35th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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

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

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

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 SETTING THE STAGE FOR THE GLOBAL SUSTAINABLE AVIATION TRACK WITH GLOBAL AIRLINES
AH Krein, Clean Aviation, Belgium
14. Sep 26 10:20 10:45 1.1.2 JAL’ CHALLENGE TO THE NET-ZERO GH GAS EMISSION
MS Suzuki, JAL, Japan
14. Sep 26 10:45 11:10 1.1.3 THE WHOLE JOURNEY: PEOPLE, PLANET AND PROGRESS AT QANTAS
F Messent, Qantas Group, Australia
14. Sep 26 11:10 11:35 1.1.4 PANEL DISCUSSION Q&A WITH THE AIRLINES
P Panel,
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 AURAL DIGITAL TWIN FOR AIRCRAFT CABIN DESIGN
M.C, Moruzzi, Università di Bologna, Italy
14. Sep 26 10:20 10:45 3.1.2 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 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 A FRAMEWORK FOR AUTOMATED SYSTEM COMPONENT PLACEMENT IN AIRCRAFT CONCEPTUAL DESIGN
J.J Vézina, Concordia University, Canada
Reserve Paper 3.1.R MULTI-STATE FLIGHT DECK DISPLAY LAYOUT OPTIMIZATION UNDER FAILURE AND REVERSION SCENARIOS
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 A LAMINAR TAILORED WING WITH CATNLF AND HLFC FOR EXTRA LONG RANGE
J. Ruberte Bailo¹, T. Streit¹, A. Seitz¹; ¹DLR, Germany
14. Sep 26 10:20 10:45 4.1.2 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 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 MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE
Eleonora Riccio¹, Rocco Bombardieri¹, Alessandro Ceresa¹, Vincenzo Rosario Baraniello¹, Francesco Tufano¹, Giuseppe Persechino¹, Domenico Coiro, University Federico II of Naples, Italy; ¹Italian Aerospace Research Centre, Italy
Reserve Paper 4.1.R 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 09:30 09:55 5.1.1 LARGE EDDY SIMULATIONS OF LOW-REYNOLDS NUMBER FLOWS IN THE COMPRESSIBLE REGIME
Pietro Catalano¹, F.-A. D'Aniello¹; ¹C.I.R.A., Italy
14. Sep 26 09:55 10:20 5.1.2 LAMINAR SEPARATION ON AN AIRFOIL WITH PERTURBATION OF BOUNDARY CONDITIONS
E. Tangermann¹, A. Jagadeesha¹, M. Klein¹; ¹Universität der Bundeswehr München, Germany
14. Sep 26 10:20 10:45 5.1.3 REYNOLDS NUMBER EFFECTS OF A BIRD-FEATHER-INSPIRED POROUS-MEDIUM AIRFOIL
ZhaoPeng Zhang¹, ZhengYin Ye¹; ¹Northwestern Polytechnical University, China
14. Sep 26 11:10 11:35 5.1.4 TURBULENCE MODELLING IN URBAN ENVIRONMENTS FOR UAV DESIGN CRITERIA
DL Laubscher, South Africa
additional information (interactive) 5.1.R NUMERICAL STUDY ON DYNAMIC STALL OF FIGHTER AIRCRAFT AT HIGH ANGLE OF ATTACK USING DYNAMIC IMPROVED DELAYED DETACHED EDDY SIMULATION
H. Wang¹, T. Lin¹, G. Wang¹, L. Xu¹; ¹Northwestern Polytechnical University, China
Presenter: Huiyue Wang, Northwestern Polytechnical University
additional information (interactive) 5.1.R 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 RESPONSE CHARACTERISTICS OF WINGTIP VORTEX INSTABILITY TO EXTERNAL DISTURBANCES
Yiming Wu¹, Zhenglin Xiao¹, Yang Xiang¹, Ziyi Zhu¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 10:20 10:45 6.1.2 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 THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW
J-M Mourad, ISAE-Supaero, France
14. Sep 26 11:10 11:35 6.1.4 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 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 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 EFFECT OF LIP/NOZZLE DEFLECTION ANGLE ON THE AERODYNAMIC AND PROPULSIVE CHARACTERISTICS OF PROPULSIVE WING UNITS
Minghao Li¹, Zhou Zhou¹, kelei Wang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 10:45 11:10 7.1.3 PROPELLER AERODYNAMICS UNDER NON-UNIFORM INFLOWS
S. Montagner¹, J. Serpieri¹, G. Cafiero¹; ¹Politecnico di Torino, Italy
Presenter: Sara Montagner, Politecnico di Torino
14. Sep 26 11:10 11:35 7.1.4 AERODYNAMIC EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT CHARACTERISTICS OF A WING–FLAP CONFIGURATION
H.-X. He, China
Reserve Paper 7.1.R DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING
Baiyang Li, China; Xiaoping Zhu, China; Zhou Zhou, China; Minghao Li, China; Rui Wang, China
Presenter: Minghao Li, School of Aeronautics, Northwestern Polytechnical University
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 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 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 4D PRINTING VIA ELECTROMAGNETISM FOR COMPOSITE STRUCTURES
S.H. Vattathurvalappil, King Fahd University of Petroleum and Minerals, Saudi Arabia
14. Sep 26 11:10 11:35 8.1.4 ACCESSIBLE MATERIAL COMPOSITES FOR UAVS IN HUMANITARIAN AND DEVELOPMENT CONTEXTS
C Koutsambasis¹, M Marino¹, N.J. Brown¹, W Wu¹; ¹RMIT University, Australia
Reserve Paper 8.1.R COMPRESSION AND FATIGUE PERFORMANCE OF ADDITIVELY MANUFACTURED NITI ARCHITECTED SHAPE MEMORY ALLOYS
B.B. Zwerink, NLR, Netherlands
Reserve Paper 8.1.R DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS
J. Rodrigues¹, M. Pelosi², W. Foster², S. Barter¹, R. Das¹; ¹RMIT University, Australia ;²DSTG, Australia
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 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 DIGITAL TWIN FOR AIR DEFENSE: LIVE-VIRTUAL-CONSTRUCTIVE INTEGRATION AND DECISION SUPPORT
S. Malka¹, O. Yakimenko¹, M. Ben-Simon¹; ¹Naval Postgraduate Shcool, United States
14. Sep 26 10:45 11:10 9.1.3 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 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 NEURAL NETWORK BASED SLIDING MODE CONTROL FOR HYPERSONIC LONGITUDINAL CONTROL
H. Kim, South Korea
14. Sep 26 10:20 10:45 10.1.2 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 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 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 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 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 FIXED-WING AIRCRAFT PORT-HAMILTONIAN DYNAMICS AND CONTROL
E. M. Fernandes, Instituto Tecnologico de Aeronautica, Brazil
Reserve Paper 11.1.R 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 IMPACT OF SYSTEM LATENCIES ON PILOT INTERACTION AND HANDLING OF AN ELECTRICALLY POWERED GYROPLANE UAV WITH FPV-BASED REMOTE CONTROL
G. Schmitz¹, I. Pruter¹, H. Duda¹, M. Laubner¹, S. Lorenz¹; ¹DLR e.V., Germany
14. Sep 26 10:20 10:45 12.1.2 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 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 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 A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING
J. Cheng, China
Reserve Paper 12.1.R 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 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 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 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 A PEAKS-OVER-THRESHOLD APPROACH TO RUNWAY COLLISION RISK ESTIMATION FOR EFFICIENT ARRIVAL OPERATIONS
N.K. Wickramasinghe, Electronic Navigation Research Institute, Japan; R. Mori, Kobe University, Japan
14. Sep 26 11:10 11:35 13.1.4 NEXT-GEN FLAP SYSTEMS: VALIDATION RESULTS AND IMPLICATIONS FOR AIR TRAFFIC MANAGEMENT
R. Sáez¹, R. Pitarque¹, B. Heesbeen, Royal Netherlands Aerospace Centre (NLR), Netherlands; Y. J. Hasan², J. Kurz², D. Vechtel², M. Gerber, Swiss Skylab Foundation (Skylab), Switzerland; ¹Technical University of Catalonia (UPC), Spain ;²German Aerospace Centre (DLR), Germany
14.1Vision & 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 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 ROBUST MOTION ESTIMATION FOR INDOOR MAVS USING WIDE-FIELD-INTEGRATION OF OPTIC FLOW
M. Yanagisawa¹, R. Okabayashi¹, T. Yamaguchi², M. Takamoto², M. Bando¹, S. Hokamoto¹; ¹Kyushu University, Japan ;²Mitsubishi Electric Corporation, Japan
14. Sep 26 10:45 11:10 14.1.3 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 A SYSTEMATIC, TUNING-FREE ATTITUDE CONTROL METHOD FOR VTOL UAVS
K. Okamoto¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan
Presenter: Kazuki Okamoto, The University of Tokyo
Reserve Paper 14.1.R DEEP LEARNING VS. TRADITIONAL COMPUTER VISION FOR UAV LANDING SITE DETECTION IN ADVERSE WEATHER
R. Schmidt¹, J. Rüter¹; ¹German Aerospace Center (DLR), Germany
additional information (interactive) 14.1.R AUTONOMOUS FLIGHT AND INTELLIGENT TARGET LOCALIZATION OF JUNGLE RECONNAISSANCE UAV
S.-K. Li¹, N.-H. Zhu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China
15.1AI Safety, Verification, and Trust
Chair(s): ,
Track 15
10 - Safety and Security
14. Sep 26 09:55 10:20 15.1.1 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 10:20 10:45 15.1.2 COVERAGE-DRIVEN VERIFICATION FOR SAFETY-BY-DESIGN IN AI-BASED COLLISION AVOIDANCE SYSTEMS
T Stefani, German Aerospace Center, Germany
14. Sep 26 10:45 11:10 15.1.3 RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING
J Gao, The University of Sydney, Australia
14. Sep 26 11:10 11:35 15.1.4 ADVANCING TRUST FOR THRUST: PAIRING AND SHARING
L.J.A. Jansen, German Aerospace Center (DLR), Germany

11:35 - 11:40CHANGEOVER BREAK

0.3GENERAL LECTURE 1 Jet Zero’s Blended Wing Body Aircraft by Tom O Leary
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 BOEING PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY
M L Drake, The Boeing Company, United States
14. Sep 26 13:55 14:20 1.2.2 AIRBUS PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY
V Roca, Airbus SAS, France
14. Sep 26 14:20 14:45 1.2.3 EMBRAER\'S PERSPECTIVES & PROGRESS TOWARDS NEXTGEN AIRLINERS
C Silva, Embraer, Brazil
14. Sep 26 14:45 15:10 1.2.4 PANEL DISCUSSION Q&A WITH THE AIRCRAFT OEMS
P Panel,
2.2High Speed Flight – Overview
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 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 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 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 ASSESSMENT OF LIQUID HYDROGEN-POWERED AIRCRAFT RANGE: A NOVEL BREGUET FORMULATION
G. Palaia, Polytechnic of Turin, Italy
Reserve Paper 3.2.R SCENARIO-BASED TECHNOLOGY ROADMAPPING IN AEROSPACE USING DBSCAN AND LLM
T. A. Brutscher, Liebherr-Aerospace Lindenberg GmbH, Germany
Reserve Paper 3.2.R FORMALIZING THE INTEGRATION BETWEEN MODEL-BASED SYSTEMS ENGINEERING AND SYSTEM ARCHITECTURE OPTIMIZATION
S Valencia-Ibáñez¹, S Liscouët-Hanke¹; ¹Concordia 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 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 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 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 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 ACCURACY AND EFFICIENCY OF TRANSITION–TURBULENCE MODELS IN PREDICTING HIGH AND LOW REYNOLDS NUMBER PROPELLER PERFORMANCE
F. Parra¹, D. Domínguez¹, A. Delgado¹, J. Gonzalo¹; ¹Universidad de León, Spain
14. Sep 26 14:20 14:45 5.2.3 RESEARCH ON TRANSITION PREDICTION METHODS FOR HELICOPTER ROTOR BLADES
Z.-K Zhou, China
14. Sep 26 14:45 15:10 5.2.4 HYPERBOLIC RECEPTIVITY TO FREESTREAM DISTURBANCES OVER A BLUNT WEDGE: A LINEARIZED NAVIER–STOKES APPROACH
Zhichao Zhu¹, Youcheng Xi¹, Song Fu¹; ¹Tsinghua 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 PHYSICAL DESIGN CONCEPTS OF VORTEX GENERATOR ARRAYS FOR AIRCRAFT AFT-BODIES DRIVEN BY DISTINCT DRAG REDUCTION MECHANISMS
Y. Mou¹, Y. Wu¹, T. Liu², D. Li², Y. Xiang¹, H. Liu¹; ¹School of Aero. & Astro., Shanghai Jiao Tong Univ., China ;²COMAC Shanghai Aircraft Design and Research Institute, China
14. Sep 26 13:55 14:20 6.2.2 ACTIVE FLOW CONTROL AND THERMAL PROTECTION FOR A WING-BODY CONFIGURATION BASED ON LATERAL JET
Liaolei He¹, Fang Chen¹, Yuqi Wei¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 14:20 14:45 6.2.3 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 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 NUMERICAL SIMULATION OF SUPERCOOLED LARGE DROPLET IMPINGEMENT ON ROTATING FAN BLADES
Hao Yan¹, Haoran Zheng¹, Zheyuan Dong¹, Wei Dong¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 13:55 14:20 7.2.2 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 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 AI-BASED FORECASTING OF ICE-INDUCED AERODYNAMIC DEGRADATION
S. Corcione, University of Naples Federico II, Italy
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 VISUAL MACHINE LEARNING ANALYSIS OF MULTIFUNCTIONAL PERFORMANCE IN GRAPHENE FRP COMPOSITES
V Kannan, The University of Sydney, Australia; A Bettens, Deneb Space, Australia
14. Sep 26 13:55 14:20 8.2.2 EFFICIENT SIMULATION AND UNCERTAINTY QUANTIFICATION OF PROGRESSIVE CRUSHING IN COMPOSITE LAMINATES
Johannes Reiner, Deakin University, Australia; Reza Vaziri, The University of British Columbia, Canada
14. Sep 26 14:20 14:45 8.2.3 DEVELOPMENT OF CONDUCTIVE COMPOSITE MATERIALS FOR HIGH VOLTAGE APPLICATIONS
S.A. Brown¹, P. Sangkarat¹, Z. Sha, Western Sydney University, Australia; C.H. Wang¹; ¹University of New South Wales, Australia
14. Sep 26 14:45 15:10 8.2.4 COMPRESSIVE PERFORMANCE OF VARIABLE-STIFFNESS COMPOSITE HYPERBOLIC STIFFENED PANELS BASED ON GEOMETRIC PATH MAPPING
R.B. Ma¹, C.Y. Wang¹, X.M. Chen, Aircraft Strength Research Institute of China, China; W.Z. Wang¹; ¹Northwestern Polytechnical University, China
Reserve Paper 8.2.R 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 ENHANCEMENT AND DEGRADATION: THE DUAL ROLE OF GRAPHENE NANOPLATELETS ON THE STRUCTURAL PERFORMANCE OF COMPOSITE T-JOINTS
M. Bhasin¹, A.P. Mouritz¹; ¹RMIT 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 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 MODELING, SIMULATION AND CASE STUDY OF LARGE-SCALE FOREST FIRE EXTINGUISHING AND RESUE SYSTEM BASED ON AVIATION METERIEL
Wenyuan CHENG¹, Si CHEN¹, Gaofeng WANG¹, He CAO¹, Yangmeng WU¹; ¹Aviation Industry Development Research Center of China (ADR), China
14. Sep 26 14:20 14:45 9.2.3 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 SYSTEM IDENTIFICATION USING FLIGHT TEST DATA AND MACHINE LEARNING
G. Larsson, Saab Aeronautics, Sweden
14. Sep 26 13:55 14:20 10.2.2 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 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 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 PHYSICS-INFORMED NEURAL NETWORK BASED MODELING OF DYNAMIC BEHAVIOR OF AERIAL REFUELING HOSE
Z. Wu¹, S. Yang¹, Z. Zhang¹, Y. Qu¹, B. Xiao¹; ¹Northwestern Polytechnical University, China
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 STABILITY AUGMENTATION SYSTEM DESIGN FOR LONGITUDINALLY UNSTABLE TAILLESS AIRCRAFT
S. Riethausen, Linköping University, Sweden
14. Sep 26 13:55 14:20 11.2.2 ROBUST ESTIMATION-AWARE GUIDANCE FOR STOCHASTIC INTERCEPTION WITH PARAMETRIC UNCERTAINTY
LM Mudrik, United States
14. Sep 26 14:20 14:45 11.2.3 DOB-BASED ADAPTIVE NONSINGULAR TERMINAL SLIDING MODE CONTROL FOR FAULT-TOLERANT CONTROL OF QUAD-TILTROTOR EVTOL
S.W. Kim¹, T.W Yun¹, D.H. Seo¹, J.Y. Suk¹, S.K. Kim¹; ¹Chungnam National University, South Korea
14. Sep 26 14:45 15:10 11.2.4 FLIGHT ENVELOPE PROTECTION FOR HIGH ALTITUDE LONG ENDURANCE AIRCRAFT
C. Weiser, DLR - German Aerospace Center, Germany
Reserve Paper 11.2.R 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 A THERMO-MECHANICAL PHASE FIELD MODEL CONSIDERING SOLID-LIQUID TRANSITION: APPLICATION TO ELECTROTHERMAL DE-ICING
Yuxuan Ying, Northwestern Polytechnical University , China; Xudan Yao¹, Ye Feng¹, Wei Huang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 13:55 14:20 12.2.2 ICE DETECTOIN: CORRELATION ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES
G. Mingione, CIRA, Italy
Presenter: Luigi Mangiacrapa, Centro Italiano Ricerche Aerospaziali
14. Sep 26 14:20 14:45 12.2.3 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 ELECTROMECHANICAL RESONANT ICE PROTECTION SYSTEMS USING VOICE COIL ACTUATORS - AIR INLET SECTION CASE STUDY
Y. R. Rafik, INSA, France
Reserve Paper 12.2.R 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 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 RUNWAY-AWARE CAPACITY ENVELOPES FOR LONG-RANGE ARRIVAL METERING UNDER OPERATING-DIRECTION CHANGES AT SINGAPORE CHANGI
Ehsan Asadi¹, Gabriele Enea, MIT Lincoln Laboratory, United States; Michael Schultz¹; ¹University of the Bundeswehr Munich, Germany
14. Sep 26 14:20 14:45 13.2.3 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 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 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 DYNAMIC RECONFIGURABLE PATH PLANNING FOR FIRE-FIGHTING UAVS
Z. Lin¹, D. Geraghty¹, S. F. Armanini¹, L. Mainini¹; ¹Imperial College London, United Kingdom
14. Sep 26 13:55 14:20 14.2.2 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 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 SIMULATION-BASED ANALYSIS OF REDUNDANT UAV NAVIGATION UNDER GNSS OUTAGES
M. Ben Simon¹, S. Malka¹, D. Chudnovsky¹, O. Yakimenko¹; ¹Naval Postgraduate School, United States
Reserve Paper 14.2.R GEOMETRY-AWARE AERIAL LIGHT SHOW: JOINT OPTIMIZATION OF SWARM SIZE AND ENERGY-EFFICIENT TRAJECTORIES
K.-G. Yuksel, Aselsan, Turkey
15.2 Aircraft Systems, Operations, and Certification
Chair(s): ,
Track 15
10 - Safety and Security
14. Sep 26 13:30 13:55 15.2.1 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 13:55 14:20 15.2.2 CONCEPT OF OPERATIONS FOR A HYDROGEN-ELECTRIC POWERED MODIFIED DASH8-300 REGIONAL AIRCRAFT: PERFORMANCE, OPERATIONAL, AND CERTIFICATION IMPACTS
B Rietdijk¹, B Sulejmanovic¹, R Coertze¹; ¹Conscious Aerospace BV, Netherlands
14. Sep 26 14:20 14:45 15.2.3 TOWARD THE INTEGRATION OF NEUROPHYSIOLOGICAL SIGNALS AND HUMAN BODY DYNAMICS FOR ADAPTIVE CONTROL ALLOCATION
T. Treichl, German Aerospace Center, Germany
14. Sep 26 14:45 15:10 15.2.4 A CENTRALIZED KEY MANAGEMENT ARCHITECTURE FOR SECURE GROUP COMMUNICATION ON IMA PLATFORM
C. A. Dautel, Institute of Aircraft Systems, University of Stuttgart, Germany

15:10 - 15:15CHANGEOVER BREAK

0.4GENERAL LECTURE 2 Airbus 400M by David Francisco Hernandez
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 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 CFM INTERNATIONAL\'S RISE PROGRAM: A STEP-CHANGE FOR DURABILITY AND EFFICIENCY
C.-A. Andrews, GE Aerospace, United States
14. Sep 26 17:20 17:45 1.3.3 PANEL DISCUSSION Q&A WITH THE PROPULSION OEMS
P Panel,
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 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 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 AI-SUPPORTED AIRCRAFT SYSTEM ARCHITECTURE SYNTHESIS
P. Krus, Linköping University, Sweden
14. Sep 26 17:45 18:10 3.3.4 DEVELOPING AN AGENTIC AI WORKFLOW FOR AUTOMATED CONCEPTUAL DESIGN OF AIRCRAFT USING RISPECT+
J. Song¹, S. Park², D. Lee², Y.-E. Kang¹, Y. Kim¹, S. Lee¹; ¹Manufacturing AI Research Center, KITECH, South Korea ;²Department of Unmanned Aircraft Systems, Hanseo University, South Korea
Presenter: Juhun Song, Korea Institute of Industrial Technology/Sungkyunkwan University
4.3Conceptual design studies - 2
Chair(s): Nicolosi, f.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 16:30 16:55 4.3.1 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 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 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 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): Slotnick, J., Azevedo, J.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 16:30 16:55 5.3.1 RIGID AND AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT TO TRANSONIC SHOCK BUFFET
M. J. Candon, RMIT University, Australia
14. Sep 26 16:55 17:20 5.3.2 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 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 AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING
Yue Zhao¹, Jiawen He¹, Xinyuan Wei¹, Tieren Chen¹, Yong Yang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 5.3.R 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 RECEPTIVITY OF NON-MODAL STREAKS IN HYPERSONIC BLUNT BOUNDARY LAYERS: FROM NUMERICS TO ASYMPTOTICS
M. Dong, Institute of Mechanics, Chinese Academy of Sciences, China; L. Zhao, Departiment of Mechanics, Tianjin University, China
14. Sep 26 16:55 17:20 6.3.2 ORIGIN OF TRANSIENT TURBULENT SPOTS IN HYPERSONIC SWEPT BOUNDARY-LAYERS WITH MORPHING SWEEP ANGLES
Jiang Genrui¹, Dong Ming¹; ¹Institute of Mechanics, Chinese Academy of Sciences, China
14. Sep 26 17:20 17:45 6.3.3 NUMERICAL SIMULATION OF HYPERSONIC PLASMA FLOW BASED ON NONLINEAR COUPLED CONSTITUTIVE RELATIONS
H. Shi¹, C. Song¹, H. Xiao¹; ¹Northwestern Polytechnical University, China
14. Sep 26 17:45 18:10 6.3.4 AFTERBODY CURVATURE EFFECTS ON FLOW LOSS CHARACTERISTICS BASED ON ENTROPY PRODUCTION
X.W. Chen¹, M.S. He¹, B. Yu¹, W. Wang¹, H. Liu¹; ¹Shanghai Jiao Tong University, China
Reserve Paper 6.3.R 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 TOWARDS AN OPTIMAL STRUT-BRACED-WING REGIONAL JET WITH NATURAL LAMINAR FLOW
Nathalie Saadeh¹, David W. Zingg¹; ¹University of Toronto, Canada
14. Sep 26 16:55 17:20 7.3.2 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 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 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 VORTEX TOPOLOGY AND DRAG REDUCTION ANALYSIS IN SPIROID WINGTIP DEVICES USING PARTICLE TRACKING VELOCIMETRY
Merina Amon Mwasandube, Australia; Matthew Marino¹, Jennifer L. Palmer¹; ¹RMIT 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 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 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 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 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 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 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 KEY PARAMETER IDENTIFICATION IN AIRCRAFT STRAIN PREDICTION MODELS
K.E. Niessen¹, D.O. Franke¹; ¹Defence Science and Technology Group, Australia
14. Sep 26 16:55 17:20 9.3.2 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 MTCL FOR COMPOSITE DAMAGE
SM Miao , Northwestern Polytechnical University, China
14. Sep 26 17:45 18:10 9.3.4 IMPACT LOAD IDENTIFICATION METHOD FOR AIRCRAFT RUDDER PLANES BASED ON NARX NEURAL NETWORK
S.Y. Liang¹, T. Yang¹, Z.C. Yang¹; ¹Northwestern Polytechnical University, China
10.3Hybrid Electric Fuel Cell Concepts
Chair(s): ,
Track 10
05 - Propulsion and Energy
14. Sep 26 16:30 16:55 10.3.1 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 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 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 FUEL CELL ASSISTED DISTRIBUTED BOUNDARY LAYER INGESTION FANS FOR CRUISE EFFICIENCY IMPROVEMENT IN SINGLE AISLE TRANSPORT AIRCRAFT
P.W.T. Somaweera, RMIT University , Australia
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 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 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 AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL
M Morales, ITA, Brazil; M Rempel, Embraer, Brazil; J.E.M Fernandes, Instituto Tecnológico de Aeronáutica, Brazil
14. Sep 26 17:45 18:10 11.3.4 KNOW YOUR LIMITS: ESTIMATING THE TILT-WING TRANSITION CORRIDOR UNDER FAILURE CONDITIONS
M. May¹, D. Milz¹, S. Armanini, Imperial College London, Germany; ¹German Aerospace Center (DLR), Germany
Reserve Paper 11.3.R 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 MULTI-OBJECTIVE OPTIMIZATION OF AERO-ENGINE BEARING CHAMBER SCAVENGE STRUCTURE BASED ON NSGA-II ALGORITHM
Z. Zhu¹, Y. Lyu¹, L. Jiang¹, Z. Liu¹, S. Li¹, F. Liu¹; ¹Northwestern Polytechnical University, China
Presenter: Fulin Liu, Northwestern Polytechnical University
14. Sep 26 16:55 17:20 12.3.2 OSCILLATORY FAILURE DETECTION IN AIRCRAFT ACTUATION SYSTEMS USING WAVELET TRANSFORM
IO Skusa, Brazil
14. Sep 26 17:20 17:45 12.3.3 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 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 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 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 FLIGHT PLANNING, THE FORGOTTEN ASSET
A. Dickinson, Australia
14. Sep 26 16:55 17:20 13.3.2 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 JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION
Alexander Lau¹, Max Mendiguchia Meuser¹, Alexander Kuenz¹, Simone Dietmüller¹, Sigrun Matthes¹, Thorsten Ehlers¹; ¹DLR, Germany
14. Sep 26 17:45 18:10 13.3.4 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 AUTONOMOUS LANDING OF UAVS ON SHIPS USING DECOUPLED REINFORCEMENT LEARNING
T. Gerner¹, M. Candon¹, A. K. Gostar¹, N. Jayarathne, Navantia Australia, Australia; J. Venning, University of Tasmania, Australia; M. Saska, Czech Technical University in Prague, Czech Republic; P. Marzocca¹; ¹RMIT University, Australia
14. Sep 26 16:55 17:20 14.3.2 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 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 ASSESSMENT OF THE LANDING CAPABILITIES OF A FLEXIBLE HIGH-ALTITUDE PLATFORM AT LONGITUDINAL AND LATERAL-DIRECTIONAL WIND
Y. J. Hasan, DLR Institute of Flight Systems, Germany
Reserve Paper 14.3.R 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 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 PILOT WORKLOAD PROFILES UNDER CONTINUOUS MULTI-TASKING AND SPARSE EVENTS VIGILANCE
W.-D. Xiao¹, C.-L. Zhao, Shanghai Aircraft Design and Research Institute, China; Y. Gao¹, Y.-Y. Lu¹, S. Fu¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 17:20 17:45 15.3.3 UNCERTAINTY ANALYSIS AND EYE-TRACKING-BASED CLUSTERING IN AIR TRAFFIC CONTROLLER WORKLOAD PREDICTION
A. Lemetti¹, L. Meyer², M. Peukert², T. Polishchuk¹, C. Schmidt¹, H. Alpfjord Wylde²; ¹Linköping University (LiU), Sweden ;²Air Navigation Services of Sweden (LFV), Research & Innovation, Sweden
14. Sep 26 17:45 18:10 15.3.4 HRV BASED PILOTS WORKLOAD PREDICTION FOR AN INTELLIGENT COCKPIT WARNING SYSTEM
A. E. Esposito, Kore University of Enna, Italy