROSPACE
D. Donovan, United States
16. Sep 26 16:30 16:55 2.8.3 AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH
S. Kumar, United States
16. Sep 26 16:55 17:20 2.8.4 A MULTI-FUEL PROPULSION SYSTEM STRATEGY FOR AVIATION TRANSPORT RESILIENCE
I. Orisamolu, United States
3.8Case Studies 2
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
16. Sep 26 15:40 16:05 3.8.1 CONCEPTUAL DESIGN OF A NOVEL VTOL UAV USING MINI TURBOJET VERTICAL LIFT
RO Bura, Republic of Indonesia Defense University, Indonesia
16. Sep 26 16:05 16:30 3.8.2 DYNAMIC ANALYSES AND FLIGHT TESTING FOR THE DESIGN OF FLOATING CANARD AIRCRAFT
N. Morita, Velocity Aeroworks Inc., Japan
16. Sep 26 16:30 16:55 3.8.3 LOW BOOM DESIGN AND ANALYSIS OF A BLENDED-WING-BODY CONFIGURATION FOR LARGE-SIZED SUPERSONIC TRANSPORT
L.-Y Lin, Northwestern Polytechnical University, China
16. Sep 26 16:55 17:20 3.8.4 STUDY ON INDUCED DRAG CALCULATION FOR BIRD-LIKE WINGTIP SLOTS USING WAKE-PLANE INTEGRATION
Xiaru Liu, China; Tianxiang Yu, China; Bifeng Song, China; Dong Xue, China
4.8Unconventional configurations - 2
Chair(s): Melkert, J.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
16. Sep 26 15:40 16:05 4.8.1 MODELING & PRELIMINARY ANALYSIS OF AN ECOFRIENDLY AIRBORNE GLOBAL LUXURY EKRANOPLAN
Mithra Sankrithi, RIC Enterprises, United States; Dimitri Mavris¹, Raaga Sundar¹; ¹Georgia Institute of Technology, United States
16. Sep 26 16:05 16:30 4.8.2 LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY
K. Abu Salem, University of Trento, Italy
16. Sep 26 16:30 16:55 4.8.3 PROPOSING A STABLE LIFTING FUSELAGE FOR AN AIRLINER OF THE IDEAL AIRCRAFT CONFIGURATION
Reinhard Joachim Huyssen, CSIR, South Africa
16. Sep 26 16:55 17:20 4.8.4 BIOMIMICRY: INSPIRATION FOR NEXT-GENERATION AIRCRAFT
N J Wood, Macromia Aviation Ltd, United Kingdom
5.8Aerodynamic Optimization
Chair(s): Prince, S., Zingg, D.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 15:40 16:05 5.8.1 WIND TURBINE AERODYNAMIC SHAPE OPTIMIZATION BASED ON A DISCRETE ADJOINT APPROACH
L. Rodrigues Arnaud¹, F. Maia Nunes Celestino¹, G. L. Olichevis Halila¹, J. L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
16. Sep 26 16:05 16:30 5.8.2 CONTINUOUS UNSTEADY ADJOINT VARIATIONAL MULTISCALE METHOD FOR AIRFOILS SHAPE OPTIMIZATION
C. Brunelli¹, M. Avirovic¹, B. Janssens¹, B. G. Marinus¹; ¹Royal Military Academy, Belgium
16. Sep 26 16:30 16:55 5.8.3 SIMULATION OF AERODYNAMIC GROUND EFFECT FOR TILTED PROPELLERS USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S Shahjahan, Siemens Digital Industries Software Inc., United States
Presenter: Shahfiq Shahjahan, Siemens Digital Software Industries Software Inc.
16. Sep 26 16:55 17:20 5.8.4 A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS
D. Dessio Junior¹, G. L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J. L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
Reserve Paper 5.8.R OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT
Dong Xue¹, Yating Gao¹, Tao Wu¹, Bifeng Song¹, Wenp[ing Song¹; ¹Northwestern Polytechnical University, China
Presenter: Gao Yating, Northwestern Polytechnical University
additional information (interactive) 5.8.R META-HEURISTIC AIRFOIL OPTIMIZATION OF VARIABLE-PITCH LIFTING SURFACES
S. J. Jain, Delhi Technological University, India
additional information (interactive) 5.8.R OPTIMIZATION OF GEOMETRIC PARAMETERS FOR STRAIGHT-THROUGH LABYRINTH SEALS USING ORTHOGONAL EXPERIMENT AND CFD DATA-DRIVEN NEURAL NETWORK SURROGATE MOD
Xiaoling Li¹, Lixin Yang¹, Yuhang Wei¹; ¹Beijing Jiaotong University, China
additional information (interactive) 5.8.R SCALABLE HIGH-FIDELITY AERODYNAMIC CHARACTERIZATION OF WIG CRAFT USING NON-SEQUENTIAL RBF SURROGATES
N-D Diaz, ITA, Brazil
6.8AI 2
Chair(s): ,
Track 6
15 - Guest lectures (by personal invitation only)
7.8Aerodynamics of Unconventional Aircraft Configurations
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
16. Sep 26 15:40 16:05 7.8.1 AERODYNAMIC OPTIMIZATION DESIGN OF FULL-WING SOLAR-POWERED UAV FOR FLOW SEPARATION CONTROL
J. Wang¹, Z. Zhou¹, K. Wang¹, M. Li¹; ¹Northwestern Polytechnical University, China
16. Sep 26 16:05 16:30 7.8.2 STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS
C. Zheng, Beihang University, China
16. Sep 26 16:30 16:55 7.8.3 AERODYNAMIC SHAPE OPTIMIZATION OF A FUEL-CELL POWERED FLYING WING CONCEPT
P. Kirschnek, FH JOANNEUM GesmbH, Austria
16. Sep 26 16:55 17:20 7.8.4 AERODYNAMIC FEASIBILITY OF A NOVEL SWIVEL ROTOR ARCHITECTURE
B.I. Soemarwoto, Royal Netherlands Aerospace Centre NLR, Netherlands
Reserve Paper 7.8.R DEVELOPMENT OF HYDROPHILIC COATINGS FOR PRACTICAL APPLICATION OF LAMINAR FLOW WINGS
H Iijima, Japan Aerospace Exploration Agency, Japan
additional information (interactive) 7.8.R FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES
Kun Qiao, China; Dasheng Wei, China; Le Han, China; Zhongyu Chen, China; Zhaowei Yan, China; Yangjia Qin, China; Guoqiang Xu, China; Hailong Tang, China
additional information (interactive) 7.8.R UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND STABILITY ANALYSIS
J. Guo, United Kingdom
8.8Turbomachinery Structures
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
16. Sep 26 15:40 16:05 8.8.1 DESIGN ASSESSMENT OF A HELICOPTER BLADE
K Warnakula¹, M Silla¹, C Barber¹, T Hallwright¹, O Kaleagasi¹, D Schoemaker, Gyro Technic Inc., United States; ¹SYOS Aerospace, New Zealand
16. Sep 26 16:05 16:30 8.8.2 CYCLOSTATIONARY ANALYSIS FOR CRACK DETECTION AND TRENDING IN HELICOPTER GEARBOX CASING
Nader Sawalhi¹, Wenyi Wang¹; ¹Defence Science and Technology Group, Australia
16. Sep 26 16:30 16:55 8.8.3 ANALYSIS OF CRACK GROWTH CHARACTERISTICS OF HOLE CORNER CRACKS IN EXPANDED FILM COOLING HOLES ON TURBINE BLADE FLANGES
N/A Yan, Beihang University, China
9.8Aeroelastic Analysis & Design 1
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
16. Sep 26 15:40 16:05 9.8.1 AEROELASTIC TAILORING FOR COMPOSITE ADAPTIVE WINGLETS
N. Tsushima, Kyushu University, Japan; R. Higuchi¹, T. Yokozeki¹; ¹The University of Tokyo, Japan
16. Sep 26 16:05 16:30 9.8.2 PARAMETRIC AEROELASTIC STUDY OF WINGLET GEOMETRY USING VORTEX LATTICE METHOD FOR FUTURE PASSIVE MORPHING APPLICATIONS
M.N.-A. Kouchlef, The University of Tokyo, Japan
16. Sep 26 16:30 16:55 9.8.3 AEROELASTIC DESIGN OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT IN AN MDO FRAMEWORK
C. Mollet, ONERA, France
16. Sep 26 16:55 17:20 9.8.4 MANEUVER LOAD ALLEVIATION OF THE DRY WING FOR HYDROGEN AIRCRAFT
Fanglin Yu¹, Mirko Hornung¹; ¹Technical University of Munich, Germany
Reserve Paper 9.8.R DYNAMICS MODELING AND EXPERIMENTAL VERIFICATION OF ROTOR WITH COMPLEX THREE-DIMENSIONAL SHAPE BLADE
J.H Huang, China
Reserve Paper 9.8.R AFP-BASED TOW STEERING FOR AEROELASTIC OPTIMIZATION OF HIGH ASPECT-RATIO WINGS WITH FOLDING WINGTIPS
M. S. Poomadath, 1Khalifa University of Science and Technology, United Arab Emirates
10.8Propellers, Compressors and Turbines 2
Chair(s): ,
Track 10
05 - Propulsion and Energy
16. Sep 26 15:40 16:05 10.8.1 MODULAR JET AND PROPELLER ENGINE – PART I: INITIAL STUDIES
T. Otten, German Aerospace Center (DLR), Germany
16. Sep 26 16:05 16:30 10.8.2 MODULAR JET AND PROPELLER ENGINE –– PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT
T. Matuschek, German Aerospace Center (DLR), Germany
16. Sep 26 16:30 16:55 10.8.3 INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY
L. Oberthür, University of the Bundeswehr Munich, Germany
16. Sep 26 16:55 17:20 10.8.4 INITIAL GEOMETRIC UNCERTAINTY ASSESMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD
K. Omoto, Osaka Metropolitan University, Japan
11.8Guidance and flight trajectory control 2
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 26 15:40 16:05 11.8.1 TRAJECTORY OPTIMIZATION OF HIT-TO-KILL INTERCEPTORS VIA SEQUENTIAL CONVEX PROGRAMMING APPROACH
Suk-jae: S.-J. Im, Korea Advanced Institute of Science and Technology (KAIST), South Korea
16. Sep 26 16:05 16:30 11.8.2 A CONVEX PREDICTOR-CORRECTOR GUIDANCE METHOD FOR REUSABLE ROCKET ENTRY FEATURING ACTIVE WIND COMPENSATION
J. K. Zhang, China
16. Sep 26 16:30 16:55 11.8.3 DUAL BEZIER SPACE-TIME OPTIMIZATION UNDER HARD OBSERVATION-WINDOW CONSTRAINTS: A FEASIBILITY-ORIENTED JERK-CAP COMPARISON
H Kim, Koomin University, South Korea; S Lee, Kookmin University, South Korea
16. Sep 26 16:55 17:20 11.8.4 OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL
S.Y Kim, Chungbuk National University, South Korea
12.8Robot Manufacturing and Assembly Technology
Chair(s): Guevara, E.
Track 12
08 - Manufacturing and Supply Chain Management
16. Sep 26 15:40 16:05 12.8.1 GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY
B Lakic ¹, R Noll¹, G Buckus¹, R Grube¹, M Walling¹; ¹Boeing, United States
16. Sep 26 16:05 16:30 12.8.2 EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE
I. Ali¹, C. Silva², E. Villani², J. M. Mello¹, W. Oliveira²; ¹Embraer, Brazil ;²ITA, Brazil
16. Sep 26 16:30 16:55 12.8.3 VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL
A Teixeira Ferraz, Brazil
16. Sep 26 16:55 17:20 12.8.4 MIXED REALITY-BASED PROGRAMMING BY DEMONSTRATION FOR ROBOTIC GRINDING OF AERO-ENGINE BLADES
Y. Liu, Chongqing University, China
13.8Strategic Planning for AAM
Chair(s): Johnson, M.
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
16. Sep 26 15:40 16:05 13.8.1 VERTIPORT FINAL APPROACH AND TAKEOFF AREA DESIGN USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS
N.-D.-S Dhamodharasamy, Politecnico di Milano, Italy
16. Sep 26 16:05 16:30 13.8.2 LOW-NOISE VERTIPORT PROCEDURE OPTIMIZATION BASED ON DEEP REINFORCEMENT LEARNING
Y. Wang, The Hong Kong University of Science and Technology, Hong Kong SAR of China
16. Sep 26 16:30 16:55 13.8.3 IMPACT OF DEMAND PATTERNS AND BOOKING LEAD TIMES ON FLEET AND INFRASTRUCTURE IN URBAN AIR MOBILITY
M. Swaid, German Aerospace Center (DLR), Germany
16. Sep 26 16:55 17:20 13.8.4 ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT
M. Corsi, Deutsches Zentrum für Luft und Raumfahrt (DLR), Germany
Reserve Paper 13.8.R ADVANCING TELE-OPERATION IN URBAN AIR MOBILITY: A STRATEGY LEVERAGING DIGITAL TWIN TECHNOLOGY
LV Nguyen, Konkuk University, South Korea
additional information (interactive) 13.8.R A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS
X. Minze, Beihang University, China
14.8Emerging Technologies for Future Air Operations (by IFAR)
Chair(s): ,
Track 14
12 - Host Nation (by personal invitation only)
16. Sep 26 15:40 16:05 14.8.1 ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES
V. Kramar, VTT Technical Research Centre of Finland, Finland
16. Sep 26 16:05 16:30 14.8.2 PREDICTION OF STRUCTURAL VIBRATIONS INDUCED BY MASS-UNBALANCED ELECTRIC PROPULSION SYSTEMS
G. R. D. Rodrigues Dias, Aeronautics Institute of Technology, Brazil
16. Sep 26 16:30 16:55 14.8.3 METHODOLOGY AND V1 PROTOTYPE OF AN ADAPTIVE/ADAPTABLE MULTI-UAV GCS HMI IN A FLOOD SAR CO-SIMULATION TESTBED
A. G. P. Sarmento, Aeronautics Institute of Technology (ITA), Brazil
16. Sep 26 16:55 17:20 14.8.4 A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS
R.F Viana, Aeronautics Institute of Technology, Brazil
15.8Condition based maintenance
Chair(s): Scott, M.
Track 15
11 - Operations and Sustainment
16. Sep 26 15:40 16:05 15.8.1 EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION
V Kekoc, Defence Science & Technology Group, Australia
16. Sep 26 16:05 16:30 15.8.2 AI-BASED MAINTENANCE CODE CORRECTION FOR RELIABLE MTBF ANALYSIS
K. Minyoung, Korea Aerospace Industries, LTD, South Korea
16. Sep 26 16:30 16:55 15.8.3 PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING
L.J. Jilke, German Aerospace Center (DLR), Germany
16. Sep 26 16:55 17:20 15.8.4 DATA-DRIVEN TECHNOLOGY INTELLIGENCE: AN APPLICATION TO AIRCRAFT ENGINE MAINTENANCE
A Dadashi, German Aerospace Center (DLR), Germany
additional information (interactive) 15.8.R REBUILDING AGRICULTURAL STATISTICS IN POST-WAR SUDAN: A STRATEGIC FRAMEWORK FOR RECOVERY AND RESILIENCE
MohamedElamin Ahmed, Sudan Central Bureau of Statistics, Sudan
additional information (interactive) 15.8.R PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE ? -PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE
Liying Hou¹, Jiantang Liu¹, Yulu Song¹, Hui Xiao¹; ¹Nanjing University of Aeronautics and Astronautics, China

0.9SPEED MENTORING
Chair:
16. Sep 26 17:20 19:00