35th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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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

Monday, 14. Sep 2026

07:00 - 08:00Registration

0.1OPENING CEREMONY
Chair:
14. Sep 26 08:00 08:40

0.2ICAS Daniel & Florence Guggenheim Memorial Lecture Adnan Raghdo – The Boeing’s MQ-28 Ghost Bat
Chair:
14. Sep 26 08:40 09:30

09:30 - 09:55COFFEE BREAK

1.1GSA2: Global Sustainable Aviation – Setting the Stage with Global Airlines
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
14. Sep 26 09:55 10:20 1.1.1
1019		 THE WHOLE JOURNEY: PEOPLE, PLANET AND PROGRESS AT QANTAS
F Messent, Qantas Group, Australia
14. Sep 26 10:20 10:45 1.1.2
0986		 JAL’ CHALLENGE TO THE NET-ZERO GH GAS EMISSION
MS Suzuki, JAL, Japan
2.1Progress in Certification
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.1Cabin
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
14. Sep 26 09:55 10:20 3.1.1
0899		 AURAL DIGITAL TWIN FOR AIRCRAFT CABIN DESIGN
M.C, Moruzzi, Università di Bologna, Italy
14. Sep 26 10:20 10:45 3.1.2
0214		 AUTOMATED KNOWLEDGE-BASED CABIN DESIGN AND EVALUATION WITHIN A PRELIMINARY AIRCRAFT DESIGN LOOP
S. Hellbrück, DLR e.V., Germany
14. Sep 26 10:45 11:10 3.1.3
0406		 ASSESSING THE POTENTIAL OF MULTI-MODEL TOPOLOGY OPTIMIZATION FOR MODULAR LIGHTWEIGHT DESIGN OF AIRCRAFT CABIN STRUCTURES
P. Inselmann, TUHH, Germany
14. Sep 26 11:10 11:35 3.1.4
0348		 A FRAMEWORK FOR AUTOMATED SYSTEM COMPONENT PLACEMENT IN AIRCRAFT CONCEPTUAL DESIGN
J.J Vézina, Concordia University, Canada
Reserve Paper 3.1.R
0604		 HYBRID OPTIMIZATION OF FLIGHT DECK DISPLAY LAYOUT USING AN AI SURROGATE MODEL AND INTEGER LINEAR PROGRAMMING
Y Yamai, Tsukuba University, Japan
4.1Application of aerodynamics in design
Chair(s): Schmollgruber, P.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 09:55 10:20 4.1.1
0187		 LAMTA: A LAMINAR TAILORED WING WITH CATNLF AND HLFC FOR EXTRA LONG RANGE
J. Ruberte Bailo, German Aerospace Center (DLR), Germany
14. Sep 26 10:20 10:45 4.1.2
0533		 AERODYNAMIC CIRCULATION CONTROL FOR ULTRA-STOL ON THE SEAFLIGHT AURA-E ELECTRIC CARGO DRONE DEMONSTRATOR
GC Doig, UNSW Sydney, Australia
14. Sep 26 10:45 11:10 4.1.3
0817		 EVALUATION OF PERCEIVED X-15 FLYING QUALITIES BASED ON RAPID AERODYNAMIC PREDICTIONS
H.B. Rogers¹, T.T. Takahashi¹, J.A. Camberos¹, R.V. Grandhi¹; ¹AFIT, United States
14. Sep 26 11:10 11:35 4.1.4
0371		 MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE
E. Riccio, Italian Aerospace Research Centre, Italy
Reserve Paper 4.1.R
0482		 RESEARCH ON OVERALL AERODYNAMIC DESIGN OF GRID-DUCT INTEGRATED VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING AIRCRAFT
B.L Li, Northwestern Polytechnical University, China
5.1Scale Resolving Simulations
Chair(s): Coder, J., Zingg, D.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 09:55 10:20 5.1.1
0267		 LARGE EDDY SIMULATIONS OF LOW-REYNOLDS NUMBER FLOWS IN THE COMPRESSIBLE REGIME
P. Catalano, CIRA - Italian Aerospace Research Center, Italy
14. Sep 26 10:20 10:45 5.1.2
0368		 LAMINAR SEPARATION ON AN AIRFOIL WITH PERTURBATION OF BOUNDARY CONDITIONS
E. Tangermann, UniBw München, Germany
14. Sep 26 10:45 11:10 5.1.3
0040		 VARIATIONAL MULTISCALE LES OF PRE-STALL SEPARATION ON A LOW-REYNOLDS AIRFOIL
C. Brunelli, Royal Military Academy, Belgium
14. Sep 26 11:10 11:35 5.1.4
0168		 REYNOLDS NUMBER EFFECTS OF A BIRD-FEATHER-INSPIRED POROUS-MEDIUM AIRFOIL
Z.-P. Zhang, China
Reserve Paper 5.1.R
0922		 TURBULENCE MODELLING IN URBAN ENVIRONMENTS FOR UAV DESIGN CRITERIA
DL Laubscher, South Africa
additional information (interactive) 5.1.R
0480		 NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION
T.L. Lin, Northwestern Polytechnical University, China
additional information (interactive) 5.1.R
0939		 ASSESSING VORTEX BREAKDOWN AND COUPLING IN DELTA WING PLANFORMS THROUGH HIGH-FIDELITY DDES SIMULATIONS
T. A. Missato, Brazil
6.1Aerodynamic Response and Wake Characteristics
Chair(s): Post, M., Breitsamter, C.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
14. Sep 26 09:55 10:20 6.1.1
0194		 RESPONSE CHARACTERISTICS OF WINGTIP VORTEX INSTABILITY TO EXTERNAL DISTURBANCES
Y.-M Wu, Shanghai Jiao Tong University, China
14. Sep 26 10:20 10:45 6.1.2
0228		 NONLINEAR 3-DOF MOTION PREDICTION OF A BOX IN WAVES USING PHYSICS-INFORMED NEURAL OPERATORS
ZP Hoffman, Australia
14. Sep 26 10:45 11:10 6.1.3
0637		 THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW
J-M Mourad, ISAE-Supaero, France
14. Sep 26 11:10 11:35 6.1.4
0655		 INTERACTION OF COUNTER-PLUNGING BIPLANE AIRFOILS WITH A FLAT PLATE BOUNDARY LAYER AND WAKE
B. Anilir, METU Aerospace Engineering Department, Turkey
Reserve Paper 6.1.R
0820		 CHARACTERISTICS AND UNDERLLYING MECHANISMS OF VORTEX WANDERING
NONE Gao, China
7.1Distributed Propulsion and Aerodynamic Interaction
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
14. Sep 26 09:55 10:20 7.1.1
0108		 INVESTIGATION OF DISTRIBUTED PROPELLER PROPULSIVE CHARACTERISTICS UNDER NON-AXIAL INFLOW
B.-X. Boming, School of Aeronautics, Northwestern Polytechnical University, China
14. Sep 26 10:20 10:45 7.1.2
0200		 EFFECT OF LIP/NOZZLE DEFLECTION ANGLE ON THE AERODYNAMIC AND PROPULSIVE CHARACTERISTICS OF PROPULSIVE WING UNITS
Ming-Hao: M. -H Li, Northwestern Polytechnical University, China
14. Sep 26 10:45 11:10 7.1.3
0444		 PROPELLER AERODYNAMICS UNDER NON-UNIFORM INFLOWS
G. Cafiero, Politecnico di Torino, Italy
14. Sep 26 11:10 11:35 7.1.4
0516		 AERODYNAMIC EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT CHARACTERISTICS OF A WING–FLAP CONFIGURATION
H.-X. He, China
Reserve Paper 7.1.R
0297		 DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING
B Y Li, Northwestern Polytechnical University, China
8.1Additive Manufacturing
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 09:55 10:20 8.1.1
0507		 FINITE ELEMENT MODELLING OF ADDITIVELY MANUFACTURED TANTALUM UNDER HIGH-HEAT CONDITIONS FOR AEROSPACE APPLICATIONS
M.J Davids, HH Industries, South Africa
14. Sep 26 10:20 10:45 8.1.2
0603		 NUMERICAL AND EXPERIMENTAL ANALYSIS OF TENSILE BEHAVIOR OF 2024-T6 ALUMINUM ALLOY OBTAINED BY DIRECT SELECTIVE LASER MELTING
R. P. Solís, University Technical Federico Santa María, Chile
14. Sep 26 10:45 11:10 8.1.3
0351		 4D PRINTING VIA ELECTROMAGNETISM FOR COMPOSITE STRUCTURES
SHV Vattathurvalappil, King Fahd University of Petroleum and Minerals, Saudi Arabia
14. Sep 26 11:10 11:35 8.1.4
0499		 ACCESSIBLE MATERIAL COMPOSITES FOR UAVS IN HUMANITARIAN AND DEVELOPMENT CONTEXTS
C Koutsambasis, RMIT University , Australia
Reserve Paper 8.1.R
0029		 COMPRESSION AND FATIGUE PERFORMANCE OF ADDITIVELY MANUFACTURED NITI ARCHITECTED SHAPE MEMORY ALLOYS
B.B. Zwerink, NLR, Netherlands
Reserve Paper 8.1.R
0250		 DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS
J. D. Rodrigues, RMIT University, Australia
9.1System of Systems 1
Chair(s): Delaurenis, D., Prakasha, P.
Track 9
02 - Systems Engineering and Integration
14. Sep 26 09:55 10:20 9.1.1
0046		 ONTOLOGY-BASED EXPLORATION OF SYSTEM-OF-SYSTEMS ARCHITECTURES USING A FEDERATED STRUCTURE
L. Knöös Franzén, Linköping University, Sweden
14. Sep 26 10:20 10:45 9.1.2
0076		 DIGITAL TWIN FOR AIR DEFENSE: LIVE-VIRTUAL-CONSTRUCTIVE INTEGRATION AND DECISION SUPPORT
S. Malka, Naval Postgraduate School, United States
14. Sep 26 10:45 11:10 9.1.3
0671		 COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER
P.F Li, Northwest Polytechnic University, China
14. Sep 26 11:10 11:35 9.1.4
0675		 INTERFACING MISSION SIMULATION WITH INTELLIGENT AGENTIC SYSTEMS FOR OPERATIONAL AND ETHICAL EVALUATION
H. Budig¹, E. Zegarra Berodt¹, N.-G. Wood¹, V. Gollnick¹; ¹Hamburg University of Technology, Germany
10.1AI applications in flight control, simulation and modeling
Chair(s): ,
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 09:55 10:20 10.1.1
0872		 NEURAL NETWORK BASED SLIDING MODE CONTROL FOR HYPERSONIC LONGITUDINAL CONTROL
H. Kim, South Korea
14. Sep 26 10:20 10:45 10.1.2
0907		 ON ROBUST AIRCRAFT CONTROL WITH AI: TARGETED TRAINING STIMULI OVER EXPERIENCE VOLUME
C Koopman, University of Malta, Malta
14. Sep 26 10:45 11:10 10.1.3
0648		 SUPPORTING PILOT SITUATIONAL AWARENESS BY EXTRACTING INSIGHTS FROM AN AI EXPERT
C Koopman, University of Malta, Malta
11.1Flight control 1
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 09:55 10:20 11.1.1
0011		 ADAPTIVE FLIGHT CONTROL LAWS APPLIED TO AIR REFUELING WITH RECEIVERS EQUIPPED WITH RECEPTACLE OUT OF THE PLANE OF SYMMET
M-J Martinez, Airbus, Spain
14. Sep 26 10:20 10:45 11.1.2
0647		 BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL
Y. L. Niu, Beihang University, China
14. Sep 26 10:45 11:10 11.1.3
0843		 AIRBRAKES CONTROL SYSTEM FOR PRECISE APOGEE CONTROL OF A SOUNDING ROCKET
N. Gee-Landman, Royal Melbourne Institute of Technology, Australia
14. Sep 26 11:10 11:35 11.1.4
0425		 FIXED-WING AIRCRAFT PORT-HAMILTONIAN DYNAMICS AND CONTROL
E. M. Fernandes, Instituto Tecnologico de Aeronautica, Brazil
Reserve Paper 11.1.R
0114		 BENEFITS AND DRAWBACKS OF USING DIFFERENTIAL THRUST WITH DEP FOR FLIGHT CONTROL ON PROPELLER DRIVEN FIXED WING AIRCRAFT
T. Sachtleben Dahmann, DLR, Germany
12.1UAV Component
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
14. Sep 26 09:55 10:20 12.1.1
0335		 IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL
G. Schmitz, Germany
14. Sep 26 10:20 10:45 12.1.2
0684		 RECONFIGURABLE MULTILEVEL BATTERY ARCHITECTURE FOR SMALL UAV PROPULSION SYSTEMS
N Sorokina, Universität der Bundeswehr München, Germany
14. Sep 26 10:45 11:10 12.1.3
0786		 ROTATIONAL STABILITY ENHANCEMENT OF A SMALL TWO STROKE ENGINE FOR SMALL UAV WITH INTEGRATED FLYWHEEL CLUTCH SYSTEM
H.-R. Gwon, Korean Air / R&D Center, South Korea
14. Sep 26 11:10 11:35 12.1.4
0833		 DYNAMIC MODELING AND STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR FOR FIXED-WING UAVS
L. H. J. Machado, UFMG, Brazil
Reserve Paper 12.1.R
0590		 A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING
J. Cheng, China
Reserve Paper 12.1.R
0921		 DEVELOPMENT OF A MODULAR SENSOR FUSION PAYLOAD FOR FLIGHT TESTING OF VISUAL-INERTIAL NAVIGATION ALGORITHM IN SMALL UAVS
A Fathurrahman, Insitute Teknologi Bandung, Indonesia
additional information (interactive) 12.1.R
0382		 SYSTEM-LEVEL ARCHITECTURE OPTIMISATION FOR GROUND AND TERMINAL OPERATIONS OF NARROW-BODY AIRCRAFT
S Lyu, United Kingdom
13.1Safety and Efficiency in Aviation
Chair(s): Maroney, D.
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
14. Sep 26 09:55 10:20 13.1.1
0995		 DIGITALISATION AND INTELLIGENT AUTOMATION IN GROUND HANDLING AND ENGINEERING: ENABLING NEXT-GENERATION AIRPORT EFFICIENCY
D. So Man Fung, Singapore
14. Sep 26 10:20 10:45 13.1.2
0247		 DESIGN AND FEASIBILITY ASSESSMENT OF TRANSPORT OPERATIONS FOR DELIVERING TYPHOON CONTROL SUBSTANCES
H. Akiyama, Yokohama National University , Japan
14. Sep 26 10:45 11:10 13.1.3
0332		 A PEAKS-OVER-THRESHOLD APPROACH TO RUNWAY COLLISION RISK ESTIMATION FOR EFFICIENT ARRIVAL OPERATIONS
N.K. Wickramasinghe, Electronic Navigation Research Institute, Japan
14. Sep 26 11:10 11:35 13.1.4
0694		 OPPORTUNITIES AND CHALLENGES FOR ARTIFICIAL INTELLIGENCE IN AIR TRAFFIC PREDICTION PROBLEMS FOR FLIGHT OPERATORS
S.M. Abdulhak, United States
Reserve Paper 13.1.R
0216		 NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT
R. Sáez, Technical University of Catalonia (UPC), Spain
14.1Vision & Control
Chair(s): , , Grabowski, T.
Track 14
06.2 - Flight Dynamics and Control (UAV related)
14. Sep 26 09:55 10:20 14.1.1
0143		 MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS
R. Perz, Institute of Aeronautics and Applied Mechanics, WUT, Poland
14. Sep 26 10:20 10:45 14.1.2
0163		 ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW
M. Yanagisawa, Kyushu University, Japan
14. Sep 26 10:45 11:10 14.1.3
0737		 FLIGHT TEST VALIDATION OF A VISION-GUIDED MULTIROTOR TERMINAL INTERCEPTION SYSTEM
Y.R. Kim, Cheongju University, South Korea
14. Sep 26 11:10 11:35 14.1.4
0096		 A SYSTEMATIC, TUNING-FREE ATTITUDE CONTROL METHOD FOR VTOL UAVS
K. Okamoto, The University of Tokyo, Japan
Reserve Paper 14.1.R
0288		 DEEP LEARNING VS. TRADITIONAL COMPUTER VISION FOR UAV LANDING SITE DETECTION IN ADVERSE WEATHER
R. Schmidt, German Aerospace Center (DLR), Germany
additional information (interactive) 14.1.R
0649		 AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION OF JUNGLE RECONNAISSANCE UAV
S. Li, China
15.1 Aircraft Systems, Operations, and Certification
Chair(s): ,
Track 15
10 - Safety and Security
14. Sep 26 09:55 10:20 15.1.1
0154		 WHO SHOULD SIT AT THE EXIT ROW? A HUMAN FACTORS APPROACH TO EMERGENCY EVACUATION PASSENGER SELECTION IN COMMERCIAL AVIAT
A Reisier¹, M Machado Cardoso Júnior ¹, C Lessa¹, P Kurka, ITA , Brazil; R Freitas¹; ¹ITA, Brazil
14. Sep 26 10:20 10:45 15.1.2
0307		 CONCEPT OF OPERATIONS FOR A HYDROGEN-ELECTRIC POWERED MODIFIED DASH8-300 REGIONAL AIRCRAFT: PERFORMANCE, OPERATIONAL, AND CERTIFICATION IMPACTS
B Rietdijk, Conscious Aerospace, Netherlands
14. Sep 26 10:45 11:10 15.1.3
0363		 TOWARD THE INTEGRATION OF NEUROPHYSIOLOGICAL SIGNALS AND HUMAN BODY DYNAMICS FOR ADAPTIVE CONTROL ALLOCATION
T. Treichl, German Aerospace Center, Germany
14. Sep 26 11:10 11:35 15.1.4
0701		 A CENTRALIZED KEY MANAGEMENT ARCHITECTURE FOR SECURE GROUP COMMUNICATION ON IMA PLATFORM
C. A. Dautel, Institute of Aircraft Systems, University of Stuttgart, Germany

11:35 - 11:40CHANGEOVER BREAK

0.3GENERAL LECTURE 1 Jet Zero’s Blended Wing Body Aircraft
Chair:
14. Sep 26 11:40 12:30

12:30 - 13:30LUNCH BREAK

1.2GSA2: Perspectives and Progress towards NextGen Airliners
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
14. Sep 26 13:30 13:55 1.2.1
0987		 BOEING PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY
M L Drake, The Boeing Company, United States
2.2High Speed Flight – Oveview
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.2Conceptual Design 1
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
14. Sep 26 13:30 13:55 3.2.1
0528		 A POINT-CLOUD-BASED METHOD FOR INTELLIGENT AIRCRAFT CONFIGURATION LAYOUT GENERATION
J.Z. Zhang, China
14. Sep 26 13:55 14:20 3.2.2
0727		 INVERSE CONSTRAINT ANALYSIS FOR DESIGN SPACE EXPANSION: DERIVING AERODYNAMIC TARGETS IN SUPERSONIC FIGHTER CONCEPTUAL DESIGN
S.-J. Kim Kim, Agency for Defense Development, South Korea
14. Sep 26 14:20 14:45 3.2.3
0806		 DEVELOPMENT OF A FRAMEWORK FOR INTEGRATION AND PERFORMANCE ANALYSIS OF NOVEL ENGINES DURING AIRCRAFT CONCEPTUAL DESIGN
S. Hosseini, Amirkabir University of Technology (Tehran Polytechnic), Iran
14. Sep 26 14:45 15:10 3.2.4
0285		 ASSESSMENT OF LIQUID HYDROGEN-POWERED AIRCRAFT RANGE: A NOVEL BREGUET FORMULATION
G. Palaia, Polytechnic of Turin, Italy
Reserve Paper 3.2.R
0015		 SCENARIO-BASED TECHNOLOGY ROADMAPPING IN AEROSPACE USING DBSCAN AND LLM
T. A. Brutscher, Liebherr-Aerospace Lindenberg GmbH, Germany
Reserve Paper 3.2.R
0229		 FORMALIZING THE INTEGRATION BETWEEN MODEL-BASED SYSTEMS ENGINEERING AND SYSTEM ARCHITECTURE OPTIMIZATION
S. Valencia-Ibanez, Concordia University, Canada
4.2Conceptual design studies - 1
Chair(s): Lott, M.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 13:30 13:55 4.2.1
0447		 PERFORMANCE COMPARISON BETWEEN PASSENGER AIRCRAFT WITH NOVEL PROPULSION SYSTEMS AT CONCEPTUAL DESIGN LEVEL
JC Chan, Cranfield University, United Kingdom
14. Sep 26 13:55 14:20 4.2.2
0888		 FUTURE LONG RANGE AIRCRAFT CONCEPT EXPLORATION AND FLIGHT TEST NEEDS IDENTIFICATION
P. Schmollgruber, ONERA, France
14. Sep 26 14:20 14:45 4.2.3
0926		 SUPPORTING THE REGULATORY COMMUNITY SHAPING THE FUTURE OF SUSTAINABLE HIGH-SPEED CIVIL AVIATION: THE ESATTO FRAMEWORK
N. Viola, Politecnico di Torino, Italy
5.2Transition Predictions
Chair(s): Prince, S., Halila, G.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 13:30 13:55 5.2.1
0936		 OVERVIEW OF VERIFICATION AND VALIDATION EFFORTS FOR PDE-BASED LAMINAR-TURBULENT TRANSITION MODELS
J. G. Coder, Penn State University, United States
14. Sep 26 13:55 14:20 5.2.2
0226		 ACCURACY AND EFFICIENCY OF TRANSITION–TURBULENCE MODELS IN PREDICTING HIGH AND LOW REYNOLDS NUMBER PROPELLER PERFORMANCE
F. Parra, Universidad de Leon, Spain
14. Sep 26 14:20 14:45 5.2.3
0463		 RESEARCH ON TRANSITION PREDICTION METHODS FOR HELICOPTER ROTOR BLADES
Z.-K Zhou, China
14. Sep 26 14:45 15:10 5.2.4
0653		 HYPERBOLIC RECEPTIVITY TO FREESTREAM DISTURBANCES OVER A BLUNT WEDGE: A LINEARIZED NAVIER–STOKES APPROACH
Zhichao Zhu, Tsinghua University, China
6.2Aircraft Flow control Applications
Chair(s): Vijgen, P., Post, M.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
14. Sep 26 13:30 13:55 6.2.1
0185		 PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS
Y.-M. Mou, Shanghai Jiaotong University, China
14. Sep 26 13:55 14:20 6.2.2
0255		 ACTIVE FLOW CONTROL AND THERMAL PROTECTION FOR A WING-BODY CONFIGURATION BASED ON LATERAL JET
L. He, China
14. Sep 26 14:20 14:45 6.2.3
0374		 REDUCED-ORDER MODELLING OF MINI-TAB SPOILER DYNAMICS FOR GUST LOAD ALLEVIATION
A. Jürisson, Royal Netherlands Aerospace Centre, Netherlands
14. Sep 26 14:45 15:10 6.2.4
0949		 MODELING, SIMULATION, AND VALIDATION OF COVERT FLAPS FOR IMPROVED TRANSITION CONTROL OF TILTWING AIRCRAFT
A.M. Comer, Oklahama State University, United States
7.2Aero-Thermal Effects, Icing and Propulsion System Integration
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
14. Sep 26 13:30 13:55 7.2.1
0242		 NUMERICAL SIMULATION OF SUPERCOOLED LARGE DROPLET IMPINGEMENT ON ROTATING FAN BLADES
H. Yan, Shanghai Jiao Tong University, China
14. Sep 26 13:55 14:20 7.2.2
0339		 STUDY OF THE SONIC AND SUBSONIC JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER IN D-DUCT FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM
D.Z Dong, Shanghai Jiao Tong University, China
14. Sep 26 14:20 14:45 7.2.3
0501		 AIRFRAME-INLET INTEGRATION DESIGN FOR AN OVER-WING-MOUNTED SUPERSONIC TRANSPORT CONFIGURATION
Q. Chen, China
14. Sep 26 14:45 15:10 7.2.4
0884		 AI-BASED FORECASTING OF ICE-INDUCED AERODYNAMIC DEGRADATION
S. Corcione, University of Naples Federico II, Italy
Reserve Paper 7.2.R
0403		 HEATING EFFECT OF DRONE DOWNWASH UNDER INVERSE TEMPERATURE CONDITIONS
P. Kirschnek, FH JOANNEUM GesmbH, Austria
8.2Aerospace-grade Composites
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 13:30 13:55 8.2.1
0491		 VISUAL MACHINE LEARNING ANALYSIS OF MULTIFUNCTIONAL PERFORMANCE IN GRAPHENE FRP COMPOSITES
V.M Kannan, Australia
14. Sep 26 13:55 14:20 8.2.2
0160		 EFFICIENT SIMULATION AND UNCERTAINTY QUANTIFICATION OF PROGRESSIVE CRUSHING IN COMPOSITE LAMINATES
J Reiner, Deakin University, Australia
14. Sep 26 14:20 14:45 8.2.3
0036		 DEVELOPMENT OF CONDUCTIVE COMPOSITE MATERIALS FOR HIGH VOLTAGE APPLICATIONS
S.A. Brown, UNSW, Australia
14. Sep 26 14:45 15:10 8.2.4
0082		 COMPRESSIVE PERFORMANCE OF VARIABLE-STIFFNESS COMPOSITE HYPERBOLIC STIFFENED PANELS BASED ON GEOMETRIC PATH MAPPING
R. Ma, Northwestern Polytechnical University, School of Aeronautics, China
Reserve Paper 8.2.R
0022		 USING LIGHTWEIGHT COMPOSITE TIE-RODS IN PLACE OF HIGH STRENGTH STEEL TIE-RODS
A.-K. Kumar, THE BOEING COMPANY, India
Reserve Paper 8.2.R
0868		 ENHANCEMENT AND DEGRADATION: THE DUAL ROLE OF GRAPHENE NANOPLATELETS ON THE STRUCTURAL PERFORMANCE OF COMPOSITE T-JOINTS
M. Bhasin, RMIT University, Australia
9.2System of Systems 2
Chair(s): Crossley, W., Jouannet, C.
Track 9
02 - Systems Engineering and Integration
14. Sep 26 13:30 13:55 9.2.1
0607		 THE CONFERENCE LOCATIONS: A QUANTITATIVE APPROACH TO REDUCING IMPACT GLOBAL TRAVEL
C. Jouannet, Linköping University, Sweden
14. Sep 26 13:55 14:20 9.2.2
0910		 MODELING, SIMULATION AND CASE STUDY OF LARGE-SCALE FOREST FIRE EXTINGUISHING AND RESUE SYSTEM BASED ON AVIATION METERIEL
W. Cheng, Aviation Industry Development Research Center of China (ADR) , China
14. Sep 26 14:20 14:45 9.2.3
0918		 FEATURE MODEL CREATION THROUGH MISSION ANALYSIS IN THE CONTEXT OF VEHICLE FAMILIES
A.M. Zarate Villazon, Georgia Institute of Technology - Aerospace Systems Design Lab, United States
10.2Machine learning in flight control, simulation, and modeling
Chair(s): ,
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 13:30 13:55 10.2.1
0622		 SYSTEM IDENTIFICATION USING FLIGHT TEST DATA AND MACHINE LEARNING
G. Larsson, Saab Aeronautics, Sweden
14. Sep 26 13:55 14:20 10.2.2
0865		 AUTOMATIC GROUND COLLISION AVOIDANCE VIA SUPERVISED LEARNING–BASED RECOVERY TRAJECTORY PREDICTION
J. Han, Korea Advanced Institute of Science and Technology (KAIST), South Korea
14. Sep 26 14:20 14:45 10.2.3
0567		 LEARNING-BASED CONTROL ALLOCATION FOR OVER-ACTUATED VTOL AIRCRAFT WITH NONLINEAR DYNAMICS
D. Kim, Korea Advanced Institute of Science and Technology, South Korea
14. Sep 26 14:45 15:10 10.2.4
0664		 RESIDUAL LEARNING FRAMEWORK FOR NONLINEAR AEROELASTIC–FLIGHT-DYNAMICS CONTROL-ORIENTED MODELING OF VERY FLEXIBLE AIRCRAFT
Carlos E. S. Cesnik, University of Michigan, United States
additional information (interactive) 10.2.R
0109		 PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE
Z.-M. Wu, Northwestern Polytechnical University, China
11.2Flight control 2
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 13:30 13:55 11.2.1
0440		 STABILITY AUGMENTATION SYSTEM DESIGN FOR LONGITUDINALLY UNSTABLE TAILLESS AIRCRAFT
S. Riethausen, Linköping University, Sweden
14. Sep 26 13:55 14:20 11.2.2
0123		 ROBUST ESTIMATION-AWARE GUIDANCE FOR STOCHASTIC INTERCEPTION WITH PARAMETRIC UNCERTAINTY
LM Mudrik, United States
14. Sep 26 14:20 14:45 11.2.3
0166		 DOB-BASED ADAPTIVE NONSINGULAR TERMINAL SLIDING MODE CONTROL FOR FAULT-TOLERANT CONTROL OF QUAD-TILTROTOR EVTOL
S Kim, Chungnam National University, South Korea
14. Sep 26 14:45 15:10 11.2.4
0441		 FLIGHT ENVELOPE PROTECTION FOR HIGH ALTITUDE LONG ENDURANCE AIRCRAFT
C. Weiser, DLR - German Aerospace Center, Germany
Reserve Paper 11.2.R
0725		 CONTROL ALLOCATION AND SIZING FOR OVER-ACTUATED AIRCRAFFT
C. Doll, ONERA, France
12.2De-icing
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
14. Sep 26 13:30 13:55 12.2.1
0025		 A THERMO-MECHANICAL PHASE FIELD MODEL CONSIDERING SOLID-LIQUID TRANSITION: APPLICATION TO ELECTROTHERMAL DE-ICING
Y.Y Ying, Northwestern Polytechnical University, China
14. Sep 26 13:55 14:20 12.2.2
0186		 ICE DETECTOIN: CORRELATION ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES
G. Mingione, CIRA, Italy
14. Sep 26 14:20 14:45 12.2.3
0660		 A MPC STRATEGY FOR THE VECTOR CONTROL OF RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS
J. Pothin, ISAE Suapero, France
14. Sep 26 14:45 15:10 12.2.4
0681		 ELECTROMECHANICAL RESONANT ICE PROTECTION SYSTEMS USING VOICE COIL ACTUATORS - AIR INLET SECTION CASE STUDY
Y. R. Rafik, INSA, France
Reserve Paper 12.2.R
0535		 DESIGN METHODOLOGY OF A LOW-COST FOREBODY FOR SUBSONIC WIND TUNNEL TESTING
NQ Nghiem, VIETTEL AEROSPACE INSTITUTE, Vietnam
13.2Air Traffic Sequencing and Flows
Chair(s): Brown, M.
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
14. Sep 26 13:30 13:55 13.2.1
0048		 TRAJECTORY ADJUSTMENTS IN JAPANESE MOVING SECTORS TO REDUCE AIR TRAFFIC COMPLEXITY
S. Goeppel, University of the Bundeswehr, Germany
14. Sep 26 13:55 14:20 13.2.2
0408		 RUNWAY-AWARE CAPACITY ENVELOPES FOR LONG-RANGE ARRIVAL METERING UNDER OPERATING-DIRECTION CHANGES AT SINGAPORE CHANGI
E. Asadi, Bundeswehr University of Munich, Germany
14. Sep 26 14:20 14:45 13.2.3
0446		 AIRCRAFT SEQUENCING UNDER UNCERTAINTY: GAME-THEORETIC OPTIMIZATION AND A COMPARATIVE ANALYSIS OF GLOBAL AND INTRA-AIRLINE COOPERATIVE DECISION FRAMEWO
S Tsuru, Osaka Metropolitan University, Japan
14. Sep 26 14:45 15:10 13.2.4
0591		 IMPACT OF DYNAMIC METERING OPERATIONS UNDER ADVERSE WEATHER AND MITIGATION THROUGH OPTIMAL SEQUENCING
Y Matsuno, Japan Aerospace Exploration Agency, Japan
Reserve Paper 13.2.R
0893		 AIRCRAFT CLIMB PROFILE PREDICTION VIA MACHINE LEARNING-BASED FRAMEWORK
H Seon, Korea Aerospace University, South Korea
14.2Mission Planning and Navigation
Chair(s): , , Hristozov, S.
Track 14
06.2 - Flight Dynamics and Control (UAV related)
14. Sep 26 13:30 13:55 14.2.1
0217		 DYNAMIC RECONFIGURABLE PATH PLANNING FOR FIRE-FIGHTING UAVS
SF Armanini, Imperial College London, United Kingdom
14. Sep 26 13:55 14:20 14.2.2
0709		 COOPERATIVE GROUND AND AERIAL SURVEILLANCE FOR TRACKING OF UNAUTHORIZED AERIAL VEHICLES
D. Y. Yoon, Hanseo University, South Korea
14. Sep 26 14:20 14:45 14.2.3
0695		 MODELING OF CRITICAL WEATHER FLIGHT PERFORMANCE OF MULTICOPTER UAVS FOR RESILIENT CONTROLLER DESIGN
A. Fallast, FH JOANNEUM, Austria
14. Sep 26 14:45 15:10 14.2.4
0079		 SIMULATION-BASED ANALYSIS OF REDUNDANT UAV NAVIGATION UNDER GNSS OUTAGES
M Ben Simon, Naval Postgraduate School, United States
Reserve Paper 14.2.R
0477		 GEOMETRY-AWARE AERIAL LIGHT SHOW: JOINT OPTIMIZATION OF SWARM SIZE AND ENERGY-EFFICIENT TRAJECTORIES
K.-G. Yuksel, Aselsan, Turkey
15.2AI Safety, Verification, and Trust
Chair(s): ,
Track 15
10 - Safety and Security
14. Sep 26 13:30 13:55 15.2.1
0210		 ON THE APPLICABILITY OF SAFETY NETS: A SAFETY-BY-DESIGN SOLUTION FOR CERTIFYING NEURAL NETWORKS
J. M. Christensen, German Aerospace Center (DLR), Germany
14. Sep 26 13:55 14:20 15.2.2
0536		 COVERAGE-DRIVEN VERIFICATION FOR SAFETY-BY-DESIGN IN AI-BASED COLLISION AVOIDANCE SYSTEMS
T Stefani, German Aerospace Center, Germany
14. Sep 26 14:20 14:45 15.2.3
0782		 RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING
J Gao, The University of Sydney, Australia
14. Sep 26 14:45 15:10 15.2.4
0942		 ADVANCING TRUST FOR THRUST: PAIRING AND SHARING
L.J.A. Jansen, German Aerospace Center (DLR), Germany

15:10 - 15:15CHANGEOVER BREAK

0.4GENERAL LECTURE 2 Airbus 400M
Chair:
14. Sep 26 15:15 16:05

16:05 - 16:30AFTERNOON BREAK

1.3GSA2: Perspectives and Progress on NextGen Propulsion for Future Airliners
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
14. Sep 26 16:30 16:55 1.3.1
1008		 PRATT & WHITNEY: MEETING THE FUTURE PROPULSION NEEDS OF COMMERCIAL AVIATION
A.M. Murphy, Pratt & Whitney, United States
14. Sep 26 16:55 17:20 1.3.2
1010		 CFM INTERNATIONAL\'S RISE PROGRAM: A STEP-CHANGE FOR DURABILITY AND EFFICIENCY
C.-A. Andrews, GE Aerospace, United States
2.3Digital Thread and Integration
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.3Conceptual Design 2
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
14. Sep 26 16:30 16:55 3.3.1
0400		 AN INTEGRATED CONCEPTUAL DESIGN WORKFLOW FOR LIQUID HYDROGEN-POWERED BOX-WING AIRCRAFT
K. Abu Salem, University of Trento, Italy
14. Sep 26 16:55 17:20 3.3.2
0575		 AGENTIC AI FOR AIRCRAFT PRELIMINARY DESIGN: PROOF OF CONCEPT
A. Kirste, RWTH Aachen University, Germany
14. Sep 26 17:20 17:45 3.3.3
0668		 AI-SUPPORTED AIRCRAFT SYSTEM ARCHITECTURE SYNTHESIS
P. Krus, Linköping University, Sweden
14. Sep 26 17:45 18:10 3.3.4
0130		 DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+
J Song, Korea Institute of Industrial Technology (KITECH), South Korea
4.3Conceptual design studies - 2
Chair(s): Nicolosi, f.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 16:30 16:55 4.3.1
0008		 BOEING 777 FREIGHTER CONVERSION STRATEGY: FORWARD \"STANDARD\" VS. REAR EXTRA-LARGE (XL) MAIN DECK CARGO DOOR
I. Berlowitz, IBAero Engineering, Israel
14. Sep 26 16:55 17:20 4.3.2
0792		 CONCEPTUAL DESIGN OF A PROPFAN-POWERED TRUSS-BRACED WING REGIONAL AIRCRAFT
S. Hosseini, Amirkabir University of Technology (Tehran Polytechnic), Iran
14. Sep 26 17:20 17:45 4.3.3
0296		 FLIGHT TESTING OF A HIGH-ALTITUDE UNCREWED AND SOLAR POWERED PLATFORM HEAVIER THAN AIR
F. Nikodem, German Aerospace Center (DLR e.V.) / Institute of Flight Systems, Germany
14. Sep 26 17:45 18:10 4.3.4
0420		 CONCEPTUAL DESIGN OF A MIDDLE-OF-THE-MARKET AIRCRAFT FOR EDUCATIONAL PURPOSES
S. J. van Heerden, University of Glasgow, United Kingdom
5.3Buffeting and Other Aeroelastic Analyses
Chair(s): Azevedo, J.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 16:30 16:55 5.3.1
0183		 NUMERICAL MODELING OF TRANSONIC BUFFET ON THE NASA COMMON RESEARCH MODEL
M. J. Candon, RMIT University, Australia
14. Sep 26 16:55 17:20 5.3.2
0927		 HIGH-FIDELITY ANALYSIS OF AIRCRAFT TAIL BUFFETING UNDER DYNAMIC MANEUVERING
Y Lua, Global Engineering and Materials, Inc., United States
14. Sep 26 17:20 17:45 5.3.3
0282		 BUFFETING SCALE EFFECTS ON A LAUNCH VEHICLE: HYBRID RANS-LES ANALYSIS
D. Palma, Sapienza university of Rome, Italy
14. Sep 26 17:45 18:10 5.3.4
0796		 AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING
Y. Zhao, Northwestern Polytechnical University, China
additional information (interactive) 5.3.R
0953		 COST-EFFECTIVE STAR-CCM+ REPRODUCTION OF DPW-7 CASE 2A: MESH EFFECTS ON CRM TRANSONIC PITCHING MOMENT AND ADAPTIVE REFINEMENT LIMITS
G. C. Ribolla¹, M. B. Stergiou¹, L. J. F. Meirelles¹, L. F. S. Gomes¹, R. M. Granzoto, Embraer, Brazil; P. Bufacchi¹; ¹Insper, Brazil
6.3Hypersonics Boundary Layer and Flow Features
Chair(s): Moreau, D., Vijgen, P.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
14. Sep 26 16:30 16:55 6.3.1
0070		 RECEPTIVITY OF NON-MODAL STREAKS IN HYPERSONIC BLUNT BOUNDARY LAYERS: FROM NUMERICS TO ASYMPTOTICS
M. Dong, Institute of Mechanics, Chinese Academy of Sciences, China
14. Sep 26 16:55 17:20 6.3.2
0094		 ORIGIN OF TRANSIENT TURBULENT SPOTS IN HYPERSONIC SWEPT BOUNDARY-LAYERS WITH MORPHING SWEEP ANGLES
G. Jiang, Institute of Mechanics, Chinese Academy of Sciences, China
14. Sep 26 17:20 17:45 6.3.3
0311		 NUMERICAL SIMULATION OF HYPERSONIC PLASMA FLOW BASED ON NONLINEAR COUPLED CONSTITUTIVE RELATIONS
H. Shi, Northwestern Polytechnical University, China
14. Sep 26 17:45 18:10 6.3.4
0781		 AFTERBODY CURVATURE EFFECTS ON FLOW LOSS CHARACTERISTICS BASED ON ENTROPY PRODUCTION
X.W. Chen, Shanghai Jiao Tong University, China
Reserve Paper 6.3.R
0708		 MASSIVELY-SEPARATED HYPERSONIC TURBULENT SWBLI ON HIFIRE-1 AXISYMMETRIC CONE-CYLINDER-FLARE IN RAREFIED FLOW
RO Bura, Republic of Indonesia Defense University, Indonesia
7.3High-Performance and Laminar Flow Wing Design
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
14. Sep 26 16:30 16:55 7.3.1
0066		 TOWARDS AN OPTIMAL STRUT-BRACED-WING REGIONAL JET WITH NATURAL LAMINAR FLOW
N Saladeh, University of Toronto, Canada
14. Sep 26 16:55 17:20 7.3.2
0087		 AERODYNAMIC SHAPE OPTIMIZATION OF NATURAL LAMINAR FLOW SWEPT WINGS FOR REGIONAL AND SINGLE-AISLE AIRCRAFT
F. Husain, University of Toronto Institute for Aerospace Studies, Canada
14. Sep 26 17:20 17:45 7.3.3
0934		 MULTIPOINT INVERSE DESIGN FOR TRANSONIC, SLOTTED, NATURAL-LAMINAR-FLOW WINGS
J. G. Coder, Penn State University, United States
14. Sep 26 17:45 18:10 7.3.4
0944		 LAMINAR-TURBULENT-SUPERCRITICAL-WING CONCEPT AND ITS AERODYNAMIC PROPERTIES IN TRANSONIC FLIGHT
W. Stalewski, ?ukasiewicz Research Network – Institute of Aviation, Poland
Reserve Paper 7.3.R
0162		 VORTEX TOPOLOGY AND DRAG REDUCTION ANALYSIS IN SPIROID WINGTIP DEVICES USING PARTICLE TRACKING VELOCIMETRY
Amon Mwasandube, RMIT University, Australia
8.3Advanced Aerostructures
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 16:30 16:55 8.3.1
0940		 A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED FABRICATION AND REPAIR OF ALUMINUM PARTS
Y Lua, Global Engineering and Materials, Inc., United States
14. Sep 26 16:55 17:20 8.3.2
0308		 MOLECULAR DYNAMICS SIMULATION OF MULTI-COMPONENT SUSTAINABLE EPOXY SYSTEMS FOR STRUCTURAL AEROSPACE APPLICATIONS
IG Garay, Australia
14. Sep 26 17:20 17:45 8.3.3
0172		 FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING
X Liu, China
14. Sep 26 17:45 18:10 8.3.4
0493		 MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK
Z.-K. Li, Beihang University, China
Reserve Paper 8.3.R
0239		 LOAD-BEARING CAPACITY AND DAMAGE MODE OF THERMOELECTRIC DEVICES WITH TEMPERATURE-DEPENDENT ASYMMETRIC ELASTOPLASTICITY
Y Lu, Northwestern Polytechnical University, China
Reserve Paper 8.3.R
0470		 A NANOINDENTATION-BASED APPROACH FOR CALIBRATING CRYSTAL PLASTICITY PARAMETERS OF TI-6AL-4V
N/A Yu, Beihang University, China
9.3Health Monitoring
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
14. Sep 26 16:30 16:55 9.3.1
0032		 KEY PARAMETER IDENTIFICATION IN AIRCRAFT STRAIN PREDICTION MODELS
K. E. Niessen, Defence Science and Technology Group, Australia
14. Sep 26 16:55 17:20 9.3.2
0706		 AIRFRAME HEALTH MONITORING ON THE BAE SYSTEMS HAWK T1A JET TRAINER AIRCRAFT
G Dessena, Universidad Carlos III de Madrid, Spain
14. Sep 26 17:20 17:45 9.3.3
0072		 MTCL FOR COMPOSITE DAMAGE
SM Miao , Northwestern Polytechnical University, China
14. Sep 26 17:45 18:10 9.3.4
0379		 IMPACT LOAD IDENTIFICATION METHOD FOR AIRCRAFT RUDDER PLANES BASED ON NARX NEURAL NETWORK
S.-Y. Liang, China
10.3Hybrid Electric Fuel Cell Concepts
Chair(s): ,
Track 10
05 - Propulsion and Energy
14. Sep 26 16:30 16:55 10.3.1
0139		 IMPACT ASSESSMENT OF COMPONENT FAILURES IN A PEM-FUEL CELL BASED PROPULISON SYSTEM FOR AIRCRAFT APPLICATIONS
S. Bäumler, MTU Aero Engines AG, Germany
14. Sep 26 16:55 17:20 10.3.2
0652		 NUMERICAL AND EXPERIMENTAL EVALUATION OF COMPACT TPMS AND OFFSET-STRIP-FIN HEAT EXCHANGERS FOR FUEL CELL SYSTEM COOLING IN AN ELECTRIC AIRCRAFT
C.K. Sain, German Aerospace Center (DLR), Germany
14. Sep 26 17:20 17:45 10.3.3
0826		 DESIGN AND OPTIMIZATION OF AXIALLY GRADED OFFSET STRIP-FIN HEAT EXCHANGERS FOR MEGAWATT-CLASS FUEL CELL ELECTRIC AIRCRAFT
Shivaji Bhapkar, German Aerospace Center (DLR), Germany
14. Sep 26 17:45 18:10 10.3.4
0890		 FUEL CELL ASSISTED DISTRIBUTED BOUNDARY LAYER INGESTION FANS FOR CRUISE EFFICIENCY IMPROVEMENT IN SINGLE AISLE TRANSPORT AIRCRAFT
P.W.T. Somaweera, RMIT University , Australia
Reserve Paper 10.3.R
0423		 INITIAL PERFORMANCE INVESTIGATION AND AIRCRAFT-INTEGRATED ASSESSMENT OF A CYCLE-INTEGRATED SOLID OXIDE FUEL CELL – GAS TURBINE HYBRID
F. Winter, Bauhaus Luftfahrt e.V., Germany
11.3Flight control 3
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 16:30 16:55 11.3.1
0891		 DATA-DRIVEN SYNTHESIS OF AIRCRAFT FEEDBACK CONTROL LAWS FOR NEW COMMERCIAL FLIGHT SCENARIOS
M.W. Szymanski, Hamburg University of Technology, Germany
14. Sep 26 16:55 17:20 11.3.2
0892		 COMPARISON OF NONLINEAR DYNAMIC INVERSION TECHNIQUES FOR FIGHTER JET LONGITUDINAL CONTROL AT TRANSONIC SPEEDS
J.M. Drummond, Brazil
14. Sep 26 17:20 17:45 11.3.3
0791		 AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL
M.T Ueda, ITA, Brazil
14. Sep 26 17:45 18:10 11.3.4
0152		 KNOW YOUR LIMITS: ESTIMATING THE TILT-WING TRANSITION CORRIDOR UNDER FAILURE CONDITIONS
M. S. May, DLR e.V., Germany
Reserve Paper 11.3.R
0506		 ROBUST ATTITUDE RECOVERY CONTROL FOR AIR-LAUNCHED FOLDING-WING UAVS VIA DISTURBANCE-COMPENSATED SUPER-TWISTING SLIDING MODE
S. Han, China
12.3Actuation fault and Optimization
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
14. Sep 26 16:30 16:55 12.3.1
0623		 MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II ALGORITHM
Z Zhu, Northwestern Polytechnical University, China
14. Sep 26 16:55 17:20 12.3.2
0683		 OSCILLATORY FAILURE DETECTION IN AIRCRAFT ACTUATION SYSTEMS USING WAVELET TRANSFORM
IO Skusa, Brazil
14. Sep 26 17:20 17:45 12.3.3
0784		 PERFORMANCE DEGRADATION ANALYSIS OF RESOLVER FAULTS IN ELECTRO-MECHANICAL ACTUATOR
S. Guan, Beihang University, China
14. Sep 26 17:45 18:10 12.3.4
0961		 MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATOR SYSTEMS
Y.T.-Q. Yang, School of Mechanical Engineering and Automation, Beihang Univers, China
Reserve Paper 12.3.R
0904		 PRACTICAL ASPECT OF FLIGHT TESTING DRONE NAVIGATION SYSTEMS UNDER GPS-DENIED CONDITIONS
Y.I. Jenie, Faculty of Mechanical and Aerospace Engineering, Institut Teknol, Indonesia
additional information (interactive) 12.3.R
0621		 INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE LASER WEAPON
S. Bai, China
13.3Pathways for Sustainable Aviation
Chair(s): Andreeva-Mori, A.
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
14. Sep 26 16:30 16:55 13.3.1
1003		 FLIGHT PLANNING, THE FORGOTTEN ASSET
A. Dickinson, Australia
14. Sep 26 16:55 17:20 13.3.2
0666		 GLOBAL AVIATION MONITORING IN 2023
M. Clococeanu¹, C.-M. Weder¹, H. Bruder¹, Z.-L. Zengerling¹; ¹German Aerospace Center, Germany
14. Sep 26 17:20 17:45 13.3.3
0212		 JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION
T Ehlers, German Aerospace Center, Germany
14. Sep 26 17:45 18:10 13.3.4
0870		 EXPOSURE-AWARE COMPOUND CLIMATE HAZARDS FOR AIRPORTS: A TIERED EXTREMES FRAMEWORK LINKED TO FLIGHT TRAFFIC
K.- S. Sumaja, University of New South Wales, Australia
14.3Launch and Recovery
Chair(s): , , Palmer, J.
Track 14
06.2 - Flight Dynamics and Control (UAV related)
14. Sep 26 16:30 16:55 14.3.1
0867		 AUTONOMOUS LANDING OF UAVS ON SHIPS USING DECOUPLED REINFORCEMENT LEARNING
T. K. Gerner, RMIT University, Australia
14. Sep 26 16:55 17:20 14.3.2
0937		 A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH
A. G. P. Sarmento, Aeronautics Institute of Technology (ITA), Brazil
14. Sep 26 17:20 17:45 14.3.3
0248		 AUTONOMOUS PATHPLANNING ALGORITHM FOR EMERGENCY LANDING OF AAM CONSIDERING WIND DISTURBANCES
H. Iwamoto, Yokohama National Univercity, Japan
14. Sep 26 17:45 18:10 14.3.4
0208		 ASSESSMENT OF THE LANDING CAPABILITIES OF A FLEXIBLE HIGH-ALTITUDE PLATFORM AT LONGITUDINAL AND LATERAL-DIRECTIONAL WIND
Y. J. Hasan, DLR - German Aerospace Center, Germany
Reserve Paper 14.3.R
0698		 A SIMULATION BENCHMARK FOR AUTONOMOUS TAXIING CONTROL BASED ON VALIDATED UAV NONLINEAR GROUND DYNAMICS
A Zajdel, ?ukasiewicz Research Network - Institute of Aviation, Poland
15.3Human Factors, Workload, and Cognition
Chair(s): ,
Track 15
10 - Safety and Security
14. Sep 26 16:30 16:55 15.3.1
0056		 QUANTIFYING THE EFFECT OF IN-CABIN AIRCRAFT NOISE ON COGNITION.
B. R. C. Molesworth , University of New South Wales Sydney, Australia
14. Sep 26 16:55 17:20 15.3.2
0091		 PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE
W. Xiao, Shanghai Jiao Tong University, China
14. Sep 26 17:20 17:45 15.3.3
0118		 UNCERTAINTY ANALYSIS AND EYE-TRACKING VARIABILITY-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION
A. Lemetti, Linköping University, Sweden
14. Sep 26 17:45 18:10 15.3.4
0422		 HRV BASED PILOTS WORKLOAD PREDICTION FOR AN INTELLIGENT COCKPIT WARNING SYSTEM
A. E. Esposito, Kore University of Enna, Italy

Tuesday, 15. Sep 2026

0.5ICAS IFAR LECTURE Quiet aviation research for sustainable tomorrow
Chair:
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): ,
Track 1
12 - Host Nation (by personal invitation only)
15. Sep 26 08:55 09:20 1.4.1
0912		 IFAR 2025 PERSPECTIVES ON NOISE REDUCTION FOR EMERGING AND CONVENTIONAL AIR TRANSPORT
K. Benameur, ONERA, France
15. Sep 26 09:20 09:45 1.4.2
0345		 CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION
B.I. Schuchard, German Aerospace Center (DLR, Germany
15. Sep 26 09:45 10:10 1.4.3
0753		 SONIC BOOM PREDICTION TECHNOLOG FOR SUPERSONIC CIVIL TRANSPORTS
W Wang, AVIC Aerodynamics Research Institute, China
15. Sep 26 10:10 10:35 1.4.4
0964		 RECENT ADVANCES IN AEROACOUSTIC DESIGN OF ADVANCED AIR MOBILITY VEHICLES
AS Sieradzki, ?ukasiewicz - Institute of Aviation, Poland
2.4Aircraft Electrification, Innovation & Certification Perspectives & Challenges
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.4Propulsion 1
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 08:55 09:20 3.4.1
0287		 IMPACT OF SERIAL-PARALLEL POWERTRAIN SIZING STRATEGIES ON HYBRID-ELECTRIC AIRCRAFT PERFORMANCE
G. Palaia, Polytechnic of Turin, Italy
15. Sep 26 09:20 09:45 3.4.2
0915		 IMPLEMNTATION OF PROPELLER-WING INTERFERENCE MODEL AND HORIZONTAL TAIL ANALYSIS INTO A VISCOUS FULL POTENTIAL FLOW SOLVER FRAMEWORK FOR AIRCRAFT DESIG
D.D.P. Di Pasquale, Cranfield University, United Kingdom
15. Sep 26 09:45 10:10 3.4.3
0837		 IMPACT OF DIFFERENT PROPELLER CONFIGURATIONS ON THE FLIGHT DYNAMICS AND STABILITY OF A SMALL REGIONAL ELECTRIC AIRCRAFT
A. H Hammad, Germany
15. Sep 26 10:10 10:35 3.4.4
0251		 PROPULSIVE EFFICIENCY AND ENERGY ANALYSIS OF AIRCRAFT CONCEPTS WITH AFT-FUSELAGE BOUNDARY-LAYER-INGESTION
Z.-C. Zhou, China
Reserve Paper 3.4.R
0484		 RESONANT ELASTIC SHAFT THRUST VECTORING: IMPLICATIONS FOR UAV DESIGNS
HF.G. Guan, Australia
4.4Hydrogen in design
Chair(s): Verstraete, D.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 08:55 09:20 4.4.1
0073		 DESIGN AND INVESTIGATION OF A SHORT-TO-MEDIUM-RANGE AIRCRAFT WITH LIQUID HYDROGEN AND SAF MULTI-FUEL PROPULSION
B. Tuerkyilmaz, Bauhaus Luftfahrt e. V., Germany
15. Sep 26 09:20 09:45 4.4.2
0213		 CHALLENGES AND SOLUTIONS FOR LIQUID HYDROGEN-POWERED UAVS: REGULATIONS AND CASE STUDY INSIGHTS
B. Legrand, ISAE-SUPAERO, France
15. Sep 26 09:45 10:10 4.4.3
0333		 ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035
M. Kotzem, German Aerospace Center (DLR), Germany
15. Sep 26 10:10 10:35 4.4.4
0316		 AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN
A. Tramposch, University of Applied Sciences FH JOANNEUM GesmbH, Austria
5.4Supersonic and Hypersonic Flows
Chair(s): , , Kiszkowiak, L.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 08:55 09:20 5.4.1
0241		 A PARAMETER-FREE ADAPTIVE LIMITER FOR HIGH-RESOLUTION SIMULATION OF COMPLEX SHOCK-DOMINATED FLOW
G. Wang, Northwestern Polytechnical University, China
15. Sep 26 09:20 09:45 5.4.2
0065		 A STUDY ON THE CELL REYNOLDS NUMBER AS A PARAMETER FOR MESH QUALITY ON HYPERSONIC FLOWS
G. M. Poltronieri, Instituto Tecnologico de Aeronautica, Brazil
15. Sep 26 09:45 10:10 5.4.3
0903		 PLUME CHARACTERIZATION OF SOLID ROCKET MOTORS: COMPARISON OF EULERIAN AND DISCRETE PHASE MODELING APPROACHES
A.O. Unsal, Roketsan Missiles Inc., Turkey
15. Sep 26 10:10 10:35 5.4.4
0043		 INVESTIGATION OF PLUME NON-EQUILIBRIUM INFRARED RADIATION CHARACTERISTICS AT DIFFERENT MACH NUMBERS
XU Jianyu, China; ZHOU Li, China; SHI Jie, China; WANG Zhanxue, China; SHI Hao, China
additional information (interactive) 5.4.R
0550		 NUMERICAL INVESTIGATION OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH 2.5 OVER A COMPRESSION RAMP
Z.A. Rana, Prince Mohammad bin Fahd University, Saudi Arabia
6.4Rotor aerodynamics and acoustics
Chair(s): Azarpeyvand, M., Gowree, E.
Track 6
03.2 - Experimental Aerodynamics
15. Sep 26 08:55 09:20 6.4.1
0069		 FLUCTUATING SURFACE PRESSURE MEASUREMENTS OF JET IMPINGEMENT ON A SMALL ROTOR
B. M. Malkki, The University of New South Wales, Australia
15. Sep 26 09:20 09:45 6.4.2
0743		 STUDY OF THE FEASIBILITY OF ACOUSTIC LINERS INSIDE THE BEAM THAT INTERACTS WITH A UAV DRONE ROTOR
F. Simon, ONERA, France
15. Sep 26 09:45 10:10 6.4.3
0033		 EXPERIMENTAL INVESTIGATION ON THE INNER DUCT SURFACE UNSTEADY PRESSURE OF A DUCTED PROPELLER
J. Li, UNSW, Australia
15. Sep 26 10:10 10:35 6.4.4
0828		 MISSION-WIDE SEMI-EMPIRICAL AEROACOUSTIC NOISE MODELING OF A CARGO EVTOL UAV WITH CONSIDERATION OF A SIMPLE URBAN FLYOVER
I. Peleshok, Technical University of Munich, Germany
7.4Boundary Layer Control and Stall Mitigation
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 26 08:55 09:20 7.4.1
0047		 VORTEX FLOW CONTROL USING JUNCTURE FILLETS ON A BLUNT-NOSED, HIGHLY SWEPT COMPOUND WING
N.L.M. van Luijk, Delft University of Technology, Netherlands
15. Sep 26 09:20 09:45 7.4.2
0221		 INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFOMANCE AT LOW REYNOLDS NUMBER
M. Avirovic, Royal Military Academy, Belgium
15. Sep 26 09:45 10:10 7.4.3
0378		 EXERGY AND INTEGRAL BOUNDARY LAYER PARAMETERS CHARACTERISTIC CURVES FOR AERODYNAMIC DESIGN
G. Bourreau-Tirel, AURA AERO/ISAE-SUPAERO, France
15. Sep 26 10:10 10:35 7.4.4
0723		 PARAMETRIC AERODYNAMIC STUDY OF THE PROPERTIES OF LEADING-EDGE SERRATIONS ON WING SECTIONS ACROSS STALL REGIMES
J.J Whittaker, Australia
additional information (interactive) 7.4.R
0752		 EFFECTS OF LEADING-EDGE HIGH-LIFT DEVICES ON THE LOW-SPEED VORTEX FIELD AND AERODYNAMIC FORCES FOR A SUPERSONIC CIVIL TRANSPORT
X. -R. Zheng Zheng, Chinese Aeronautical Establishment, China
8.4Fuselage Structures
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 08:30 08:55 8.4.1
0115		 COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT
Y. C. Roth, Airbus, Germany
15. Sep 26 08:55 09:20 8.4.2
0117		 COMPOSITE PLATE OPTIMIZATION UNDER COMBINED COMPRESSION AND SHEAR BUCKLING LOAD
R.P Pereira da Silva, Boeing, Brazil
15. Sep 26 09:20 09:45 8.4.3
0830		 FIVE DECADES OF T-38 WING TEARDOWNS
TJ Moran, Southwest Research Institute, United States
15. Sep 26 10:10 10:35 8.4.4
0071		 GEOMETRICALLY EXACT MODEL OF CANTILEVER BEAM UNDERGOING LARGE DEFLECTION AND LINEARIZED DYNAMICS CHARACTERIZATION
C. Yang, Northwestern Polytechnical University, China
9.4Impact & Vibration 1
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 08:30 08:55 9.4.1
0290		 ENERGY ABSORPTION OF THIN-WALLED CONCENTRIC SPHERES FOR CARGO AIRDROP
A.E. Lloyd, The University of Sydney, Australia
15. Sep 26 08:55 09:20 9.4.2
0153		 GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL
A. Das, RMIT University, Australia
15. Sep 26 09:20 09:45 9.4.3
0364		 NUMERICAL PREDICTION OF CABIN NOISE FOR FUTURE SHORT-HAUL AIRCRAFT IN EARLY AIRCRAFT DESIGN
C. Hesse, DLR e.V., Germany
15. Sep 26 10:10 10:35 9.4.4
0846		 DATA-DRIVEN MULTI-MODAL PREDICTION OF IMPACT RESPONSE IN COMPOSITE LAMINATES: FORCE–TIME HISTORIES AND INTERLAMINAR DELAMINATION
G.J.-Zh Zhang, China
10.4Advanced vehicle concepts
Chair(s): ,
Track 10
05 - Propulsion and Energy
15. Sep 26 08:55 09:20 10.4.1
0487		 ASSESSMENT OF ENGINE-OUT ATMOSPHERIC EMISSIONS FROM COCONUT-OIL-DERIVED BIOJET FUEL
S. Ogawa, Osaka Metropolitan University, Japan
15. Sep 26 09:20 09:45 10.4.2
0739		 MAGNETOPLASMAIONIC (MPI) ENGINE
N. K. Chaudhary, Australia
15. Sep 26 09:45 10:10 10.4.3
0898		 EXPERIMENTAL EVALUATION OF THE PERFORMANCE & EMISSION FORMATION IN A MICRO-GAS TURBINE UTILISING SUSTAINABLE AVIATION FUEL (SAF)
M.R Muhammad, NATIONAL AEROSPACE INDUSTRY CORPORATION MALAYA (NAICO MALAYSIA), Malaysia
15. Sep 26 10:10 10:35 10.4.4
0963		 SYSTEM-LEVEL MODELLING OF TURBOFAN NOISE SUPPRESSION AND ACOUSTIC LINER ATTENUATION
X Zhao, Chalmers University of Technology, Sweden
Reserve Paper 10.4.R
0551		 EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY
P. Kirschnek, FH JOANNEUM GesmbH, Austria
11.4Guidance and flight trajectory control 1
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 08:55 09:20 11.4.1
0164		 TRAJECTORY OPTIMIZATION FOR TAKEOFF/LANDING BASED ON FLAP-AND-GLIDE FOR FLAPPING-WING UNMANNED AERIAL VEHICLE
W. Lee, Chungnam National University, South Korea
15. Sep 26 09:20 09:45 11.4.2
0821		 SENSITIVITY-BASED REFERENCE TRAJECTORY UPDATES FOR AIRCRAFT PATH-FOLLOWING MODEL PREDICTIVE CONTROL
S. Fuchsgruber, Technische Universität München, Germany
15. Sep 26 09:45 10:10 11.4.3
0563		 OPTIMAL ZEM-BASED MIDCOURSE GUIDANCE FOR INTERCEPTORS USING TRAJECTORY PREDICTION
S. Kim¹, K.-W. Jung¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea
15. Sep 26 10:10 10:35 11.4.4
0951		 TRAJECTORY OPTIMIZATION FOR ENERGY STATE RECOVERY DURING APPROACH: ENHANCING LOW ENERGY AWARENESS AND AUTOMATION
J.L Nunes de Jesus Luz, Institute of Aeronautical Technology, Brazil
additional information (interactive) 11.4.R
0532		 CONVEX OPTIMIZATION-BASED EMERGENCY LANDING TRAJECTORY GENERATION FOR UAM VEHICLES
Y. Jung, Korea Aerospace Research Institute, South Korea
12.4Concent design/MBSE
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
15. Sep 26 08:55 09:20 12.4.1
0265		 DYN-MARS: A NEW CONCEPT ENABLING THE BEST APPROACH FLIGHT PROFILE
P. Thöne, German Aerospace Center - DLR, Germany
15. Sep 26 09:20 09:45 12.4.2
0438		 WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH
Z. R. Milani, National Research Council of Canada, Canada
15. Sep 26 09:45 10:10 12.4.3
0650		 A CONCEPT FOR SMARTPHONE-BASED EMERGENCY FLIGHT DATA INDICATION SYSTEM IN LIGHT AIRCRAFT
P. Chudý, Julius-Maximilians-Universität Würzburg, Germany
15. Sep 26 10:10 10:35 12.4.4
0809		 AUTOMATING SYSTEM MODELING USING LARGE LANGUAGE MODELS
I. S. Rehder, Brazil
Reserve Paper 12.4.R
0170		 A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-1763 STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES
N.-V. Nguyen, Viettel Aerospace, Vietnam
additional information (interactive) 12.4.R
0322		 CAPABILITY ANALYSIS OF CHINA’S AERIAL EMERGENCY COMMUNICATION SYSTEM: AN EFFECTIVENESS EVALUATION METHOD FOR AERIAL EMERGENCY COMMUNICATION SYSTEMS
L Zhao, Aerial Industry Development Research Center of China, China
13.4Architecting , Production and Supply chain
Chair(s): , , Prakasha, P.
Track 13
02 - Systems Engineering and Integration
15. Sep 26 08:55 09:20 13.4.1
0336		 VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS
G. Donelli, German Aerospace Center DLR, Germany
15. Sep 26 09:20 09:45 13.4.2
0966		 ENABLING HIGH RATE COMPOSITE MANUFACTURING THROUGH A ROBUST MANUFACTURING DIGITAL ECOSYSTEM
M.A. Rabiega, The Boeing Company, United States
15. Sep 26 09:45 10:10 13.4.3
0667		 A SYSTEMS-LEVEL MACHINE LEARNING FRAMEWORK FOR PREDICTIVE TRACKING IN AIRCRAFT DESIGN AND PRODUCTION
S. Dutta, India
15. Sep 26 10:10 10:35 13.4.4
0337		 AIRCRAFT AND INDUSTRIAL SYSTEMS CO-ARCHITECTING BASED ON VALUE-DRIVEN MBPLE APPROACH
G. Donelli, German Aerospace Center DLR, Germany
14.4UAV Design
Chair(s): , , Bil, C.
Track 14
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 26 08:55 09:20 14.4.1
1012		 DISCRIMINATORY AUTONOMY: OPERATING FASTER, SMARTER, AND WITH PURPOSE
J. Garth, Australia
15. Sep 26 09:20 09:45 14.4.2
0237		 CFD/MBD-COUPLED FLIGHT SIMULATION OF FOLDING MORPHING UAV
L. Qiao, Northwestern Polytechnical University, China
15. Sep 26 09:45 10:10 14.4.3
0929		 SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION
B. Kunwar, Auburn University, United States
15. Sep 26 10:10 10:35 14.4.4
0845		 A WORKFLOW FOR RAPID DESIGN, SIMULATION, FABRICATION, AND SUBSCALE FLIGHT-TESTING OF NOVEL AIRCRAFT CONCEPTS
I Chakraborty, Auburn University, United States
Reserve Paper 14.4.R
0128		 CASCADE ADRC FOR TRAJECTORY TRACKING OF A FLYING-WING SOLAR AIRCRAFT UNDER WIND DISTURBANCES
S.Q. Song, Northwestern Polytechnical University, China
15.4Human Performance, Training, and Communication
Chair(s): ,
Track 15
10 - Safety and Security
15. Sep 26 08:55 09:20 15.4.1
0059		 FACTORS AFFECTING COMMUNICATION IN AVIATION
D Estival, UNSW, Australia
15. Sep 26 09:20 09:45 15.4.2
0074		 EVALUATION OF THE USE OF THE EYE TRACKER IN AERONAUTICAL PRODUCT DEVELOPMENT AS A HUMAN FACTORS METHOD
G. Cicelini, Brazil
15. Sep 26 09:45 10:10 15.4.3
0086		 INVESTIGATING PILOT COMMUNICATION BEHAVIOURS DURING TAXI OPERATIONS UNDER DEGRADED COMMUNICATION CONDITIONS
Y Yan, Australia
15. Sep 26 10:10 10:35 15.4.4
0685		 SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES
A.M. Comer, Oklahoma State University, United States

10:35 - 11:00COFFEE BREAK

1.5GSA2: Perspectives and Progress on Airliners for 2050+ Energy Landscapes
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
15. Sep 26 11:00 11:25 1.5.1
0992		 ECONOMIC, ENVIRONMENTALLY SUSTAINABLE AVIATION ENERGY
J.I. Hileman, Boeing, United States
15. Sep 26 11:25 11:50 1.5.2
0983		 NASA RESEARCH FOR AIRLINERS OF 2050 AND BEYOND
N.K. Madavan, NASA/ARMD, United States
2.5EASN Response to Emerging Challenges in Sustainable and Competitive Aviation
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
15. Sep 26 11:00 11:25 2.5.1
0975		 AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES
A. Filippatos, University of Patras, Greece
15. Sep 26 11:25 11:50 2.5.2
0976		 CHALLENGES AND BREAKTHROUGHS IN AIR TRANSPORT SYSTEM: VISION FROM EUROPE
G. Alonso-Rodrigo, Universidad Politecnica de Madrid, Spain
15. Sep 26 11:50 12:15 2.5.3
0981		 CURRENT AND ALTERNATIVE PROPULSION SYSTEMS IN EUROPE; TECHNOLOGIES AND THEIR INTEGRATION
O. Isaksson, Chalmers University of Technology, Sweden
15. Sep 26 12:15 12:40 2.5.4
0984		 OVERVIEW OF CRITICAL ISSUES AND OPPORTUNITIES FOR NEW A/C WITH HYBRID AND FULL-ELECTRIC POWERTRAIN
F. Nicolosi, University of Naples Federico II, Italy
3.5Propulsion 2
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 11:00 11:25 3.5.1
0687		 A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION
Q.-H.-T.-X. Hoang Thi Xuan, Viettel Aerospace Institute, Vietnam
15. Sep 26 11:25 11:50 3.5.2
0353		 TOWARDS AN ONTOLOGY-BASED APPROACH FOR DISCIPLINE-SPECIFIC ENGINEERING VIEWS IN ENGINE DESIGN
K. Becker, German Aerospace Center (DLR), Germany
15. Sep 26 11:50 12:15 3.5.3
0836		 MIXED-FIDELITY, NONLINEAR AIRCRAFT MISSION MODELING FOR HYBRID REGIONAL AIRCRAFT DESIGN VERIFICATION
Agostino: A. De Marco, University of Naples Federico II, Italy
15. Sep 26 12:15 12:40 3.5.4
0293		 EFFECT OF ENGINE RESPONSE TIME IN AIRCRAFT CONCEPTUAL DESIGN
A.P.S. Inderawan, Delft University of Technology, Netherlands
4.5Application of advanced propulsion concepts
Chair(s): Ying, A.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 11:00 11:25 4.5.1
0319		 INTEGRATION OF A SOLID OXIDE FUEL CELL PROPULSION SYSTEM: A TECHNOLOGY DEVELOPMENT GOAL FOR REGIONAL AIRCRAFT
N. Schneiders, German Aerospace Center (DLR), Germany
15. Sep 26 11:25 11:50 4.5.2
0360		 HYBRID-ELECTRIC AND HYDROGEN-FUEL-CELL PROPULSION AS ALTERNATIVES TO KEROSENE FOR REGIONAL AIRCRAFT
F. Nicolosi, UNIVERSITY OF NAPLES , Italy
15. Sep 26 11:50 12:15 4.5.3
0673		 EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION
M. Bouchard, Createk Innovation Group, Canada
15. Sep 26 12:15 12:40 4.5.4
0062		 AERODYNAMIC EFFECTS OF DISTRIBUTED PROPULSION WING CONFIGURATION PARAMETERS
K. W. Wang, Northwestern Polytechnical University, China
Reserve Paper 4.5.R
0401		 PROPULSION SYSTEM MODELING AND OPTIMIZATION FOR CONCEPTUAL DESIGN OF HYBRID-ELECTRIC VTOL AIRCRAFT
D. E. Lampl, Technical University of Munich, Germany
Reserve Paper 4.5.R
0688		 PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS
S. Trivedi, Indian Institute Technology Bombay, Mumbai, India, India
5.5CFD Applications
Chair(s): , , Imamura, T.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 11:00 11:25 5.5.1
0572		 NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE
N. Montella, CIRA (Centro Italiano Ricerche Aerospaziali), Italy
15. Sep 26 11:25 11:50 5.5.2
0283		 NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING
M.H. Mohsin, Cranfield University, United Kingdom
15. Sep 26 11:50 12:15 5.5.3
0119		 SIMULATION OF FIFTH-GENERATION HIGH-PERFORMANCE AIRCRAFT USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S Shahjahan, 1Siemens Digital Industries Software Inc., United States
15. Sep 26 12:15 12:40 5.5.4
0373		 EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT
H.C. Yang, Northwestern Polytechnical University, China
Reserve Paper 5.5.R
0258		 INFLUENCE OF ADDITIVE MANUFACTURING ON IMPROVING THE TRADITIONAL MICRO JET COMBUSTOR PERFORMANCE
M Muddada, Powertech, EDGE Group, United Arab Emirates
Reserve Paper 5.5.R
0931		 INVESTIGATING A STABLE LIFTING FUSELAGE FOR A TWO SEAT SAILPLANE OF THE GULL WING CONFIGURATION
B Huyssen, University of Pretoria, South Africa
additional information (interactive) 5.5.R
0263		 EFFECTS OF FLYING WING CONFIGURATION PARAMETERS ON AERODYNAMICS AND STABILITY
G.-Y. Gao, Northwestern Polytechnical University, China
additional information (interactive) 5.5.R
0849		 STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS?
X.-T XIE, Northwestern Polytechnical University, China
6.5Complex flow phenomena
Chair(s): Coder, J., Gowree, E.
Track 6
03.2 - Experimental Aerodynamics
15. Sep 26 11:00 11:25 6.5.1
0472		 EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL
J. G. Coder, Penn State University, United States
15. Sep 26 11:25 11:50 6.5.2
0965		 EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROLLED CAVITY FLOW FOR PIEZOELECTRIC ENERGY HARVESTING APPLICATIONS
M Kirkness, The University of Sydney, Australia
15. Sep 26 11:50 12:15 6.5.3
0362		 REYNOLDS NUMBER SCALING EFFECTS IN TRANSONIC CAVITY AERODYNAMIS: A HIGH-FIDELITY EXPERIMENTAL AND NUMERICAL FRAMEWORK
A. Goerttler, German Aerospace Center, Germany
15. Sep 26 12:15 12:40 6.5.4
0748		 INTERMITTENT LOW FREQUENCY EXPERIMENTAL CAVITY DYNAMICS
J. McCarthy, Defence Science and Technology Group, Australia
additional information (interactive) 6.5.R
0545		 EFFECTS OF SLOT LOCATION ON FLOW AND HEAT TRANSFER IN A LATTICEWORK COOLING CHANNEL: AN MRV EXPERIMENT AND NUMERICAL STUDY
Y. Jia, Xian Jiaotong University, China
7.5Transonic and Supersonic Aerodynamics for Advanced Configurations
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 26 11:00 11:25 7.5.1
0223		 AERODYNAMIC TRANSONIC DESIGN AND ADJOINT-BASED OPTIMIZATION OF A STRUT-BRACED WING IN AN MDO STRATEGY
DLC Losada Costoso, ONERA, France
15. Sep 26 11:25 11:50 7.5.2
0235		 SPARSE POLYNOMIAL CHAOS-BASED ROBUST OPTIMIZATION DESIGN OF AERODYNAMIC AND SONIC BOOM
S. Wang, Northwestern Polytechnical University, China
15. Sep 26 11:50 12:15 7.5.3
0598		 SUPERSONIC GROUND EFFECT AERODYNAMICS OF A SLENDER BODY
Y. Xun, Beihang University, China
15. Sep 26 12:15 12:40 7.5.4
0632		 FLOW SOLUTIONS AROUND VON KARMAN NOSES AT SUPERSONIC SPEEDS USING PHYSICS INFORMED NEURAL NETWORKS AND PRESSURE-SENSITIVE PAINT
MAE Escudero, Cranfield University, United Kingdom
8.5Fatigue & Progressive Damage
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 11:00 11:25 8.5.1
0365		 FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS
H. Park, Korea Institute of Materials Science, South Korea
15. Sep 26 11:25 11:50 8.5.2
0253		 LABORATORY METHOD FOR REPLICATING FASTENER HOLE CORROSION IN AA 7085
NB Tugwell, Defence Science and Technology Group, Australia
15. Sep 26 11:50 12:15 8.5.3
0234		 NEW INSIGHTS INTO AA7085 ENVIRONMENTALLY ASSISTED CRACKING THROUGH HIGH RESOLUTION FRACTOGRAPHY
I.C.W. Field, DSTG, Australia
15. Sep 26 12:15 12:40 8.5.4
0243		 INCREMENTAL LEARNING-DRIVEN XGBOOST MODEL FOR FATIGUE LIFE PREDICTION OF AA7050-T7451 ALUMINUM ALLOY UNDER LIMITED EXPER
X.-C. Chen, China
9.5Impact & Vibration 2
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 11:00 11:25 9.5.1
0309		 INTERNAL I-DVA FOR 6U CUBESAT LAUNCH RANDOM VIBRATION MITIGATION
K.-A. Kassa, King Fahd University of Petroleum and Minerals, Saudi Arabia
15. Sep 26 11:25 11:50 9.5.2
0724		 VALIDATION OF A LOW-COST DATA COLLECTION SYSTEM FOR AIRCRAFT VIBRATION TESTING
G Dessena, Universidad Carlos III de Madrid, Spain
15. Sep 26 11:50 12:15 9.5.3
0885		 IMPACT RESISTANCE ENHANCEMENT IN FIBER-REINFORCED COMPOSITES USING CARBON/BASALT HYBRIDIZATION APPROACHES
A.H. Baluch¹, Z. Sajid¹, T. Rehman¹; ¹King Fahd University of Petroleum & Minerals, Saudi Arabia
Presenter: Abrar Ul Haq Khan Baluch, King Fahd University of Petroleum & Minerals
10.5Hybrid Electric UAVs
Chair(s): ,
Track 10
05 - Propulsion and Energy
15. Sep 26 11:00 11:25 10.5.1
0613		 A MPC STRATEGY FOR THE ENERGY MANAGEMENT OF HYBRID ELECTRIC PROPULSION SYSTEMS IN FIXED-WING UAVS
A. Suti, INSA Toulouse, France
15. Sep 26 11:25 11:50 10.5.2
0619		 POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS
A. Suti, INSA Toulouse, France
15. Sep 26 11:50 12:15 10.5.3
0882		 TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS
B.P. van Magill, The University of Sydney, Australia
15. Sep 26 12:15 12:40 10.5.4
0597		 IN-FLIGHT LOW-COST THRUST MEASUREMENT SYSTEM FOR SMALL UNMANNED AERIAL VEHICLES
C. Rieger, Technical University of Munich - Chair of Aircraft Design, Germany
Reserve Paper 10.5.R
0678		 HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION
H A Abid, Queen Mary, University of London, United Kingdom
11.5System modeling
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 11:00 11:25 11.5.1
0060		 PREFERENCE INCORPORATION INTO GENERALIZED MULTI-OBJECTIVE ISLAND MODEL FOR FLIGHT CONTROL SYSTEM CLEARANCES
P. Piprek, Airbus Defence and Space GmbH, Germany
15. Sep 26 11:25 11:50 11.5.2
0240		 ANALYSIS OF HOVER CONTROL CAPABILITY DEGRADATION OF EVTOL AIRCRAFT UNDER PITCH ACTUATOR JAMMING
C. Wu, Northwestern Polytechnical University, China
15. Sep 26 11:50 12:15 11.5.3
0246		 FLIGHT DYNAMICS AND GUIDANCE CONTROL FOR AERCRAFT IN TYPHOON ENVIRONMENT FOR DELIVERLY OF TYPHOON CONTROL SUBSTANCE
T. Sakurai, Yokohama National University, Japan
15. Sep 26 12:15 12:40 11.5.4
0581		 SYNCHRONIZATION CONTROL OF AEROSPACE ELECTROMECHANICAL ACTUATORS BASED ON MECHANISM-DATA FUSION MODELING
Y.T.-Q. Yang, School of Mechanical Engineering and Automation, Beihang Univers, China
12.5Electric aircraft
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
15. Sep 26 11:00 11:25 12.5.1
0093		 DEMONSTRATION AND VALIDATION CAPABILITIES FOR NEXT-GENERATION FLIGHT CONTROL SYSTEMS
O. Bertram, DLR e.V., Germany
15. Sep 26 11:25 11:50 12.5.2
0303		 EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN
A. Testera, Leonardo S.p.A, Italy
15. Sep 26 11:50 12:15 12.5.3
0557		 HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL MULTILEVEL BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT
P Panchal, University of the Bundeswehr Munich, Germany
15. Sep 26 12:15 12:40 12.5.4
0715		 AN EMBEDDED PHYSICS-INFORMED NEURAL NETWORK (PINN) FRAMEWORK FOR HIGH-FIDELITY REAL-TIME SIMULATION OF A FLIGHT CONTROL SURFACE ACTUATION SYSTEM
D.C. Lyu, China
Reserve Paper 12.5.R
0831		 NEUROMORPHIC ASCENT: REVOLUTIONISING AIRCRAFT STORES COMPATIBILITY AND AUTONOMOUS SYSTEMS
M.G. Tutty, JAIME AMERICA, LLC, United States
additional information (interactive) 12.5.R
0561		 POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH
L.-J. Jiang, Beihang University, China
13.5Aviation & Energy
Chair(s): , , Jouannet, C.
Track 13
02 - Systems Engineering and Integration
15. Sep 26 11:00 11:25 13.5.1
0016		 MODEL PREDICTIVE CONTROL AND ENERGY MANAGEMENT OF AIRPORT MICROGRIDS INTEGRATING ELECTRIC AND HYDROGEN AIRCRAFT
Y. Chen, University of New South Wales, Australia
15. Sep 26 11:25 11:50 13.5.2
0722		 SYSTEM OF SYSTEMS ENGINEERING ROADMAP FOR INTEGRATING SUSTAINABLE AVIATION FUEL INTO MEXICO\'S AIRPORT FUEL INFRASTRUCTURE
G.-L. Gomez Falcon, UNIVERSIDAD AUTÓNOMA DE BAJA CALIFORNIA, Mexico
15. Sep 26 11:50 12:15 13.5.3
0957		 SOFTWARE ARCHITECTURE FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT
W. Bliemetsrieder, UniBw Munich, Germany
15. Sep 26 12:15 12:40 13.5.4
0023		 IMPACT OF GNSS INTERFERENCE ON AIRCRAFT NAVIGATION SYSTEMS: OPERATIONAL RISKS, SAFETY IMPLICATIONS, AND EARLY ASSESSMENT
PP Pinheiro, Universidade Beira do interior, Portugal
14.5Propulsion & Control
Chair(s): , , Bil, C.
Track 14
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 26 11:00 11:25 14.5.1
0689		 MODELING PROPELLER-WING INTERACTIONS FOR SUBSCALE LIFT + CRUISE VTOL UAV
- Bhandari, Oklahoma State University, United States
15. Sep 26 11:25 11:50 14.5.2
0874		 RAPID FLIGHT DYNAMICS EVALUATION OF STRONGLY COUPLED DISTRIBUTED PROPULSION
Y. Zhu, Northwestern Polytechnical University, China
15. Sep 26 11:50 12:15 14.5.3
0529		 ENSEMBLE MACHINE LEARNING FOR UAV PROPELLER PERFORMANCE PREDICTION WITH UNCERTAINTY QUANTIFICATION
M. I. Alam, King Fahd University of Petroleum and Minerals (KFUPM), Saudi Arabia
15. Sep 26 12:15 12:40 14.5.4
0219		 STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION
T. Goetzendorf-Grabowski, Warsaw University of Technology Institute of Aeronautics and App, Poland
Reserve Paper 14.5.R
0404		 FLIGHT TESTING CONTROL LAWS OF A TANDEM TILT-WING EVTOL DEMONSTRATOR THROUGH TETHERED HOVER FLIGHTS
D. Milz, German Aerospace Center (DLR), Germany
additional information (interactive) 14.5.R
0180		 COMPARISON OF TWO METHODS FOR OBTAINING LONGITUDINAL AERODYNAMIC DERIVATIVES AND THEIR DYNAMIC STABILITY ANALYSIS OF HIR
G Gao, Northwestern Polytechnical University, China
15.5Operational Safety Monitoring and Data Analytics
Chair(s): ,
Track 15
10 - Safety and Security
15. Sep 26 11:00 11:25 15.5.1
0038		 ACCELERATING THE LEARNING CURVE: GENERATIVE AI FOR WORKED EXAMPLES IN HUMAN FACTORS ANALYSIS
A. Reisier¹, M.M. Cardoso-Junior¹; ¹Technological Institute of Aeronautics, Brazil
Presenter: Moacyr Cardoso-Junior, Technological Institute of Aeronautics
15. Sep 26 11:25 11:50 15.5.2
0192		 ASSESSING AN ALTERNATE AIRPORT ASSISTANT
J. I. Gonzalez Cabeza, DLR e.V., Germany
15. Sep 26 11:50 12:15 15.5.3
0291		 EVALUATION OF METHODS FOR ANOMALY DETECTION IN THE APPROACH PHASE OF OPERATIONAL FLIGHT DATA
R. Haehnel, German Aerospace Centre (DLR), Germany
15. Sep 26 12:15 12:40 15.5.4
0875		 PRELIMINARY SAFETY AND CERTIFICATION RISK ASSESSMENT FOR AN INNOVATIVE REGIONAL HYBRID AIRCRAFT CONFIGURATION
G. B Buzzo, CIRA - Italian Aerospace Research Centre, Italy
Reserve Paper 15.5.R
0969		 EVALUATION OF A MULTI-SENSOR OBSTACLE TRACKING SYSTEM FOR AIRCRAFT USING REAL-WORLD DATA
K.D. Theuma, MCAST, Malta
additional information (interactive) 15.5.R
0409		 CONTEXT-AWARE FLIGHT SAFETY EVENT DETECTION AND CLASSIFICATION USING A TWO-STAGE HYBRID MACHINE LEARNING MODEL
T. Asghar, National University of Sciences and Technology (NUST), Pakistan

12:40 - 13:40LUNCH BREAK

1.6GSA2: Regional Airliners: Electrified/H2 Prospects and Demonstrations
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
15. Sep 26 13:40 14:05 1.6.1
0993		 REGIONAL ELECTRIFIED/HYDROGEN DEMONSTRATIONS PANEL
G.M. Bezos-O'Connor, NASA, United States
2.6X-59 Detail Session
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
15. Sep 26 13:40 14:05 2.6.1
0758		 X-59: THE FIRST CHAPTER IN THE QUESST FOR QUIET COMMERICAL SUPERSONIC FLIGHT
C.M Bahm, NASA, United States
15. Sep 26 14:05 14:30 2.6.2
1007		 X-59: PART 2 BY C.M.BAHM AND P.G.COEN
C. Bahm, United States
15. Sep 26 14:30 14:55 2.6.3
0769		 X-59 EXTERNAL VISION SYSTEM FLIGHT TESTING
R.E. Bailey, NASA, United States
15. Sep 26 14:55 15:20 2.6.4
0839		 X-59 FLIGHT DYNAMICS AND CONTROL
M.J. Boucher, NASA, United States
3.6MDO 1
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 13:40 14:05 3.6.1
0524		 A SINGLE-LOOP OPTIMIZATION METHOD FOR MULTIDISCIPLINARY DESIGN UNDER UNCERTAINTY
B Wang, The University of Sydney, Australia
15. Sep 26 14:05 14:30 3.6.2
0088		 MULTIDISCIPLINARY PHYSICS-CONSTRAINED GENERATIVE DESIGN OF DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
W. Wei, Northwestern Polytechnical University, China
15. Sep 26 14:30 14:55 3.6.3
0215		 A MULTI-FIDELITY ROBUST OPTIMIZATION APPROACH FOR HYPERSONIC WAVERIDERS DESIGN
A. Perlini, Politecnico di Milano, Italy
15. Sep 26 14:55 15:20 3.6.4
0469		 A MIXED-FIDELITY VISCOUS-INVISCID INTERACTION APPROACH FOR THE DESIGN OPTIMIZATION OF NOVEL AIRCRAFT CONCEPTS
S.A. Bakhshi, University of Michigan, United States
Reserve Paper 3.6.R
0305		 METHODOLOGICAL APPROACH TO MULTI-CRITERIA OPTIMISATION OF PRODUCT FAMILY ARCHITECTURES UTILISING SYSTEM MODELS
F. H. Christiansen, Hamburg University of Technology, Germany
4.6UAVs and advanced air mobility
Chair(s): Kanazaki, M.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 13:40 14:05 4.6.1
0636		 ENDURANCE EVALUATION OF DIFFERENT UAV CONFIGURATIONS AND POWERTRAIN ARCHITECTURES
A. Orgiu, Concordia University, Canada
15. Sep 26 14:05 14:30 4.6.2
0880		 DEVELOPMENT OF A 130-KG-CLASS LIFT-CRUISE VTOL UAV INCORPORATING A FUEL CELL–BATTERY HYBRID POWER SYSTEM
J. Jeong, Korea Aerospace Research Institute, South Korea
15. Sep 26 14:30 14:55 4.6.3
0801		 COMMON RESEARCH MODELS FOR SMALL UNCREWED AERIAL VEHICLES
J.-A. Rasines Mazo, The University of Sydney, Australia
15. Sep 26 14:55 15:20 4.6.4
0594		 DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE
P.-P. Kapoor, University of Hull, United Kingdom
Reserve Paper 4.6.R
0331		 FLIGHT OPERATIONS AND TESTING OF A 450?KG EXPERIMENTAL GYROPLANE UAV
I. Pruter, Deutsches Zentrum für Luft- und Raumfahrt e.V., Germany
Reserve Paper 4.6.R
0834		 AN INTEGRATED CONCEPTUAL-DESIGN FRAMEWORK FOR MULTICOPTER URBAN AIR MOBILITY VEHICLES
B Mufti, National University of Science and Technology, Pakistan
5.6Turbulence Modeling
Chair(s): Coder, J., Viviani, A.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 13:40 14:05 5.6.1
0468		 DATA-DRIVEN RANS CLOSURES USING AN ADAPTIVE CURVATURE-BASED CLASSIFIER FOR VORTEX FLOWS
P West, Williams F1 team, United Kingdom
15. Sep 26 14:05 14:30 5.6.2
0112		 DATA-DRIVEN TURBULENCE MODELING FOR MULTI-MECHANISM SEPARATED FLOWS OVER ICED AIRFOILS
Z.Z. HE¹, Y.F. ZHANG¹; ¹Tsinghua University, China
15. Sep 26 14:30 14:55 5.6.3
0064		 AN EVALUATION OF NONLINEAR EDDY-VISCOSITY MODELS FOR HIGH REYNOLDS NUMBER TURBULENT FLOW SIMULATIONS
T. Chagas Silva, Instituto Tecnologico de Aeronautica, Brazil
15. Sep 26 14:55 15:20 5.6.4
0785		 NUMERICAL INVESTIGATION OF GUST LOAD ALLEVIATION FOR ULTRA-HIGH ASPECT RATIO WINGS WITH PASSIVELY RELEASED FFWT
TR Chen, NorthWestern Polytechnical University, China
Reserve Paper 5.6.R
0054		 CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER
J. Fernandez Anton, Instituto Nacional de Técnica Aeroespacial, Spain
additional information (interactive) 5.6.R
0634		 MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELLING
P. Kovár, Czech Republic
6.6Flow interactions and integration
Chair(s): Prince, S., Lawson, N.
Track 6
03.2 - Experimental Aerodynamics
15. Sep 26 13:40 14:05 6.6.1
0705		 UNSTEADY SWIRL AND TOTAL PRESSURE DISTORTION ANALYSIS IN AN ASPIRATED SHORT INTAKE IN CROSSWIND CONDITIONS USING STEREOSCOPIC PIV DATA
T. Piovesan, Cranfield University, United Kingdom
15. Sep 26 14:05 14:30 6.6.2
0970		 EXPERIMENTAL STUDY OF GROUND EFFECT ON A HEAVING NACA0012 AEROFOIL
M. Li, University of Sydney, Australia
15. Sep 26 14:30 14:55 6.6.3
0218		 LOW-SPEED EXPERIMENTAL INVESTIGATION OF PODDED ENGINE INTEGRATION OF FLYING V AIRCRAFT
A. Kumar, TU Delft Faculty of Aerospace Engineering, Netherlands
15. Sep 26 14:55 15:20 6.6.4
0804		 WHEN ROTOR WAKE MEETS THE GROUND: INFLUENCE OF BLADE COUNT AND BLADE PITCH ON ROTOR OUTWASH
- Pradyumna, The University of Sydney, Australia
Reserve Paper 6.6.R
0049		 WIND TUNNEL INVESTIGATION OF HELICOPTER LOADS DURING URBAN OPERATIONS ON A BUILDING WITH COLUMNAR VORTEX GENERATORS (CVG
J.C.M. Matías, INTA, Spain
additional information (interactive) 6.6.R
0700		 INFLUENCE OF PROPELLER ON SIDE EDGE VORTICES IN A STOL UAV
D.-P. Pastuszko, Poland
7.6Unsteady and Bio-Inspired Aerodynamics
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 26 13:40 14:05 7.6.1
0542		 AERODYNAMIC EFFECT OF PITCHING MOTION FOR FLAPPING AIRFOIL ACROSS DIFFERENT SWEEPING TRAJECTORIES
- Liu, China
15. Sep 26 14:05 14:30 7.6.2
0665		 AERODYNAMIC OPTIMISATION OF BIOINSPIRED CORRUGATED WINGS FOR HIGH-EFFICIENCY MAV GLIDING
M Krasniqi, Flat 63 Nottingwood House, United Kingdom
15. Sep 26 14:30 14:55 7.6.3
0777		 AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK
H.-H. Yang, Korea Advanced Institute of Science and Technology, South Korea
15. Sep 26 14:55 15:20 7.6.4
0916		 THREE-DIMENSIONAL FLOW STRUCTURES OVER A LOW-ASPECT-RATIO PLUNGING WING
B. Anilir, METU Aerospace Engineering Department, Turkey
Reserve Paper 7.6.R
0184		 AERODYNAMIC PERFORMANCE ANALYSIS OF A NOVEL LIFT-THRUST INTEGRATED ROTARY FLAPPING AERIAL VEHICLE
L Liu, School of Aeronautics, Northwestern Polytechnical University, China
additional information (interactive) 7.6.R
0147		 STUDY ON AERODYNAMICS OF THE WING WITH FLAP INSPIRED FROM BIRD COVERTS
X Xu, Northwestern Polytechnical University, China
additional information (interactive) 7.6.R
0182		 INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATION
C. Cao, Northwestern Polytechnical University, China
8.6Structural Optimization
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 13:40 14:05 8.6.1
0943		 TOPOLOGY-OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR COST-EFFICIENT UAVS
A.M. Comer, Oklahoma State University, United States
15. Sep 26 14:05 14:30 8.6.2
0640		 TRACING MATERIAL PROPERTIES TO SYSTEM-LEVEL PERFORMANCE: A NORMALISED SENSITIVITY ANALYSIS FOR A BOEING 737 CLASS AIRCRAFT
S Stekovic, Linköping University, Sweden
15. Sep 26 14:30 14:55 8.6.3
0930		 GRADIENT-BASED STRUCTURAL OPTIMISATION OF COMPOSITE WING STRUCTURES USING HIGH-ORDER BEAM MODELS
D. Cardone, Universidad Carlos III de Madrid, Spain
15. Sep 26 14:55 15:20 8.6.4
0005		 THE STUDY ON STIFFNESS OPTIMIZATION ANALYSIS OF CIVIL AIRCRAFT FUSELAGE DOOR OPENINGS
Kaijun Yin, China
Reserve Paper 8.6.R
0018		 SENSITIVITY ANALYSIS OF THE JOHNSON-COOK MODEL PARAMETERS FOR AL2024-T3 IN BIRD STRIKE ANALYSIS ON FIXED LEADING EDGES
R. Martins Martins, Boeing, Brazil
9.6Testing & Demonstrator
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 13:40 14:05 9.6.1
0157		 A FULL-SCALE DEMONSTRATOR FOR RAPID TESTING OF HELICOPTER AIRFRAMES USING ADVANCED CONTROL SYSTEM METHODOLOGIES
G. Swanton, Defence Science and Technology Group, Australia
15. Sep 26 14:05 14:30 9.6.2
0312		 HIGH SPEED ACTUATION SYSTEM DESIGN AND VALIDATION FOR A TRANSONIC WIND TUNNEL MODEL
C.C.W. van der Post, Netherlands Aerospace Centre, Netherlands
15. Sep 26 14:30 14:55 9.6.3
0014		 WIND TUNNEL TESTING OF WHIRL FLUTTER AEROELASTIC DEMONSTRATOR
J. Cecrdle, VZLU AEROSPACE, Czech Republic
15. Sep 26 14:55 15:20 9.6.4
0852		 EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL
N. Kishimoto, Kwansei Gakuin University, Japan
10.6Supersonic
Chair(s): ,
Track 10
05 - Propulsion and Energy
15. Sep 26 13:40 14:05 10.6.1
0788		 NUMERICAL INVESTIGATION OF GEOMETRIC EFFECT ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES
Y. Wu, Northwestern Polytechnical University, China
15. Sep 26 14:05 14:30 10.6.2
0207		 COMPARATIVE ASSESSMENT OF PROPULSION SYSTEM ARCHITECTURES TAILORED FOR SUPERSONIC APPLICATIONS
L. Carrea, Mälardalen University, Sweden
15. Sep 26 14:30 14:55 10.6.3
0418		 SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET
H. Miki, JAXA, Japan
15. Sep 26 14:55 15:20 10.6.4
0510		 NUMERICAL STUDY OF UNSTEADY DISTORTION IN AN S-DUCT INTAKE SUBJECTED TO BLAST SHOCK WAVES
L. Shi, China
Reserve Paper 10.6.R
0911		 TOWARDS SUSTAINABLE SUPERSONIC PROPULSION: INTEGRATED PROPULSIVE-EMISSIONS MODEL FOR MACH-2 MIXED-FLOW TURBOFAN ENGINES
Fabrizio Borgna¹, Roberta Fusaro¹, Davide Ferretto¹, Nicole Viola¹, Marco Marini, Italian Aerospace Research Centre (CIRA), Italy; ¹Politecnico di Torino, Italy
11.6Optimization
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 13:40 14:05 11.6.1
0099		 A HYBRID CNN-LSTM AND PSEUDOSPECTRAL METHOD FOR RAPID SPACECRAFT REENTRY OPTIMIZATION
Y.X. Yang¹, Z. Xu¹; ¹Northwestern Polytechnical University, China
15. Sep 26 14:05 14:30 11.6.2
0505		 OPTIMAL GUIDANCE ALGORITHM FOR BOOST-BACK OF REUSABLE LAUNCH VEHICLES
J. Shim, Korea Advanced Institute of Science and Technology, South Korea
15. Sep 26 14:30 14:55 11.6.3
0224		 AIRSPACE CAPACITY IMPLICATIONS OF CONTRAIL-AWARE TRAJECTORY OPTIMIZATION
T. Polishchuk, LiU, Sweden
15. Sep 26 14:55 15:20 11.6.4
0377		 TRIM OPTIMIZATION FOR AN AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION AND A TAIL THRUST UNIT
C. Varriale, TU Delft , Netherlands
Reserve Paper 11.6.R
0744		 CALIBRATED AIRSPEED AS A DECISION VARIABLE FOR LOW-CARBON OPERATIONS: ESF METRICS, SAF, AND FUZZY CONTROL
Celia Mendez Cubillos, Opencadd Advanced Technology , Brazil
12.6Thermal
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
15. Sep 26 13:40 14:05 12.6.1
0030		 DESIGN AND OPERATION OF LOW-COST MULTI-SCALE TEST BEDS FOR THERMAL RUNAWAY INITIATION AND PROPAGATION
W Mooney, Canada
15. Sep 26 14:05 14:30 12.6.2
0663		 MODAL-BASED FUEL LEVEL ESTIMATION OF CRYOGENIC PROPELLANT TANKS
S Pfeifer, FH JOANNEUM Ges.mbH, Austria
15. Sep 26 14:30 14:55 12.6.3
0807		 SIZING OF LINEAR ACTUATORS FOR SPAN EXTENSION OF HALE UAV
T Prakash, India
15. Sep 26 14:55 15:20 12.6.4
0847		 DYNAMIC PERFORMANCE DEGRADATION OF FLIGHT CONTROL EHA UNDER HIGH-TEMPERATURE CONDITIONS
M. -W. Sun, Beihang University, China
Reserve Paper 12.6.R
0593		 NONLINEAR FRICTION MODELING OF HELIX SWING HYDRAULIC CYLINDERS FOR MORPHING AIRCRAFT USING PHYSICS-INFORMED NEURAL NETWORKS
S. Chen, Beihang University, China
Reserve Paper 12.6.R
0991		 LIGHTWEIGHT BIMETALLIC GEARS FOR AEROSPACE TRANSMISSIONS ENABLED BY OPEN-AIR DIFFUSION BONDING
J Jiang, Imperial College London, United Kingdom
additional information (interactive) 12.6.R
0483		 HIGH-PRECISION EDDY CURRENT TIP CLEARANCE SENSOR WITH EXCEPTIONAL HIGH-TEMPERATURE RESISTANCE
F. L. Liu, Northwestern Polytechnical University, China
13.6Air Traffic Operational Safety
Chair(s): Maroney, D.
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
15. Sep 26 13:40 14:05 13.6.1
0863		 APPROPRIATE ATC GO-AROUND INSTRUCTION TIMING TO PREVENT RUNWAY COLLISIONS
S. Kontani, Graduate School of Maritime Sciences, Kobe University, Japan
15. Sep 26 14:05 14:30 13.6.2
0568		 COMPARATIVE VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS
J. Meier, German Aerospace Center (DLR), Germany
15. Sep 26 14:30 14:55 13.6.3
0178		 FLIGHT CENTRIC ATC – HOW TO SOLVE CONFLICTS WITHOUT COMMUNICATION AND COORDINATION OVERLOADS?
T. Finck, German Aerospace Center, Germany
15. Sep 26 14:55 15:20 13.6.4
0811		 AUGMENTED REALITY SAFETY NETS FOR INCREASED AIRPORT SAFETY
T. Fadda, University of Bologna - Italy, Italy
Reserve Paper 13.6.R
0302		 EVALUATING HUMAN-MACHINE-TEAMING CONCEPTS FOR A HIGHLY AUTOMATED GROUND CONTROLLER WORKING POSITION
L. Nöhren, DLR, Germany
14.6Swarm Control
Chair(s): , , Palmer, J.
Track 14
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 26 13:40 14:05 14.6.1
0670		 AN AUTONOMY ARCHITECTURE FOR COLLABORATIVE UAV SWARMS - A BOTTOM-UP PERSPECTIVE
Pranav Nagarajan¹, Simon Schopferer¹, Karolin Thomessen¹; ¹German Aerospace Center (DLR), Germany
Presenter: Karolin Thomessen, German Aerospace Center (DLR)
15. Sep 26 14:05 14:30 14.6.2
0167		 SOFTWARE-IN-THE-LOOP SIMULATION OF DISTRIBUTED 3D INTEGRATED SWARM GUIDANCE FOR FIXED-WING UAVS
Y. Yang, Chungnam National University, South Korea
15. Sep 26 14:30 14:55 14.6.3
0765		 REINFORCEMENT LEARNING-BASED ADAPTIVE WEIGHTING OF SWARM GUIDANCE LAWS FOR SMALL FIXED-WING UAVS
C Kang, Hanseo University, South Korea
15. Sep 26 14:55 15:20 14.6.4
0735		 2D AND 3D TRAJECTORY PLANNING FOR UAVS FORMATION SYSTEM USING DYNAMIC WINDOW APPROACH
RB.-Z. Zhu, Northwestern Polytechnical University, China
Reserve Paper 14.6.R
0771		 IMPLEMENTATION OF DISTRIBUTED SWARM GUIDANCE ALGORITHMS ON LOW-COST UAVS
J.L. McGuire, DSTG, Australia
additional information (interactive) 14.6.R
0037		 ADAPTIVE PRESCRIBED-TIME COOPERATIVE CONTROL FOR FORMATION OF SMALL TANDEM-ROTOR UAVS
X Li, China
additional information (interactive) 14.6.R
0098		 PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION
F. Fang, Northwestern Polytechnical University, China
additional information (interactive) 14.6.R
0531		 RESEARCH ON OFFENSIVE AUTONOMOUS VEHICLE TRAJECTORY PREDICTION METHOD BASED ON IMPROVED INVERSE REINFORCEMENT LEARNING IN AIRCRAFT ACTIVE DEFENSE MODE
H.-Z Zhang, China
15.6Safety, Environment, and Hazard Mitigation
Chair(s): ,
Track 15
10 - Safety and Security
15. Sep 26 13:40 14:05 15.6.1
0041		 A MODEL OF DISEASE TRANSMISSION AND MITIGATION OPTIONS FOR AVIATION FROM GATE BOARDING TO IN-FLIGHT, A BOEING/FAA/US CDC
J W Armstrong, Boeing, Australia
15. Sep 26 14:05 14:30 15.6.2
0161		 PROBABILISTIC VALIDATION OF A NUMERICAL MODEL FOR RUN-BACK ICE SHAPES PREDICTION
M. Gallia, TU Braunschweig, Germany
15. Sep 26 14:30 14:55 15.6.3
0439		 EARLY WARNING FOR POTENTIAL BIRD STRIKES: STRATEGIC OPTIMIZATION OF PAN-TILT-ZOOM SENSOR NETWORKS FOR BIRD HAZARD DECREASE IN AIRPORT ENIRONMENT
- Mei, The University of Sydney, Australia
15. Sep 26 14:55 15:20 15.6.4
0457		 REAL-TIME AIRPORT BIRD-STRIKE PROTECTION WITH IMPROVED EDGE DEVICE DETECTION METHOD
J Gao, The University of Sydney, Australia

15:20 - 15:25CHANGEOVER BREAK

0.6GENERAL LECTURE 3 X59 Low Boom Demonstrator
Chair:
15. Sep 26 15:25 16:15

16:15 - 16:40AFTERNOON BREAK

1.7GSA2: Future Sustainable Aviation Infrastructure: Prospects and Challenges
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
15. Sep 26 16:40 17:05 1.7.1
0985		 JET ZERO: ATJ SAF PROJECT DEVELOPER
J Mason, Jet Zero Australia, Australia
2.7GARTEUR 1
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
15. Sep 26 16:40 17:05 2.7.1
0989		 THE GARTEUR GROUP OF RESPONSABLES IN AERODYNAMICS (GOR AD) AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES
M. Tormalm, Sweden
15. Sep 26 17:05 17:30 2.7.2
0996		 GARTEUR AG59 IMOLA: IMPROVING THE MODELLING OF LAMINAR SEPARATION BUBBLES
P. Catalano, CIRA, Italy
15. Sep 26 17:30 17:55 2.7.3
1009		 AI IN AVIATION CYBERSECURITY RISK ASSESSMENT: OPPORTUNITIES AND CHALLENGES
C. Doll, ONERA, France
3.7MDO 2
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 16:40 17:05 3.7.1
0445		 COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS
J.C Chan, Cranfield University, United Kingdom
15. Sep 26 17:05 17:30 3.7.2
0278		 DEEP LEARNING-BASED INVERSION OF NEAR-FIELD OVERPRESSURE SIGNATURES FOR LOW-BOOM SUPERSONIC TRANSPORT
Y.-P. Peng, Northwestern Polytechnical University, China
15. Sep 26 17:30 17:55 3.7.3
0606		 EASIBILITY-AWARE MULTISOURCE DESIGN METHODOLOGIES FOR HYDROGEN-POWERED SUSTAINABLE AVIATION
R Obasa, Imperial College London, United Kingdom
15. Sep 26 17:55 18:20 3.7.4
0876		 AN INCREMENTAL MODULAR MDO FRAMEWORK FOR HYDROGEN-ELECTRIC POWERTRAIN SIZING AND INTEGRATION IN GENERAL AVIATION AIRCRAFT
Pablo Moreno-Escolástico, Universidad Carlos III de Madrid, Spain
4.7Optimization in design
Chair(s): Gerhards, R.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 16:40 17:05 4.7.1
0416		 A MULTI-SCALE COMPUTATIONAL FRAMEWORK FOR EVALUTATING TECHNOLOGY IMPACTS ON FUTURE AIRCRAFT FLEETS
ES Cassidy, University of Michigan, United States
15. Sep 26 17:05 17:30 4.7.2
0369		 MULTIDISCIPLINARY DESIGN OPTIMIZATION OF HYBRID AIRCRAFT: INFLUENCE OF THE RANGE OF MISSION PROFILES ON OPTIMAL DESIGN
D.-B. Brousset-Matheu, ONERA, France
15. Sep 26 17:30 17:55 4.7.3
0783		 COST-DRIVEN MULTIDISCIPLINARY OPTIMIZATION OF WINGLETS FOR A REGIONAL AIRCRAFT
L Falcone, University of Naples Federico II, Italy
15. Sep 26 17:55 18:20 4.7.4
0703		 TOP-LEVEL AIRCRAFT REQUIREMENT TRADE STUDIES FOR HYDROGEN FUEL CELL REGIONAL AIRCRAFT
M. Di Stasio, University of Naples Federico II, Italy
Reserve Paper 4.7.R
0696		 MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY
G. Shen, Northwestern Polytechnical University, China
5.7Aeroacoustics and Noise Predictions
Chair(s): , , Lawson, N.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 16:40 17:05 5.7.1
0488		 THE NUMERICAL SIMULATIONS OF THE ACOUSTIC SHIELDING EFFECTS ON THE BLADE-VORTEX INTERACTION NOISE OF THE HART-II MODEL
T. Ikeda, Japan Aerospace Exploration Agency, Japan
15. Sep 26 17:05 17:30 5.7.2
0569		 NOISE-OPTIMIZED HOVER PROPELLER DESIGN FOR VTOL CARGO DRONES IN TRANSIENT FLIGHT CONDITIONS
T. Moses, Technical University of Munich, Germany
15. Sep 26 17:30 17:55 5.7.3
0693		 HIGH-FIDELITY AEROACOUSTIC AND UNSTEADY FLOW ANALYSIS OF WIND TURBINE BLADES
H A Abid, King Fahd University of Petroleum and Minerals, Saudi Arabia
15. Sep 26 17:55 18:20 5.7.4
0855		 LOWERING THE BARRIER TO AEROACOUSTIC PREDICTION: GPU-COMPUTED SBES FOR FAR-FIELD LANDING GEAR NOISE PREDICTION
B. P. Edmonds, LEAP Australia Pty. Ltd., Australia
Reserve Paper 5.7.R
0923		 PRACTICAL ASPECTS OF ROTOR AERODYNAMIC AND AEROACOUSTIC DESIGN OPTIMIZATION
W. A. Klimczyk, Lukasiewicz Research Network - Institute of Aviation, Poland
6.7Morphing and shape adaptation
Chair(s): Imamura, T., Allen, N.
Track 6
03.2 - Experimental Aerodynamics
15. Sep 26 16:40 17:05 6.7.1
0730		 EXPERIMENTAL STUDY OF LOAD ALLEVIATION WITH PASSIVE ADAPTIVE CAMBER AIRFOILS
A. Sumi, Tokyo University of Agriculture and Technology, Japan
15. Sep 26 17:05 17:30 6.7.2
0789		 EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY
M. A. Marciniuk, Wroc?aw University of Science and Technology, Poland
15. Sep 26 17:30 17:55 6.7.3
0799		 GUST RESILIENCE: PASSIVE GUST MITIGATION MECHANISMS USED BY GLIDING KESTRELS
D Penn, RMIT University, Australia
15. Sep 26 17:55 18:20 6.7.4
0347		 AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC REGIME AT REYNOLDS NUMBER OF 1 MILLION
J.A.K. Abu Kalil, ICUBE/IMFT, France
Reserve Paper 6.7.R
0810		 WIND-TUNNEL FORCE BALANCE AND MOUNTING SYSTEM FOR INFLATABLE WINGS
B Desale, IITB-Monash Research Academy, India
additional information (interactive) 6.7.R
0517		 EFFECTS OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS
Y Tanahashi, Chubu University, Japan
7.7Data-Driven Design, Optimization and Reduced-Order Modeling
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 26 16:40 17:05 7.7.1
0358		 A GRAPH NEURAL NETWORK SIMULATOR FOR TRANSONIC VORTEX-DOMINATED FLOWS ON THE DLR-F23 CONFIGURATION
A. Goerttler, German Aerospace Center, Germany
15. Sep 26 17:05 17:30 7.7.2
0502		 SUPERVISED DIMENSIONALITY-REDUCED MULTI-FIDELITY SURROGATE MODEL ASSISTED HIGH-DIMENSIONAL NATURAL LAMINAR FLOW OPTIMIZATION
Y. Gan, Northwestern Polytechnical University, China
15. Sep 26 17:30 17:55 7.7.3
0546		 AIRFOIL DESIGN OPTIMIZATION FOR HIGH-LIFT AND HIGH-EFFICIENCY APPLICATIONS USING DEEP REINFORCEMENT LEARNING
P Scavella, UNIVERSITY OF NAPLES FEDERICO II, Italy
15. Sep 26 17:55 18:20 7.7.4
0767		 UNSTEADY AERODYNAMIC OPTIMIZATION OF THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH LEVEL SET METHOD
D Sasaki, Osaka Metropolitan University, Japan
Reserve Paper 7.7.R
0473		 MULTI-SCALE LINEAR FEATURE MODULATION DEEP NEURAL OPERATOR FOR RAPID PRESSURE COEFFICIENT PREDICTION
ZWF Zhang, NWPU, China
8.7Damage Tolerance
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 16:40 17:05 8.7.1
0053		 ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS
George Catalin: Cristea, INCAS, Romania
15. Sep 26 17:05 17:30 8.7.2
0145		 AN EFFICIENT MULTIPARAMETRIC METHODOLOGY FOR DAMAGE PROGNOSTICS AND SHM OF ICE PROTECTION COMPOSITE LAMINATES
S B Bushpalli, Collins Aerospace , Ireland
15. Sep 26 17:30 17:55 8.7.3
0146		 IMPACT OF COATING COLOR ON THERMAL RESPONSE OF GFRP/CFRP AIRCRAFT STRUCTURES UNDER SOLAR RADIATION
B Goliszek, Warsaw University of Technology, Poland
15. Sep 26 17:55 18:20 8.7.4
0083		 MULTIPHYSICS COUPLING EFFECT ON INTERFACIAL PROPERTIES OF CNT/GFRP/CFRP COMPOSITES FOR ELECTROTHERMAL AI/DI APPLICATIONS
X. Yao, Northwestern Polytechnical University, China
Reserve Paper 8.7.R
0276		 NUMERICAL SIMULATION OF STRESS-OXIDATION DAMAGE IN C/SIC COMPOSITES AT HIGH TEMPERATURES
G. Chen, Northwestern Polytechnical University, China
Reserve Paper 8.7.R
0357		 IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITE
A.M. Caporale, Politecnico di Milano, Italy
9.7Composite Structure
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 16:40 17:05 9.7.1
0355		 COMBINED TOPOLOGY AND COMPOSITE LAMINATE OPTIMIZATION OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT
LEM Vertonghen, France
15. Sep 26 17:05 17:30 9.7.2
0614		 OPTIMIZATION APPROACHES FOR THE SHEAR-POSTBUCKLING DESIGN OF THERMOPLASTIC THIN-PLY COMPOSITE SHELLS IN HELICOPTERS
M. Mauersberger¹, J. Rehfeldt¹, F. Hähnel¹, J. Markmiller¹; ¹Dresden University of Technology (TUD), Germany
15. Sep 26 17:30 17:55 9.7.3
0948		 AN AUTOMATED PARAMETRIC FRAMEWORK FOR EARLY-STAGE STRUCTURAL DESIGN AND OPTIMIZATION OF COMPOSITE AIRFRAMES
N Ziakos, Universidad Carlos III de Madrid, Spain
15. Sep 26 17:55 18:20 9.7.4
0902		 DYNAMIC BUCKLING ANALYSIS OF VARIABLE STIFFNESS COMPOSITE CYLINDRICAL SHELLS
Y. Guo, Nanjing University of Aeronautics and Astronautics, China
Reserve Paper 9.7.R
0092		 MULTIAXIAL MECHANICAL BEHAVIOR OF PLAIN-WOVEN CFRP TUBES UNDER COMBINED TENSION–TORSION LOADING
Z.-L. Liu, Northwestern Polytechnical University, China
Reserve Paper 9.7.R
0853		 CURVATURE-CONTROLLED MORPHING OF FOLDING WINGTIPS USING HONEYCOMB PLATES
Rui Yang¹, Shenghua Li¹, Shiyong Sun  ???¹; ¹School of Mechanical Engineering Dalian University of Technology, China
additional information (interactive) 9.7.R
0101		 DESIGN CONCEPT FOR STRUCTURAL ELEMENTS MANUFACTURED FROM THICK LAMINATED COMPOSITE MATERIALS
G. C. Fonseca, Embraer Minas Gerais, Brazil
10.7Hypersonic
Chair(s): ,
Track 10
05 - Propulsion and Energy
15. Sep 26 16:40 17:05 10.7.1
0370		 PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN
K. Tsukuda, Osaka Metropolitan University, Japan
15. Sep 26 17:05 17:30 10.7.2
0504		 NUMERICAL PREDICTION AND EXPERIMENTAL VALIDATION ON THRUST PERFORMANCE OF SCRAMJET EXTERNAL NOZZLES
T.-I. Isono, Japan Aerospace Exploration Agency, Japan
15. Sep 26 17:30 17:55 10.7.3
0508		 REPRESENTATIVE THERMO-STRUCTURAL TESTING OF SCRAMJETS USING COMMERCIAL ROCKET ENGINE TEST
A Lockley, Australia
15. Sep 26 17:55 18:20 10.7.4
0780		 GREEN PROPULSION VIA SUSTAINABLE 3D-PRINTED METAL-DOPED PLA HYBRID ROCKET FUELS
N. Binti Abd Razak, Malaysia
Reserve Paper 10.7.R
0608		 A COUPLED ANALYTICAL AND NUMERICAL FRAMEWORK FOR PREDICTING MIXING DEVICE PERFORMANCE IN HYBRID ROCKET ENGINES
G.-P. Puri, Australia
11.7Flight control system simulation
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 16:40 17:05 11.7.1
0125		 PILOT-IN-THE-LOOP SIMULATION OF OPTIMAL DEEP-STALL RECOVERY FOR T-TAIL AIRLINER
K. Yoshioka¹, T. Tsuchiya¹; ¹The university of Tokyo, Japan
15. Sep 26 17:05 17:30 11.7.2
0662		 A SIMULATION STUDY ON THE EFFECT OF EXTENDED ROTATIONAL KINEMATICS IN HEXAPOD MOTION SIMULATORS
T. Bernhofer, Germany
15. Sep 26 17:30 17:55 11.7.3
0869		 HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS
S. Joshin, The University of Osaka, Japan
15. Sep 26 17:55 18:20 11.7.4
0496		 A CFD-BASED METHODOLOGY FOR SEPARATING COUPLED PITCH-DAMPING DERIVATIVES AND ASSESSING MOTION-PARAMETER SENSITIVITY
L-E Strydom, Council for Scientific and Industrial Research , South Africa
Reserve Paper 11.7.R
0174		 HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL
H. S. Choi, Korea Aerospace Research Institute, South Korea
Reserve Paper 11.7.R
0629		 A FRAMEWORK FOR VIRTUAL CERTIFICATION OF AIRCRAFT IN ICING CONDITIONS: WORKFLOW IMPLEMENTATION AND ASSESSMENT
H. P. Heramarwan, Politecnico di Milano, Italy
12.7Informatic modeling
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
15. Sep 26 16:40 17:05 12.7.1
0028		 ANOMALY B-VALUE DETECTION AND EXCLUSION OF GBAS BASED ON WAVELET MULTI-RESOLUTION ANALYSIS
R.-X. GONG, Airbus (Tianjin) Final Assembly Company Limited, China; S.-G. SUN¹, M. XU¹, Y. ZHENG, Northeast Air Traffic Management Bureau of Civil Aviation of Chi, China; ¹civil aviation university of China, China
15. Sep 26 17:05 17:30 12.7.2
0460		 MODELING OF AIRCRAFT COMPONENT PLACEMENTS WITH BIN PACKING
J Chang, McGill University, Canada
15. Sep 26 17:30 17:55 12.7.3
0474		 HYBRID RF-LIFI CONNECTIVITY WITH PREDICTIVE SWITCHING: TRANSFORMING PASSENGER AND CREW COMMUNICATION INSIDE AIRCRAFT CABINS
N/A Kodukula, Boeing India Engineering and Technolog Center, India
15. Sep 26 17:55 18:20 12.7.4
0661		 LOW-COST MACH-2 SUPERSONIC FREE-JET FACILITY USING COMMERCIAL OFF-THE-SHELF COMPONENTS
N.M Hoang, Viettel Aerospace Institute, Vietnam
13.7Dynamic Modeling of Aviation Systems
Chair(s): Pinon-Fischer, O.
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
15. Sep 26 16:40 17:05 13.7.1
0838		 WEATHER-DRIVEN DEEP LEARNING FOR AIRPORT RUNWAY CONFIGURATION FORECASTING
H.W. Kim¹, Y.J. Eun¹, D.K. Jeon¹; ¹Korea Aerospace Research Institute, South Korea
15. Sep 26 17:05 17:30 13.7.2
0697		 A PRELIMINARY STUDY ON DYNAMIC AIRSPACE CONFIGURATION USING FLEXIBLE VERTICAL BOUNDARIES IN DOUBLE-LAYER AIRSPACE
H Suizu, Electronic Navigation Research Institute, Japan
15. Sep 26 17:30 17:55 13.7.3
0779		 EVALUATING IMPACT OF INTERNATIONAL DEPARTURE TIME CONTROL ON DOMESTIC ARRIVAL DELAYS IN JAPAN USING MULTI-OBJECTIVE SIMULATION-BASED OPTIMIZATION
Katsuhiro Sekine¹, Tomoaki Tatsukawa, Tokyo University of Science, Japan; Yoshiaki Kawagoe, Tohoku University, Japan; Eri Itoh¹; ¹The University of Tokyo, Japan
15. Sep 26 17:55 18:20 13.7.4
0521		 UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS
J.H. Kim, Sejong University, South Korea
Reserve Paper 13.7.R
0860		 SENSITIVITY STUDY OF DEPARTURE TIME ACCURACY FOR AIRPORT COLLABORATIVE DECISION MAKING USING FAST-TIME SIMULATION
Y. Iwatsuki, Mitsubishi Research Institute, Inc., Japan
additional information (interactive) 13.7.R
0298		 QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY
G. Wang, Aerial Industry Development Research Center of China, China
14.7ICAS Council Meeting
Chair(s): ,
Track 14
15.7Design challenges and Training enablers
Chair(s): ,
Track 15
14 - Education and Training
15. Sep 26 16:40 17:05 15.7.1
0827		 DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY
B. Sebastiani, University of Bologna, Italy
15. Sep 26 17:05 17:30 15.7.2
0721		 A STRUCTURED CONCEPTUAL AND PRELIMINARY DESIGN FOR A SMALL-SCALE ELECTRICALLY POWERED FIXED-WING AIRCRAFT
N.A Azmitia, Universidad Panamericana, Mexico
15. Sep 26 17:30 17:55 15.7.3
0464		 EVALUATING LEARNING EFFECTIVENESS THROUGH A MIXED REALITY TRAINING FRAMEWORK FOR AEROSPACE MAINTENANCE TASKS
MA Higinio, RMIT UNIVERSITY, Australia
15. Sep 26 17:55 18:20 15.7.4
0692		 FROM DATA TO DEBRIEF: A FRAMEWORK FOR PILOT PERFORMANCE ASSESSMENT
P. B. Kurka, ITA, Brazil
Reserve Paper 15.7.R
0443		 EDUCATING UNDERGRADUATE STUDENTS WORKING IN HANDS-ON ENGINEERING PROJECTS ON REQUIREMENT DEFINITION AND DOCUMENTATION IN MEXICO.
A Pedroza-Díaz, Universidad Panamericana, Mexico
Reserve Paper 15.7.R
0639		 TOWARDS AN ECOSYSTEM FOR AERONAUTICAL RESEARCH IN MEXICO
A. M. Zarate Villazon, Georgia Institute of Technology - Aerospace Systems Design Lab, United States

Wednesday, 16. Sep 2026

0.7ICAS LECTURE FOR INNOVATION IN AERONAUTICS Veronique Roca – Airbus Beluga X
Chair:
16. Sep 26 08:00 08:50

08:50 - 09:15COFFEE BREAK

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

10:45 - 10:50CHANGEOVER BREAK

1.8GSA2: Super Panel: Pathways to Global Sustainable Aviation
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
16. Sep 26 10:50 11:15 1.8.1
0982		 GLOBAL SUSTAINABLE AVIATION SUPER PANEL
R.A. Wahls, NASA, Retired, United States
2.8GARTEUR 2
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
16. Sep 26 10:50 11:15 2.8.1
1006		 MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS
F. J. San Millan, INTA, Spain
16. Sep 26 11:15 11:40 2.8.2
1005		 ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS
L. Montero-Sistiaga, Royal Netherlands Aerospace Centre, Netherlands
16. Sep 26 11:40 12:05 2.8.3
1004		 CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING
F Roudolff, ONERA, France
16. Sep 26 12:05 12:30 2.8.4
1011		 GARTEUR RESEARCH GROUP AG60 EXPERIENCE AND ACTIVITIES ON MACHINE LEARNING AND DATA-DRIVEN APPROACHES FOR AERODYNAMICS AND UNCERTAINTY QUANTIFICATION
P. Catalano, Italy
3.8Case Studies 1
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
16. Sep 26 10:50 11:15 3.8.1
0602		 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 3.8.2
0596		 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 3.8.3
0209		 A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION
L.L. Liu, HONG KONG UNIVERSITY OF SCIENCE AND TECHNOLOGY, Hong Kong SAR of China
16. Sep 26 12:05 12:30 3.8.4
0631		 OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES
M. A. Hariansyah, The Hong Kong University of Science and Technology, Hong Kong SAR of China
Reserve Paper 3.8.R
0610		 MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY
L Mainini, Imperial College London, United Kingdom
Reserve Paper 3.8.R
0873		 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
4.8Unconventional 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 4.8.1
0625		 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 4.8.2
0431		 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 4.8.3
0078		 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 4.8.4
0576		 RESEARCH PLATFORM AIRSHIP: DESIGN AND FLIGHT CHARACTERISTICS FOR URBAN OPERATIONS
H. Reindle, Technical University of Munich, Germany
Reserve Paper 4.8.R
0274		 EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT
E. M. Künstler, University of Stuttgart, Germany
additional information (interactive) 4.8.R
0274		 EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT
E. M. Künstler, University of Stuttgart, Germany
5.8Machine Learning Applications
Chair(s): , , Halila, G.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 10:50 11:15 5.8.1
0492		 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 5.8.2
0530		 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 5.8.3
0051		 A COMPARATIVE STUDY OF PHYSICS-INFORMED NEURAL NETWORK FORMULATIONS FOR PARABOLIZED STABILITY EQUATIONS
L. Olichevis Halila, PUCPR, Brazil
16. Sep 26 12:05 12:30 5.8.4
0490		 EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN
Y. Fan, NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
Reserve Paper 5.8.R
0462		 RESEARCH ON AERODYNAMIC-STEALTH INTEGRATED DESIGN METHODOLOGY BASED ON MPPO ALGORITHM
K.-G Gan, China
additional information (interactive) 5.8.R
0509		 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) 5.8.R
0762		 A HYBRID MACHINE LEARNING PIPELINE FOR AIRFOIL AERODYNAMICS: COMPARING UNIVERSAL AND CLUSTER-SPECIFIC PREDICTION STRATEGIES
R. M. Coelho, Universidade Federal de Uberlândia, Brazil
6.8AI 1
Chair(s): ,
Track 6
15 - Guest lectures (by personal invitation only)
16. Sep 26 10:50 11:15 6.8.1
0990		 TOWARDS A FOUNDATIONAL AI MODEL FOR AIRCRAFT DESIGN: FROM HIGH-FIDELITY DATASETS TO SCALING LAWS
n. Ashton, United States
7.8Configuration Aerodynamics and Coupled Flight Behaviour
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
16. Sep 26 10:50 11:15 7.8.1
0269		 FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH
Z.G. Zhang, Northwestern Polytechnical University, China
16. Sep 26 11:15 11:40 7.8.2
0284		 MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLIGHT REGIMES
D. Palma, Sapienza university of Rome, Italy
16. Sep 26 11:40 12:05 7.8.3
0330		 STUDY ON THE IMPACT OF TRIM CONDITION ON LATERAL AND DIRECTIONAL STABILITY FOR A TAILLESS AIRCRAFT
K. Kania, Warsaw University of Technology, Poland
16. Sep 26 12:05 12:30 7.8.4
0456		 GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY
P. Kantzidis, RMIT University, Australia
Reserve Paper 7.8.R
0759		 NUMERICAL STUDY OF MEDIUM-WEIGHT UAV AERODYNAMIC CHARACTERISTICS DURING APPROACH AND RECOVERY TO JUAN CARLOS/CANBERRA CLASS LHDS
M. J Ericksen, The University of Sydney, Australia
8.8Non 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 8.8.1
0895		 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 8.8.2
0861		 ULTRASONIC NON-DESTRUCTIVE TESTING: SYSTEM SELECTION FOR CHARACTERISATION AND DETECTION OF DEFECTS IN REPAIRED COMPOSITE MATERIALS
H.R Spratling, Defence Science and Technology Group, Australia
16. Sep 26 11:40 12:05 8.8.3
0776		 EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECTS ON TRANSPIRATION COOLING IN LATTICE POROUS MEDIA
J Jaeseung, KAIST, South Korea
16. Sep 26 12:05 12:30 8.8.4
0127		 EXPERIMENTAL INVESTIGATION OF FRETTING WEAR IN TI6-AL-4V DOVETAIL ASSEMBLIES UNDER RESONANT VIBRATION
X.-Z. Zhang, Beihang University School of Energy and Power Engineering, China
Reserve Paper 8.8.R
0313		 ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS
R. Degenhardt, DLR, Germany
Reserve Paper 8.8.R
0656		 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
9.8Flutter
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
16. Sep 26 10:50 11:15 9.8.1
0627		 A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY
W. Qian, Dalian University of Technology, China
16. Sep 26 11:15 11:40 9.8.2
0887		 FLUTTER RESPONSE OF NOZZLE AFT DECK IN UNSTEADY ACCELERATING FLOW CONDITIONS
Haibo Zheng, Northwestern Polytechnical University, China
16. Sep 26 11:40 12:05 9.8.3
0566		 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 9.8.4
0620		 TIME-VARYING AEROELASTIC MODELING AND FLUTTER ANALYSIS OF TELESCOPIC WINGS
C. Li, China
Reserve Paper 9.8.R
0356		 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) 9.8.R
0179		 FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING
Z.-Y. Xi, Beihang University, China
additional information (interactive) 9.8.R
0494		 MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION
C. -Z. Zhao, Northwestern Polytechnical University, China
10.8Propellers, Compressors and Turbines 1
Chair(s): ,
Track 10
05 - Propulsion and Energy
16. Sep 26 10:50 11:15 10.8.1
0261		 CONCEPTUAL PERFORMANCE AND MASS ASSESSMENT OF AN OPEN FAN ENGINE FOR A SHORT-MEDIUM RANGE AIRCRAFT
P. Wehrel, German Aerospace Center (DLR), Germany
16. Sep 26 11:15 11:40 10.8.2
0712		 SURROGATE-BASED OPTIMIZATION OF AIRCRAFT PROPELLER PERFORMANCE USING A HIGH-FIDELITY AND EFFICIENT RANS FRAMEWORK
A W Stuermer, DLR, Germany
16. Sep 26 11:40 12:05 10.8.3
0084		 FEASIBILITY OF ELECTRIC DUCTED FANS TO REPLACE OPEN PROPELLERS ON AN ELECTRIFIED TRAINING AIRCRAFT
Keith F. Joiner, University of New South Wales, Australia
16. Sep 26 12:05 12:30 10.8.4
0690		 FLIGHT-DATA-DRIVEN PHYSICS-INFORMED COMPONENT MAP DERIVATION WITH STRUCTURAL COMPLIANCE
Y. Liu, Northwestern Polytechnical University, China
Reserve Paper 10.8.R
0500		 ENHANCED T-MATS MODELING OF COMPRESSOR SURGE AND STALL DYNAMICS USING THE MOORE-GREITZER FRAMEWORK
Huy Nguyen, Viettel Aerospace Institute, Vietnam
11.8System identification
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 26 10:50 11:15 11.8.1
0176		 SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION
E Kim, Chungnam National University, South Korea
16. Sep 26 11:15 11:40 11.8.2
0361		 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 11.8.3
0633		 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 11.8.4
0742		 WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING
Y. He, China
Reserve Paper 11.8.R
0344		 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 11.8.R
0680		 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
12.8CRM-HL 1
Chair(s): , , Imamura, T.
Track 12
03.2 - Experimental Aerodynamics
16. Sep 26 10:50 11:15 12.8.1
0793		 A COMPARATIVE WMLES STUDY OF THE CRM-HL IN FREE-AIR AND IN THE NTF FACILITY
C. B. Sousa, United States
16. Sep 26 11:15 11:40 12.8.2
0256		 AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMISPAN CRM-HL AT THE JAXA 6.5M X 6.5M LOW SPEED WIND TUNNEL
M. Kohzai, JAXA, Japan
16. Sep 26 11:40 12:05 12.8.3
0328		 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
13.8Optimizing AAM Networks
Chair(s): ,
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
16. Sep 26 10:50 11:15 13.8.1
0587		 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 13.8.2
0325		 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 13.8.3
0103		 SCHEDULING AND ROUTING FOR TIMETABLE-BOUND URBAN AIR MOBILITY OPERATIONS
A. Edsel, Purdue University, United States
16. Sep 26 12:05 12:30 13.8.4
0802		 ESTIMATION AND ANALYSIS OF RNP REQUIREMENTS FOR HETEROGENEOUS UAM CONFIGURATIONS: INSIGHTS FROM K-UAM GRAND CHALLENGE OPPAV DEMONSTRATION
J. Lee, Korea Aerospace Research Institute (KARI), South Korea
Reserve Paper 13.8.R
0958		 WHAT UAM CNS NEEDS AND WHAT IT COSTS: AN EXPERT SURVEY
FN Naeem, TUHH, Germany
additional information (interactive) 13.8.R
0900		 OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES
A. Tiwari, Indian Institute of Technology Bombay, India
14.8Multidisciplinary 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 14.8.1
0195		 AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS
D. Skrna, TU Wien, Austria
16. Sep 26 11:15 11:40 14.8.2
0755		 PREDICTION OF BOUNDARY LAYER TRANSITION FOR SUPERSONIC CIVIL AIRCRAFT BASED ON NEURAL NETWORK
S.H. Yu, China
16. Sep 26 11:40 12:05 14.8.3
1001		 ON THE GROUND AND IN FLIGHT: AERODYNAMIC AND AEROELASTIC TESTING SUPPORTING INNOVATION IN AERONAUTICS
C. Mertens, Royal Netherlands Aerospace Centre, Netherlands
Presenter: Christoph Mertens, Royal Netherlands Aerospace Centre
16. Sep 26 12:05 12:30 14.8.4
1002		 UNDERSTANDING HYPERSONIC BOUNDARY LAYER LAMINAR TO TURBULENT TRANSITION IN WIND TUNNEL ENVIRONMENT
M. Lugrin, France
15.8Education enablers
Chair(s): ,
Track 15
14 - Education and Training
16. Sep 26 10:50 11:15 15.8.1
0453		 PREPARING AERONAUTICAL ENGINEERING UNDERGRADUATES FOR WORKING IN GLOBAL TEAMS
J. Abulawi, HAW Hamburg, Germany
16. Sep 26 11:15 11:40 15.8.2
0549		 REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR
K Ramotsabi, CSIR, South Africa
16. Sep 26 11:40 12:05 15.8.3
0718		 AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME
N. Moser, Germany
16. Sep 26 12:05 12:30 15.8.4
0933		 EDUCATION-ORIENTED MODEL-BASED SYSTEMS ENGINEERING FOR AERONAUTICAL ENGINEERING TRAINING AND INNOVATION
L. H. J. Machado, UFMG, Brazil
Reserve Paper 15.8.R
0436		 DESIGNING AND DELIVERING A NEW PROJECT-BASED CAPSTONE AIRCRAFT DEVELOPMENT COURSE
S.J. van Heerden, University of Glasgow, United Kingdom
additional information (interactive) 15.8.R
0380		 INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION
C. Varriale, TU Delft, Netherlands

12:30 - 13:30LUNCH BREAK

0.9GENERAL LECTURE 4 Aeronautics Outlook -the Director\'s Cut
Chair:
16. Sep 26 13:30 15:15

15:15 - 15:40AFTERNOON BREAK

1.9ECSC pitch session
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
2.9Shaping 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 2.9.1
1014		 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 2.9.2
1013		 PRACTICAL INNOVATION IN AEROSPACE
D. Donovan, United States
16. Sep 26 16:30 16:55 2.9.3
1015		 AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH
S. Kumar, United States
16. Sep 26 16:55 17:20 2.9.4
1016		 A MULTI-FUEL PROPULSION SYSTEM STRATEGY FOR AVIATION TRANSPORT RESILIENCE
I. Orisamolu, United States
3.9Case Studies 2
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
16. Sep 26 15:40 16:05 3.9.1
0746		 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 3.9.2
0346		 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 3.9.3
0552		 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 3.9.4
0466		 STUDY ON INDUCED DRAG CALCULATION FOR BIRD-LIKE WINGTIP SLOTS USING WAKE-PLANE INTEGRATION
Xia-Ru?X.-R. Liu, Northwestern Polytechnical University, China
4.9Unconventional 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 4.9.1
0055		 MODELING & PRELIMINARY ANALYSIS OF AN ECOFRIENDLY AIRBORNE GLOBAL LUXURY EKRANOPLAN
M.K.V. Sankrithi, RIC Enterprises, United States
16. Sep 26 16:05 16:30 4.9.2
0407		 TECHNOLOGY OPPORTUNITIES FOR CIVIL BLENDED WING BODY AIRCRAFT
J. R. O'Doherty-Jennings, Aerospace Technology Institute, United Kingdom
16. Sep 26 16:30 16:55 4.9.3
0643		 LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY
K. Abu Salem, University of Trento, Italy
16. Sep 26 16:55 17:20 4.9.4
0960		 PROPOSING A STABLE LIFTING FUSELAGE FOR AN AIRLINER OF THE IDEAL AIRCRAFT CONFIGURATION
Reinhard Joachim Huyssen, CSIR, South Africa
Reserve Paper 4.9.R
0419		 BIOMIMICRY: INSPIRATION FOR NEXT-GENERATION AIRCRAFT
N J Wood, Macromia Aviation Ltd, United Kingdom
5.9Aerodynamic Optimization
Chair(s): Prince, S., Zingg, D.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 15:40 16:05 5.9.1
0052		 WIND TURBINE AERODYNAMIC SHAPE OPTIMIZATION BASED ON A DISCRETE ADJOINT APPROACH
L. Olichevis Halila, PUCPR, Brazil
16. Sep 26 16:05 16:30 5.9.2
0105		 CONTINUOUS UNSTEADY ADJOINT VARIATIONAL MULTISCALE METHOD FOR AIRFOILS SHAPE OPTIMIZATION
C. Brunelli, Royal Military Academy, Belgium
16. Sep 26 16:30 16:55 5.9.3
0120		 SIMULATION OF AERODYNAMIC GROUND EFFECT FOR TILTED PROPELLERS USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S Shahjahan, Siemens Digital Industries Software Inc., United States
Presenter: Shahfiq Shahjahan, Siemens Digital Software Industries Software Inc.
16. Sep 26 16:55 17:20 5.9.4
0061		 A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS
L. Olichevis Halila, PUCPR, Brazil
Reserve Paper 5.9.R
0089		 OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT
Dong Xue¹, Jian-Lin Xuan¹; ¹Northwestern Polytechnical University, China
Reserve Paper 5.9.R
0812		 A NOVEL POLYTROPIC POROUS ZONE APPROACH FOR EFFICIENT AEROTHERMAL FLOW SIMULATIONS: A FIRST APPLICATION TO COMPLEX HEAT EXCHANGERS
J. Inkoferer, University of the Bundeswehr Munich, Germany
additional information (interactive) 5.9.R
0704		 META-HEURISTIC AIRFOIL OPTIMIZATION OF VARIABLE-PITCH LIFTING SURFACES
S. J. Jain, Delhi Technological University, India
additional information (interactive) 5.9.R
0862		 OPTIMIZATION OF GEOMETRIC PARAMETERS FOR STRAIGHT-THROUGH LABYRINTH SEALS USING ORTHOGONAL EXPERIMENT AND CFD DATA-DRIVEN NEURAL NETWORK SURROGATE MOD
L.-X.-L Li, China
additional information (interactive) 5.9.R
0909		 SCALABLE HIGH-FIDELITY AERODYNAMIC CHARACTERIZATION OF WIG CRAFT USING NON-SEQUENTIAL RBF SURROGATES
N-D Diaz, ITA, Brazil
6.9AI 2
Chair(s): ,
Track 6
15 - Guest lectures (by personal invitation only)
7.9Aerodynamics of Unconventional Aircraft Configurations
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
16. Sep 26 15:40 16:05 7.9.1
0122		 AERODYNAMIC OPTIMIZATION DESIGN OF FULL-WING SOLAR-POWERED UAV FOR FLOW SEPARATION CONTROL
J.-W. Wang, Northwestern Polytechnical University, China
16. Sep 26 16:05 16:30 7.9.2
0295		 STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS
C. Zheng, Beihang University, China
16. Sep 26 16:30 16:55 7.9.3
0318		 AERODYNAMIC SHAPE OPTIMIZATION OF A FUEL-CELL POWERED FLYING WING CONCEPT
P. Kirschnek, FH JOANNEUM GesmbH, Austria
16. Sep 26 16:55 17:20 7.9.4
0866		 AERODYNAMIC FEASIBILITY OF A NOVEL SWIVEL ROTOR ARCHITECTURE
B.I. Soemarwoto, Royal Netherlands Aerospace Centre NLR, Netherlands
Reserve Paper 7.9.R
0841		 DEVELOPMENT OF HYDROPHILIC COATINGS FOR PRACTICAL APPLICATION OF LAMINAR FLOW WINGS
H Iijima, Japan Aerospace Exploration Agency, Japan
additional information (interactive) 7.9.R
0171		 FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES
K.-Q. Qiao, Beihang University, China
additional information (interactive) 7.9.R
0392		 UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND STABILITY ANALYSIS
J. Guo, United Kingdom
8.9Turbomachinery Structures
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
16. Sep 26 15:40 16:05 8.9.1
0225		 DESIGN ASSESSMENT OF A HELICOPTER BLADE
C.P. Pagwiwoko, SYOS Aerospace, New Zealand
16. Sep 26 16:05 16:30 8.9.2
0019		 CYCLOSTATIONARY ANALYSIS FOR CRACK DETECTION AND TRENDING IN HELICOPTER GEARBOX CASING
N Sawalhi, Defence Science and Technology Group (DSTG), Australia
16. Sep 26 16:30 16:55 8.9.3
0471		 ANALYSIS OF CRACK GROWTH CHARACTERISTICS OF HOLE CORNER CRACKS IN EXPANDED FILM COOLING HOLES ON TURBINE BLADE FLANGES
N/A Yan, Beihang University, China
9.9Aeroelastic Analysis & Design 1
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
16. Sep 26 15:40 16:05 9.9.1
0448		 AEROELASTIC TAILORING FOR COMPOSITE ADAPTIVE WINGLETS
N. Tsushima, Kyushu University, Japan
16. Sep 26 16:05 16:30 9.9.2
0326		 PARAMETRIC AEROELASTIC STUDY OF WINGLET GEOMETRY USING VORTEX LATTICE METHOD FOR FUTURE PASSIVE MORPHING APPLICATIONS
M.N.-A. Kouchlef, The University of Tokyo, Japan
16. Sep 26 16:30 16:55 9.9.3
0342		 AEROELASTIC DESIGN OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT IN AN MDO FRAMEWORK
C. Mollet, ONERA, France
16. Sep 26 16:55 17:20 9.9.4
0277		 MANEUVER LOAD ALLEVIATION OF THE DRY WING FOR HYDROGEN AIRCRAFT
F. Yu, Technical University of Munich, Germany
Reserve Paper 9.9.R
0814		 DYNAMICS MODELING AND EXPERIMENTAL VERIFICATION OF ROTOR WITH COMPLEX THREE-DIMENSIONAL SHAPE BLADE
J.H Huang, China
Reserve Paper 9.9.R
0974		 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
10.9Propellers, Compressors and Turbines 2
Chair(s): ,
Track 10
05 - Propulsion and Energy
16. Sep 26 15:40 16:05 10.9.1
0813		 MODULAR JET AND PROPELLER ENGINE – PART I: INITIAL STUDIES
T. Otten, German Aerospace Center (DLR), Germany
16. Sep 26 16:05 16:30 10.9.2
0829		 MODULAR JET AND PROPELLER ENGINE –– PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT
T. Matuschek, German Aerospace Center (DLR), Germany
16. Sep 26 16:30 16:55 10.9.3
0334		 INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY
L. Oberthür, University of the Bundeswehr Munich, Germany
16. Sep 26 16:55 17:20 10.9.4
0768		 INITIAL GEOMETRIC UNCERTAINTY ASSESMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD
K. Omoto, Osaka Metropolitan University, Japan
11.9Guidance and flight trajectory control 2
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 26 15:40 16:05 11.9.1
0534		 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 11.9.2
0588		 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 11.9.3
0805		 DUAL BEZIER SPACE-TIME OPTIMIZATION UNDER HARD OBSERVATION-WINDOW CONSTRAINTS: A FEASIBILITY-ORIENTED JERK-CAP COMPARISON
H Kim, Kookmin University, South Korea
16. Sep 26 16:55 17:20 11.9.4
0858		 OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL
S.Y Kim, Chungbuk National University, South Korea
12.9Robot Manufacturing and Assembly Technology
Chair(s): Guevara, E.
Track 12
08 - Manufacturing and Supply Chain Management
16. Sep 26 15:40 16:05 12.9.1
0058		 GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY
MT Tatar, Boeing, United States
16. Sep 26 16:05 16:30 12.9.2
0080		 EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE
I.F. Frascareli Ali, Embraer S.A., Brazil
16. Sep 26 16:30 16:55 12.9.3
0198		 VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL
A Teixeira Ferraz, Brazil
16. Sep 26 16:55 17:20 12.9.4
0741		 MIXED REALITY-BASED PROGRAMMING BY DEMONSTRATION FOR ROBOTIC GRINDING OF AERO-ENGINE BLADES
Y. Liu, Chongqing University, China
13.9Strategic 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 13.9.1
0150		 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 13.9.2
0580		 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 13.9.3
0672		 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 13.9.4
0897		 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 13.9.R
0905		 ADVANCING TELE-OPERATION IN URBAN AIR MOBILITY: A STRATEGY LEVERAGING DIGITAL TWIN TECHNOLOGY
LV Nguyen, Konkuk University, South Korea
additional information (interactive) 13.9.R
0538		 A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS
X. Minze, Beihang University, China
14.9Emerging 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 14.9.1
0871		 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 14.9.2
0901		 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 14.9.3
0932		 METHODOLOGY AND V1 PROTOTYPE OF AN ADAPTIVE/ADAPTABLE MULTI-UAV GCS HMI IN A FLOOD SAR CO-SIMULATION TESTBED
A. G. P. Sarmento, Aeronautics Institute of Technology (ITA), Brazil
16. Sep 26 16:55 17:20 14.9.4
0947		 A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS
R.F Viana, Aeronautics Institute of Technology, Brazil
15.9Condition based maintenance
Chair(s): Scott, M.
Track 15
11 - Operations and Sustainment
16. Sep 26 15:40 16:05 15.9.1
0738		 EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION
V Kekoc, Defence Science & Technology Group, Australia
16. Sep 26 16:05 16:30 15.9.2
0770		 AI-BASED MAINTENANCE CODE CORRECTION FOR RELIABLE MTBF ANALYSIS
K. Minyoung, Korea Aerospace Industries, LTD, South Korea
16. Sep 26 16:30 16:55 15.9.3
0027		 V-MODEL-BASED DEVELOPMENT OF A SPATIOTEMPORAL AIRFRAME CORROSION DIGITAL TWIN
W.Y. Chia, RMIT University, Australia
16. Sep 26 16:55 17:20 15.9.4
0573		 PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING
L.J. Jilke, German Aerospace Center (DLR), Germany
Reserve Paper 15.9.R
0908		 REDUCING OPERATIONAL DISRUPTION: DECISION-AUTOMATION FOR CBM UNDER UNCERTAINTY
F Enayatollahi, Mount Royal University, Canada
additional information (interactive) 15.9.R
0010		 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) 15.9.R
0264		 PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE ? -PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE
L. Hou, Nanjing University of Aeronautics and Astronautics, China

0.10SPEED MENTORING
Chair:
16. Sep 26 17:20 19:00

Thursday, 17. Sep 2026

0.11GENERAL LECTURE 5 ISABE and the next generation of aircraft propulsion
Chair:
17. Sep 26 08:00 08:50

08:50 - 09:15COFFEE BREAK

1.10Explainable and Human?Centered AI in Aviation
Chair(s): Toebben, H.
Track 1
15 - Guest lectures (by personal invitation only)
17. Sep 26 09:15 09:40 1.10.1
0177		 EXPLAINABILITY AT ALL LEVELS OF SYSTEM DEVELOPMENT: INSIGHTS FROM THE DESIGN OF INTELLIGENT SYSTEMS IN AVIATION
J Wuerfel, German Aerospace Center (DLR), Germany
17. Sep 26 09:40 10:05 1.10.2
0359		 APPLYING HUMAN-CENTERED DESIGN: A PRACTICAL CASE STUDY OF A PILOT DIGITAL ASSISTANT
A. Mayima, Penrose Business Centre, Ireland
17. Sep 26 10:05 10:30 1.10.3
0450		 OFFLINE MULTIMODAL LARGE LANGUAGE MODELS FOR DECISION SUPPORT IN AIR OPERATIONS
J. Dantas, Instituto de Estudos Avançados, Brazil
17. Sep 26 10:30 10:55 1.10.4
0547		 AI IN THE COCKPIT, A JARVIS STORY
R. De Masellis, Collins Aerospace, Ireland
2.10Failures
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.10Military
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 09:15 09:40 3.10.1
0155		 AERODYNAMIC SHAPE OPTIMISATION USING A STRUCTURAL MODAL PARAMETERISATION METHOD
A. R. Wang, Boeing Aerostructures Australia, Australia
17. Sep 26 09:40 10:05 3.10.2
0201		 MODELLING COUPLED ON-BOARD SYSTEMS AND THEIR TOP-LEVEL IMPACT ON FIGHTER AIRCRAFT DESIGN
E. Espinosa-Juárez, Linköping University, Sweden
17. Sep 26 10:05 10:30 3.10.3
0485		 MULTI-FIDELITY BAYESIAN NEURAL NETWORKS FOR STEALTH/AERODYNAMIC DATA FUSION METHOD
J. He, China
17. Sep 26 10:30 10:55 3.10.4
0515		 FAST INTEGRATED EVALUATION AND OPTIMIZATION DESIGN METHOD FOR AERODYNAMIC AND STEALTH PERFORMANCE OF INLETS WITH ENTRANCE GRIDS
J.-W. He, Northwestern Polytechnical University, China
Reserve Paper 3.10.R
0421		 CONCEPTUAL DESIGN AND AERODYNAMIC ANALYSIS OF A GENERIC FUTURE FIGHTER AIRCRAFT
P.-D. Bravo-Mosquera, EESC-USP, Brazil
4.10Configuration/Aero/Aerothermal/Flight-Performance
Chair(s): ,
Track 4
15 - Guest lectures (by personal invitation only)
5.10Propeller Aerodynamics and Rotor Flows
Chair(s): , , Kiszkowiak, L.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 09:15 09:40 5.10.1
0375		 AERODYNAMICS OF OPEN FAN INTEGRATION FOR THE DLR-25 CONCEPT
I.J. Pawlikow, DLR, Germany
17. Sep 26 09:40 10:05 5.10.2
0761		 STUDY OF THE AERODYNAMIC INTERFERENCE OF STRUT-BRACED WINGS WITH DISTRIBUTED PROPELLERS
n/a Fossati, Unniversity of Strathclyde, United Kingdom
17. Sep 26 10:05 10:30 5.10.3
0654		 UNSTEADY EXERGY ANALYSIS OF A HIGHLY LOADED HIGH-SPEED ROTOR UNDER ROTATING STALL
C Paillard, ISAE-SUPAERO, France
17. Sep 26 10:30 10:55 5.10.4
0795		 COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM
J.-W He, Northwestern Polytechnical University, China
Reserve Paper 5.10.R
0352		 INVESTIGATION AND ONE-DIMENSIONAL MODELING OF THE DUAL-ROTOR GEROTOR PUMP AT HIGH ALTITUDES
SZC Su, Northwestern Polytechnical University, China
6.10Advanced measurement technique
Chair(s): Moreau, D., Allen, N.
Track 6
03.2 - Experimental Aerodynamics
17. Sep 26 09:15 09:40 6.10.1
0133		 COMPARATIVE ATMOSPHERIC MEASUREMENTS USING UAV-MOUNTED ULTRASONIC ANEMOMETER AND DOPPLER LIDAR
N Gavrilovic, ISAE-SUPAERO, France
17. Sep 26 09:40 10:05 6.10.2
0749		 CONCURRENT UNSTEADY SURFACE PRESSURE FIELD AND SCHLIEREN MEASUREMENTS OF THE COMMON FRONT END HYPERSONIC GEOMETRY IN TRANSONIC CONDITIONS
C.W Marshall, Defence Science and Technology Group, Australia
17. Sep 26 10:05 10:30 6.10.3
0317		 FFECT OF THE FST ON THE BOUNDARY LAYER, THE WALL-PRESSURE FLUCTUATIONS, AND THE TRAILING-EDGE NOISE OF AIRFOILS
L Botero-Bolivar, Universidad Industrial de Santander, Colombia
additional information (interactive) 6.10.R
0775		 ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM
D.-T Rajeepan, School of Aerospace, Mechanical and Mechatronics Engineering, Australia
7.10Flight Dynamics and Control
Chair(s): , , Grabowski, T.
Track 7
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 09:15 09:40 7.10.1
0435		 SIMULATION-BASED AUTOPILOT TUNING FOR FIXED-WING UAVS
C.-V. Boruga, Linkoping University, Sweden
17. Sep 26 09:40 10:05 7.10.2
0713		 A 3D-PRINTED TESTBED FOR FLIGHT CONTROL SYSTEM RESEARCH.
D Lundström, Sweden
17. Sep 26 10:05 10:30 7.10.3
0138		 SLIPSTREAM MODELING AND CONTROL ALLOCATION OF A DISTRIBUTED HETEROGENEOUS ELECTRIC PROPULSION TANDEM-WING UAV
Y.-H. Xie, China
17. Sep 26 10:30 10:55 7.10.4
0815		 RESEARCH ON FLIGHT DYNAMICS AND CONTROL CHARACTERISTICS OF MULTI-UAVS WINGTIP-LINKED FLIGHT
R. Wang, Northwestern Polytechnical University, P.R.China, China
Reserve Paper 7.10.R
0259		 EXPERIMENTAL FLIGHT DYNAMICS AND CONTROL OF AN AGILE FIXED-WING UAV USING HYBRID ONBOARD & OFFBOARD CONTROL
Y. Huang, the University of Sydney, Australia
Reserve Paper 7.10.R
0417		 MODEL-PREDICTIVE-CONTROL-BASED TRAJECTORY GENERATION ENHANCED WITH REINFORCEMENT LEARNING FOR FORMATION MANEUVERING
A. Rossi, Airbus Defence and Space GmbH, Germany
8.10Material Properties & Certifications
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
17. Sep 26 09:15 09:40 8.10.1
0173		 STRENGTH DESIGN AND TEST VERIFICATION OF AIRCRAFT SUSPENSION TRACK CONNECTION ZONE
K. Yin, China
17. Sep 26 09:40 10:05 8.10.2
0181		 INTERNATIONAL RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION
R. Degenhardt, DLR, Germany
17. Sep 26 10:05 10:30 8.10.3
0323		 DIGITAL-PHYSICAL SYNERGY: FEM-DRIVEN CERTIFICATION OF AT-5 AND AT-6 AIRCRAFT
M. Kowalski, Warsaw University of Technology, Poland
9.10Aeroelastic Analysis & Design 2
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
17. Sep 26 09:15 09:40 9.10.1
0141		 AN AEROELASTIC DYNAMICS MODELING METHOD FOR INSECT-INSPIRED FLEXIBLE FLAPPING-WING UAV
Y Guo, Northwestern Polytechnical University, China
17. Sep 26 09:40 10:05 9.10.2
0381		 ENABLING FORWARD SWEPT WING DESIGNS
J E Cooper, University of Bristol, United Kingdom
17. Sep 26 10:05 10:30 9.10.3
0452		 DEVELOPMENT OF CONTROL LAWS FOR ENHANCED PERFORMANCE AND AEROELASTIC STABILITY OF EVTOL AIRCRAFT
P. Kantzidis, RMIT University, Australia
17. Sep 26 10:30 10:55 9.10.4
0262		 AEROSERVOELASTIC MODELING AND ANALYSIS OF THRUST VECTORING LAUNCH VEHICLE CONSIDERING RIGID-ELASTIC INTERACTION
W. Weili, China
Reserve Paper 9.10.R
0973		 AEROELASTIC TAILORING OF A SBW USING AFP TOW STEERED COMPOSITES
T. Huang, Khalifa University, United Arab Emirates
10.10Hydrogen Propulsion Concepts
Chair(s): ,
Track 10
05 - Propulsion and Energy
17. Sep 26 09:15 09:40 10.10.1
0275		 ADVANCING CRYOGENIC COOLING AND ELECTRICAL DISTRIBUTION SYSTEMS FOR FUTURE HYDROGEN-POWERED AVIATION
D. Kierbel, AIRBUS NL, Netherlands
17. Sep 26 09:40 10:05 10.10.2
0299		 EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS
F. Thilker, FH JOANNEUM GesmbH, Austria
17. Sep 26 10:05 10:30 10.10.3
0338		 REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION
G. Marinaro¹, L. Garbarino¹, M. Inverno¹, C. Serpico¹, A. Bono¹, G. Malaponte¹, A. Pagano¹; ¹Italian Research Centre - CIRA, Italy
17. Sep 26 10:30 10:55 10.10.4
0574		 HEAT EXCHANGER MODELLING METHODS FOR HYDROGEN POWERED AERO ENGINES DURING THERMODYNAMIC CYCLE DESIGN
F.-H. Görtz, German Aerospace Center, Germany
Reserve Paper 10.10.R
0954		 AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES
F. Pak, Eindhoven University of Technology, Netherlands
11.10Flight testing
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 09:15 09:40 11.10.1
0624		 PHYSICS-INFORMED LSTM-BASED LONGITUDINAL STALL AEROFYNAMIC MODELING FRAMEWORK OF CIVIL AIRCRAFT USING FLIGHT TEST DATA
J.-W. Wang, Beihang University, China
17. Sep 26 09:40 10:05 11.10.2
0719		 AERO–PROPULSIVE MODELING AND PRELIMINARY FLIGHT TESTING OF INDIVIDUAL THRUST CONTROL FOR A DISTRIBUTED ELECTRIC PROPULSION DEMONSTRATOR
G.F. Filippoli, Politecnico di Milano, Italy
17. Sep 26 10:05 10:30 11.10.3
0686		 PHYSICS-INFORMED MACHINE LEARNING FOR FLIGHT DYNAMICS IDENTIFICATION OF THE SAAB 340 USING FLIGHT TEST DATA
M Alam, Cranfield University, United Kingdom
17. Sep 26 10:30 10:55 11.10.4
0518		 EVALUATION OF STALL BEHAVIOUR OF T-TAIL AIRCRAFT: MODELING AND FLIGHT TEST
MH Lowenberg, University of Bristol, United Kingdom
Reserve Paper 11.10.R
0642		 HANDLING QUALITIES ASSESSMENTS IN A FIXED-BASED AND FULL FLIGHT SIMULATOR FOR A FLEXIBLE TRANSPORT AIRCRAFT
B. Boche, Berlin Institute of Technology, Germany
12.10Advanced Aircraft Design and Manufacturing
Chair(s): ,
Track 12
08 - Manufacturing and Supply Chain Management
17. Sep 26 09:15 09:40 12.10.1
0260		 MATERIAL-STRUCTURE INTEGRATED LASER ADDITIVE MANUFACTURING OF HIGH-PERFORMANCE PARTS FOR AERONAUTICAL APPLICATIONS
D.D. Gu, Nanjing University of Aeronautics and Astronautics, China
17. Sep 26 09:40 10:05 12.10.2
0327		 RESEARCH ON A DIGITAL-DRIVEN LIFE-CYCLE SUPPLY CHAIN MANAGEMENT SYSTEM FOR COLLABORATIVE AIRCRAFT DEVELOPMENT
J. Chai, AVIC The First Aircraft Institute, , China
17. Sep 26 10:05 10:30 12.10.3
0840		 RE-THINKING END OF LIFE AIRCRAFT INTERIORS THROUGH CO-DESIGN AND REPURPOSING
TJH Mahr, University of Melbourne, Australia
17. Sep 26 10:30 10:55 12.10.4
0945		 A FORMALLY VERIFIED, EVENT-DRIVEN ROS SCADA SUPERVISORY SYSTEM ARCHITECTURE FOR SAFETY-CRITICAL ROBOTIC CELLS IN AEROSPACE MANUFACTURING
F. S. Braga, Aeronautics Institute of Technology (ITA), Brazil
13.10Global Airport and Network Operations
Chair(s): Mori, R.
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
17. Sep 26 09:15 09:40 13.10.1
0329		 FEASIBILITY STUDY ON LANDING CAPACITY ENHANCEMENT AT CONGESTED AIRPORTS VIA ARRIVAL TRAJECTORY ANALYSIS
R. Kajikawa, Graduate School of Systems Design, Tokyo Metropolitan University, Japan
17. Sep 26 09:40 10:05 13.10.2
0272		 AN AUGMENTED AIRPORT MODEL FOR GROUND OPERATIONS ANALYSIS: A CASE STUDY OF NARITA INTERNATIONAL AIRPORT
S. X. Ng, The University of Tokyo, Japan
17. Sep 26 10:05 10:30 13.10.3
0412		 A COMPARISON OF TRAJECTORY-BASED OPERATIONS IN UNITED STATES AND EUROPE IN SUPPORT OF GLOBAL HARMONIZATION
G Enea, MIT Lincoln Laboratory, United States
17. Sep 26 10:30 10:55 13.10.4
0560		 AVIATION NETWORK MODELLING IN THE CONTEXT OF SMALL ISLAND DEVELOPING STATES: CONSTRAINTS, LIMITATIONS AND OPPORTUNITIES FOR AVIATION IN FIJI
P.F.D. Bowes, Australia
Reserve Paper 13.10.R
0227		 ATTRIBUTION OF ATFM DELAY AS A RESULT OF A GROUND DELAY PROGRAM (GDP)
C.A. Tait, Airservices Australia, Australia
14.10MBSE - Model based Systems Engineering
Chair(s): , , Wiels, V.
Track 14
02 - Systems Engineering and Integration
17. Sep 26 09:15 09:40 14.10.1
0399		 PROPAGATING SAFETY ASSESSMENT RESULTS FOR SYSTEM ARCHITECTURE CANDIDATES IN MBSE
S. M. Lübbe, German Aerospace Center (DLR), Germany
17. Sep 26 09:40 10:05 14.10.2
0674		 MODEL-BASED FUNCTIONAL HAZARD ASSESSMENT BASED ON ARP4761A USING SYSML V1 AND SYSML V2
M. Schäfer, German Aerosapce Center (DLR), Germany
17. Sep 26 10:05 10:30 14.10.3
0913		 ARCADIA VIEWPOINTS FOR ENTERPRISE ARCHITECTING COMPARISON WITH UAF VIEWS THROUGH AN EVTOL COMPANY OPERATION MODELING
R.M. Machado Cezar, Technological Institute of Aeronautics (ITA), Brazil
17. Sep 26 10:30 10:55 14.10.4
0959		 MANEUVER- AND DELAY-ROBUST DISTRIBUTED SATELLITE SSA VIA SPATIO-TEMPORAL GRAPH FORECASTING
H.-M. Rizk, The University of Osaka, Japan
Reserve Paper 14.10.R
0917		 MODEL-BASED SYSTEMS ENGINEERING APPLICATION USING FLIGHT-TEST DATA FROM THE ACS-100 SORA AIRCRAFT
L. H. J. Machado, UFMG, Brazil
15.10Maintenance technologies
Chair(s): Anderson, K.
Track 15
11 - Operations and Sustainment
17. Sep 26 08:50 09:15 15.10.1
0803		 ON THE FEASIBILITY OF MACHINE LEARNING-BASED DETECTION OF AIRCRAFT LIGHTNING STRIKE RISK AREAS
E Yoshikawa, The University of Osaka, Japan
17. Sep 26 09:15 09:40 15.10.2
0716		 ONTOLOGY-BASED SENSOR HEALTH MONITORING: A DYNAMIC ONTOLOGY-BASED FAULT DETECTION AND CLASSIFICATION FOR TIMESERIES DATA
C. Klein, Deutsches Zentrum für Luft- und Raumfahrt, Germany
17. Sep 26 09:40 10:05 15.10.3
0244		 ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085
J. P Rogers, RMIT University, Australia
17. Sep 26 10:30 10:55 15.10.4
0159		 INFRARED AND GREEN FEMTOSECOND LASER PAINT STRIPPING ON AIRCRAFT COATINGS: EXPERIMENTAL AND NUMERICAL ASSESSMENT
S. Zhu, Western Sydney University, Australia
additional information (interactive) 15.10.R
0134		 LIGHTWEIGHT AND ROBUST REAL-TIME DETECTION SYSTEM FOR AIRCRAFT SKIN DEFECTS UNDER COMPLEX UAV INSPECTION CONDITIONS
Wenqing Yang¹, Jianlin Xuan¹; ¹Northwestern Polytechnical University, China

10:55 - 11:00CHANGEOVER BREAK

1.11Air transport resilience to climate change and weather hazards
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
17. Sep 26 11:00 11:25 1.11.1
0994		 COMBINED IMPACT OF JET STREAM AND TURBULENCE ON LONG-TERM TRANS-OCEANIC FLIGHT ROUTES
J.-H. Kim, Seoul National University, South Korea
17. Sep 26 11:25 11:50 1.11.2
0997		 PROGRESS IN AIRCRAFT-BASED METEOROLOGICAL OBSERVATIONS
T.F. Rahmes, The Boeing Company, United States
2.11Sharing the Air (Airspace)
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
17. Sep 26 11:00 11:25 2.11.1
0988		 A HOLISTIC APPROACH TO ENABLE ADVANCED AIR MOBILITY FOR REGIONAL, RURAL AND REMOTE AUSTRALIA
P Burka, Swinburne University of Technology, Australia
17. Sep 26 11:25 11:50 2.11.2
1017		 THE ROLE OF COMMUNITY ENGAGEMENT IN INTRODUCING UNMANNED AERIAL VEHICLE TECHNOLOGY: A RAPID SCOPING REVIEW
J. Porter, Australia
3.11Aerostructures
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 11:00 11:25 3.11.1
0042		 ROBUST HIGH-FIDELITY DATASET-BASED AEROELASTIC OPTIMIZATION FOR AIRCRAFT DESIGN
M. Maier¹, K. Sørensen-Libik², Ö. Petersson², C. Breitsamter¹; ¹Technical University of Munich (TUM), Germany ;²Airbus Defence and Space GmbH, Germany
17. Sep 26 11:25 11:50 3.11.2
0925		 LARGE-SCALE AEROSTRUCTURAL OPTIMISATION WITH MODAL AND NONLINEAR BUCKLING CONSTRAINTS ASSISTED BY ALGORITHMIC DIFFERENTIATION
L Scalia, Universidad Carlos III de Madrid, Spain
17. Sep 26 11:50 12:15 3.11.3
0034		 MULTI-OBJECTIVE OPTIMISATION OF AERIAL VEHICLES USING REINFORCEMENT LEARNING
T Batty, Defence Science and Technology Group, Department of Defence, Australia
17. Sep 26 12:15 12:40 3.11.4
0100		 INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING
Y. Ma, Northwestern Polytechnical University, China
Reserve Paper 3.11.R
0609		 COMPARISON OF CONFIGRATIONS FOR FLEXIBLE AIRCRAFT USING AEROELASTIC ANALYSIS
N.O. Okubo, The University of Tokyo, Japan
4.11CFD Needs and Progress Towards Vision 2030 & Beyond
Chair(s): Cary, A., Azevedo, J.
Track 4
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 11:00 11:25 4.11.1
0998		 CFD VISION 2030 PROGRESS AND NEXT STEPS
J. P. Slotnick, United States
17. Sep 26 11:25 11:50 4.11.2
1000		 GEOMETRY AND MESHING ADVANCEMENTS TOWARD CFD VISION 2030
N. J. Wyman, Cadence Design Systems, Inc., United States
17. Sep 26 11:50 12:15 4.11.3
0999		 CFD VISION 2030 LOOKING FORWARD: PANEL DISCUSSION
A. W. Cary, United States
5.11UAS and AAM Design Applications
Chair(s): , , Lawson, N.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 11:00 11:25 5.11.1
0238		 SUPERIOR CRUISE EFFICIENCY OF A NOVEL EVTOL CONFIGURATION FEATURING INCLINED PROPELLERS AND A PARASOL WING
E. Shima¹, K. Yonezawa, CRIEPI, Japan; M. SATO, Kogakuin Univ., Japan; A. Oyama¹; ¹JAXA, Japan
Presenter: Eiji Shima
17. Sep 26 11:25 11:50 5.11.2
0196		 PREDICTION OF PROPELLER NOISE IN LOW REYNOLDS NUMBER OPERATION USING MACHINE LEARNING MODELS
M. de Rosa Jacinto, TU Wien, Austria
17. Sep 26 11:50 12:15 5.11.3
0280		 A COMPARATIVE STUDY OF THE AERODYNAMIC CHARACTERISTICS OF TWO CONFIGURATIONS
K. You, Northwestern Polytechnical University, China
Presenter: Kai You
17. Sep 26 12:15 12:40 5.11.4
0197		 INTEGRATION OF ACOUSTIC LINERS AND INTERNAL BYPASS CHANNELS INTO AAM PROPELLERS FOR NOISE REDUCTION
D. Skrna, TU Wien, Austria
Reserve Paper 5.11.R
0747		 RESEARCH ON AN AERODYNAMIC LOAD METHODOLOGY FOR FLAPPING WINGS BASED ON EXPERIMENTALLY ACQUIRED DEFORMATION
K.-Y. Yang, Northwestern Polytechnical University, China
additional information (interactive) 5.11.R
0558		 ARODYNAMIC COUPLING OF TYPICAL FORMATION CONFIGURATION
JY.-Z. Zhao, Northwestern Polytechnical University, China
6.11Flow seperation and control
Chair(s): Atkin, C., Gowree, E.
Track 6
03.2 - Experimental Aerodynamics
17. Sep 26 11:00 11:25 6.11.1
0203		 WIND-TUNNEL STATIC AND DYNAMIC TESTING OF A TRANSPORT AIRCRAFT MODEL IN-STALL AND POST-STALL FLIGHT REGIMES
D. Farcy, ONERA, France
17. Sep 26 11:25 11:50 6.11.2
0220		 SIDE JET-CROSSFLOW INTERACTION: PRESSURE DISTRIBUTION AND FLOW FIELD ANALYSIS IN SUBSONIC, TRANSONIC AND SUPERSONIC FLOW
B. Ilic, Military Technical Institute, Serbia
17. Sep 26 11:50 12:15 6.11.3
0763		 WATER TUNNEL EXPERIMENTS AND CFD ANALYSES OF A COMBAT AIRCRAFT WITH LEADING-EDGE VORTEX CONTROLLERS
?. P. Malicki, Wroc?aw University of Science and Technology , Poland
17. Sep 26 12:15 12:40 6.11.4
0410		 EXPERIMENTAL ASSESSMENT OF SIDE JET EFFECTS ON AERODYNAMIC FORCES AND MISSILE CONTROL IN SUBSONIC, TRANSONIC, AND SUPERSONIC FLOWS
M.-Dj Samardzic, Military Technical Institute (VTI), Serbia
Reserve Paper 6.11.R
0232		 EXPERIMENTAL INVESTIGATION OF WISHBONE VORTEX GENERATOR EFFECTS ON THE NACA 4412 AIRFOIL AT LOW REYNOLDS NUMBERS
D. Domínguez, Universidad de León, I4 Institute, Spain
additional information (interactive) 6.11.R
0427		 DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE.
E. Barroso, INTA, Spain
7.11Flight Simulation and Testing
Chair(s): , , Krus, P.
Track 7
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 11:00 11:25 7.11.1
0156		 FLIGHT TRIALS OF DRONES CONTROLLED BY AI LARGE LANGUAGE MODELS
S Crase, Australia
17. Sep 26 11:25 11:50 7.11.2
0204		 FAMILARIZATION, OPERATION AND DEBRIEFING: AN ADAPTIVE AUGMENTED REALITY SUPPORT SYSTEM FOR UAV FLIGHT TESTING
M. Zintl, Institute of Flight System Dynamics - Technical University of Mu, Germany
17. Sep 26 11:50 12:15 7.11.3
0513		 INFORMATIVE PATH PLANNING BASED ON REDUCED-RANK GAUSSIAN PROCESS FOR HAZARDOUS SUBSTANCE MONITORING
C.M lee, South Korea
17. Sep 26 12:15 12:40 7.11.4
0158		 SENSOR-DRIVEN CONTROL OF UAS UTILISING AI IN SIMULATION
S. R. Pywell, Australia
Reserve Paper 7.11.R
0289		 ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES
K. Thomessen, DLR (German Aerospace Center), Germany
8.11High-Temperature Materials/Structures
Chair(s): ,
Track 8
15 - Guest lectures (by personal invitation only)
9.11Student Final
Chair(s): Rein Weston, K.
Track 9
10.11Propulsion optimization 1
Chair(s): ,
Track 10
05 - Propulsion and Energy
17. Sep 26 11:00 11:25 10.11.1
0110		 NOVEL METHODS FOR THE CHARACTERISATION OF INTAKE FLOW DISTORTION
J. Hueso Rebassa, Cranfield Univeristy, United Kingdom
17. Sep 26 11:25 11:50 10.11.2
0612		 RUBBER ENGINE INTEGRATED OPTIMIZATION STRATEGY FOR OVERALL AIRCRAFT DESIGN
J. Häßy, DLR, Germany
17. Sep 26 11:50 12:15 10.11.3
0740		 ON THE ACCURACY AND ROBUSTNESS OF TRANSIENT PNEUMATIC TRAVERSES: AN EXPERIMENTAL STUDY ON SYSTEM PARAMETERS
S. Eilers, University of the Bundeswehr Munich, Germany
17. Sep 26 12:15 12:40 10.11.4
0111		 EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION
J. Hueso Rebassa, Cranfield Univeristy, United Kingdom
11.11Performances
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 11:00 11:25 11.11.1
0306		 STUDY ON FLIGHT PERFORMANCE DEGRADATION CHARACTERISTICS OF ABLATION-INDUCED DAMAGE IN LOITERING MUNITIONS
MX-Z zhang, China
17. Sep 26 11:25 11:50 11.11.2
0372		 GAIN OPTIMIZATION FOR CASCADED INDI CONTROL WITH INTEGRATED PERFORMANCE AND ROBUSTNESS REQUIREMENTS
D. Surmann, University of the Bundeswehr Munich, Germany
17. Sep 26 11:50 12:15 11.11.3
0630		 LATERAL-DIRECTIONAL HANDLING AND FLYING QUALITIES ASSESSMENT OF A BLENDED WING BODY (BWB) ACFA 2020 CONFIGURATION
M Alam, Cranfield University, United Kingdom
17. Sep 26 12:15 12:40 11.11.4
0539		 FLIGHT PERFORMANCE ANALYSIS OF ELECTRIC AIRCRAFT UNDER MOTOR FAILURE CONDITIONS USING REDUCED-ORDER MODELING
L. Hein¹, S. Myschik¹; ¹University of the Bundeswehr Munich, Germany
Reserve Paper 11.11.R
0009		 ACHIEVING ACCURATE AND CONSISTENT AIRSPEED MEASUREMENT FOR AIRCRAFT DEVELOPMENT AND CERTIFICATION
J. Luo, The Boeing Company, United States
additional information (interactive) 11.11.R
0106		 AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE
R. Wang, China
12.11Additive Manufacturing and Intelligent Manufacturing
Chair(s): van Manen, R.
Track 12
08 - Manufacturing and Supply Chain Management
17. Sep 26 11:00 11:25 12.11.1
0124		 BALANCING STRENGTH AND THERMAL CONDUCTIVITY IN LPBF-PROCESSED ALUMINUM-BASED MATERIALS
H. Z Zhang, Nanjing University of Aeronautics and Astronautics, China
17. Sep 26 11:25 11:50 12.11.2
0140		 3D ANALYSIS AND PREDICTION OF ASSEMBLY STEP DEVIATIONS IN FOUR-BAR LINKAGE BAY DOORS
R. Yang, Dalian University of Technology, China
17. Sep 26 11:50 12:15 12.11.3
0270		 A NOVEL MULTI-TASK LEARNING METHOD FOR DEFECT SUPPRESSION IN AERONAUTICAL PARTS DURING LASER POWDER BED FUSION
Y.S. Chen, Nanjing University of Aeronautics and Astronautics, China
17. Sep 26 12:15 12:40 12.11.4
0766		 A QUALITATIVE FRAMEWORK FOR AIRCRAFT WING MANUFACTURING AND DECISION MAKING
Y. A. Martins, Aeronautics Institute of Technology, Brazil
13.11AAM Trajectory and Integration
Chair(s): ,
Track 13
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
17. Sep 26 11:00 11:25 13.11.1
0292		 THREE-DIMENSIONAL ADAPTIVE TRAJECTORY OPTIMIZATION FOR RPAS-BASED ATMOSPHERIC MEASUREMENTS
K.-A. Buchtal, German Aerospace Center, Germany
17. Sep 26 11:25 11:50 13.11.2
0605		 A FIELD-THEORETIC FRAMEWORK FOR AUTONOMOUS COLLISION AVOIDANCE IN URBAN AIR MOBILITY
F. Y. Wu, Hong Kong SAR of China
17. Sep 26 11:50 12:15 13.11.3
0682		 EXPLORING DETROIT METROPOLITAN WAYNE COUNTY AIRPORT AS A TESTBED FOR RESOLVING EVTOL INTEGRATION CHALLENGES FOR AIR TAXI OPERATIONS
S.M. Abdulhak, United States
17. Sep 26 12:15 12:40 13.11.4
0946		 STANDARDIZED TAKE-OFF AND LANDING PROCEDURES FOR AIR TAXIS: URBAN AIR MOBILITY
FN Naeem, TUHH, Germany
Reserve Paper 13.11.R
0554		 DETERMINATION OF SAFE SEPARATION FOR UAVS: CONSIDERING AIRSPACE STRUCTURE AND MANEUVERING STRATEGIES
K.H. Low, Civil Aviation University of China, China
14.11AI & SE
Chair(s): , , Stoufflet, B.
Track 14
02 - Systems Engineering and Integration
17. Sep 26 11:00 11:25 14.11.1
0279		 LLM-ASSISTED GENERATION OF SYSML V2 MODELS FROM HETEROGENEOUS SYSTEM REPORTS
V. Voth, German Aerospace Center (DLR), Germany
17. Sep 26 11:25 11:50 14.11.2
0257		 INTEGRATED SYSTEMS ARCHITECTURE FOR AEROSPACE DIGITAL THREAD ECOSYSTEM: A HUB-N-SPOKE TO MODELLING AND SIMULATION
K Dang, Boeing, United States
17. Sep 26 11:50 12:15 14.11.3
0205		 COMMON ONTOLOGY FOR PROPULSION ARCHITECTURES - COPA
S. Reitenbach, German Aerospace Center (DLR), Germany
17. Sep 26 12:15 12:40 14.11.4
0479		 AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS
Y. REN, Beihang University, China
Reserve Paper 14.11.R
0252		 BEYOND THE HARDWARE: REGULATION AND CERTIFICATION AS THE CRITICAL PATH TO ADF AUTONOMOUS CAPABILITY
K.J. Joyce, RAAF / UNSW, Australia
15.11Operations optimisation
Chair(s): Stamoulis, K.
Track 15
11 - Operations and Sustainment
17. Sep 26 11:00 11:25 15.11.1
0315		 FLIGHT MISSION MODELLING WITH VARYING BASELINE DATA: APPLICAITON IN BUSINESS AVIATION
A. Lau, German Aerospace Center (DLR), Germany
17. Sep 26 11:25 11:50 15.11.2
0611		 PROVIDING SENSOR INFORMATION FOR BORDING TIME PREDICTION
M. Schultz, Unibw M, Germany
17. Sep 26 11:50 12:15 15.11.3
0396		 INVESTIGATION OF DECARBONISATION PATHWAYS FOR SHORT HAUL AVIATION USING A DISCRETE OPTIMISATION DECISION-MAKING ALGORITHM
N Barry, Trinity College Dublin, The University of Dublin, Ireland
17. Sep 26 12:15 12:40 15.11.4
0031		 ASSESSING AIRLINE PURCHASE MOTIVATION FOR HYDROGEN AIRCRAFT UNDER FUTURE CORSIA
H. Nakamura, The University of Tokyo, Japan
Reserve Paper 15.11.R
0816		 LIMITED-HORIZON LOOK-AHEAD SCHEDULING FOR DEMAND-RESPONSIVE OVERNIGHT CARGO AIRLINE OPERATIONS
Palak Singh¹, Rajkumar.S Pant¹, Geetika Kapil, Independent Researcher, United States; ¹IIT Bombay, India
Presenter: Rajkumar S. Pant, Indian Institute of Technology (IIT) Bombay
additional information (interactive) 15.11.R
0822		 LOSS OF RELIABILITY OF NEW GENERATION ENGINES IN COMMERCIAL AVIATION: THE BUSINESS IMPACT OF THE PW1100G ENGINE RECALL ON MEXICAN AVIATION
A Sanchez Mata, SANMATC Consulting, Mexico

12:40 - 13:40LUNCH BREAK

1.12tbd1
Chair(s): ,
Track 1
2.12DPI workshop results
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.12Aero Optimization
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
17. Sep 26 13:40 14:05 3.12.1
0894		 INVERSE AIRFOIL DESIGN USING CONDITIONAL VARIATIONAL AUTOENCODERS
K. Swannet, Delft University of Technology, Netherlands
17. Sep 26 14:05 14:30 3.12.2
0476		 DATA-DRIVEN SHAPE PARAMETERIZATION FOR EFFECTIVE AERODYNAMIC DESIGN OPTIMIZATION OF PROPELLERS
J. L. Li, Northwestern Polytechnical University, China
17. Sep 26 14:30 14:55 3.12.3
0615		 AN INVESTIGATION OF KRIGING MODELS USING CORRELATED INDEPENDENT VARIABLES FOR AERODYNAMIC DESIGN
T. Kanno, Purdue University, United States
17. Sep 26 14:55 15:20 3.12.4
0393		 META-ENHANCED MULTI-OBJECTIVE REINFORCEMENT LEARNING FOR WIDE-SPEED-RANGE AIRFOIL OPTIMIZATION
Z. Li, Northwestern Polytechnical University, China
Reserve Paper 3.12.R
0254		 AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS
J.-W Wu, Northwestern Polytechnical University, China
Reserve Paper 3.12.R
0458		 RESEARCH ON GENERALIZED REPRESENTATION OF FLYING-WING CONFIGURATIONS BASED ON DEEP LEARNING
Xiaomeng Zhang, China
4.12Propulsion/Propulsion-Integration
Chair(s): ,
Track 4
15 - Guest lectures (by personal invitation only)
5.12Applied CFD Approaches
Chair(s): ,
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 13:40 14:05 5.12.1
0193		 EFFECTS OF FLAPPING–PITCHING PHASE DIFFERENCE ON THE AERODYNAMIC PERFORMANCE OF HOVERING DRAGONFLY WINGS
H Wang, Northwestern Polytechnical University, China
17. Sep 26 14:05 14:30 5.12.2
0281		 UNCERTAINTY QUANTIFICATION AND CROSS-CORRELATION EFFECTS IN AERODYNAMIC COEFFICIENTS DERIVED QUANTITIES
L. Pirillo, Italy
17. Sep 26 14:30 14:55 5.12.3
0720		 A STALL EXTENSION TO LIFTING-LINE THEORY: IMPLEMENTATION AND VALIDATION IN ASWING
L. Avoni, ISAE-Supaero, France
17. Sep 26 14:55 15:20 5.12.4
0879		 FALCON: FRAMEWORK FOR AIRFOIL CFD AND ANALYSIS OPTIMIZATION
P. Desai, Manipal Institute of Technology, India
6.12Challenges in wind tunnel testing
Chair(s): Jagadeesh, C., Allen, N.
Track 6
03.2 - Experimental Aerodynamics
17. Sep 26 13:40 14:05 6.12.1
0592		 PROPOSAL FOR DISTINGUISHING USALE DATA UNDER HIGH WIND TUNNEL BLOCKAGE USING AN RAE2822 TEST CASE
M.H. Mohsin, Cranfield University, United Kingdom
17. Sep 26 14:05 14:30 6.12.2
0151		 EXPERIMENTAL VALIDATION OF A COANDA-BASED FLUIDIC THRUST VECTORING NOZZLE USING A HIGH-SPEED WIND TUNNEL
N. Schwagerus¹, M. Stößel¹, D. Kozulovic¹; ¹University of the Bundeswehr Munich, Germany
17. Sep 26 14:30 14:55 6.12.3
0790		 FORCE RECONSTRUCTION TECHNIQUES FOR DYNAMIC LOAD ESTIMATION ON A HEMISPHERE IN LOW-SPEED WIND TUNNEL TESTING
C.J.K Brown, RMIT University , Australia
17. Sep 26 14:55 15:20 6.12.4
0428		 METROLOGY METHODS FOR ISOLATING PROFILE FORM, WAVINESS, STEPS, AND TWIST FROM SCANS OF SMALL-SCALE LAMINAR FLOW WIND TUNNEL MODELS
C Hiemcke, General Atomics Aeronautical Systems, Inc., United States
Reserve Paper 6.12.R
0395		 GROUND EFFECT EXPERIMENTAL ANALYSIS IN A NAVAL TESTING TANK AS AN ALTERNATIVE TO WIND TUNNEL
L.G. Souza, Instituto Tecnológico de Aeronáutica, Brazil
7.12Guidance and Path Planning
Chair(s): , , Hristozov, S.
Track 7
06.2 - Flight Dynamics and Control (UAV related)
17. Sep 26 13:40 14:05 7.12.1
0498		 ONLINE TRAJECTORY PLANNING FOR FIXED-WING UAVS BASED ON PSEUDO-SPECTRAL CONVEX PROGRAMMING
Y. Peng, National University of Defense Technology, China
17. Sep 26 14:05 14:30 7.12.2
0121		 THREE-DIMENSIONAL PATH PLANNING OF UAV IN WIND FIELD ENVIRONMENT OF PLATEAU MOUNTAINOUS AREA
F. H.-F. Fan, Northwestern Polytechnical University, China
17. Sep 26 14:30 14:55 7.12.3
0859		 VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A TEMPORAL RESIDUAL NETWORK APPROACH WITH CHANNEL ATTENTION
Z. Zhang, Northwestern Polytechnical University , China
17. Sep 26 14:55 15:20 7.12.4
0132		 TRAJECTORY FEASIBILITY AND CONTROL FOR DYNAMIC SOARING IN 6-DOF FLIGHT
Y. Zhu, Northwestern Polytechnical University, China
Reserve Paper 7.12.R
0454		 MPPI-BASED COMPUTATIONAL GUIDANCE FOR MOTION PLANNING OF A MULTIROTOR UAV USING DEPTH-CAMERA-BASED OBSTACLE REPRESENTATION
K.W. Jang, Electronics and Telecommunications Research Institute, South Korea
additional information (interactive) 7.12.R
0881		 UAV-SENSING MULTI-STRATEGY FULL-DOMAIN WIND INVERSION
X Zhang, Northwestern Polytechnical University, China
8.12 Aircraft Electrification, Systems and Certification
Chair(s): ,
Track 8
12 - Host Nation (by personal invitation only)
9.12Aircraft Design
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
17. Sep 26 13:40 14:05 9.12.1
0367		 EFFECT OF UNCERTAINTY ON ROBUST JIG SHAPE DESIGN OF A HIGH ASPECT RATIO WING
G. Yang, University of Bristol, United Kingdom
17. Sep 26 14:05 14:30 9.12.2
0628		 METHODOLOGY FOR CRITICAL LOAD-CASE AND CONSTRAINT IDENTIFICATION IN PRELIMINARY COMPOSITE WING SIZING USING RAPID DESIGN TOOLS
M Alam, Cranfield University, United Kingdom
17. Sep 26 14:30 14:55 9.12.3
0230		 NOVEL MULTIDISCIPLINARY MISSION-OPTIMISED AIRCRAFT DEVELOPMENT METHODOLOGY IN CONSIDERATION OF PASSIVE/ACTIVE CONTROL
V. N. Mueller, Technical University of Munich, Germany
17. Sep 26 14:55 15:20 9.12.4
0211		 AIRCRAFT MASS EVALUATION MODEL: FROM TUBE-AND-WING TO BLENDED WING BODY USING WHALE.
V Priasso¹, A Lannoo¹; ¹DMAS, ONERA, 59000, Lille, France, France
additional information (interactive) 9.12.R
0857		 A STOCHASTIC GRADIENT ONLINE LEARNING AND PREDICTION METHOD FOR ACCELERATING TOPOLOGY OPTIMIZATION AND ITS APPLICATION IN THE DESIGN OF MORPHING WING
Y. Xing, The University of Sydney, Australia
10.12Propulsion optimization 2
Chair(s): ,
Track 10
05 - Propulsion and Energy
17. Sep 26 13:40 14:05 10.12.1
0906		 INLET OPTIMIZATION DESIGN OF A BOUNDARY LAYER INGESTION PROPULSION SYSTEM
X.K. Ma, Northwestern Polytechnical University , China
17. Sep 26 14:05 14:30 10.12.2
0314		 PD-STGNN: A PHYSICS-INFORMED DYNAMIC SPATIO-TEMPORAL GRAPH NEURAL NETWORK FOR AERO-ENGINE THRUST PREDICTION
C. Song, Northwestern Polytechnical University, China
17. Sep 26 14:30 14:55 10.12.3
0579		 PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES
T.-D Dinh, Vietnam
17. Sep 26 14:55 15:20 10.12.4
0366		 GPU-ENABLED SURROGATE MODEL-BASED AEROACOUSTIC OPTIMISATION FOR JET FLOWS
G. Yang, University of Bristol, United Kingdom
11.12Flight dynamics
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
17. Sep 26 13:40 14:05 11.12.1
0191		 MULTI-BODY DYNAMIC MODELING OF A BIRD-LIKE FLAPPING-WING VEHICLE: ANALYSIS OF FLAPPING-AERODYNAMIC COUPLING EFFECTS
L.Z. Zhou, China
17. Sep 26 14:05 14:30 11.12.2
0206		 AIRCRAFT BUFFET QUANTIFICATION
Jia Luo, The Boeing Company, United States
17. Sep 26 14:30 14:55 11.12.3
0938		 METHODOLOGY FOR VERIFYING DYNAMIC PARAMETERS OF A STEWART PLATFORM FOR FLIGHT SIMULATION
M. D. Dutra Turazza, University of São Paulo, Brazil
17. Sep 26 14:55 15:20 11.12.4
0658		 A NEW APPROACH TO MODELLING THE FLIGHT DYNAMICS OF A TAILLESS AIRCRAFT
A. Kwiek, Warsaw University of Technology, Poland
Reserve Paper 11.12.R
0924		 EFFECTS OF LIFT DISTRIBUTION AND WING POSTURE ON THE STABILITY AND CONTROL OF TAILLESS AIRCRAFT
MR de Kock, University of Pretoria, South Africa
12.12Advanced Forming Technology for Aviation
Chair(s): Gu, D.
Track 12
08 - Manufacturing and Supply Chain Management
17. Sep 26 13:40 14:05 12.12.1
0126		 ACHIEVING HIGH-PERFORMANCE MAGNESIUM MATRIX COMPOSITES BY LASER POWDER BED FUSION
L.X.XI Xi, China
17. Sep 26 14:05 14:30 12.12.2
0286		 HIGH-RATE AUTOMATED STAMP FORMING OF CF/LM-PAEK COMPOSITES FOR NEXT-GENERATION UAV AEROSTRUCTURES
M. Ravandi, Aerostructures Innovation Research (AIR) Hub, Swinburne Universi, Australia
17. Sep 26 14:30 14:55 12.12.3
0651		 THE MAKING OF LUCHTVAART IN TRANSITIE (LIT) – AND THE REMAKING OF A STRONG GLOBALLY CONNECTED NATIONAL AERONAUTICS INDUSTRY
R. van Manen, Stichting Luchtvaart in Transitie, Netherlands
17. Sep 26 14:55 15:20 12.12.4
0825		 A MULTI-STAGE FORMING APPROACH FOR MANUFACTURING TITANIUM BIPOLAR PLATES FOR FUEL CELLS
J.-H. Hong, Korea Institute of Materials Science, South Korea
13.12CRM-HL 2
Chair(s): Rivers, M.
Track 13
03.2 - Experimental Aerodynamics
17. Sep 26 13:40 14:05 13.12.1
0756		 AEROACOUSTIC WIND TUNNEL TESTING AND CFD STUDY USING JAXA 8% SEMISPAN HIGH-LIFT COMMON RESEARCH MODEL IN JAXA FQUROH-2 PROJECT
M. Murayama, Japan Aerospace Exploration Agency, Japan
17. Sep 26 14:05 14:30 13.12.2
0844		 CROSS-TEST COMPARISONS AND REYNOLDS NUMBER EFFECTS IN THE CRM-HL ECOSYSTEM
S.M. Rivers, NASA Langley Research Center, United States
Presenter: Courtney Winski
17. Sep 26 14:30 14:55 13.12.3
0896		 ICING EXPERIMENTAL DATABASE USING THE COMMON RESEARCH MODEL(ICED CRM)
D.D.P. Di Pasquale, Cranfield University, United Kingdom
17. Sep 26 14:55 15:20 13.12.4
0977		 ICING EXPERIMENTAL DATA ON THE NASA HIGH-LIFT CRM MODEL
D.D.P. Di Pasquale, Cranfield University, United Kingdom
14.12tbd2
Chair(s): ,
Track 14
15.12Through-Life support
Chair(s): Kelly, M.
Track 15
11 - Operations and Sustainment
17. Sep 26 13:40 14:05 15.12.1
0914		 INTEGRATING MAINTENANCE, REPAIR, AND OVERHAUL (MRO) ASPECTS INTO SUSTAINABILITY-DRIVEN DESIGN OF AIRCRAFT STRUCTURES
A.F. Filippatos, Department of Mechanical Engineering & Aeronautics, University o, Greece
17. Sep 26 14:05 14:30 15.12.2
0710		 FROM DATA TO DECISIONS: A CONCEPTUAL FRAMEWORK FOR DATA-DRIVEN AIRLINE OPERATIONS AND SUSTAINMENT
A. Apostolidis, KLM Royal Dutch Airlines, Netherlands
17. Sep 26 14:30 14:55 15.12.3
0451		 LIFE CYCLE ANALYSIS OF EMISSIONS IN AVIATION: IDENTIFIYING AND ADJUSTING FACTORS TO REDUCE CARBON EMISSIONS
J. Roesing, RWTH Aachen University, Germany
17. Sep 26 14:55 15:20 15.12.4
0856		 PERFORMANCE DEGRADATION ASSESSMENT METHOD FOR AERO-ENGINES ACROSS THE FULL-LIFE-CYCLE BASED ON DIGITAL TWIN
D. Xiao, China
Reserve Paper 15.12.R
0582		 ENGINEERING COMMERCIAL AIRCRAFT FOR SUSTAINABLE THROUGH-LIFE SUPPORT
RG Ramachandran, Boeing, India
additional information (interactive) 15.12.R
0222		 KEY STAKEHOLDERS IN AEROSPACE FOR A SUSTAINABLE AND CIRCULAR PRODUCT DEVELOPMENT - A SYSTEMATIC APPROACH
I. Hallstedt, Chalmers University of Technology, Sweden

15:20 - 15:25CHANGEOVER BREAK

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

0.13CLOSING CEREMONY
Chair:
17. Sep 26 15:15 17:00