35th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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

Monday, 14. Sep 2026

07:00 - 08:00Registration

0.1OPENING CEREMONY
Chair: C. Atkin ICAS President
14. Sep 26 08:00 08:30

0.2ICAS Daniel & Florence Guggenheim Memorial Lecture Adnan Raghdo –The Boeing’s MQ-28 Ghost Bat to Australian Aerospace Industry & MQ-28 Development
Chair: F. Haselbach ICAS EC Member
14. Sep 26 08:30 09:30

09:30 - 09:55COFFEE BREAK

1.1GSA2: Global Sustainable Aviation – Setting the Stage with Global Airlines
Chair(s): Wahls, R., Krein, A.
Track 1 Pyrmont Theatre
15 - Guest lectures
14. Sep 26 09:55 10:20 1.1.1 SETTING THE STAGE FOR THE GLOBAL SUSTAINABLE AVIATION TRACK WITH GLOBAL AIRLINES
A Krein, Clean Aviation, Germany
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
Hudson, 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 by Analysis
Chair(s): Slotnick, J., Aponso, B.L.
Track 2 C4.1
15 - Guest lectures
14. Sep 26 09:55 10:20 2.1.1 TOWARDS CERTIFICATION BY ANALYSIS: A MILITARY AIRWORTHINESS PERSPECTIVE
S. Geisbauer, DLR, Germany; S. Shaw, MBDA, United Kingdom
Presenter: Andreas Goerttler, DLR,
14. Sep 26 10:20 10:45 2.1.2 EXPLORING AIRWORTHINESS CBA: A STALL SPEED CASE STUDY BASED ON AERO-STRUCTURAL COUPLED ANALYSIS
M. Amano, Japan
14. Sep 26 10:45 11:10 2.1.3 PROGRESS TOWARDS AIRCRAFT CERTIFICATION BY ANALYSIS WITHIN THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTIC
J. Schaefer, United States
14. Sep 26 11:10 11:35 2.1.4 AN EFFORT TOWARD PROCESS DEVELOPMENT OF CBA FOR FLIGHT CHARACTERISTICS
T. Ishida, Japan
3.1Cabin
Chair(s): Hesse, C.
Track 3 C4.2
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. Moruzzi¹, T. Fadda¹, E. Caligari¹, S. Bagassi¹; ¹Università 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. Hellbrück¹, P. Zemke¹, C. Hesse¹, M. Fuchs¹, J. Biedermann¹, B. Nagel¹; ¹DLR 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. Inselmann¹, F.D. Bischop¹, F.H. Christiansen¹, M. Höhner¹, T. Schüppstuhl¹, D. Krause¹; ¹Hamburg University of Technology, Germany
14. Sep 26 11:10 11:35 3.1.4 A FRAMEWORK FOR AUTOMATED SYSTEM COMPONENT PLACEMENT IN AIRCRAFT CONCEPTUAL DESIGN
J. Vézina¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada
Reserve Paper 3.1.R MULTI-STATE FLIGHT DECK DISPLAY LAYOUT OPTIMIZATION UNDER FAILURE AND REVERSION CONDITIONS
Y. Yamai¹, M. Itoh¹, M.-P. Pacaux-Lemoine, Université Polytechnique Hauts-de-France, France; ¹University of Tsukuba, Japan
4.1Application of Aerodynamics in Design
Chair(s): Schmollgruber, P.
Track 4 C4.3
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 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 10:45 11:10 4.1.3 MULTIDISCIPLINARY APPROACH FOR THE AERODYNAMIC CHARACTERIZATION OF AN INFLATABLE CLOSED-WING HYBRID HIGH-ALTITUDE PSEUDO-SATELLITE
E. Riccio¹, R. Bombardieri¹, A. Ceresa¹, V.R. Baraniello¹, F. Tufano¹, G. Persechino¹, D. Coiro, University Federico II of Naples, Italy; ¹Italian Aerospace Research Centre, Italy
14. Sep 26 11:10 11:35 4.1.4 RESEARCH ON OVERALL AERODYNAMIC DESIGN OF GRID-DUCT INTEGRATED VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING AIRCRAFT
B. Li¹, B. Mi¹; ¹Northwestern Polytechnical University, China
5.1Scale Resolving Simulations
Chair(s): Coder, J., Zingg, D.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 09:55 10:20 5.1.1 LAMINAR SEPARATION ON AN AIRFOIL WITH PERTURBATION OF OUTER AND INNER BOUNDARY CONDITIONS
E. Tangermann¹, A. Jagadeesha¹, M. Klein¹; ¹Universität der Bundeswehr München, Germany
14. Sep 26 10:20 10:45 5.1.2 LARGE EDDY SIMULATIONS OF LOW-REYNOLDS NUMBER FLOWS IN THE COMPRESSIBLE REGIME
P. Catalano¹, F.A. D'Aniello¹; ¹C.I.R.A., Italy
14. Sep 26 10:45 11:10 5.1.3 REYNOLDS NUMBER EFFECTS OF A BIRD-FEATHER-INSPIRED POROUS-MEDIUM AIRFOIL
Z.P. Zhang¹, Z.Y. Ye¹; ¹Northwestern Polytechnical University, China
14. Sep 26 11:10 11:35 5.1.4 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. Missato¹, R.G. Annes da Silva¹, A.F. de Castro da Silva¹, T. Wainwright, Zenotech, United Kingdom; ¹Instituto Tecnológico de Aeronáutica, Brazil
6.1Aerodynamic Response and Wake Characteristics
Chair(s): Vijgen, P.
Track 6 C4.5
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
Y. Wu¹, Z. Xiao¹, Y. Xiang¹, Z.Y. Zhu¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 10:20 10:45 6.1.2 NON-LINEAR PARAMETRIC MODEL FOR THE 3DOF MOTION OF A BOX IN WAVES USING SPARSE REGRESSION
Z. Hoffman¹, S. Vahaji¹, A. Das¹, M. Candon¹, N. Jayarathne, Navantia Australia, Australia; P. Marzocca¹; ¹RMIT, Australia
14. Sep 26 10:45 11:10 6.1.3 THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW
J. Mourad¹, V. Ferrand¹, E. Gowree¹; ¹ISAE-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. Anilir¹, D.F. Kurtulus¹, M.F. Platzer, University of California, Davis, United States; ¹Middle East Technical University, Turkey
7.1Distributed Propulsion and Aerodynamic Interaction
Chair(s): Lacy, D.
Track 7 C4.6
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.-M. Xu¹, K.-L. Wang¹, Z. Zhou¹, S.-K. Li¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
Presenter: Shao-Kun LI
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 UNIT
M. Li¹, Z. Zhou¹, K. 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 EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT ENHANCEMENT OF A HIGH-LIFT CONFIGURATION
H.-X. He¹, W.-P. Song¹, Y. Wang¹, Y.-H. Wang¹, Y.-J. Shi, China Ship Scientific Research Center, China; ¹Northwestern Polytechnical University, China
8.1Advanced Aerostructures
Chair(s): Bayandor, J.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 09:55 10:20 8.1.1 INTERNATIONAL AND EUROPEAN RESEARCH AND TECHNOLOGY INFRASTRUCTURE DATA BASES IN AVIATION
R. Degenhardt, DLR, Italy; F. Ferrigno, CIRA, Italy; A. Gliszczynski, Lodz University of Technology, Poland; A.-L. Delot, ONERA, France
Presenter: Adrian Gliszczynski, Lodz University of Technology
14. Sep 26 10:20 10:45 8.1.2 MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK
Z. Li¹, D. Wei¹, W. Zeng, Chinese Academy of Sciences, China; K.K. Alynur¹, X. Liu¹, B. Zhao¹, S. Li¹, L. Ma, KUCH ENERGY Technology Co., Ltd., China; S. Yang¹; ¹Beihang University, China
14. Sep 26 10:45 11:10 8.1.3 A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED REPAIR OF ALUMINUM PARTS
J. Lua¹, M.R. Rajanna¹, H. Yu, Virginia Tech, United States; A. Timmons², G. Murray², N. Phan²; ¹Global Engineering and Materials, Inc., United States ;²Naval Air Systems Command, United States
14. Sep 26 11:10 11:35 8.1.4 MULTIPHYSICS COUPLING EFFECT ON INTERFACIAL PROPERTIES OF CNT/GFRP/CFRP COMPOSITES FOR ELECTROTHERMAL ANTI-/DE-ICING APPLICATIONS
X. Yao¹, Y. Wang¹, H. Wang¹, Y. Wang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 8.1.R FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING
X. Liu¹, D.S. Wei¹, S.Z. Jin, AVIC Manufacturing Technology Institute, China; S. Yang¹, D.X. Yin², B. Niakate², D. Lasne²; ¹Beihang university, China ;²BSS Turbotech Ltd., China
9.1System of Systems 1
Chair(s): Amadori, K., Prakasha, P.
Track 9 C4.8
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; C. Jouannet, Saab Aeronautics, 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, M. Ben Simon¹, O. Yakimenko¹; 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. Li¹, W.Z. Liu¹, B.L. Shang¹, Y.Z. Wang¹, R.X. Lin¹; ¹Northwestern Polytechnical 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): Kiszkowiak, L.
Track 10 C4.9
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.J. Kim¹, J.H. Shin¹; ¹Chungbuk national University, South Korea
14. Sep 26 10:20 10:45 10.1.2 SUPPORTING PILOT SITUATIONAL AWARENESS BY EXTRACTING INSIGHTS FROM AN AI EXPERT
C. Koopman¹, D. Zammit Mangion¹; ¹University of Malta, Malta
14. Sep 26 10:45 11:10 10.1.3 MULTI-SENSOR BASED ADAPTIVE FUSION SCHEME FOR POSITION ESTIMATION OF MULTIROTOR UAV SYSTEMS IN GPS-DENIED ENVIRONMENTS
L. Busse¹, M. Kumar¹; ¹University of Cincinnati, United States
11.1Flight Control 1
Chair(s): Shaferman, V., Rogalski, T.
Track 11 C4.10
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 SYMMETRY
V. Martinez Jimenez¹, F. Asensio Nieto¹, I. Romo Martinez¹, A. Sanz De Blas¹, D. Lodares Gomez¹; ¹AIRBUS, Spain
14. Sep 26 10:20 10:45 11.1.2 BACKSTEPPING-BASED PREDICTIVE PERFORMANCE CONTROL FOR AERIAL REFUELING BOOM ATTITUDE CONTROL
Y.L. Niu¹, L.X. Wang¹, J.X. Li², Y.N. Gao², S.H. Xu, COMAC Beijing Aircraft Technology Research Institute, China; T. Yue¹, S. Tai¹, H.L. Liu¹; ¹Beihang University, China ;²The First Aircraft Institute AVIC, China
14. Sep 26 10:45 11:10 11.1.3 AIRBRAKES CONTROL SYSTEM FOR PRECISE APOGEE CONTROL OF A SOUNDING ROCKET
N. Gee-Landman¹, J.L. Palmer¹; ¹RMIT University, Australia
14. Sep 26 11:10 11:35 11.1.4 FIXED-WING AIRCRAFT PORT-HAMILTONIAN DYNAMICS AND CONTROL
J.E.M. Fernandes¹, F.L. Cardoso-Ribeiro¹, M.A.V. Morales¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
12.1UAV Component
Chair(s): Alexander, M.
Track 12 C2.3
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. Sorokina¹, W. Bliemetsrieder¹, P. Panchal¹, L. Hein¹, T. Weyh¹; ¹Universität der Bundeswehr München, Germany
14. Sep 26 10:45 11:10 12.1.3 STATE-SPACE SIMULATION OF PASSIVE LANDING GEAR IMPACT RESPONSE FOR LIGHTWEIGHT FIXED-WING UAVS
A.A.J. Oliveira¹, L.H.J. Machado¹, M.S. Ferreira¹, J.P.B. Souza¹, E.J.T. Santos¹, J.V.N. Oliveira¹, P.H.C. Picanço¹; ¹Universidade Federal de Minas Gerais, Brazil
14. Sep 26 11:10 11:35 12.1.4 A DISTRIBUTED MULTI-SOURCE SENSOR FUSION METHOD FOR COLLABORATIVE TARGET TRACKING
J.B. Cheng¹, J. Li, AVIC Chengdu Aircraft Design and Research Institute, China; B.X. Wang¹, C. Chen, Information Center of the National Administration of Defense Sci, China; P. He, AVIC Luoyang Institute of Electro-Optical Equipment, China; K. Zhang¹; ¹Northwestern Polytechnical University, China
13.1Safety and Efficiency in Aviation
Chair(s): Maroney, D.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
14. Sep 26 09:55 10:20 13.1.1 DESIGN AND FEASIBILITY ASSESSMENT OF TRANSPORT OPERATIONS FOR DELIVERING TYPHOON CONTROL SUBSTANCES
H. Akiyama¹, S. Ueno¹, T. Higuchi¹, T. Sakurai¹; ¹Yokohama National University, Japan
14. Sep 26 10:20 10:45 13.1.2 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 10:45 11:10 13.1.3 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. Sep 26 11:10 11:35 13.1.4 EVALUATING HUMAN-MACHINE-TEAMING CONCEPTS FOR A HIGHLY AUTOMATED GROUND CONTROLLER WORKING POSITION
L. Nöhren¹, A. Simon¹, M. Schaper¹; ¹DLR, Germany
14.1Vision & Control
Chair(s): , , Grabowski, T.
Track 14 C2.5
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, WUT, Institute of Aeronautics and Applied Mechanics, Poland; P. Wozniak¹, R. Chalupczynski¹, K. Barys², J. Konowalski², A. Abratanski², J. Swierk¹, I. Dabrowski²; ¹Uavionics Ltd Poland, Poland ;²Rafal Perz Scientific Network, 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. Kim¹, J.H. Hong¹, Y.J. Jang¹, J.H. Moon¹; ¹Cheongju 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 FOR JUNGLE RECONNAISSANCE UAVS
S.K. Li¹, N.H. Zhu¹, Z. Zhou¹; ¹Northwestern Polytechnical University, China
15.1AI Safety, Verification, and Trust
Chair(s): Würfel, J.
Track 15 C2.6
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. Christensen¹, T. Stefani¹, E. Hoemann¹, F. Köster¹, S. Hallerbach¹; ¹German Aerospace Center, 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. Stefani¹, J.M. Christensen¹, E. Hoemann¹, F. Koester¹, S. Hallerbach¹; ¹DLR, Germany
14. Sep 26 10:45 11:10 15.1.3 RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING
J. Gao¹, T. Wang, Taiyuan University of Technology, China; H. Gao¹, Y. Ding¹, Z. Wang¹; ¹ University of Sydney, Australia

11:35 - 11:40CHANGEOVER BREAK

0.3GENERAL LECTURE 1 The Time Has Come for an All-Wing Airplane by Florentina Viscotchi, Jet Zero
Chair: F. Collier ICAS PPSC Chair
14. Sep 26 11:40 12:30

12:30 - 13:30LUNCH BREAK

1.2GSA2: Perspectives and Progress towards NextGen Airliners
Chair(s): Krein, A., Vijgen, P.
Track 1 Pyrmont Theatre
15 - Guest lectures
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
V di Nucci, 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: Progress and Prospects
Chair(s): Bowcutt, K., Neely, A.
Track 2 C4.1
15 - Guest lectures
14. Sep 26 13:30 13:55 2.2.1 RECENT DEVELOPMENTS IN HYPERSONIC INNOVATION, SCIENCE & TECHNOLOGY IN AUSTRALIA
A. Neely, UNSW, Australia
14. Sep 26 13:55 14:20 2.2.2 EUROPEAN HYPERSONICS OVERVIEW
N. Viola, Politecnico di Torino, Italy
14. Sep 26 14:20 14:45 2.2.3 HYPERSONIC RESEARCH AND DEVELOPMENT IN THE REPUBLIC OF KOREA: FROM FUNDAMENTAL AEROTHERMODYNAMICS TO FLIGHT DEMONSTRATION
B.J. Lee, Seoul National University, South Korea
14. Sep 26 14:45 15:10 2.2.4 AN OVERVIEW OF JAXA’S HIGH-SPEED FLIGHT R&D: FROM SUPERSONIC FLIGHT TO HYPERSONIC TRANSPORTATION
J. Akatsuka¹, S. Takahashi¹, Y. Makino¹, S. Tomioka¹, M. Takegoshi¹, M. Koga¹, T. Isono¹; ¹JAXA, Japan
3.2Conceptual Design 1
Chair(s): Alexander, M., Nagel, B.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
14. Sep 26 13:30 13:55 3.2.1 POINT-CLOUD-BASED INTELLIGENT DESIGN OF FLYING-WING CONFIGURATIONS WITH CONDITIONAL GENERATION AND PRESSURE PREDICTION
J.-Z, Zhang¹, Z.-H. Han¹, W.-P. Song¹, K.-S. Zhang¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 13:55 14:20 3.2.2 ASSESSMENT OF LIQUID HYDROGEN-POWERED AIRCRAFT RANGE: A NOVEL BREGUET FORMULATION
G. Palaia, Polytechnic of Turin, Italy; K. Abu Salem, University of Trento, Italy; A.A. Quarta, University of Pisa, Italy; P.D. Bravo-Mosquera, University of São Paulo, Brazil
Presenter: Karim Abu Salem, University of Trento
14. Sep 26 14:20 14:45 3.2.3 INTEGRATING SYSTEM ARCHITECTURE OPTIMIZATION INTO MODEL-BASED SYSTEMS ENGINEERING METHODS
S. Valencia-Ibáñez¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada
additional information (interactive) 3.2.R CST PARAMETRIC MODELING AND MULTI-OBJECTIVE OPTIMIZATION RECONFIGURATION STUDY OF A BLENDED-WING-BODY AIRCRAFT
X. Lu¹, S. Chen¹, X. Wang¹, J. Yu¹, D. Li¹; ¹Northwestern Polytechnical University, China
4.2Conceptual Design Studies - 1
Chair(s): Lott, M.
Track 4 C4.3
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
J.L.C Chan¹, H Smith¹; ¹Cranfield 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. Schmollgruber¹, S. Defoort¹, E. Nguyen-Van¹, J. Gauvrit-Ledogar¹, J. Chan², C. Lawson², L. Kugler³, T. Zill³, J. Kos, NLR, Netherlands; ¹ONERA, France ;²Cranfield University, United Kingdom ;³DLR, Germany
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. Viola¹, R. Fusaro¹, D. Feretto¹; ¹Politecnico di Torino, Italy
14. Sep 26 14:45 15:10 4.2.4 PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS
S. Trivedi¹, A.K. Munshi¹, R.S. Pant¹; ¹Indian Institute Technology Bombay, India
5.2Transition Predictions
Chair(s): , , Halila, G.
Track 5 C4.4
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 A ROTOR TRANSITION PREDICTION METHOD BASED ON GALILEAN INVARIANCE AND THE C1 CROSSFLOW TRANSITION CRITERION
K.Y. Zhou¹, W.P. Song¹, J.H. Xu¹; ¹Northwestern Polytechnical University, China
14. Sep 26 14:45 15:10 5.2.4 HYPERSONIC RECEPTIVITY TO FREESTREAM DISTURBANCES OVER A BLUNT WEDGE: A LINEARIZED NAVIER-STOKES APPROACH
Z. Zhu¹, Y. Xi¹, S. Fu¹; ¹Tsinghua University, China
6.2Aircraft Flow Control Applications
Chair(s): Moreau, D.
Track 6 C4.5
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
L. He¹, F. Chen¹, Y. 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. Jürisson¹, P.H.L. Blom¹; ¹Royal Netherlands Aerospace Centre, Netherlands
7.2Aero-Thermal Effects, Icing and Propulsion System Integration
Chair(s): Herbert, L.
Track 7 C4.6
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
H. Yan¹, H. Zheng¹, Z. Dong¹, W. Dong¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 13:55 14:20 7.2.2 JET-INDUCED SWIRLING FLOW AND WALL HEAT TRANSFER FOR AERO-ENGINE NACELLE SWIRL ANTI-ICING SYSTEM
Z.Y. Dong, China; H.R. Zheng, China; H. Yan, China; P.Y. Wang, China; W. Dong, China
14. Sep 26 14:20 14:45 7.2.3 AIRFRAME-INLET INTEGRATION DESIGN FOR AN OVER-WING-MOUNTED SUPERSONIC TRANSPORT CONFIGURATION
Q. Chen¹, Z.-H. Han¹, K.-S. Zhang¹, K. Song¹; ¹Northwestern Polytechnical University, China
14. Sep 26 14:45 15:10 7.2.4 DATA-DRIVEN AERODYNAMIC MODEL OF THE DISTRIBUTED PROPULSION WING
B. Li, China; X. Zhu, China; Z. Zhou, China; M. Li, China; R. Wang, China
8.2Damage Tolerance
Chair(s): Bayandor, J.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 13:30 13:55 8.2.1 IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITES
A.M. Caporale¹, G. Janszen¹, A.S. Jambhulkar¹, M. Ursic², A. Tasca², R. Passoni², A. Airoldi¹; ¹Politecnico di Milano, Italy ;²Brembo N.V., Italy
14. Sep 26 13:55 14:20 8.2.2 EFFICIENT SIMULATION AND UNCERTAINTY QUANTIFICATION OF PROGRESSIVE CRUSHING IN COMPOSITE LAMINATES
J. Reiner, Deakin University, Australia; R. Vaziri, The University of British Columbia, Canada
14. Sep 26 14:20 14:45 8.2.3 PROGRESSIVE FAILURE TIMELINE RECOUNT OF AN ATMOSPHERIC REENTRY TRAGEDY - IN MEMORY OF STS-107 CREW, AND DR. FRANK ABDI
J. Bayandor, United States
9.2System of Systems 2
Chair(s): Crossley, W., Jouannet, C.
Track 9 C4.8
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. Jouannet¹, K. Amadori¹, R. Perez, Royal Military College of Canada, Canada; E. Moerland, DLR, Germany; ¹Saab Aeronautics an Linköpings University, Sweden
Presenter: christopher Jouannet
14. Sep 26 13:55 14:20 9.2.2 MODELING, SIMULATION AND EVALUATION OF LARGE FOREST FIRE EXTINGUISHING AND RESCUE BASED ON AVIATION MATERIEL
W. Cheng¹, S. Chen¹, G. Wang¹, H. Cao¹, Y. 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 Villazon¹, M. Balchanos¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
10.2Hydrogen Propulsion Concepts
Chair(s): Bezos O Connor, G.
Track 10 C4.9
05 - Propulsion and Energy
14. Sep 26 13:30 13:55 10.2.1 EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS
F. Thilker¹, R. Krewinkel, Graz University of Technology , Austria; A. Tramposch¹; ¹University of Applied Sciences JOANNEUM GmbH, Austria
14. Sep 26 13:55 14:20 10.2.2 HEAT EXCHANGER MODELING METHODS FOR HYDROGEN POWERED AERO ENGINES DURING THERMODYNAMIC CYCLE DESIGN
A. Görtz¹, J. Häßy¹, M. Baier Schmelcher¹, M. El-Soueidan¹, F. Herbst¹; ¹German Aerospace Center, Germany
14. Sep 26 14:20 14:45 10.2.3 REAL-TIME EMULATION TESTBENCH FOR FUEL-CELL/BATTERY HYBRIDIZATION IN HYDROGEN-ELECTRIC AVIATION
G. Marinaro¹, C. Serpico¹, L. Garbarino¹, M. Inverno¹, G. Malaponte¹, A. Bono¹, A. Pagano¹; ¹Italian Research Centre - CIRA, Italy
11.2Flight Control 2
Chair(s): Rogalski, T., Woszidlo, R.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
14. Sep 26 13:30 13:55 11.2.1 ROBUST ESTIMATION-AWARE GUIDANCE FOR STOCHASTIC INTERCEPTION WITH PARAMETRIC UNCERTAINTY
L. Mudrik, Naval Postgraduate School, United States; Y. Oshman, Technion---Israel Institute of Technology, Israel
Presenter: Yaakov Oshman, Technion---Israel Institute of Technology
14. Sep 26 13:55 14:20 11.2.2 DISTURBANCE OBSERVER-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 14:20 14:45 11.2.3 FLIGHT ENVELOPE PROTECTION FOR HIGH ALTITUDE LONG ENDURANCE AIRCRAFT
C. Weiser, German Aerospace Center (DLR), Germany
14. Sep 26 14:45 15:10 11.2.4 CONTROL ALLOCATION AND SIZING FOR OVER-ACTUATED AIRCRAFT
C. Doll, ONERA, France
12.2De-icing
Chair(s): Stumpf, E.
Track 12 C2.3
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
Y. Ying, Northwestern Polytechnical University , China; X. Yao¹, Y. Feng¹, W. Huang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 13:55 14:20 12.2.2 ICE DETECTION: CORRELATION OF ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES TESTED IN ICING WIND TUNNEL
L. Mangiacrapa¹, T. Klaas², N. Rehfeld², F. Amoroso, Eurotech s.r.l., Italy; G. Mingione¹, S. Ameduri¹; ¹Italian Aerospace Research Centre, Italy ;²Fraunhofer IFAM , Germany
Presenter: Luigi Mangiacrapa, Italian Aerospace Research Centre
14. Sep 26 14:20 14:45 12.2.3 A MPC–MHE STRATEGY FOR FREQUENCY TRACKING AND PARAMETERS ESTIMATION OF RESONANT DE-ICING SYSTEMS
A. Suti¹, J. Pothin², M. Budinger¹, V. Pommier-Budinger², A. Reysset¹; ¹INSA Toulouse, France ;²Isae Supaero, France
Presenter: Aleksander SUTI
13.2Air Traffic Sequencing and Flows
Chair(s): Brown, M.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
14. Sep 26 13:30 13:55 13.2.1 REDUCING AIR TRAFFIC COMPLEXITY IN JAPANESE AIRSPACE THROUGH MINOR LATERAL TRAJECTORY ADJUSTMENTS
S.B. Goeppel¹, E. Asadi¹, E. Itoh, he University of Tokyo, Japan; M. Schultz, University of the Bundeswehr, Germany; ¹University of the Bundeswehr Munich, Germany
Presenter: Simon Goeppel, University of the Bundeswehr Munich
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
E. Asadi¹, G. Enea, MIT Lincoln Laboratory, United States; M. 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 ASSESSMENT OF GLOBAL AND INTRA-AIRLINE COOPERATIVE DECISION FRAMEWORKS
S. Tsuru¹, A. Andreeva-Mori¹; ¹Osaka 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. Matsuno¹, H. Matsuda¹; ¹Japan Aerospace Exploration Agency, Japan
14.2Mission Planning and Navigation
Chair(s): , , Hristozov, S.
Track 14 C2.5
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 TRACKING ALGORITHM OF MULTIPLE UAVS USING PSO FOR AERIAL SURVEILLANCE
D.Y. Yoon¹, J.Y. Ka¹, D.J. Lee¹, Z. Wang², K.C. Wong²; ¹Hanseo University, South Korea ;²The University of Sydney, Australia
14. Sep 26 14:20 14:45 14.2.3 MODELING OF CRITICAL WEATHER FLIGHT PERFORMANCE OF MULTICOPTER UAVS FOR RESILIENT CONTROLLER DESIGN.
A. Fallast¹, S. Lesak¹; ¹FH JOANNEUM University of Applied Sciences, Austria
Presenter: Samuel Lesak, FH JOANNEUM University of Applied Sciences
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
15.2 Aircraft Systems, Operations, and Certification
Chair(s): Finck, T.
Track 15 C2.6
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 AVIATION
A. Reis¹, C. Lessa¹, P. Kurka¹, R. Santos Alencar, ITA , Brazil; M. Machado Cardoso Júnior ¹; ¹ITA, Brazil
14. Sep 26 13:55 14:20 15.2.2 CONCEPT OF OPERATIONS FOR A HYDROGEN-ELECTRIC POWERED MODIFIED DASH 8-300 REGIONAL AIRCRAFT: PERFORMANCE, OPERATIONAL, AND REGULATORY IMPACTS
B. Rietdijk¹, B. Sulejmanovic¹, R. Coertze¹; ¹Conscious Aerospace BV, Netherlands
14. Sep 26 14:20 14:45 15.2.3 TOWARDS THE INTEGRATION OF NEUROPHYSIOLOGICAL SIGNALS AND HUMAN BODY DYNAMICS FOR ADAPTIVE CONTROL ALLOCATION
T. Treichl, German Aerospace Center, Germany; T.S. Paul, Thales France, France
14. Sep 26 14:45 15:10 15.2.4 VLSEC: A CONCEPT FOR SECURING VIRTUAL LINKS IN AVIONICS NETWORKS THROUGH CENTRALIZED GROUP KEY MANAGEMENT
C.A. Dautel¹, M. Werthwein¹, M. Homolya¹, M. Lehmann¹, S. Queiroz¹, B. Annighoefer¹; ¹University of Stuttgart, Institute of Aircraft Systems (ILS), Germany

15:10 - 15:15CHANGEOVER BREAK

0.4GENERAL LECTURE 2 Airbus 400M by Francisco Hernandez
Chair: G. Holmberg ICAS PC 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): Haselbach, F., Drake, M.
Track 1 Pyrmont Theatre
15 - Guest lectures
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 RR PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS
T Newby, Rolls-Royce plc, United Kingdom
14. Sep 26 17:20 17:45 1.3.3 CFM INTERNATIONAL'S RISE PROGRAM: A STEP-CHANGE FOR DURABILITY AND EFFICIENCY
C.-A. Andrews, GE Aerospace, United States
14. Sep 26 17:45 18:10 1.3.4 PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS FROM SAFRAN’S STANDPOINT
E. Dalbies, SAFRAN, France
2.3Digital Thread and Integration
Chair(s): Jouannet, C.
Track 2 C4.1
15 - Guest lectures
14. Sep 26 16:30 16:55 2.3.1 COMPUTATIONAL AVENUES TO ADVANCE DIGITAL CAPABILITIES AND EMPOWER SYNERGIES FOR THE BLUE SKIES
L. Mainini, please select...
14. Sep 26 16:55 17:20 2.3.2 MBSE AS A KEY ENABLER IN AEROSPACE DIGITAL ENGINEERING
A. Habibi Husain, please select...
14. Sep 26 17:20 17:45 2.3.3 DIGITAL ENGINEERING FOR TRANSFORMATIVE AEROSPACE
O. Pinon-Fischer, United States
3.3Conceptual Design 2
Chair(s): Alexander, M., Bagassi, S.
Track 3 C4.2
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
G. Palaia, Politecnico di Torino, Italy; K. Abu Salem, University of Trento, Italy; A.A. Quarta, University of Pisa, Italy; P.D. Bravo-Mosquera, São Carlos School of Engineering, University of São Paulo, Brazil
14. Sep 26 16:55 17:20 3.3.2 AGENTIC AI FOR AIRCRAFT PRELIMINARY DESIGN: PROOF OF CONCEPT
A. Kirste¹, L. Faltum¹, E. Stumpf¹; ¹Institute of Aerospace Systems, 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, W.I. Choi¹, 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 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 16:30 16:55 4.3.1 FLIGHT TESTING OF A HIGH-ALTITUDE UNCREWED AND SOLAR POWERED PLATFORM HEAVIER THAN AIR
F. Nikodem¹, C. Weiser¹; ¹DLR e.V., Germany
Presenter: Christian Weiser, DLR e.V.
14. Sep 26 16:55 17:20 4.3.2 CONCEPTUAL DESIGN OF A MIDDLE-OF-THE-MARKET AIRCRAFT FOR EDUCATIONAL PURPOSES
A.S.J. van Heerden¹, N.M. Ahamad¹, J.F. Castiblanco Aponte¹, J. Gibbs¹, I.J. Taylor¹; ¹University of Glasgow, United Kingdom
14. Sep 26 17:20 17:45 4.3.3 INVESTIGATING A STABLE LIFTING FUSELAGE FOR A TWO SEAT SAILPLANE OF THE GULL WING CONFIGURATION
B.-B. Huyssen¹, D. Fenthum¹, J. Huyssen, CSIR, South Africa; ¹University of Pretoria, South Africa
14. Sep 26 17:45 18:10 4.3.4 PROPOSING A STABLE LIFTING FUSELAGE FOR AN AIRLINER OF THE IDEAL AIRCRAFT CONFIGURATION
Joachim Huyssen, CSIR, South Africa; Eduard van Heerden, University of Pretoria, South Africa
5.3Buffeting and Other Aeroelastic Analyses
Chair(s): Slotnick, J., Azevedo, J.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
14. Sep 26 16:30 16:55 5.3.1 TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT
M. Candon¹, T. Gerner¹, A. Das¹, Z. Hoffman¹, P. Marzocca¹, L. Munholand², V. Viti², E. H. Dowell, Duke University, United States; ¹RMIT University, Australia ;²ANSYS, United States
14. Sep 26 16:55 17:20 5.3.2 HIGH-FIDELITY ANALYSIS OF AIRCRAFT TAIL BUFFETING UNDER DYNAMIC MANEUVERING
M.R. Rajanna¹, J. Lua¹, N. Phan, Naval Air System Command, United States; M.-C. Hsu, Iowa State University, United States; ¹Global 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. Palma¹, L. Pirillo¹, M. Bernardini¹, F. Stella¹; ¹Sapienza university of Rome, Italy
14. Sep 26 17:45 18:10 5.3.4 AILERON EFFICIENCY ANALYSIS OF FLEXIBLE HIGH-ASPECT-RATIO WING
Y. Zhao¹, J. He¹, X. Wei¹, T. Chen¹, Y. Yang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 5.3.R COST-EFFECTIVE CFD REPRODUCTION OF DPW-7 CASE 2A FOR CRM TRANSONIC PITCHING-MOMENT PREDICTION AND ADAPTIVE-REFINEMENT ASSESSMENT
G.C. Ribolla¹, L.J.F. Meirelles¹, L.F.S. Gomes¹, M.B. Stergiou¹, R.M. Granzoto, Embraer, Brazil; P. Bufacchi¹; ¹Insper, Brazil
6.3Hypersonics Boundary Layer and Flow Features
Chair(s): , , Vijgen, P.
Track 6 C4.5
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
G. Jiang¹, M. Dong¹; 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
7.3High-Performance and Laminar Flow Wing Design
Chair(s): Rivers, M.
Track 7 C4.6
03.4 - Applied Aerodynamics
14. Sep 26 16:30 16:55 7.3.1 SWEEP ANGLE STUDY OF A STRUT-BRACED-WING REGIONAL JET WITH NATURAL LAMINAR FLOW
N. Saadeh¹, D.W. Zingg¹; ¹University of Toronto, Canada
14. Sep 26 16:55 17:20 7.3.2 AERODYNAMIC SHAPE OPTIMIZATION OF INFINITE SWEPT WINGS FOR NATURAL LAMINAR FLOW AT TRANSONIC CRUISE CONDITIONS
F. Husain¹, D.W. Zingg¹; ¹University 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
A. Heletkanycz¹, C.J. Axten¹, J.G. Coder¹; ¹Penn State University, United States
14. Sep 26 17:45 18:10 7.3.4 VORTEX TOPOLOGY AND CORE-UNWINDING MECHANISM IN SPIROID WINGTIP DEVICES USING LAGRANGIAN PARTICLE TRACKING
M.A. Mwasandube¹, M. Marino¹, J.L. Palmer¹; ¹RMIT University, Australia
8.3Aerospace-Grade Composites
Chair(s): Bayandor, J., Denquin, A.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
14. Sep 26 16:30 16:55 8.3.1 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 16:55 17:20 8.3.2 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
14. Sep 26 17:20 17:45 8.3.3 ENHANCEMENT AND DEGRADATION: THE DUAL ROLE OF GRAPHENE NANOPLATELETS ON THE STRUCTURAL PERFORMANCE OF COMPOSITE T-JOINTS AND MECHANISTIC INSIGHTS
M. Bhasin¹, A.P. Mouritz¹; ¹RMIT University, Australia
Presenter: Mukesh Bhasin, RMIT University
14. Sep 26 17:45 18:10 8.3.4 NUMERICAL SIMULATION OF STRESS-OXIDATION DAMAGE IN C/SIC COMPOSITES AT HIGH TEMPERATURES
G. Chen¹, L. Yao¹, B. Li¹, X. Tong¹; ¹Northwestern Polytechnical University, China
9.3Health Monitoring
Chair(s): Alaimo, A., Coppotelli, G.
Track 9 C4.8
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. Niessen¹, D. 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
G. Dessena¹, M. Civera², E.P. Mottola², O.E. Bonilla-Manrique¹; ¹Universidad Carlos III de Madrid, Spain ;²Politecnico di Torino, Italy
14. Sep 26 17:20 17:45 9.3.3 SEMI-SUPERVISED MULTI-TASK CONSISTENCY LEARNING FOR DEFECT DETECTION AND DEPTH ESTIMATION
S. Miao¹, Y. Ge¹, Y. Pei¹; ¹Northwestern 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): Bezos O Connor, G.
Track 10 C4.9
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 PROPULSION SYSTEM FOR AIRCRAFT APPLICATIONS FOCUSING ON WATER MANAGEMENT
S. Bäumler, Chair of Electrified Aero Engines, BTU Cottbus-Senftenberg, Germany; S. Kazula¹, A. Zwingler, Department of Mechanical Engineering, TU Munich, Germany; L. Enghardt¹; ¹DLR Institute of Electrified Aero Engines, 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. Sain¹, S. Bhapkar¹, M. Kober¹, S. Kazula¹; ¹German Aerospace Center (DLR), Germany
14. Sep 26 17:20 17:45 10.3.3 THERMAL–HYDRAULIC OPTIMIZATION OF AXIALLY GRADED OFFSET STRIP-FIN HEAT EXCHANGERS FOR MEGAWATT-CLASS FUEL CELL ELECTRIC AIRCRAFT
S. Bhapkar¹, C. Sain¹, M. Kober¹, S. Kazula¹; ¹German Aerospace Center, Germany
Presenter: Chetan Sain, German Aerospace Center
11.3Flight Control 3
Chair(s): Kim, S., Kiszkowiak, L.
Track 11 C4.10
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. Szymanski¹, V. Gollnick¹; ¹Hamburg University of Technology, Germany
14. Sep 26 16:55 17:20 11.3.2 AUTOPILOT DESIGN OF AN UNSTABLE FIGHTER USING MODEL PREDICTIVE CONTROL
M.T. Morales¹, M.A. Rempel, Embraer, Brazil; M.A.V. Morales¹, J.E.M. Fernandes¹; ¹ITA, Brazil
14. Sep 26 17:20 17:45 11.3.3 KNOW YOUR LIMITS: ESTIMATING THE TILT-WING TRANSITION CORRIDOR UNDER FAILURE CONDITIONS
M. May¹, D. Milz¹, S.F. Armanini, Imperial College London, Germany; ¹German Aerospace Center (DLR), Germany
14. Sep 26 17:45 18:10 11.3.4 ROBUST ATTITUDE RECOVERY CONTROL FOR AIR-LAUNCHED FOLDING-WING UAVS VIA DISTURBANCE-COMPENSATED SUPER-TWISTING SLIDING MODE
S.W. Han¹, T.L. Ma¹, J.C. Fu¹, X.O. Zhang¹, Q.L. Zhang¹, L.Z. Wang¹; ¹Beihang University, China
12.3Actuation Fault and Optimization
Chair(s): Viola, N.
Track 12 C2.3
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
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
I.O. Skusa, ITA/Embraer, Brazil; R.N. Calvo, Embraer, Brazil; A.A. Filho, ITA, Brazil
Presenter: Isabella Ono Skusa
14. Sep 26 17:20 17:45 12.3.3 PERFORMANCE DEGRADATION ANALYSIS OF RESOLVER FAULTS IN ELECTRO-MECHANICAL ACTUATOR
S. Guan¹, J. Fu¹, T.Q. Yang¹, Z.H. Ge¹, T.Y. Zhang², Z.Y. Zhao²; ¹Beihang University, China ;²AVIC Shenyang Aircraft Design Institute, China
Presenter: Taoqing YANG, Beihang University,
14. Sep 26 17:45 18:10 12.3.4 MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEMS
T.Q. Yang¹, J. Fu¹, S. Guan¹, J. Pan², C.F. Yao², H.L. Qu²; ¹Beihang University, China ;²AVIC Xi'an Flight Automatic Control Research Institute, China
additional information (interactive) 12.3.R INTEGRATED CONTROL STRATEGY BASED ON PHYSICS-INFORMED MODEL-BASED REINFORCEMENT LEARNING FOR AIRBORNE HIGH-ENERGY SYSTEMS
S. Bai¹, Y. Li¹, L. Jiang¹, Z. Li¹, K. He¹, Z. Jiao¹; ¹Beihang University, China
13.3Pathways for Sustainable Aviation
Chair(s): Andreeva-Mori, A.
Track 13 C2.4
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, Qantas Airways Limited, Australia
14. Sep 26 16:55 17:20 13.3.2 GLOBAL EMISSION MONITOR FOR 2023
M. Clococeanu¹, C.M. Weder¹, H. Bruder¹, Z.L. Zengerling¹; ¹German Aerospace Center, Germany
Presenter: Maximilian Clococeanu, Deutsches Zentrum für Luft- und Raumfahrt e.V.
14. Sep 26 17:20 17:45 13.3.3 JOINT TRAJECTORY OPTIMIZATION AND DECONFLICTION FOR CLIMATE IMPACT MITIGATION
T. Ehlers¹, A. Lau¹, M. Mendiguchia Meuser¹, A. Kuenz¹, S. Dietmüller¹, S. Matthes¹; ¹DLR, Germany
14. Sep 26 17:45 18:10 13.3.4 CLIMATE HAZARD TIMING AND FLIGHT DEMAND COOCCURRENCE: A DEMAND-WEIGHTED EXPOSURE FRAMEWORK
K. Sumaja¹, T.-R.T. Koo¹, S. Mooney, School of Biological, Earth and Environmental Sciences, UNSW, Australia; T.H. Rashidi¹; ¹School of Civil and Environmental Engineering, UNSW, Australia
14.3Launch and Recovery
Chair(s): Gerner, T., Palmer, J.
Track 14 C2.5
06.2 - Flight Dynamics and Control (UAV related)
14. Sep 26 16:30 16:55 14.3.1 A SIMULATION METHODOLOGY FOR MULTIROTOR-ASSISTED UAV LAUNCH
A.G.P. Sarmento¹, C.C. Duarte da Silva¹, G.V. Ferreira¹, E. Villani¹, D. Rade¹; ¹Aeronautics Institute of Technology (ITA), Brazil
Presenter: Caroline Cristine Duarte da Silva, Aeronautics Institute of Technology (ITA)
14. Sep 26 16:55 17:20 14.3.2 AUTONOMOUS PATH PLANNING ALGORITHM FOR EMERGENCY LANDING OF AAM CONSIDERING WIND DISTURBANCES
H. Iwamoto¹, N. Yokoyama, Japan Aerospace Exploration Agency, Japan; T. Higuchi¹; ¹Yokohama National University, Japan
14. Sep 26 17:20 17:45 14.3.3 ASSESSMENT OF THE LANDING CAPABILITIES OF A FLEXIBLE HIGH-ALTITUDE PLATFORM AT LONGITUDINAL AND LATERAL-DIRECTIONAL WIND DISTURBANCES
Y.J. Hasan, DLR Institute of Flight Systems, Germany
14. Sep 26 17:45 18:10 14.3.4 DECOUPLED DEEP REINFORCEMENT LEARNING FOR AUTONOMOUS LANDING OF UAVS ON SHIPS
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
15.3Human Factors, Workload, and Cognition
Chair(s): Fadda, T.
Track 15 C2.6
10 - Safety and Security
14. Sep 26 16:30 16:55 15.3.1 QUANTIFYING THE EFFECT OF IN-CABIN AIRCRAFT NOISE ON COGNITION.
Brett R.C. Molesworth, UNSW Sydney, School of Aviation, Australia; Marion Burgess, UNSW Sydney, School of Built Environment, 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
C.R. Vindigni¹, A. Esposito¹, C. Orlando¹, A. Alaimo¹; ¹University of Enna Kore, Italy