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:
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
14. Sep 26 09:55 10:20 1.1.1
1020		 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
0986		 JAL’ CHALLENGE TO THE NET-ZERO GH GAS EMISSION
MS Suzuki, JAL, Japan
14. Sep 26 10:45 11:10 1.1.3
1019		 THE WHOLE JOURNEY: PEOPLE, PLANET AND PROGRESS AT QANTAS
Hudson, Qantas Group, Australia
14. Sep 26 11:10 11:35 1.1.4
1028		 PANEL DISCUSSION Q&A WITH THE AIRLINES
P Panel,
2.1Progress in Certification
Chair(s): ,
Track 2
15 - Guest lectures
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. Moruzzi¹, T. Fadda¹, E. Caligari¹, S. Bagassi¹; ¹Università 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 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
0406		 ASSESSING THE POTENTIAL OF MULTI-MODEL TOPOLOGY OPTIMIZATION FOR MODULAR LIGHTWEIGHT DESIGN OF AIRCRAFT CABIN STRUCTURES
P. Inselmann¹, F.-D. Bischop¹, F.-H. Christiansen¹, D. Krause¹; ¹Hamburg University of Technology, Germany
14. Sep 26 11:10 11:35 3.1.4
0348		 A FRAMEWORK FOR AUTOMATED SYSTEM COMPONENT PLACEMENT IN AIRCRAFT CONCEPTUAL DESIGN
J. Vézina¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada
Reserve Paper 3.1.R
0604		 MULTI-STATE FLIGHT DECK DISPLAY LAYOUT OPTIMIZATION UNDER FAILURE AND REVERSION SCENARIOS
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
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
14. Sep 26 09:55 10:20 4.1.1
0187		 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
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
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
0482		 RESEARCH ON OVERALL AERODYNAMIC DESIGN OF GRID-DUCT INTEGRATED VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING AIRCRAFT
LI BOLE, 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
0368		 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 5.1.2
0267		 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 10:45 11:10 5.1.3
0168		 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
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
H. Wang¹, T. Lin¹, G. Wang¹, L. Xu¹; ¹Northwestern Polytechnical University, China
Presenter: Huiyue Wang, Northwestern Polytechnical University
additional information (interactive) 5.1.R
0939		 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): 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
Yiming Wu¹, Zhenglin Xiao¹, Yang Xiang¹, Ziyi Zhu¹; ¹Shanghai Jiao Tong University, China
14. Sep 26 10:20 10:45 6.1.2
0228		 NONLINEAR 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
0637		 THIN AEROFOILS OSCILLATING IN A CONFINED INVISCID FLOW
J Mourad¹, V Ferrand¹, E.-R Gowree¹; ¹ISAE-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. ANILIR¹, D. F. KURTULUS¹, M. F. PLATZER, University of California, Davis, United States; ¹Middle East Technical University, 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.-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
0200		 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
0444		 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
0516		 AERODYNAMIC EFFECTS OF DISTRIBUTED PROPELLER PLACEMENT ON LIFT CHARACTERISTICS OF A WING–FLAP 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
Reserve Paper 7.1.R
0297		 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
0507		 LASER SCANNING STRATEGIES TO INVESTIGATE THE EFFECTS OF OXIDATION IN PURE TANTALUM
M Davids, HH Industries, University of Cape Town, South Africa; J Strauss¹, D Hagedorn-Hansen¹, T. H Becker, University of Cape Town, South Africa; ¹HH 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
S.H. 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 Koutsambasis¹, M Marino¹, N.J. Brown¹, W Wu¹; ¹RMIT University, Australia
Reserve Paper 8.1.R
0250		 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
0046		 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
0076		 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
0671		 COARSE–FINE COUPLED MBSE FOR SURVIVABILITY PARAMETER DESIGN OF STEALTH CARRIER-BASED TANKER
PF LI¹, WZ LIU¹, BL SHANG¹, YZ WANG¹, RX LIN¹; ¹Northwestern Polytechnical 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.J. Kim¹, J.H. Shin¹; ¹Chungbuk national University, South Korea
14. Sep 26 10:20 10:45 10.1.2
0648		 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
1033		 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): ,
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
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
0647		 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
0843		 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
0425		 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): ,
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. Schmitz¹, I. Pruter¹, H. Duda¹, M. Laubner¹, S. Lorenz¹; ¹DLR e.V., Germany
14. Sep 26 10:20 10:45 12.1.2
0684		 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
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
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
Reserve Paper 12.1.R
0590		 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
Reserve Paper 12.1.R
0921		 DEVELOPMENT OF A MODULAR SENSOR FUSION PAYLOAD FOR FLIGHT TESTING OF VISUAL-INERTIAL NAVIGATION ALGORITHM IN SMALL UAVS
Aziz Fathurrahman¹, Yazdi Ibrahim Jenie¹, Ony Arifianto¹, Hari Muhammad¹; ¹Institut 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
Hiroki Akiyama¹, Seiya Ueno¹, Takehiro Higuchi¹, Tomohiro Sakurai¹; ¹Yokohama 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; R. Mori, Kobe University, Japan
14. Sep 26 11:10 11:35 13.1.4
0216		 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
0143		 MULTI-CAMERA PANORAMIC SENSING FOR LOCALISATION AND MULTI-OBJECT TRACKING IN UAVS
Rafal Perz, WUT, Institute of Aeronautics and Applied Mechanics, Poland; Pawel Wozniak¹, Igor Dabrowski², Julian Konowalski², Konrad Barys², Artur Abratanski², Lukasz Popek², Jakub Swierk¹, Rafal Chalupczynski¹; ¹Uavionics Ltd Poland, Poland ;²Rafal Perz Scientific Network, 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. 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
0737		 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
0096		 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
0288		 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
0649		 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
0210		 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
0536		 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
0782		 RINGCO-DETR: INFERENCE-NEUTRAL STABILIZATION OF ORIENTED TRANSFORMER DETECTION FOR AERIAL SENSING
JIANQIN GAO¹, TianQi Wang, Taiyuan University of Technology, China; Hongyi Gao¹, Yujie Ding¹, Zihao Wang¹; ¹ University of Sydney, Australia
14. Sep 26 11:10 11:35 15.1.4
0942		 ADVANCING TRUST FOR THRUST: PAIRING AND SHARING
L.J.A. Jansen¹, T. Strang¹; ¹German 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
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
14. Sep 26 13:55 14:20 1.2.2
1023		 AIRBUS PRODUCT DEVELOPMENT - CHALLENGES AND OPPORTUNITIES IN SUSTAINABILITY
V Roca, Airbus SAS, France
14. Sep 26 14:20 14:45 1.2.3
1026		 EMBRAER\'S PERSPECTIVES & PROGRESS TOWARDS NEXTGEN AIRLINERS
C Silva, Embraer, Brazil
14. Sep 26 14:45 15:10 1.2.4
1029		 PANEL DISCUSSION Q&A WITH THE AIRCRAFT OEMS
P Panel,
2.2High Speed Flight – Overview
Chair(s): ,
Track 2
15 - Guest lectures
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
Jun-zhe:J.-Z, Zhang¹, Zhong-Hua:Z.-H. Han¹, Wen-Ping:W.-P. Song¹, Ke-shi:K.-S. Zhang¹, Yang:Y. Zhang¹; ¹Northwestern Polytechnical University, China
14. Sep 26 13:55 14:20 3.2.2
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 14:20 14:45 3.2.3
0285		 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 14:45 15:10 3.2.4
0229		 FORMALIZING THE INTEGRATION BETWEEN MODEL-BASED SYSTEMS ENGINEERING AND SYSTEM ARCHITECTURE OPTIMIZATION
S Valencia-Ibáñez¹, S Liscouët-Hanke¹; ¹Concordia University, Canada
Reserve Paper 3.2.R
0015		 SCENARIO-BASED TECHNOLOGY ROADMAPPING IN AEROSPACE USING DBSCAN AND LLM
T. A. Brutscher, Liebherr-Aerospace Lindenberg GmbH, Germany
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
J.L.C Chan¹, H Smith¹; ¹Cranfield 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 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
0926		 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
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. Parra¹, D. Domínguez¹, A. Delgado¹, J. Gonzalo¹; ¹Universidad de León, Spain
14. Sep 26 14:20 14:45 5.2.3
0463		 RESEARCH ON TRANSITION PREDICTION METHODS FOR HELICOPTER ROTOR BLADES
Kang-Yuan:K.-Y. Zhou¹, Wen-Ping:W.-P. SONG¹, Jian-Hua:J.-H. Xu¹; ¹Northwestern Polytechnical University, 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 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
0185		 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
0255		 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
0374		 REDUCED-ORDER MODELLING OF MINI-TAB SPOILER DYNAMICS FOR GUST LOAD ALLEVIATION
A. Jürisson¹, P. H. L. Blom¹; ¹Royal 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
Hao Yan¹, Haoran Zheng¹, Zheyuan Dong¹, Wei Dong¹; ¹Shanghai 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
Z.Y. Dong, China; H.R Zheng, China; H. Yan, China; W. Dong, China; P.Y. Wang, 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. Chen¹, Z.H. Han¹, K.S. Zhang¹, K. Song¹; ¹Northwestern Polytechnical University, 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
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 Kannan, The University of Sydney, Australia; A Bettens, Deneb Space, Australia
14. Sep 26 13:55 14:20 8.2.2
0160		 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
0036		 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
0082		 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
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. 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
0607		 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
0910		 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
0918		 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
10.2Machine 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
R 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. Han¹, S. Kim¹, M. Jung¹, J. Woo¹, S. Jung, APPIA Engineering Co., Ltd., South Korea; H. Bang¹; ¹Korea Advanced Institute of Science and Technology, 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. Kim¹, J. D. Lee¹, H. Lee¹, Y. Kim¹, H. Bang¹; ¹KAIST, 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
Divya Sanghi, United States; Carlos E. S. Cesnik, United States
additional information (interactive) 10.2.R
0109		 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
0440		 STABILITY AUGMENTATION SYSTEM DESIGN FOR LONGITUDINALLY UNSTABLE TAILLESS AIRCRAFT
Stefan Riethausen¹, David Lundström¹, Petter Krus¹; ¹Linköping University, Sweden
14. Sep 26 13:55 14:20 11.2.2
0123		 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 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.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
0441		 FLIGHT ENVELOPE PROTECTION FOR HIGH ALTITUDE LONG ENDURANCE AIRCRAFT
C. Weiser, German Aerospace Center (DLR), 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
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
0186		 ICE DETECTOIN: CORRELATION ICE ACCRETIONS AND DYNAMIC RESPONSES ON SMALL-SCALE AIRFOIL PROTOTYPES
L. Mangiacrapa¹, T. Klaas², N. Rehfled², 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
0660		 A MPC STRATEGY FOR THE VECTOR CONTROL OF RESONANT ELECTROMECHANICAL DE-ICING SYSTEMS
A. SUTI¹, J. POTHIN², M. BUDINGER¹, V. POMMIER-BUDINGER², A. REYSSET¹; ¹INSA Toulouse, France ;²Isae Supaero, 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
Simon Goeppel¹, Ehsan Asadi¹, Eri Itoh, he University of Tokyo, Japan; Michael 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
0408		 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
0446		 AIRCRAFT SEQUENCING UNDER UNCERTAINTY: GAME-THEORETIC OPTIMIZATION AND A COMPARATIVE ANALYSIS OF GLOBAL AND INTRA-AIRLINE COOPERATIVE DECISION FRAMEWO
Sakura Tsuru¹, Adriana Andreeva-Mori¹; ¹Osaka 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. Matsuno¹, H. Matsuda¹; ¹Japan Aerospace Exploration Agency, Japan
Reserve Paper 13.2.R
0893		 AIRCRAFT CLIMB PROFILE PREDICTION VIA MACHINE LEARNING-BASED FRAMEWORK
H Seon¹, K Lee¹, M Brown², H Hirabayashi²; ¹Korea Aerospace University, South Korea ;²Electronic Navigation Research Institute, Japan
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
Z. Lin¹, D. Geraghty¹, S. F. Armanini¹, L. Mainini¹; ¹Imperial College London, United Kingdom
14. Sep 26 13:55 14:20 14.2.2
0709		 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
0695		 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
0079		 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
0477		 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
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 13:55 14:20 15.2.2
0307		 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
0363		 TOWARD THE INTEGRATION OF NEUROPHYSIOLOGICAL SIGNALS AND HUMAN BODY DYNAMICS FOR ADAPTIVE CONTROL ALLOCATION
Tobias Treichl, German Aerospace Center, Germany; Tanya Sarah Paul, Thales France, France
14. Sep 26 14:45 15:10 15.2.4
0701		 A CENTRALIZED KEY MANAGEMENT ARCHITECTURE FOR SECURE GROUP COMMUNICATION ON IMA PLATFORM
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 David Ferro Romero and 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
14. Sep 26 16:30 16:55 1.3.1
1037		 RR PERSPECTIVES & PROGRESS ON NEXTGEN PROPULSION FOR FUTURE AIRLINERS
T Newby, Rolls-Royce plc, United Kingdom
14. Sep 26 16:55 17:20 1.3.2
1008		 PRATT & WHITNEY: MEETING THE FUTURE PROPULSION NEEDS OF COMMERCIAL AVIATION
A.M. Murphy, Pratt & Whitney, United States
14. Sep 26 17:20 17:45 1.3.3
1010		 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
1030		 PANEL DISCUSSION Q&A WITH THE PROPULSION OEMS
P Panel,
2.3Digital Thread and Integration
Chair(s): ,
Track 2
15 - Guest lectures
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. Kirste¹, L. Faltum¹, E. Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany
14. Sep 26 17:20 17:45 3.3.3
0668		 AI-SUPPORTED AIRCRAFT SYSTEM ARCHITECTURE SYNTHESIS
Petter 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. 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
0792		 CONCEPTUAL DESIGN OF A PROPFAN-POWERED TRUSS-BRACED WING REGIONAL AIRCRAFT
E. MAROOFIZADEH, Iran; S. Hosseini¹, M. A. Vaziry-Zanjany¹; ¹Tehran Polytechnic, Iran
14. Sep 26 16:55 17:20 4.3.2
0296		 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 17:20 17:45 4.3.3
0420		 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
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
0183		 TRANSONIC BUFFET AND STATIC AEROELASTIC RESPONSE OF A COMMERCIAL TRANSPORT AIRCRAFT
M. Candon¹, T. Gerner¹, Z. Hoffman¹, A. Das¹, 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
0927		 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
0282		 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
0796		 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
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; L. Zhao, Departiment of Mechanics, Tianjin University, 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
Jiang Genrui¹, Dong Ming¹; ¹Institute 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. Shi¹, C. Song¹, H. Xiao¹; ¹Northwestern 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. Chen¹, M.S. He¹, B. Yu¹, W. Wang¹, H. Liu¹; ¹Shanghai 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
Romie Oktovianus Bura, Republic of Indonesia Defense University, Indonesia; Wahyu Widhi Dyatmika, Indonesia Aerospace Industry, 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		 SWEEP ANGLE STUDY OF A 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
0087		 AERODYNAMIC SHAPE OPTIMIZATION OF INFINITE SWEPT WINGS FOR NATURAL LAMINAR FLOW AT TRANSONIC CRUISE CONDITIONS
Fizaa Husain¹, David W. Zingg¹; ¹University 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
A. Heletkanycz¹, C. J. Axten¹, J. G. Coder¹; ¹Penn 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
Merina Amon Mwasandube¹, 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 16:05 16:30 8.3.1
0493		 MODELING CREEP DEFORMATION AND PREDICTING RUPTURE LIFE OF STRESS-CONCENTRATED DZ411 SUPERALLOY COMPONENTS USING A THREE-STAGE CREEP FRAMEWORK
Zhikun Li¹, Dasheng Wei¹, Wu Zeng, Chinese Academy of Sciences, China; KarKash Alynur¹, Xin Liu¹, Bin Zhao¹, Suqi Li¹, Li Ma, KUCH ENERGY Technology Co., Ltd., China; Shun Yang¹; ¹Beihang University, China
14. Sep 26 16:05 16:30 8.3.2
0940		 A PROCESS-STRUCTURE-PROPERTY-PERFORMANCE FRAMEWORK FOR DIGITAL ENGINEERING-ENABLED FABRICATION AND REPAIR OF ALUMINUM PARTS
J. Lua¹, M. 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 16:05 16:30 8.3.3
0172		 FRACTURE AND GRAIN BOUNDARY DAMAGE IN AM NI-BASED SUPERALLOYS UNDER HIGH-TEMPERATURE TENSILE LOADING
X Liu¹, DS Wei¹, SZ Jin, AVIC Manufacturing Technology Institute, China; S Yang¹, DX Yin², B Niakate², D Lasne²; ¹Beihang university, China ;²BSS Turbotech Ltd., China
14. Sep 26 17:45 18:10 8.3.4
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. Niessen¹, D.O. Franke¹; ¹Defence 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. 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
0072		 MTCL FOR COMPOSITE DAMAGE
Shimeng Miao¹, Yuxue Ge¹, Yang Pei¹; ¹Northwestern 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. 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
0139		 IMPACT ASSESSMENT OF COMPONENT FAILURES IN A PEM-FUEL CELL BASED PROPULISON SYSTEM FOR AIRCRAFT APPLICATIONS
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
0652		 NUMERICAL AND EXPERIMENTAL EVALUATION OF COMPACT TPMS AND OFFSET-STRIP-FIN HEAT EXCHANGERS FOR FUEL CELL SYSTEM COOLING IN AN ELECTRIC AIRCRAFT
Chetan Kumar Sain¹, Sahil Bhapkar¹, Markus Kober¹, Stefan Kazula¹; ¹German 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
Sahil Bhapkar¹, Chetan Sain¹, Markus Kober¹, Stefan Kazula¹; ¹German Aerospace Center, Germany
Presenter: Chetan Sain, German Aerospace Center
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
Sasmitha 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
0891		 DATA-DRIVEN SYNTHESIS OF AIRCRAFT FEEDBACK CONTROL LAWS FOR NEW COMMERCIAL FLIGHT SCENARIOS
M. W. Szymanski¹, V. Gollnick¹; ¹Hamburg 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 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
0152		 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
0506		 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): ,
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. 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
0683		 OSCILLATORY FAILURE DETECTION IN AIRCRAFT ACTUATION SYSTEMS USING WAVELET TRANSFORM
I.O. Skusa, ITA/Embraer, Brazil; R.N. Calvo, Embraer, Brazil
Presenter: Isabella Ono Skusa
14. Sep 26 17:20 17:45 12.3.3
0784		 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
14. Sep 26 17:45 18:10 12.3.4
0961		 MECHANISM-DATA FUSION MODELING METHOD FOR AEROSPACE ELECTROMECHANICAL ACTUATOR 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
Reserve Paper 12.3.R
0904		 PRACTICAL ASPECT OF FLIGHT TESTING DRONE NAVIGATION SYSTEMS UNDER GPS-DENIED CONDITIONS
Y.I. Jenie¹, A. Fathurrahman¹, O. Arifianto¹, H. Muhammad¹; ¹FTMD, Institut Teknologi Bandung, Indonesia
additional information (interactive) 12.3.R
0621		 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
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
s. Sukkarieh, University of Sydney, 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
Presenter: Maximilian Clococeanu, Deutsches Zentrum für Luft- und Raumfahrt e.V.
14. Sep 26 17:20 17:45 13.3.3
0212		 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
0870		 EXPOSURE-AWARE COMPOUND CLIMATE HAZARDS FOR AIRPORTS: A TIERED EXTREMES FRAMEWORK LINKED TO FLIGHT TRAFFIC
Kadek Sumaja¹, Tay Koo¹, Scott Mooney, School of Biological, Earth and Environmental Sciences, The Univ, Australia; Taha H. Rashidi¹; ¹Research Centre for Integrated Transport Innovation (rCITI), Sch, 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. 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
0937		 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
14. Sep 26 17:20 17:45 14.3.3
0248		 AUTONOMOUS PATHPLANNING ALGORITHM FOR EMERGENCY LANDING OF AAM CONSIDERING WIND DISTURBANCES
Hikaru Iwamoto¹, Nobuhiro Yokoyama, Japan Aerospace Exploration Agency, Japan; Takehiro Higuchi¹; ¹Yokohama National University, 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 Institute of Flight Systems, 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.-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
0118		 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
0422		 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

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 Benameur¹, M Jacinto, TU Wien, Austria; L Bertsch², B Schuchardt², F Simon¹; ¹ONERA, France ;²DLR, Germany
Presenter: Kaouthar Benameur, ONERA
15. Sep 26 09:20 09:45 1.4.2
0345		 CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION
B.I. Schuchardt¹, A.J. Torija, University of Salford, United Kingdom; I. Legriffon, Office National d’Études et de Recherches Aérospatiales (ONERA), France; D. Casalino, Delft University of Technology, Netherlands; L. Bertsch¹, R. Aalmoes, Netherlands Aerospace Centre (NLR), Netherlands; ¹German Aerospace Center (DLR), Germany
15. Sep 26 09:45 10:10 1.4.3
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
W Klimczyk¹, P Kekus-Kumor¹, M Rajek¹, A Sieradzki¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland
Presenter: Witold Klimczyk, Lukasiewicz Research Network - Institute of Aviation
2.4Air transport resilience to climate change and weather hazards
Chair(s): ,
Track 2
15 - Guest lectures
15. Sep 26 08:55 09:20 2.4.1
0994		 COMBINED IMPACT OF JET STREAM AND TURBULENCE ON LONG-TERM TRANS-OCEANIC FLIGHT ROUTES
J.-H. Kim, Seoul National University, South Korea
15. Sep 26 09:20 09:45 2.4.2
0997		 PROGRESS IN AIRCRAFT-BASED METEOROLOGICAL OBSERVATIONS
T.F. Rahmes, The Boeing Company, United States
15. Sep 26 09:45 10:10 2.4.3
1035		 ADAPTING AVIATION TO A CHANGING CLIMATE: A GLOBAL AND REGIONAL PERSPECTIVE
R. Burbidge, EUROCONTROL, Belgium
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
0915		 IMPLEMNTATION OF PROPELLER-WING INTERFERENCE MODEL AND HORIZONTAL TAIL ANALYSIS INTO A VISCOUS FULL POTENTIAL FLOW SOLVER FRAMEWORK FOR AIRCRAFT DESIG
T.A. Ramprakash¹, D Di Pasquale¹, S Kumar¹; ¹Cranfield University, United Kingdom
15. Sep 26 09:20 09:45 3.4.2
0837		 IMPACT OF DIFFERENT PROPELLER CONFIGURATIONS ON THE FLIGHT DYNAMICS AND STABILITY OF A SMALL REGIONAL ELECTRIC AIRCRAFT
G. Babunaidu¹, A. Hammad¹; ¹Technical University of Munich, Germany
15. Sep 26 09:45 10:10 3.4.3
0251		 PROPULSIVE EFFICIENCY AND ENERGY ANALYSIS OF AIRCRAFT CONCEPTS WITH AFT-FUSELAGE BOUNDARY-LAYER-INGESTION
C.Q. Zhou¹, Y.Y. Ma¹, Z.H. Han¹; ¹Northwestern Polytechnical University, China
15. Sep 26 10:10 10:35 3.4.4
0484		 RESONANT ELASTIC SHAFT THRUST VECTORING: IMPLICATIONS FOR UAV DESIGNS
Haofei Guan, Australia; KC Wong, 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. Türkyilmaz¹, M. G. Kolb¹, X. Zhao, Chalmers University of Technology, Sweden; M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
15. Sep 26 09:20 09:45 4.4.2
0213		 CHALLENGES AND SOLUTIONS FOR LIQUID HYDROGEN-POWERED UAVS: REGULATIONS AND CASE STUDY INSIGHTS
B. Legrand¹, N. Gavrilovic¹; ¹Département Aérodynamique, Energie et Propulsion, ISAE-SUPAERO, France
15. Sep 26 09:45 10:10 4.4.3
0333		 ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035
M. Kotzem¹, J. Häßy¹, V. Kriewall Peters, Hamburg University of Technology (TUHH), Germany; P. Schatrow¹, S. Wöhler¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 10:10 10:35 4.4.4
0316		 AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN
Andreas Tramposch¹, Fynn Thilker¹, Simon Pfeifer¹, Philip Kirschnek¹; ¹University of Applied Sciences FH Joanneum GesmbH, Austria
5.4Supersonic and Hypersonic Flows
Chair(s): Pezzella, G., 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
Gang Wang¹, Zhi-Kan Liu¹, Tian-Yu Lin¹, Hui-Yue Wang¹; ¹Northwestern 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. Poltronieri¹, F. C. Moreira¹, J. L. F. Azevedo¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
Presenter: Joao Azevedo, Instituto Tecnologico de Aeronautica
15. Sep 26 09:45 10:10 5.4.3
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
S. Gunasekaran, Cranfield Univeristy, United Kingdom; Z.A Rana, Prince Mohammad Bin Fahd University, Saudi Arabia; S. Prince, Cranfield University, United Kingdom
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
Santiago Montoya-Ospina¹, Romain Gojon¹, Hélène Parisot-Dupuis¹, Frank Simon, DMPE-ONERA, France; ¹ISAE-SUPAERO, 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. Li¹, Y. Yendrew¹, D. Moreau¹, C. Doolan¹; ¹University of New South Wales, 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. Peleshok¹, M. Hornung¹; ¹Technical 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, CRANKED SWEPT WING
N. van Luijk¹, A. van Meenen¹, R. Vos¹; ¹Delft University of Technology, Netherlands
15. Sep 26 09:20 09:45 7.4.2
0221		 INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFOMANCE AT LOW REYNOLDS NUMBER
M. Avirovic¹, C. Brunelli¹, B. G. Marinus¹, J. Degroote, University of Ghent, Belgium; J. van Beeck, von Karman Insititute for Fluid Dynamics , Belgium; E. Van Vaerenbergh¹; ¹Royal Military Academy, Belgium
15. Sep 26 09:45 10:10 7.4.3
0378		 EXERGY AND INTEGRAL BOUNDARY LAYER PARAMETERS CHARACTERISTIC CURVES FOR AERODYNAMIC DESIGN AND OPTIMIZATION
G. Bourreau-Tirel¹, S. Duplaa, ISAE-SUPAERO, France; J. P. Ruscio¹; ¹Aura Aero, France
15. Sep 26 10:10 10:35 7.4.4
0723		 PARAMETRIC AERODYNAMIC STUDY OF LEADING-EDGE SERRATIONS ON WING SECTIONS ACROSS REYNOLDS NUMBERS
J.J. Whittaker, University of New South Wales, 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 08:55 09:20 8.4.1
0115		 COMPOSITE FUSELAGE TECHNOLOGIES FOR NEXT GENERATION COMMERCIAL AIRCRAFT
Y. C. Roth, Airtbus Operations GmbH, Germany; P. Joern, Airbus Operations GmbH, Germany; A. Sadelfeld, Airbus Aerostructures GmbH, Germany; C. Rowedder, CTC GmbH, Germany; J. Buck, CTC GmbH, Germany; B. Demel, Airbus Helicopters Deutschland GmbH, Germany
15. Sep 26 09:20 09:45 8.4.2
0830		 FIVE DECADES OF T-38 WING TEARDOWNS
C King, United States Air Force, United States; I Grothe¹, P Clark, PhD¹, L Hunt¹; ¹Southwest Research Institute, United States
15. Sep 26 09:45 10:10 8.4.3
0071		 GEOMETRICALLY EXACT MODEL OF CANTILEVER BEAM UNDERGOING LARGE DEFLECTION AND LINEARIZED DYNAMICS CHARACTERIZATION
C.-Y. Yang¹, R. Zhao¹, Y.-S. Gu¹, Z.-C. Yang¹; ¹Northwestern Polytechnical University School of Aeronautics, China
Presenter: Changyun Yang, School of Aeronautics, Northwestern Polytechnical University
9.4Impact & Vibration 1
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 08:55 09:20 9.4.1
0290		 ENERGY ABSORPTION OF THIN-WALLED CONCENTRIC SPHERES FOR CARGO AIRDROP
A.E. Lloyd¹, K.C. Wong¹; ¹University of Sydney, Australia
15. Sep 26 09:20 09:45 9.4.2
0153		 GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL
Jianchun Yao¹, Giuliano Coppotelli, University of Rome, La Sapienza, Italy; Michael Candon¹, Mohammad Fard¹, Pier Marzocca¹; ¹RMIT University, Australia
15. Sep 26 09:45 10:10 9.4.3
0364		 NUMERICAL PREDICTION OF CABIN NOISE FOR FUTURE SHORT-HAUL AIRCRAFT IN EARLY AIRCRAFT DESIGN
Christian Hesse¹, Pia Allebrodt¹, Stanislav Proskurov¹, Björn Nagel¹; ¹DLR, 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. Zhang¹, K. Li, Shanghai University, China; M. Tong, Nanjing University of Aeronautics and Astronautics , China; W. Qu¹; ¹Zhejiang University, China
Presenter: Kun Li, Shanghai University
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
Shinichiro Ogawa¹, Takuto Hongo¹, Yasuaki Maeda¹, H. P. Uyen Nguyen¹, Koichi Mori¹; ¹Osaka 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
Xin Zhao, Chalmers University of Technology, Sweden; Evangelia Maria Thoma, GKN Aerospace Sweden AB, Sweden
Reserve Paper 10.4.R
0551		 EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY
P. Kirschnek¹, A. Görtz², M. Schmelcher², F. Thilker¹, J. Häßy²; ¹FH JOANNEUM, Austria ;²Deutsches Zentrum für Luft- und Raumfahrt, Germany
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.S. Lee¹, S.J. Kim¹, S.K. Kim¹; ¹Chungnam 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 Fuchsgruber¹, M Gerdts, University of the Bundeswehr Munich, Germany; F Holzapfel¹; ¹Technical University of Munich, Germany
15. Sep 26 09:45 10:10 11.4.3
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; S. Cho, Cheongju University, 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. Thöne¹, F. Abdelmoula¹, M. Gerber², A. Winhard², F. Schwerzmann², C. Deiler¹; ¹German Aerospace Center - DLR, Germany ;²Swiss Skylab Foundation, Switzerland
15. Sep 26 09:20 09:45 12.4.2
0438		 WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH
Z Milani¹, L Nichman², E Matida¹, M Wolde², A Brown², A Benmeddour², M Mamou², R. S. Martins, ONERA, France; D Orchard²; ¹Carleton University, Canada ;²National Research Council of Canada, Canada
15. Sep 26 09:45 10:10 12.4.3
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
Ivan de Souza Rehder¹, Emili Villani¹, Petter Krus, LIU, Sweden; ¹ITA, Brazil
Presenter: Emilia Villani, ITA
Reserve Paper 12.4.R
0170		 A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-1763 STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES
Quoc-Viet Pham, Viettel Aeropsace, Vietnam; Van-Truong Nguyen¹, Thien-Bach Nguyen¹, Phi-Minh Nguyen¹, Nhu-Van Nguyen¹; ¹Viettel 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
Luodi Zhao¹, Wenyuan Cheng¹, Gaofeng Wang¹; ¹Aviation 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. Donelli¹, P. Pantelas¹, H. Niemann², C. Ozkan², C. Christen ², L. Boggero¹, B. Nagel¹; ¹DLR, Germany ;²Airbus Operation, Germany
15. Sep 26 09:20 09:45 13.4.2
0966		 ENABLING HIGH RATE COMPOSITE MANUFACTURING THROUGH A ROBUST MANUFACTURING DIGITAL ECOSYSTEM
M. Rabiega¹, C. Reynolds¹; ¹The Boeing Company, United States
15. Sep 26 09:45 10:10 13.4.3
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. Donelli¹, L. Boggero¹, M. Forlingieri, PTL, Germany; ¹DLR, 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
James Garth, BAE SYSTEMS Australia, Australia
15. Sep 26 09:20 09:45 14.4.2
0237		 QUASI-STEADY AERODYNAMIC AND MBD COUPLED FLIGHT SIMULATION OF FOLDING MORPHING UAV
Y.-K. Bu¹, L. Qiao¹, L. Li, Chang’an University, China; H.-J. Feng¹, J.-Q. Bai¹; ¹Northwestern Polytechnical University, China
Presenter: Yikai Bu, Northwestern Polytechnical University
15. Sep 26 09:45 10:10 14.4.3
0929		 SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION
Bikash Kunwar¹, Stefanus Putra¹, Rajan Bhandari¹, Cole McCormick¹, Imon Chakraborty¹; ¹Auburn University, United States
Presenter: Imon Chakraborty, Auburn University
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
Imon Chakraborty¹, Bikash Kunwar¹, Stefanus Putra¹, Rajan Bhandari¹, Cole McCormick¹; ¹Department of Aerospace Engineering, 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. Song¹, X. Zhu¹, Z. Zhou¹; ¹Northwestern 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
Brett R. C. Molesworth¹, Dominique Estival¹, Leo Chow¹; ¹UNSW, Australia
15. Sep 26 09:20 09:45 15.4.2
0086		 A HUMAN-CENTRIC APPROACH TO UNDERSTANDING THE CONTRIBUTING FACTORS OF PILOT-RELATED RUNWAY INCURSIONS
Y Yan¹, S Boufous¹, B Molesworth¹; ¹School of Aviation, University of New South Wales, Australia
Presenter: Yan Yan
15. Sep 26 09:45 10:10 15.4.3
0685		 SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES
A. Chappell¹, S. Karunathilake¹, A. Comer¹, P. Saravanan¹; ¹Oklahoma State University, United States
Presenter: Antonio Chappell, Oklahoma State University

10:35 - 11:00COFFEE BREAK

1.5GSA2: Perspectives and Progress on Airliners for 2050+ Energy Landscapes
Chair(s): ,
Track 1
15 - Guest lectures
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
1024		 AIRBUS\' PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES
F Haselbach, Airbus, France
15. Sep 26 11:50 12:15 1.5.3
0983		 NASA RESEARCH FOR AIRLINERS OF 2050 AND BEYOND
N.K. Madavan, NASA/ARMD, United States
15. Sep 26 12:15 12:40 1.5.4
1031		 PANEL DISCUSSION Q&A WITH THE SPEAKERS
P Panel,
2.5EASN Response to Emerging Challenges in Sustainable and Competitive Aviation
Chair(s): ,
Track 2
15 - Guest lectures
15. Sep 26 11:00 11:25 2.5.1
0975		 AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES
A Filippatos¹, Th Kyriazis¹, Sp Pantelakis¹, D. Markatos¹; ¹Department of Mechanical Engineering and Aeronautics, University, 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. Nicolosi¹, M. Di Stasio¹; ¹UNINA, 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
T. X. Q. Hoang¹, T. A. Pham¹, X. H. Vu¹, H. H. Nguyen¹, C. A. Pham¹, D. L. Chu¹; ¹Viettel Aerospace Institute, Vietnam
15. Sep 26 11:25 11:50 3.5.2
0353		 TOWARDS AN ONTOLOGY-BASED APPROACH FOR DISCIPLINE-SPECIFIC ENGINEERING VIEWS IN ENGINE DESIGN
K. Becker¹, J. P. Haug¹, M. Schuff¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 11:50 12:15 3.5.3
0836		 MIXED-FIDELITY, NONLINEAR AIRCRAFT MISSION MODELING FOR HYBRID REGIONAL AIRCRAFT DESIGN VERIFICATION
Danilo Ciliberti¹, Agostino De Marco¹, Fabrizio Nicolosi¹; ¹University 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. Inderawan¹, Maurice Hoogreef¹; ¹Delft 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. Schneiders¹, D. Keller¹, A. Link¹, T. Burschyk¹, G. Atanasov¹; ¹German 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
S. Trepiccione¹, G. Melone¹, F. Nicolosi¹, G. Piscopo, Leonardo, Italy; M. Di Stasio¹; ¹UNINA, Italy
15. Sep 26 11:50 12:15 4.5.3
0673		 EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION
M. Bouchard¹, M. Bashir², D. Rancourt¹, S. Liscouët-Hanke², F. Sirois, Polytechnique Montréal, Canada; S. Lloyd², A. Tfaily³, M. Mark³, R. Freer, Pratt & Whitney Canada, Canada; J. Moriot, Calogy Solutions, Canada; ¹Université de Sherbrooke, Canada ;²Concordia University, Canada ;³Bombardier, Canada
Presenter: David Rancourt, Université de Sherbrooke
15. Sep 26 12:15 12:40 4.5.4
0062		 AERODYNAMIC EFFECTS OF DISTRIBUTED PROPULSION WING CONFIGURATION PARAMETERS
Kelei Wang¹, Zhou Zhou¹, Jiaxu Wang¹; ¹Northwestern Polytechnical University, China
Presenter: Jiaxu Wang, Northwestern Polytechnical University
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; S. F. Armanini, Imperial College London, United Kingdom
Reserve Paper 4.5.R
0688		 PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS
Shashwat Trivedi¹, Akhileshwer K Munshi¹, Rajkumar S Pant¹; ¹Indian Institute Technology Bombay, India
5.5CFD Applications
Chair(s): Marzocca, P., 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. Montella¹, D. Quagliarella¹, L. Iuspa², A. Aprovitola², G. Pezzella², A. Viviani ²; ¹CIRA (Centro Italiano Ricerche Aerospaziali), Italy ;²University of Campania , Italy
15. Sep 26 11:25 11:50 5.5.2
0283		 NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING
H Mohsin¹, S.A. Prince¹, D Di Pasquale¹; ¹Cranfield University, United Kingdom
Presenter: Davide Di Pasquale, Cranfield University
15. Sep 26 11:50 12:15 5.5.3
0119		 SIMULATION OF FIFTH-GENERATION HIGH-PERFORMANCE AIRCRAFT USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S Shahjahan¹, E Sirak¹, V Ahuja¹; ¹Siemens Digital Software Industries, United States
15. Sep 26 12:15 12:40 5.5.4
0373		 EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT
H.-C. Yang¹, X.-K. Ma¹, R.-B. Zhu¹, K. You¹, Z.-L. Chen¹; ¹Northwestern Polytechnical University, China
Presenter: Rongbo Zhu, Northwestern Polytechnical University
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
Barbara-Barbieri Huyssen¹, Dylan Fenthum¹, Joachim Huyssen, CSIR, South Africa; ¹University of Pretoria, South Africa
additional information (interactive) 5.5.R
0263		 EFFECTS OF FLYING WING CONFIGURATION PARAMETERS ON AERODYNAMICS AND STABILITY
Y. Gao¹, H. Zhao¹, K. Gan¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 5.5.R
0849		 STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS?
P-F ZHU¹, T-S XIE¹, R-S FENG¹, S ZHANG¹, C ZHANG¹; ¹Northwestern Polytechnical University, China
6.5Complex 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
K.J. Groot, University of Wyoming, United States; N.J. Porfido¹, H.L. Reed¹, J.G. Coder, Penn State University, United States; D.M. Somers, Airfoils, Incorporated, United States; ¹Texas A&M University, United States
15. Sep 26 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. Goerttler¹, S. Koch¹, M. Werner¹, F. Tocci¹, F. Mayer, Airbus Defence and Space GmbH, Germany; A. Wagner¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 12:15 12:40 6.5.4
0748		 INTERMITTENT LOW FREQUENCY EXPERIMENTAL CAVITY DYNAMICS
J. M. McCarthy¹, C. W. Marshall¹, C. Brown, RMIT University, Australia; M. B. Jones¹; ¹Defence Science and Technology Group, Australia
Presenter: Connor Marshall, Defence Science and Technology Group
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.X. Jia¹, H.R. Shen¹, J.M. Wu¹; ¹Xian 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 OF A STRUT-BRACED WING
D Losada Costoso¹, O Atinault¹, M Meheut¹, G Starck¹, E Stragiotti¹, E Nguyen Van¹; ¹ONERA, France
15. Sep 26 11:25 11:50 7.5.2
0235		 SPARSE POLYNOMIAL CHAOS-BASED ROBUST OPTIMIZATION DESIGN OF AERODYNAMIC AND SONIC BOOM
S. K. Wang¹, H. Zhao¹; ¹Northwestern Polytechnical University, China
15. Sep 26 11:50 12:15 7.5.3
0598		 SUPERSONIC GROUND EFFECT AERODYNAMICS OF A SLENDER BODY
Y.-Y. XUN¹, Q.-L. Qu¹, P.-Q. Liu¹; ¹Beihang University, China
15. Sep 26 12:15 12:40 7.5.4
0632		 FLOW SOLUTIONS AROUND VON KARMAN NOSES AT SUPERSONIC SPEEDS USING PHYSICS INFORMED NEURAL NETWORKS AND PRESSURE-SENSITIVE PAINT
M. A. Escudero¹, B.G. Marinus, Royal Military Academy, Belgium; K. Depuru-Mohan¹; ¹Cranfield 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 Park¹, D Lee¹, M Seok¹, H Choi¹, Y Kwon¹; ¹Korea Institute of Materials Science, South Korea
15. Sep 26 11:25 11:50 8.5.2
0253		 LABORATORY METHOD FOR REPLICATING FASTENER HOLE CORROSION IN AA 7085
N Tugwell¹, M Salagaras¹, J Rogers, RMIT, Australia; ¹DSTG, Australia
15. Sep 26 11:50 12:15 8.5.3
0234		 NEW INSIGHTS INTO AA7085 ENVIRONMENTALLY ASSISTED CRACKING THROUGH HIGH RESOLUTION FRACTOGRAPHY
I. Field¹, J. Rogers, RMIT, Australia; N. Tugwell¹; ¹DSTG, 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. Dessena¹, A. Dell'Edera, Politecnico di Bari, Italy; F.M.A. Mitrotta, University of Bristol, United Kingdom; O. Bonilla-Manrique¹; ¹Universidad 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
Z. Sajid¹, T. Rehman¹, A.H. Baluch¹; ¹King Fahd University of Petroleum & Minerals, Saudi Arabia
Presenter: Abrar Ul Haq Khan Baluch, King Fahd University of Petroleum & Minerals
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. Suti¹, M. Budinger¹, G. Di Rito, Università di Pisa, Italy; A. Reysset¹, I. Hazyuk¹; ¹INSA Toulouse, France
15. Sep 26 11:25 11:50 10.5.2
0619		 POWER-HIL TESTING OF LI-PO BATTERY PACKS FOR LIGHTWEIGHT EVTOL UAVS
A. Suti¹, M. Budinger¹, G. Di Rito, Università di Pisa, Italy; A. Reysset¹, I. Hazyuk¹; ¹INSA Toulouse, France
15. Sep 26 11:50 12:15 10.5.3
0882		 TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS
B Van Magill¹, D Verstraete¹; ¹The University of Sydney, Australia
15. Sep 26 12:15 12:40 10.5.4
0597		 IN-FLIGHT LOW-COST THRUST MEASUREMENT SYSTEM FOR SMALL UNMANNED AERIAL VEHICLES
C. Rieger¹, M. Hornung¹; ¹Chair of Aircraft Design, Technical University of Munich, Germany
Reserve Paper 10.5.R
0678		 HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION
Hussain Ali Abid¹, Igor SOLNTSEV, GPU Prime LTD, United Kingdom; Andrea RAPISARDA¹, Hassan Ali Abid, King Fahd University of Petroleum and Minerals, Saudi Arabia; Sergey A. Karabasov¹; ¹Queen Mary University of London, United Kingdom
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
Tomohiro Sakurai¹, Seiya Ueno¹, Takehiro Higuchi¹, Hiroki Akiyama¹; ¹Yokohama 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		 A MULTIDIMENSIONAL FRAMEWORK FOR DEMONSTRATION AND V&V CAPABILITIES FOR NEXT-GENERATION FLIGHT CONTROL SYSTEMS
O. Bertram¹, H. Schumann¹, R. Kowalski¹, A. Bagdahn¹; ¹DLR (German Aerospace Center), Germany
15. Sep 26 11:25 11:50 12.5.2
0303		 EXPERIMENTAL VALIDATION OF A FUEL CELL SYSTEM DIGITAL TWIN FOR A FULL-ELECTRIC AIRCRAFT POWERTRAIN
A. Testera¹, G. Ferrara¹, F. Di Fede¹, S. Caggese¹, V. Barba¹, G. Accardo¹, R. Pennino¹; ¹Leonardo SpA, Italy
15. Sep 26 11:50 12:15 12.5.3
0557		 HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL RECONFIGURABLE BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT
W. Bliemetsrieder¹, N. Sorokina¹, S. Myschik¹; ¹University 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. Lyu¹, J. Fu¹, S.-J. Zhao, Beijing Institute of Precision Mechatronics and Controls, China; Y.-Y. Wang¹; ¹Beihang University, China
Reserve Paper 12.5.R
0831		 NEUROMORPHIC ASCENT: REVOLUTIONISING AIRCRAFT STORES COMPATIBILITY AND AUTONOMOUS SYSTEMS
Malcolm Tutty¹, Susana McKee¹, Andrew Cenko¹; ¹JAIME AMERICA LLC, Australia
additional information (interactive) 12.5.R
0561		 POWER FLOW DYNAMICS AND COUPLING MECHANISMS IN POWER-BY-WIRE ACTUATION: A COMPREHENSIVE MODELING AND ANALYSIS APPROACH
Linlin Jiang¹, Yang Li¹, Shilong Bai¹, Zhuo Li¹, Kaixiang Jia¹, Yaoxing Shang¹; ¹Beihang 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
L. Gómez Falcón¹, V. Montiel Viruel¹, E. Espinosa Juárez, Linköping University, Sweden; ¹Universidad Autonoma de Baja California, Mexico
Presenter: Erick Espinoza Juárez, Linköping University
15. Sep 26 11:50 12:15 13.5.3
0957		 SOFTWARE ARCHITECTURE FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT
W. Bliemetsrieder¹, P. Panchal¹, N. Sorokina¹, S. Diecke, Ingenieurbüro Stephan Diecke, Germany; T. Weyh¹; ¹University of the Bundeswehr Munich, Germany
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. Zhu¹, R. Wang¹, Y.H. Xie¹, Z. Zhou¹; ¹Northwestern Polytechnical University, School of Aeronautics, China
Presenter: Yuhang Xie, Northwestern Polytechnical University
15. Sep 26 11:50 12:15 14.5.3
0529		 ENSEMBLE MACHINE LEARNING FOR UAV PROPELLER PERFORMANCE PREDICTION WITH UNCERTAINTY QUANTIFICATION
M. I. Alam¹, A. H. Baluch¹, S. H. Vattathurvalappil¹; ¹King Fahd University of Petroleum and Minerals, Saudi Arabia
15. Sep 26 12:15 12:40 14.5.4
0219		 STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION
C. Galinski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland
Reserve Paper 14.5.R
0404		 FLIGHT TESTING CONTROL LAWS OF A TANDEM TILT-WING EVTOL DEMONSTRATOR THROUGH TETHERED HOVER FLIGHTS
D. Milz¹, L. Ott¹, M. May¹; ¹German 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. González Cabeza¹, S. Petersen¹, J.-P. Buch¹, D. Niedermeier¹, M. Wies¹, A. Papenfuß¹; ¹DLR e.V., Germany
15. Sep 26 11:50 12:15 15.5.3
0291		 EVALUATION OF METHODS FOR ANOMALY DETECTION IN THE APPROACH PHASE OF OPERATIONAL FLIGHT DATA
Robin Hähnel, German Aerospace Centre (DLR), Germany
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
15. Sep 26 13:40 14:05 1.6.1
0993		 REGIONAL ELECTRIFIED/HYDROGEN DEMONSTRATIONS PANEL DAVID SERCOMBE, IREWOLE ORISAMOLU, ERIKA HOLTZ, CHRISTINE ANN ANDREWS
G.M. Bezos-O'Connor, NASA, United States
2.6X-59 The first chapter in the QUESST for quiet commercial supersonic flight
Chair(s): Bahm, C..M., Coen, P.G.
Track 2
15 - Guest lectures
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
Randall E Bailey¹, Steven Williams¹, J.J. (Trey) Arthur¹, Kemper Kibler¹; ¹NASA, 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
Bingran Wang, The University of Sydney, Australia; Dongjin Lee¹, Gyeolhee Lee¹; ¹Hanyang University, South Korea
15. Sep 26 14:05 14:30 3.6.2
0088		 MULTIDISCIPLINARY PHYSICS-CONSTRAINED GENERATIVE DESIGN OF DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
Wenyu Wei¹, Yiyuan Ma¹, Zhonghua Han¹; ¹ School of Aeronautics, 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. Perlini¹, G. Gori¹; ¹Politecnico 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. Bakhshi¹, A. Yildirim¹, J. R. R. A. Martins¹; ¹University of Michigan, United States
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, ISAE-SUPAERO, Concordia University, Canada; S. Delbecq, ISAE-SUPAERO, France; J. Liscouët, Concordia University, Canada
15. Sep 26 14:05 14:30 4.6.2
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. Rasines Mazo¹, B. Van Magill¹, D. Verstraete¹; ¹The University of Sydney, Australia
Presenter: Dries Verstraete, The University of Sydney
15. Sep 26 14:55 15:20 4.6.4
0594		 DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE
Pruthvi Paresh Kapoor¹, Rajkumar S Pant, IIT Bombay, India; Mohammed S Ismail¹, Mustafa Abdelrahman¹, Mohd-Nasir Diana, University of Sheffield , United Kingdom; ¹University of Hull, United Kingdom
Reserve Paper 4.6.R
0331		 FLIGHT OPERATIONS AND TESTING OF A 450?KG EXPERIMENTAL GYROPLANE UAV
I. Pruter¹, G. Schmitz¹, H. Duda¹, M. Laubner¹, S. Lorenz¹; ¹DLR e.V., Germany
Presenter: Gregor Schmitz, DLR e.V.
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
Tyler Buchanan, Delft University of Technology, Netherlands; Alastair P West, Williams F1, United Kingdom; Richard P Dwight, Delft, University of Technology, Netherlands
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
0785		 NUMERICAL INVESTIGATION OF GUST LOAD ALLEVIATION FOR ULTRA-HIGH ASPECT RATIO WINGS WITH PASSIVELY RELEASED FFWT
Tieren CHEN¹, Zhuqing ZENG¹, Yue ZHAO¹, Jiawen HE¹, Yong YANG¹; ¹NorthWestern Polytechnical University, China
15. Sep 26 14:55 15:20 5.6.4
0054		 CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER
J Fernández Antón¹, R Bardera¹, J.C. Matías García¹, E Barroso Barderas¹, A. A. Rodríguez-Sevillano, Universidad Politécnica de Madrid, Spain; ¹Instituto Nacional de Técnica Aeroespacial, Spain
additional information (interactive) 5.6.R
0634		 MORPHING TRAILING-EDGE AERODYNAMICS AND THE ROLE OF TURBULENCE MODELLING
P. Kovar, Czech Technical University in Prague, 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		 MIDAS: A MODULAR SOFTWARE FOR INTAKE FLOW DISTORTION ANALYSIS
T Piovesan¹, A Giannouloudis¹, J Hueso Rebassa¹, M Migliorini¹, P Zachos¹, D. G. MacManus¹; ¹Cranfield University, United Kingdom
Presenter: Josep Hueso Rebassa, Cranfield University
15. Sep 26 14:05 14:30 6.6.2
0970		 EXPERIMENTAL STUDY OF GROUND EFFECT ON A HEAVING NACA0012 AEROFOIL
M. Li¹, M. Legovich, Cranfield University, United Kingdom; N. Lawson¹; ¹The 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
Ankit Kumar¹, Roelof Vos¹; ¹Delft University of Technology, 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
N Pradyumna¹, M Li¹, D Verstraete¹; ¹The 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. Matias¹, R. Bardera¹, E. Barroso¹, J. Fernández¹; ¹INTA, 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
YiChi Liu, China; Bifeng Song, China; Libing Zhou, China
15. Sep 26 14:05 14:30 7.6.2
0665		 AERODYNAMIC OPTIMISATION OF BIOINSPIRED CORRUGATED WINGS FOR HIGH-EFFICIENCY MAV GLIDING
M. Krasniqi¹, S.-F. Armanini¹; ¹Imperial College London, United Kingdom
15. Sep 26 14:30 14:55 7.6.3
0777		 AERO-MECHANICAL ANALYSIS OF A BIRD-INSPIRED ORNITHOPTER USING AN INTEGRATED SIMULATION FRAMEWORK
H.-H. Yang¹, S.-G. Lee¹, E.-H. Lee¹, H.-S. Ko¹, J.-H. Han¹; ¹Korea Advanced Institude of Science and Technology, South Korea
Presenter: Jae-Hung Han, Korea Advanced Institude of Science and Technology
15. Sep 26 14:55 15:20 7.6.4
0916		 THREE-DIMENSIONAL FLOW STRUCTURES OVER A LOW-ASPECT-RATIO PLUNGING WING
B. ANILIR¹, D. F. KURTULUS¹, M. F. PLATZER, University of California, Davis, United States; ¹Middle East Technical University, Turkey
Reserve Paper 7.6.R
0184		 AERODYNAMIC PERFORMANCE ANALYSIS OF A NOVEL LIFT-THRUST INTEGRATED ROTARY FLAPPING AERIAL VEHICLE
J. LIU¹, W. YANG¹, Y. GUO¹, Y. ZHANG¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 7.6.R
0147		 STUDY ON AERODYNAMICS OF THE WING WITH FLAP INSPIRED FROM BIRD COVERTS
X. Xu¹, W. Yang¹, J. Xuan¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 7.6.R
0182		 INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATION
S.-S. Cao¹, W.-Q. Yang¹, Y.-G. Zhang¹, X.-L. Xu¹; ¹Northwestern 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		 OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR UAVS
C.D. Scott¹, A. Comer¹, J.C. Hanan¹, A. Nunley¹; ¹Oklahoma 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. Stekovic¹, P. Krus¹; ¹Linköping 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
DONATO CARDONE¹, RAUNO CAVALLARO, Barcelona Supercomputing Center, Spain; ANDREA CINI¹; ¹Universidad 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
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. Swanton¹, A. Manning¹, B. Evans¹, M. Chipper, RMIT University, Australia; ¹Defence Science and Technology Group, Australia
15. Sep 26 14:05 14:30 9.6.2
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. Cecrdle¹, O. Vich¹, P. Malinek¹, R. Kulhanek¹; ¹VZLU 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 Kishimoto¹, R Sakata¹, Y Iwami², N Tomita², M Tamayama, JAXA, Japan; Y Tanahashi³, T Ikeda³; ¹Kwansei Gakuin University, Japan ;²Yamashina Institute for Ornithology, Japan ;³Chubu University, Japan
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. Wu¹, L. Zhou¹, J. Shi¹, Y. Meng¹, Z. Wang¹; ¹Northwestern 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. Carrea¹, K. Kyprianidis¹; ¹Mälardalen University, Sweden
15. Sep 26 14:30 14:55 10.6.3
0418		 SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET
H. Miki¹, J. Akatsuka¹, R. Nimura, Tokyo University of Agriculture and Technology, Japan; ¹JAXA, Japan
15. Sep 26 14:55 15:20 10.6.4
0510		 NUMERICAL STUDY OF UNSTEADY DISTORTION IN AN S-DUCT INTAKE SUBJECTED TO BLAST SHOCK WAVES
L.-L. Shi¹, Y. Fan¹, B.-G. Mi¹; ¹Northwestern Polytechnical University, China
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. Shim¹, J.-I. Jang¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea
15. Sep 26 14:30 14:55 11.6.3
0224		 AIRSPACE CAPACITY IMPLICATIONS OF CONTRAIL-AWARE TRAJECTORY OPTIMIZATION
Anastasia Lemetti¹, Tatiana Polishchuk¹, Lucie Smetanova¹; ¹LiU, Sweden
15. Sep 26 14:55 15:20 11.6.4
0377		 TRIM PERFORMANCE EXPLORATION FOR AN AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION AND A TAIL THRUST UNIT
G. Fernandes Lourenço¹, C. Varriale¹; ¹Delft University of Technology, Netherlands
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 BATTERY THERMAL RUNAWAY INITIATION AND PROPAGATION
W. Mooney¹, M. Gendron, Calogy Solutions, Canada; X. Arcand¹, D. Francoeur¹, D. Rancourt¹; ¹Université de Sherbrooke, Canada
15. Sep 26 14:05 14:30 12.6.2
0663		 MODAL-BASED FUEL LEVEL ESTIMATION OF CRYOGENIC PROPELLANT TANKS
S Pfeifer¹, F Thilker¹, A Tramposch¹, A Buchroithner, University of Technology, Austria; ¹FH JOANNEUM, Austria
15. Sep 26 14:30 14:55 12.6.3
0807		 SIZING OF LINEAR ACTUATORS FOR SPAN EXTENSION OF HALE UAV
Tanvi Prakash, Larsen and Toubro, India; Rajkumar Pant, Indian Institute of Technology Bombay, India
Presenter: Tanvi Prakash, Larsen and Toubro
15. Sep 26 14:55 15:20 12.6.4
0847		 DYNAMIC PERFORMANCE DEGRADATION OF FLIGHT CONTROL EHA UNDER HIGH-TEMPERATURE CONDITIONS
M. -W. SUN¹, J. FU¹, Z. -R. ZHAO², M.- C. WU², J. -N. LUO²; ¹Beihang University, China ;²AVIC Shenyang Aircraft Design and Research Institute, China
Reserve Paper 12.6.R
0593		 NONLINEAR FRICTION MODELING OF HELIX SWING HYDRAULIC CYLINDERS FOR MORPHING AIRCRAFT USING PHYSICS-INFORMED NEURAL NETWORKS
S.-Y. Chen¹, J. Fu¹, K. Ci¹, H.-Z. Song, Beijing Institute of Precision Mechatronics and Controls, China; Z.-L. Li¹, D.-C. Lyu¹; ¹Beihang University, China
Reserve Paper 12.6.R
0991		 LIGHTWEIGHT BIMETALLIC GEARS FOR AEROSPACE TRANSMISSIONS ENABLED BY OPEN-AIR DIFFUSION BONDING
Z.C. Xu¹, E. Tang¹, N Teyssier¹, M.F. Humphreys¹, J Jiang¹; ¹Imperial College London, United Kingdom
additional information (interactive) 12.6.R
0483		 HIGH-PRECISION EDDY CURRENT TIP CLEARANCE SENSOR WITH EXCEPTIONAL HIGH-TEMPERATURE RESISTANCE
Liu Fulin¹, Lingqiang Zhao¹, Yaguo Lyu¹, Bosen Chang¹, Zhenxia Liu¹; ¹Northwestern 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. Kontani¹, R. Mori¹; ¹Kobe 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. Meier¹, M.-M. Temme¹, R. Hunger¹, S. Shetty¹, M. Hagl¹, O. Ohneiser¹, M. Finke¹; ¹German Aerospace Center (DLR), Germany
15. Sep 26 14:30 14:55 13.6.3
0178		 FLIGHT CENTRIC ATC – HOW TO SOLVE CONFLICTS WITHOUT COMMUNICATION AND COORDINATION OVERLOADS?
T. Finck¹, V, Bottino¹, M. Weber¹, B. Korn¹; ¹German Aerospace Center, Germany
15. Sep 26 14:55 15:20 13.6.4
0811		 AUGMENTED REALITY SAFETY NETS FOR INCREASED AIRPORT SAFETY
S. Bagassi¹, Tommaso Fadda¹; ¹University of Bologna, Italy
Reserve Paper 13.6.R
0302		 EVALUATING HUMAN-MACHINE-TEAMING CONCEPTS FOR A HIGHLY AUTOMATED GROUND CONTROLLER WORKING POSITION
L. Nöhren¹, A. Simon¹, M. Schaper¹; ¹DLR, 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. C. Yang¹, J. H. Jeong, Hanseo University, South Korea; S. K. Kim¹, J. Y. Suk¹; ¹Chungnam National University, South Korea
Presenter: Yechan Yang, Chungnam National University
15. Sep 26 14:30 14:55 14.6.3
0765		 REINFORCEMENT LEARNING-BASED ADAPTIVE WEIGHTING OF SWARM GUIDANCE LAWS FOR SMALL FIXED-WING UAVS
C. KANG¹, J. JEONG¹; ¹Hanseo University, South Korea
15. Sep 26 14:55 15:20 14.6.4
0735		 2D AND 3D TRAJECTORY PLANNING FOR UAVS FORMATION SYSTEM USING DYNAMIC WINDOW APPROACH
R.B. Zhu¹, K. You¹, H.C. Yang¹, X.K. Ma¹, Z.L. Chen¹; ¹Northwestern Polytechnical University, China
Reserve Paper 14.6.R
0771		 IMPLEMENTATION OF DISTRIBUTED SWARM GUIDANCE ALGORITHMS ON LOW-COST UAVS
J McGuire¹, B McIvor¹, S Crase¹; ¹DSTG, Australia
additional information (interactive) 14.6.R
0037		 ADAPTIVE PRESCRIBED-TIME COOPERATIVE CONTROL FOR FORMATION OF SMALL TANDEM-ROTOR UAVS
X.-L. Li¹, C.-Q. Wang¹, Y. Guo¹, A.-J. Li¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 14.6.R
0098		 PREDEFINED-TIME AFFINE FORMATION FAULT-TOLERANT CONTROL FOR FIXED-WING UAVS WITH INPUT SATURATION
Jun Fang¹, Yong Guo¹, Aijun Li¹, Changqing Wang¹; ¹Northwestern 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. ZHANG¹, J.-N LIU¹, Z. XU¹, Y.-X. YANG¹; ¹School of Astronautics, Northwestern Polytechnical University, 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
JA Armstrong¹, OM Ozcakir¹, LL Waite¹, Thomas Austin¹, CA Pepper¹, A Tvaryanas², H Uyhelji², S Gearhart, US CDC, United States; P Lebbin, Canadian NRC, Canada; I Koolhof¹; ¹Boeing, Australia ;²FAA, United States
15. Sep 26 14:05 14:30 15.6.2
0439		 EARLY WARNING FOR POTENTIAL BIRD STRIKES: STRATEGIC OPTIMIZATION OF PAN-TILT-ZOOM SENSOR NETWORKS FOR BIRD HAZARD DECREASE IN AIRPORT ENIRONMENT
Y.H. Mei¹, Z.H. Wang¹; ¹The university of Sydney, Australia
15. Sep 26 14:30 14:55 15.6.3
0457		 REAL-TIME AIRPORT BIRD-STRIKE PROTECTION WITH IMPROVED EDGE DEVICE DETECTION METHOD
JIANQIN GAO¹, TianQi Wang, Taiyuan University of Technology, China; Hongyi GAO¹, Yujie Ding¹, Z WAN¹; ¹ University of Sydney, Australia

15:20 - 15:25CHANGEOVER BREAK

0.6GENERAL LECTURE 3 X59 Low Boom Demonstrator by KC Wong
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
15. Sep 26 16:40 17:05 1.7.1
1025		 FUTURE SUSTAINABLE AVIATION INFRASTRUCTURE: PROSPECTS & CHALLENGES FROM EUROCONTROL\'S PERSPECTIVE
T Cardoso Simões, EUROCONTROL, Belgium
15. Sep 26 17:05 17:30 1.7.2
0985		 JET ZERO: ATJ SAF PROJECT DEVELOPER
J Mason, Jet Zero Australia, Australia
15. Sep 26 17:30 17:55 1.7.3
1027		 FUTURE SUSTAINABLE AVIATION INFRASTRUCTURE: PROSPECTS & CHALLENGES FROM CHRISTCHURCH AIRPORT\'S PERSPECTIVE
C Waghorn, Christchurch International Airport, New Zealand
15. Sep 26 17:55 18:20 1.7.4
1032		 PANEL DISCUSSION Q&A WITH THE SPEAKERS
P Panel,
2.7GARTEUR 1
Chair(s): ,
Track 2
15 - Guest lectures
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
Pietro Catalano, C.I.R.A., 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.L.C Chan¹, D Pasquale¹, W Widjaja¹, S Lyu¹, J Rispin¹, H Smith¹; ¹Cranfield 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.-H. Peng¹, K.-S. Zhang¹, Q. Chen¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China
Presenter: Yuhuan Peng, Northwestern Polytechnical University
15. Sep 26 17:30 17:55 3.7.3
0876		 AN INCREMENTAL MODULAR MDO FRAMEWORK FOR HYDROGEN-ELECTRIC POWERTRAIN SIZING AND INTEGRATION IN GENERAL AVIATION AIRCRAFT
P. Moreno-Escolastico¹, M. Raiola¹, R. Castellanos¹, A. Cini¹; ¹Universidad Carlos III de Madrid, Spain
15. Sep 26 17:55 18:20 3.7.4
0305		 METHODOLOGICAL APPROACH TO MULTI-CRITERIA OPTIMISATION OF PRODUCT FAMILY ARCHITECTURES UTILISING SYSTEM MODELS
F. H. Christiansen¹, M. C. Berschik¹, S. Wehrend¹, D. Krause¹; ¹Hamburg Univeristy of Technology, TUHH, Germany
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
Emma Cassidy¹, Ana Garcia, Collins Aerospace, France; Gokcin Cinar¹; ¹University 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. Falcone¹, S. Corcione¹, F. Nicolosi¹, S. Trepiccione¹; ¹University 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 Stasio¹, F. Nicolosi¹; ¹UNINA, Italy
Reserve Paper 4.7.R
0696		 MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY
G. Shen¹, X. Zhang¹, W. Hao¹, Z. Wang¹; ¹Northwestern Polytechnical University, China
5.7Aeroacoustics and Noise Predictions
Chair(s): Thomber, B., Lawson, N.
Track 5
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. IKEDA¹, K. YASUE¹, M. KANAYAMA, Ryoyu Systems, Japan; ¹JAXA, 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. Moses¹, M. Hornung¹; ¹Technical 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
Hassan Ali 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 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
S Otomo¹, H Nishida¹; ¹Tokyo 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. Marciniuk¹, M. Szumski², Z. Szczerba², L. Kiszkowiak³, L. Malicki¹, P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; K. Sibilski, Air Force Institute of Technology, Poland; S. Kachel³; ¹Wroclaw University of Science and Technology, Poland ;²Rzeszow University of Technology, Poland ;³Military University of Technology, Poland
Presenter: Łukasz Kiszkowiak, Military University of Technology
15. Sep 26 17:30 17:55 6.7.3
0347		 AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC REGIME AT REYNOLDS NUMBER OF 1 MILLION
X. Delon¹, J. Abou Khalil, ONERA - Toulouse, France; N. Maynard², A. Marouf¹, R. El Akoury³, Y. Hoarau¹, C. Doll, Onera - Toulouse, France; J.-F. Rouchon², M. Braza³; ¹ICUBE - Strasbourg, France ;²LAPLACE - Toulouse, France ;³IMFT - Toulouse, France
additional information (interactive) 6.7.R
0517		 EFFECTS OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS
Y. TANAHASHI¹, F. SAKAI¹, S. NISHIZUKA¹, T. IKEDA¹, N. KISHIMOTO, Kwansei Gakuin University, Japan; M. TAMAYAMA, Japan Aerospace Exploration Agency, Japan; Y. IWAMI², N. TOMITA²; ¹Chubu University, Japan ;²Yamashina Institute for Ornithology, Japan
7.7Data-Driven Design, Optimization and Reduced-Order Modeling
Chair(s): ,
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. Goerttler¹, D. Hines¹, A. Wagner¹; ¹German Aerospace Center (DLR), 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. Gan¹, H. Zhao¹, S. Wang¹; ¹Northwestern Polytechnical University, China
Presenter: Shekun Wang, Northwestern Polytechnical University
15. Sep 26 17:30 17:55 7.7.3
0546		 AIRFOIL DESIGN OPTIMIZATION FOR HIGH-LIFT AND HIGH-EFFICIENCY APPLICATIONS USING DEEP REINFORCEMENT LEARNING
P. Scavella¹, G. Paolillo¹, C.S. Greco¹; ¹University Of Naples Federico II, Italy
Presenter: Gerardo Paolillo, UNIVERSITY OF NAPLES FEDERICO II
15. Sep 26 17:55 18:20 7.7.4
0767		 UNSTEADY AERODYNAMIC OPTIMIZATION OF THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH LEVEL SET METHOD
D Sasaki¹, C Yuma¹, Y Kawamoto¹, M Okamoto, Kanazawa Institute of Technology, Japan; H Nagai, Institute of Fluid Science, Tohoku University, Japan; ¹Osaka Metropolitan University, Japan
Reserve Paper 7.7.R
0473		 MULTI-SCALE LINEAR FEATURE MODULATION DEEP NEURAL OPERATOR FOR RAPID PRESSURE COEFFICIENT PREDICTION
W.-F. Zhang¹, H. Zhao¹, S.-K. Wang¹; ¹Northwestern Polytechnical University, China
Presenter: She-Kun Wang, Northwestern Polytechnical University
8.7Damage 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
G.-C. Cristea¹, M. Pop¹, A. Stefan¹, M. Botan¹, A. Dragomirescu¹; ¹INCAS, 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. Yao¹, Y. Wang¹, H. Wang¹, Y. Wang¹; ¹Northwestern Polytechnical University, China
Reserve Paper 8.7.R
0276		 NUMERICAL SIMULATION OF STRESS-OXIDATION DAMAGE IN C/SIC COMPOSITES AT HIGH TEMPERATURES
Guoqing chen¹, Leijiang Yao¹, Bin Li¹, Xiaoyan Tong¹; ¹Northwestern Polytechnical University, China
Reserve Paper 8.7.R
0357		 IMPACT TOLERANCE OF DRILLED THICK C/SIC CERAMIC MATRIX COMPOSITE
A. M. Caporale¹, G. Janszen¹, A. S. Jambhulkar¹, M. Ursic², A. Tasca², R. Passoni², A. Airoldi¹; ¹Politecnico di Milano, Italy ;²Brembo N.V., 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
L. Vertonghen¹, C. Mollet, DAAA, ONERA, Institut Polytechnique de Paris, France; C. Julien¹, F.-X. Irisarri¹; ¹DMAS, ONERA, Université Paris-Saclay, France
15. Sep 26 17:05 17:30 9.7.2
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, Spain; A. Cini, 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): , , Bura, R.
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. Tsukuda¹, H. Kato¹, D. Sasaki¹, C. Fujio², S. Takahashi², T. Isono², M. Koga², M. Takegoshi²; ¹Osaka Metropolitan University, Japan ;²Japan Aerospace Exploration Agency, Japan
15. Sep 26 17:05 17:30 10.7.2
0504		 NUMERICAL PREDICTION AND EXPERIMENTAL VALIDATION ON THRUST PERFORMANCE OF SCRAMJET EXTERNAL NOZZLES
T Isono, Japan Aerospace Exploration Agency, Japan
15. Sep 26 17:30 17:55 10.7.3
0508		 REPRESENTATIVE THERMO-STRUCTURAL TESTING OF SCRAMJETS USING COMMERCIAL ROCKET ENGINE TEST
A Roco¹, H Chisholm, Advanced Composite Structures Australia, Australia; D Hartley¹; ¹Defence Science and Technology Group, Australia
Presenter: Alison Roco
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
Thomas Bernhofer¹, Andreas Seefried¹; ¹German Aerospace Center (DLR), 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. Joshin¹, F. Tanaka, RIKEN R-CCS, Japan; T. Amano¹, A. Hiromori¹, A. Uchiyama¹, H. Yamaguchi¹, S. Morioka², T. Inagawa²; ¹The University of Osaka, Japan ;²Interstellar Technologies Inc., Japan
15. Sep 26 17:55 18:20 11.7.4
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
Hyoung Sik Choi¹, Seungchan Shin¹, Hak Min Lee¹, Inyoung Yang¹, Chang-Hun Lee, KAIST, South Korea; ¹KARI, South Korea
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; M Kokkolaras, Clemson University, United States
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. Suizu¹, H. Hirabayashi¹, N. Takeichi, Tokyo Metropolitan University, Japan; ¹Electronic 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
K. Sekine¹, T. Tatsukawa, Tokyo University of Science, Japan; Y. Kawagoe, Tohoku University, Japan; E. Itoh¹; ¹The University of Tokyo, Japan
15. Sep 26 17:55 18:20 13.7.4
0521		 UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS
Yeongseok Cho, South Korea; Jaewon Lee, South Korea; Yeseo Kim, South Korea; Chanyoung Jung, South Korea; Seokjun Kang, South Korea; Junghyun Kim, South Korea
Reserve Paper 13.7.R
0860		 SENSITIVITY STUDY OF DEPARTURE TIME ACCURACY FOR AIRPORT COLLABORATIVE DECISION MAKING USING FAST-TIME SIMULATION
Yota Iwatsuki, Mitsubishi Research Institute, Inc./ Kyushu University, Japan; Akinori Harada¹, Shin-ichiro Higashino¹; ¹Kyushu University, 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. Wang¹, W. Cheng¹, Y. Wu¹, L. Zhao¹; ¹Aerial Industry Development Research Center of China, China
Presenter: Luodi Zhao, Aerial Industry Development Research Center of China
14.7BLI/Embedded Propulsion
Chair(s): ,
Track 14
15 - Guest lectures
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
Sara Bagassi¹, Tommaso Fadda¹; ¹University 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
NX Azmitia¹, LA Rosas¹, DE Orozco¹, V Mier y Concha¹, E Luis¹; ¹Universidad Panamericana, Mexico
15. Sep 26 17:30 17:55 15.7.3
0464		 A MIXED REALITY FRAMEWORK FOR EVALUATING AIRCRAFT PRE-FLIGHT WALK-AROUND TRAINING
Miguel A. Higinio¹, Michael J. Scott¹, Wim J.C. Verhagen¹; ¹RMIT University, Australia
15. Sep 26 17:55 18:20 15.7.4
0692		 FROM DATA TO DEBRIEF: A FRAMEWORK FOR PILOT PERFORMANCE ASSESSMENT
P Kurka¹, E Villani¹; ¹Aeronautics Institute of Technology, Brazil
Presenter: Emilia Villani, Aeronautics Institute of Technology
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 Villazon¹, E Espinosa Juarez, Linköping Universitet, Sweden; F Perez Fuentes, Consejo Mexicano de Educacion Aeroespacial, Mexico; D Mavris¹; ¹Georgia Institute of Technology, 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
16. Sep 26 10:50 11:15 1.8.1
0982		 GLOBAL SUSTAINABLE AVIATION PANEL DISCUSSION WITH FIONA MESSENT, VERONIQUE ROCA, ALAN NEWBY, JIM HILEMAN, CHRISTINE ANDREWS AND CLAIRE WAGHORN
R.A. Wahls, NASA, Retired, United States
2.8GARTEUR 2
Chair(s): ,
Track 2
15 - Guest lectures
16. Sep 26 10:50 11:15 2.8.1
1006		 MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS
J. Garcia-Martinez¹, P. Pflueger Tejero¹, I. Martinez Teres¹, U. Dincer², M. Misol², P. Wierach², A. Riccio³, A. Garofano³, M. Battaglia³, J. Berthe*, R. Ortiz*, J. Germain*, F. Roudolff*, W. W. Witsº, B. Noordmanº, O. Erartsinº; ¹INTA, Spain ;²DLR, Germany ;³University of Campania, Italy ;*ONERA, France ;ºNLR, Netherlands
16. Sep 26 11:15 11:40 2.8.2
1005		 ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS
M.L. Montero-Sistiaga¹, M. de Smit¹, A. Pastor Muro², N. Redondo Torrico², M. Thomas³, A Morel³, S Drawin³, F. Palm, Airbus, Central Research & Technology (CRT), Germany; ¹Royal NLR-Netherlands Aerospace Centre, Netherlands ;²National Institute of Aerospace Technology (INTA), Spain ;³DMAS, ONERA, France
Presenter: Francisco Javier San Millan Fiel, INTA- Spanish National Institute for Aerospace Research
16. Sep 26 11:40 12:05 2.8.3
1004		 CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING
Frédéric LAURIN¹, Yelitza DELGADO GONZALEZ, NLR, Netherlands; Stefan REH, DLR, Germany; Angela RUSSO, 4Università degli Studi della Campania , Italy; Charles FOOTER, QINETIQ, United Kingdom; Florence Roudolff¹; ¹ONERA, 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
Andrés Esther¹, Quagliarella Domenico, CIRA, Italy; Hines Derrick², Bekemeyer Philipp², Nieto-Centenero Javier ¹, Taddei Tommaso, Sapienza University of Rome, Italy; Peter Jacques, ONERA, France; Amoignon Olivier, FOI, Sweden; Alaia Alessandro³, Scardigli Angela³, Castellanos Rodrigo, UC3M, Spain; ¹INTA, Spain ;²DLR, Germany ;³OPTIMAD/ESTECO, 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
Enrico Stragiotti¹, Eric Nguyen Van¹, Romain Parello¹, Sébastien Defoort¹, Diego Losada Costoso², Charly Mollet², Michaël Méheut², Olivier Atinault², Frédéric Moëns², Lander Vertonghen³, Cédric Julien³, Antoine Lannoo*, Valentin Priasso*; ¹DTIS, ONERA, Université de Toulouse, France ;²DAAA, ONERA, Institut Polytechnique de Paris, France ;³DMAS, ONERA, Université Paris-Saclay, France ;*DMAS, 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.-Z. LIU, China; B.-L. SHANG, China; P.-F. LI, China; R.-X. LING, China; Y.-Z. WANG, China; K.-A. XING, China; H.-X. LI, China; M.-Z. HOU, 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. LIU¹, Y. WU¹, M.A. Hariansyah¹, R.-P. LIEM, ICL, Department of Aeronautics, United Kingdom; ¹HKUST, Department of Mechanical and Aerospace Engineering, Hong Kong SAR of China
Presenter: Yiran Wu, HKUST,Department of Mechanical and Aerospace Engineering
16. Sep 26 12:05 12:30 3.8.4
0631		 OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES
M. A. Hariansyah¹, C. Reyner¹, R. P. Liem, Imperial College London, United Kingdom; P. S. Palar, Institut Teknologi Bandung, Indonesia; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China
Reserve Paper 3.8.R
0610		 MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY
Bradley Blaxall¹, Francesco Di Fiore¹, Demetrios Venetsanos¹, Laura Mainini¹; ¹Imperial 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, Y. Lee¹, H. Choi¹, B. Cho¹, Y. Kim¹, 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 MULTI-RANGE HYBRID-ELECTRIC OPEN-ROTOR AIRCRAFT CONCEPT FOR THE WIDE-BODY PASSENGER CLASS
G. Atanasov¹, D. Silberhorn¹, V. Nugnes¹; ¹German Aerospace Center (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
LI Li¹, DAI Erfan¹, LI Zhangrongyi¹, CHAO Minxin¹, LIU Yiran¹, WANG Libao, AVIC (CHENGDU) UAS CO., LTD., China; ZHONG Jiaxiang, School of Aeronautics, Northwestern Polytechnical University, China; ¹School of Future Transportation, 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. Reindle¹, J. Hoffelner¹, N. Sekyra¹, N. Schlautmann¹, M. Weber¹, V. Sittel¹, C. Mishra¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany
5.8Machine Learning Applications
Chair(s): Ashton, N., Halila, G.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 10:50 11:15 5.8.1
0492		 AERODYNAMIC OPTIMIZATION DESIGN METHOD FOR ROTORS USING A MULTI-FIDELITY NEURAL NETWORK MODEL
S. LI¹, W.-P. SONG¹, Z.-Q. SHEN¹; ¹ 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. S. Abulela¹, M. I. Alam¹; ¹King Fahd University of Petroleum and Minerals, 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
G. Dalinajara Abreu Smith Borges¹, V. Silva Figueredo¹, G. L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J. L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
16. Sep 26 12:05 12:30 5.8.4
0490		 EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN
Yi Fan¹, Yu Sun¹, Jiashuai Xue¹, Yilin Wang¹, Baigang Mi¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
Reserve Paper 5.8.R
0462		 RESEARCH ON AERODYNAMIC-STEALTH INTEGRATED DESIGN METHODOLOGY BASED ON MPPO ALGORITHM
Keyao Gan¹, Huan Zhao¹, Shekun Wang¹; ¹Northwestern Polytechnical University, China
Presenter: Zhengang Zhang, Northwestern Polytechnical University
6.8Certification by Analysis (CbA)
Chair(s): ,
Track 6
15 - Guest lectures
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
Zhengang Zhang¹, Huan Zhao¹, Weifeng Zhang¹, Jiayi He¹, Zhenghong Gao¹; ¹Northwestern 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
A. Petrillo¹, D. Palma¹, L. Pirillo¹, P. P. Ciottoli¹, M. Bernardini¹, F. Stella¹; ¹Sapienza 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
Presenter: Agnieszka Kwiek, Warsaw University of Technology
16. Sep 26 12:05 12:30 7.8.4
0456		 GROUND-EFFECT ANALYSIS OF SMALL DUCTED PROPELLERS: A NUMERICAL–EXPERIMENTAL STUDY
F Kuci¹, N Railean¹, P Kantzidis², P Marzocca², V Muscarello²; ¹Polytechnic University of Turin, Italy ;²Royal Melbourne Institute of Technology, 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. Ericksen¹, N. J. Lawson¹; ¹The 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
0861		 ULTRASONIC NON-DESTRUCTIVE TESTING: SYSTEM SELECTION FOR CHARACTERISATION AND DETECTION OF DEFECTS IN REPAIRED COMPOSITE MATERIALS
H.R. Spratling¹, M.E. Ibrahim¹; ¹Defence Science and Technology Group, Australia
16. Sep 26 11:15 11:40 8.8.2
0776		 EXPERIMENTAL INVESTIGATION OF BLOWING RATIO EFFECT ON THE FLOW REGIMES OF TRANSPIRATION COOLING IN LATTICE POROUS MEDIA
J. Heo¹, J. Lee¹, A.-A. Reynolds¹, J. Cho¹, J.-H. Han¹; ¹KAIST, South Korea
16. Sep 26 11:40 12:05 8.8.3
0127		 EXPERIMENTAL INVESTIGATION OF FRETTING WEAR IN TI6-AL-4V DOVETAIL ASSEMBLIES UNDER RESONANT VIBRATION
Xiyuan Zhang¹, Dasheng Wei¹, Shun Yang¹; ¹Beihang University School of Energy and Power Engineering, China
16. Sep 26 12:05 12:30 8.8.4
0313		 ADVANCES IN NON-DESTRUCTIVE BUCKLING PREDICTION OF THIN-WALLED STRUCTURES BY VIBRATIONS
A Gliszczynski, Lodz University of Technology, Poland; R. Degenhardt¹, F Franzoni¹, T.D. Baciu, PFH, Germany; ¹DLR, Germany
Presenter: Adrian Gliszczynski, Lodz University of Technology
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. Qian¹, J. Liu¹, X. Hu¹, C. Han¹, X. He¹, X. Ran¹, X. Ai¹; ¹Dalian 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
Hai-Bo Zheng¹, Ying Li, Shaanxi Provincial Party Committee Service and Support Center, China; Bin Wu¹, Ri-Hua Yan¹, Chao Gao¹, Yao Tian¹; ¹Northwestern Polytechnical University, China
Presenter: Haibo Zheng, Northwestern Polytechnical University
16. Sep 26 11:40 12:05 9.8.3
0566		 MECHANISM OF ALL-MOVABLE RUDDER NONLINEAR AEROELASTIC BEHAVIOR INDUCED BY BENDING FREEPLAY
X. Ai¹, Z. Chen¹, Z. Liang¹, Z. An¹, X. Xu¹, Y. Lu¹, W. Qian¹; ¹Dalian 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.-Y. Li¹, S. He¹, Z.-C. Yang¹; ¹Northwestern Polytechnical University, 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. Xi¹, Y. T. Dai¹, C. Yang¹; ¹Beihang 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.Y. Zhao, China; B.G. Mi, China; X. Bai, 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. Wehrel¹, J. Häßy¹, R. Schnell¹, S. Wöhler¹; ¹German 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
G Braggett¹, K. F. Joiner¹, A. Somerville¹, D. Hill, Altavia Aerospace, Australia; ¹University of New South Wales, Australia
Presenter: Georgia Braggett, University of New South Wales
16. Sep 26 12:05 12:30 10.8.4
0690		 FLIGHT-DATA-DRIVEN PHYSICS-INFORMED COMPONENT MAP DERIVATION WITH STRUCTURAL COMPLIANCE
Y. Liu¹, L. Gou¹, Y. Huang, Shenzhen Research Institute of Northwestern Polytechnical Univer, China; ¹School of Power and Energy, Northwestern Polytechnical Universit, China
Reserve Paper 10.8.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.J. Kim¹, B. Seo¹, S.K. Kim¹, J.Y. Suk¹; ¹Chungnam 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
Joshua Clarendon¹, Travis Fields¹, Justin Nguyen¹, Alec Chance¹, Oleg Yakimenko, Naval Postgraduate School, United States; ¹University 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
J Cox¹, KC Wong¹, G Chamitoff, Texas A&M University College of Engineering, United States; ¹The 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
Yinglong He, China; Xiaoping Xu, China; Zhou Zhou, China; Shiqi Song, China
Presenter: Shiqi Song
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
V Sousa¹, E Sozer², K Ravikumar¹, S Hosseini², J Duensing²; ¹Analytical Mechanics Associates, United States ;²NASA, United States
16. Sep 26 11:15 11:40 12.8.2
0256		 AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMISPAN CRM-HL AT THE JAXA 6.5M X 6.5M LOW SPEED WIND TUNNEL
M. Kohzai¹, M. Murayama¹, A. Sansica¹, D. Lusher¹, T. Takaishi¹, H. Abe¹; ¹Japan Aerospace Exploration Agency, Japan
16. Sep 26 11:40 12:05 12.8.3
0328		 NEW TEST RESULTS OF THE 3.23% FULL-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT KHI AERO-ACOUSTIC LOW-SPEED WIND TUNNEL
T. Hashioka¹, Y. Murahashi¹, H. Yasuda¹, Y. Sawaki¹, S. Suzuki¹, W. Suzuki¹, T. Kawamura¹; ¹KHI, 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. He¹, Y. Wang¹, F. Wu¹, J. Guo¹, Z. Gao¹; ¹HKUST, 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
Pavithra Sathya Kumar¹, Michael Schultz¹, Ehsan Asadi¹; ¹Universität 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. Edsel¹, W. A. Crossley¹, D. A. DeLaurentis¹; ¹Purdue 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.S. Lee¹, K. R. Oh¹; ¹Korea Aerospace Research Institute, 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 Tiwari¹, R S Pant¹; ¹Indian 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. Skrna¹, M. de Rosa Jacinto¹, L. Frei¹, B. Mittenecker¹, J. Nagl¹, H. Mad¹, M. Berens¹; ¹Technische Universität Wien, Austria
16. Sep 26 11:15 11:40 14.8.2
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, ONERA, France
Presenter: Mathieu Lugrin, ONERA
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; P. Raj, Virginia Tech, United States
16. Sep 26 11:15 11:40 15.8.2
0549		 REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR
Katleho Ramotsabi¹, Lauren Strydom¹, Lindo Zwane¹; ¹CSIR, 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. Moser¹, V. N. Müller¹, N. Singer¹, T. Siemer¹, F. Daoud¹; ¹TU Munich, Germany
Presenter: Valentin Müller
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. Machado¹, J. L. C. Reis¹, M. Lott², R. Carlana²; ¹Universidade Federal de Minas Gerais, Brazil ;²Boeing, Brazil
additional information (interactive) 15.8.R
0380		 INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION
C. Varriale¹, F. Angioni¹; ¹Delft University of Technology, Netherlands

12:30 - 13:30LUNCH BREAK

0.9GENERAL LECTURE 4 Aeronautics Outlook - Directors Cut (Lane Ballard, Boeing, Veronique Roca, Airbus, Dimitri Mavris, Georgia Tech, Alan Newby, Rolls-Royce, Per Olof Marklund, SAAB. Markus Fischer, DLR
Chair:
16. Sep 26 13:30 15:15

15:15 - 15:40AFTERNOON BREAK

1.9ECSC pitch session
Chair(s): ,
Track 1
15 - Guest lectures
2.9Shaping aviation for society ETF
Chair(s): Holmberg, G., Collier, F.
Track 2
15 - Guest lectures
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
William Dean Donovan, DiamondStream Partners, United States
16. Sep 26 16:30 16:55 2.9.3
1015		 AVIATION VISION 2050: THE POTENTIAL FOR CLIMATE NEUTRAL GROWTH
X.S. Zheng, United States; J. Mukhopadhaya, United States; J. Benoit, United States; S.N. Kumar, United States; D. Rutherford, United States; D. Rhode, Germany; D. Sitompul, 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
Akhmad Farid Widodo¹, Romie Oktovianus Bura, Republic of Indonesia Defense University, Indonesia; Apid Rustandi¹; ¹National Research and innovation Agency, 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 Morita¹, N Okubo¹, T Ogawa¹, Y Sasaki¹; ¹Velcity 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
Y Lin¹, K.S Zhang¹, Z.H Han¹, Q Chen¹; ¹Northwestern 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
Xiaru Liu, China; Tianxiang Yu, China; Bifeng Song, China; Dong Xue, 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
Mithra Sankrithi, RIC Enterprises, United States; Dimitri Mavris¹, Raaga Sundar¹; ¹Georgia Institute of Technology, United States
16. Sep 26 16:05 16:30 4.9.2
0643		 LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY
K. Abu Salem, University of Trento, Italy
16. Sep 26 16:30 16:55 4.9.3
0960		 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
16. Sep 26 16:55 17:20 4.9.4
0274		 EMISSION REDUCTION POTENTIAL OF UNCONVENTIONAL CONFIGURATIONS FOR LONG-RANGE AIRCRAFT
E. M. Künstler¹, S. Roscher², A. Bardenhagen², A. Strohmayer¹; ¹University of Stuttgart, Germany ;²Technische Universität Berlin, Germany
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. Rodrigues Arnaud¹, F. Maia Nunes Celestino¹, G. L. Olichevis Halila¹, J. L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
16. Sep 26 16:05 16:30 5.9.2
0105		 CONTINUOUS UNSTEADY ADJOINT VARIATIONAL MULTISCALE METHOD FOR AIRFOILS SHAPE OPTIMIZATION
C. Brunelli¹, M. Avirovic¹, B. Janssens¹, B. G. Marinus¹; ¹Royal Military Academy, Belgium
16. Sep 26 16:30 16:55 5.9.3
0120		 SIMULATION OF AERODYNAMIC GROUND EFFECT FOR TILTED PROPELLERS USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S Shahjahan¹, V Ahuja¹; ¹Siemens Digital Software Industries, 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
D. Dessio Junior¹, G. L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J. L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
Reserve Paper 5.9.R
0089		 OPTIMIZATION OF MORPHOLOGICAL AND KINEMATIC PARAMETER FOR FLAPPING WING IN FORWARD FLIGHT
Dong Xue¹, Yating Gao¹, Tao Wu¹, Bifeng Song¹, Wenp[ing Song¹; ¹Northwestern Polytechnical University, China
Presenter: Gao Yating, Northwestern Polytechnical University
additional information (interactive) 5.9.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
Xiaoling Li¹, Lixin Yang¹, Yuhang Wei¹; ¹Beijing Jiaotong University, 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
6.9Failures
Chair(s): ,
Track 6
15 - Guest lectures
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. Wang¹, Z. Zhou¹, K. Wang¹, M. Li¹; ¹Northwestern Polytechnical University, China
16. Sep 26 16:05 16:30 7.9.2
0295		 STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS
Chen Zheng¹, Qiulin Qu¹, Peiqing Liu¹, Tianxiang Hu¹; ¹Beihang University, China
16. Sep 26 16:30 16:55 7.9.3
0318		 AERODYNAMIC AND STABILITY-DRIVEN PRE-DESIGN OF A FUEL-CELL POWERED FLYING WING AIRCRAFT
P. Kirschnek¹, S. Lesak¹, A. Tramposch¹; ¹FH JOANNEUM, 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
Hidetoshi Iijima, JAXA, Japan
additional information (interactive) 7.9.R
0171		 FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES
Kun Qiao, China; Dasheng Wei, China; Le Han, China; Zhongyu Chen, China; Zhaowei Yan, China; Yangjia Qin, China; Guoqiang Xu, China; Hailong Tang, China
additional information (interactive) 7.9.R
0392		 UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND STABILITY ANALYSIS
J. Guo¹, Y. Sun¹; ¹Cranfield University, 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
K Warnakula¹, M Silla¹, C Barber¹, T Hallwright¹, O Kaleagasi¹, D Schoemaker, Gyro Technic Inc., United States; ¹SYOS Aerospace, New Zealand
16. Sep 26 16:05 16:30 8.9.2
0019		 CYCLOSTATIONARY ANALYSIS FOR CRACK DETECTION AND TRENDING IN HELICOPTER GEARBOX CASING
Nader Sawalhi¹, Wenyi Wang¹; ¹Defence Science and Technology Group, Australia
16. Sep 26 16:30 16:55 8.9.3
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; R. Higuchi¹, T. Yokozeki¹; ¹The University of Tokyo, 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 Kouchlef¹, N Tsushima¹, T Yokozeki¹; ¹The 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. Mollet¹, L. Vertonghen¹, C. Julien¹; ¹ONERA, France
16. Sep 26 16:55 17:20 9.9.4
0277		 MANEUVER LOAD ALLEVIATION OF THE DRY WING FOR HYDROGEN AIRCRAFT
Fanglin Yu¹, Mirko Hornung¹; ¹Technical University of Munich, Germany
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. Otten¹, T. Matuschek¹, J. Häßy¹, J. Frank¹, R. Brakmann¹; ¹German 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. Matuschek¹, T. Otten¹, J. Häßy¹, J. Frank¹, R. Brakmann¹, P. Wehrel¹; ¹German 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. Oberthür¹, M. Stößel¹, D. Kozulovic¹, M. Krummenauer, Bundeswehr Technical Center for Aircraft and Aeronautical Equipm, Germany; ¹University 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 Omoto¹, D Sasaki¹, K Matsui², M Yamagami²; ¹Osaka Metropolitan University, Japan ;²IHI Corporation, 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. Im¹, Chang-hun: C.-H. Lee¹, Jae-hyun: J.-H. Jin, Sunchon National University, South Korea; Hyo-choong:H.-C. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea
16. Sep 26 16:05 16:30 11.9.2
0805		 DUAL BEZIER SPACE-TIME OPTIMIZATION UNDER HARD OBSERVATION-WINDOW CONSTRAINTS: A FEASIBILITY-ORIENTED JERK-CAP COMPARISON
H Kim, Koomin University, South Korea; S Lee, Kookmin University, South Korea
16. Sep 26 16:30 16:55 11.9.3
0858		 OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL
Seongyeon Kim¹, Jongho Shin¹, Hyeong-Geun Kim, Konkuk University, South Korea; ¹Chungbuk 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
M Tatar¹, B Lakic¹, G Buckus¹, R Grube¹, O Weckner¹, R Noll, United States; ¹Boeing, 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. Ali¹, C. Silva², E. Villani², J. M. Mello¹, W. Oliveira²; ¹Embraer, Brazil ;²ITA, Brazil
16. Sep 26 16:30 16:55 12.9.3
0198		 VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL
A.T. Ferraz¹, E. Villani¹, C.C.D Silva¹, J.M.G Mello, EMBRAER, Brazil; ¹ITA, Brazil
Presenter: Emilia Villani, ITA
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 ORIENTATION IDENTIFICATION USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS
Nithya D S¹, Francesca Monteleone¹, Vincenzo Muscarello, RMIT University, Australia; Giuseppe Quaranta¹; ¹Politecnico 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. WANG¹, J. GUO¹, Y. HE¹, F. WU¹, Z. GAO¹; ¹The 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
Majed 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, DLR German Aerospace Center, Institute of Flight Guidance, Germany; K. Schweiger¹, C. Bettremieux¹, C. Nava Gaxiola², A. Mangas Pita², M. Hardt³, A. Tutku Altun³, S. McNamee Freire, URBANV S.p.A., Italy; G. Riccardi, ENAV S.p.A., Italy; E. Fornaciari, D-Flight S.p.A., Italy; ¹EUROCONTROL Innovation Hub, France ;²AENA S.M.E., Spain ;³Boeing Aerospace Spain, Spain
additional information (interactive) 13.9.R
0538		 A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS
Xu Minze¹, Wang Lizhi, School of Reliability and Systems Engineering, Beihang universi, China; Ma Tielin¹, Wang Xiaohong, School of Reliability and Systems Engineering, Beihang universit, China; Fu Jingcheng¹; ¹Institute of Unmanned System, 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 (VTT) , Finland; L Asmer¹, B Schuchardt¹, A Badea², J Teutsch², J Vreeken², E Sunil², B Gungen², J Kok², M Murça, Technological Institute of Aeronautics (ITA), Brazil; I Borshchova³, J Keillor³, L Pinjala*, A Hebbar*, G Madhuranath*, D-M Manindrakumar*, N Yokoyama, Japan Aerospace Exploration Agency (JAXA), Japan; H-U Park, Korea Aerospace Administration (KASA), South Korea; P Kopardekar, National Aeronautics and Space Administration (NASA), United States; ¹German Aerospace Center (DLR) , Germany ;²Royal Netherlands Aerospace Centre (NLR), Netherlands ;³National Research Council Canada (NRC) , Canada ;*Council of Scientific & Industrial Research (CSIR), India
16. Sep 26 16:05 16:30 14.9.2
0901		 PREDICTION OF STRUCTURAL VIBRATIONS INDUCED BY MASS-UNBALANCED ELECTRIC PROPULSION SYSTEMS
G. R. Dias¹, D. V. R. Silva¹, A. G. Heck¹, D. A. Rade¹; ¹Aeronautics 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. Sarmento¹, P. Krus, Linköping University (LiU), Sweden; E. Villani¹; ¹Aeronautics 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
Ramon Fernandes Viana¹, Carolina Rutili de Lima¹, Vinicius Abrão S. Marques, Federal University of Triângulo Mineiro, Brazil; Mayara Condé Rocha Murça¹, Marcos R. O. A. Maximo¹, Q. Forster Carlos Henrique¹; ¹Aeronautics Institute of Technology, Brazil
Presenter: Vinicius Abrão da Silva Marques, Federal University Of Triângulo Mineiro
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
0573		 PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING
L. Jilke¹, M. Schubert¹, N. Hosters², F. Raddatz¹, M. Behr², G. Wende¹; ¹German Aerospace Center (DLR), Germany ;²RWTH Aachen University, Germany
16. Sep 26 16:55 17:20 15.9.4
1034		 DATA-DRIVEN TECHNOLOGY INTELLIGENCE: AN APPLICATION TO AIRCRAFT ENGINE MAINTENANCE
A Dadashi, German Aerospace Center (DLR), Germany
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
Liying Hou¹, Jiantang Liu¹, Yulu Song¹, Hui Xiao¹; ¹Nanjing 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 (by Frank Haselbach ISABE president)
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
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 Würfel¹, B Djartov¹, M Friedrich¹, S Schog¹, A Papenfuss¹; ¹German 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. Mayima¹, C. Bejarano Espada¹, A. Gampe², A. Hamann², R. De Masellis¹, A. Fuchs¹, M. Athanasiadou¹, H. Palop¹, D. Watkins¹; ¹Collins Aerospace, Applied Research & Technology, Ireland ;²German Aerospace Center, Institute of Flight Guidance, Germany
17. Sep 26 10:05 10:30 1.10.3
0450		 OFFLINE MULTIMODAL LARGE LANGUAGE MODELS FOR DECISION SUPPORT IN AIR OPERATIONS
J. P. A. Dantas¹, J. A. Cunha¹, G. Dietzsch¹; ¹Instituto de Estudos Avançados, Brazil
17. Sep 26 10:30 10:55 1.10.4
0547		 AI IN THE COCKPIT, A JARVIS STORY
R. De Masellis¹, A. Fuchs¹, A. Mayima¹, C. Bejarano Espada¹, M. Athanasiadou¹, H. Palop¹, D. Watkins¹; ¹Collins Aerospace, Applied Research & Technology, Italy
Presenter: Riccardo De Masellis, Collins Aerospace
2.10Aircraft Electrification, Innovation & Certification Perspectives & Challenges
Chair(s): ,
Track 2
15 - Guest lectures
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. Wang¹, R. Carrese¹, L. Brown¹, J. Collins¹, P. Marzocca, RMIT University, Australia; ¹Boeing 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-Juárez¹, A Dell'Amico¹; ¹Linköping 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.-Y He¹, H Zhao¹; ¹Northwestern Polytechnical University, 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 HE¹, B G MI¹, J Y ZHANG¹; ¹School of Aeronautics of 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
5.10Propeller Aerodynamics and Rotor Flows
Chair(s): Rana, Z., Kiszkowiak, L.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
17. Sep 26 08:50 09:15 5.10.1
0761		 STUDY OF THE AERODYNAMIC INTERFERENCE OF STRUT-BRACED WINGS WITH DISTRIBUTED PROPELLERS
n/a Fossati, Unniversity of Strathclyde, United Kingdom
17. Sep 26 09:15 09:40 5.10.2
0654		 EPSILON V4: AN OPEN-SOURCE TOOL FOR EXTENDED AERODYNAMICS EXERGY ANALYSIS
C Paillard¹, G Bourreau-Tirel, Aura Aero, France; S Duplaa¹, M Fiore¹; ¹ISAE-SUPAERO, France
17. Sep 26 09:40 10:05 5.10.3
0795		 COMPARATIVE ANALYSIS OF DIFFERENT NUMERICAL SIMULATION METHODS FOR PROPELLER SLIPSTREAM
Jiawen He¹, Yue Zhao¹, Xinyuan Wei¹, Tieren Chen¹, Yong Yang¹; ¹Northwestern Polytechnical University, China
17. Sep 26 10:30 10:55 5.10.4
0352		 INVESTIGATION AND ONE-DIMENSIONAL MODELING OF THE DUAL-ROTOR GEROTOR PUMP AT HIGH ALTITUDES
Z.C. Su, China; P.F. Zhu, China; G.L. Li, China; C.H. Zhong, China; Y.G. Lyu, 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 Gavrilovic¹, D Lanot¹, M Bronz, ENAC, France; ¹ISAE-SUPAERO, France
Presenter: Nikola Gavrilovic, ISAE-SUPAERO
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 Marshall¹, N Heath², D Handford², J Smith², P Manovski¹, M Jones¹, A Neely²; ¹Defence Science and Technology Group, Australia ;²University of New South Wales, 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
17. Sep 26 10:30 10:55 6.10.4
0775		 ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM
D. T Rajeepan¹, N. J Lawson¹, A Galffy, Turbulence Solutions, Austria; ¹University of Sydney, Australia
additional information (interactive) 6.10.R
0775		 ANALYSIS OF A DUAL AIR DATA AND MULTI-HOLE PRESSURE PROBE BOOM
D. T Rajeepan¹, N. J Lawson¹, A Galffy, Turbulence Solutions, Austria; ¹University of Sydney, 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. Boruga¹, N. Zalewska¹, D. Lundström¹, P. Krus¹; ¹Linköping University, Sweden
17. Sep 26 09:40 10:05 7.10.2
0713		 A 3D-PRINTED TESTBED FOR FLIGHT CONTROL SYSTEM RESEARCH.
D. Lundström¹, C.-V. Boruga¹, S. Riethausen¹, R. Larsson¹; ¹Linköping University, 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. Xie, School of Aeronautics, Northwestern Polytechnical University Cit, China; Z. Zhou, Northwestern Polytechnical University, 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
Rui Wang¹, Yunheng Wu¹, Zhou Zhou¹, Sensen Yao¹, Ziyang Zhang¹; ¹Northwestern Polytechnical University, 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, Australia; KC Wong, Australia
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, Italy; F. Ferrigno, CIRA, Italy; A. Gliszczynski, Lodz University of Technology, Poland; A.-L. Delot, ONERA, France
Presenter: Adrian Gliszczynski, Lodz University of Technology
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. Guo¹, W. Yang¹, X. Xu¹, Z. Li¹, J. Liu¹, S. Cao¹; ¹Northwestern Polytechnical University, China
17. Sep 26 09:40 10:05 9.10.2
0381		 ENABLING FORWARD SWEPT WING DESIGNS
F. Saachi¹, F. Healy¹, D. Rezgui¹, J.E. Cooper¹; ¹University 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
N Demant, FH Aachen University of Applied Sciences, Germany; P Kantzidis¹, G Lazzaro, Polytechnic University of Milan, Italy; V Muscarello¹; ¹Royal Melbourne Institute of Technology, 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.-L. Lei, China; Y.-S. Gu, China; Z.-C. Yang, China
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. KIERBEL¹, R. ABDOUH², D. Chamoro³, A. te Nijenhuis*, M. Schoonmade *, F. Wokke*, R. Alderliesten, TUD, Netherlands; M. Dhalle, UT, Netherlands; G. Knol , Cryoworld, Netherlands; F. Dioguardi, Stirling Cryogenics, Netherlands; F. van Duin, Futura Composites B.V., Netherlands; M. Van Vliet³, T. Hope³, B. Eastment³, M. Tassisto², E. Nilsson², J. Monin-Baroille², J.-W. van Zwieten¹; ¹AIRBUS Netherlands, France ;²AIRBUS UpNext, France ;³GKN Fokker Aerospace B.V., Netherlands ;*NLR, Netherlands
17. Sep 26 09:40 10:05 10.10.2
0299		 EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYDROGEN FLAMES UNDER COLD INJECTION CONDITIONS
F. Thilker¹, R. Krewinkel, Graz University of Technology , Austria; T. Tramposch¹; ¹University of Applied Sciences JOANNEUM GmbH, 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, C. Serpico¹, L. Garbarino¹, M. Inverno¹, 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
A. Görtz¹, J Häßy¹, M Baier Schmelcher¹, M El-Soueidan¹, F Herbst¹; ¹German Aerospace Center, Germany
Reserve Paper 10.10.R
0954		 AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES
F. Pak¹, U. Perra¹, F. P. T. Willems¹, T. Hofman¹, M. Salazar¹; ¹Eindhoven 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.H. Wang¹, L.X. Wang¹, R. Zhao², Z. Wu², Y.F. Xu¹, H.L. Liu¹, S. Tai¹, T. Yue¹; ¹Beihang University, China ;²COMAC Shanghai Aircraft Customer Service Co. Ltd., 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
A. Navarro¹, M. Alam¹, A. Elliott¹, E. Jinks, Siemens Digital Industries Software, United Kingdom; ¹Cranfield 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
M H Lowenberg¹, D Pusztai¹; ¹University of Bristol, United Kingdom
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
T Mahr¹, L Whiteman¹, A Daley¹, S Hewa Witharange¹, J Prpic¹, K Holtta-Otto¹, M Das¹; ¹University of Melbourne, Australia
Presenter: Lily Whiteman, University of Melbourne
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. Souza Braga¹, E. Bernieri Schiavon de Andrade¹, W. Rodrigues de Oliveira¹; ¹ITA, 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 IMPROVING ARRIVAL-SEPARATION STABILITY THROUGH ARRIVAL TRAJECTORY ANALYSIS AT CONGESTED AIRPORTS
Ryo Kajikawa¹, Noboru Takeichi¹; ¹Tokyo 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
C.S.X. Ng¹, M. Schultz, University of Bundeswehr Munich, Germany; E. Itoh¹; ¹The 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
Gabriele Enea¹, Vilmar Mollwitz², Tobias Finck², Tom Reynolds¹, Bernd Korn²; ¹MIT Lincoln Laboratory, United States ;²DLR Institute of Flight Guidance, Germany
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
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. Lübbe¹, M. Schäfer¹, O. Bertram¹, A. Bierig¹; ¹German 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. Schäfer¹, S. Lübbe¹, O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany
Presenter: Sascha Lübbe, German Aerospace Center (DLR)
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
Hamada Rizk¹, Hirozumi Yamaguchi¹, Sumio Morioka², Takahiro Inagawa²; ¹Osaka University, Japan ;²Interstellar Technologies Inc., 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. Machado¹, J. L. C. Reis¹, A. Zaramella, ACS Aviation / MOYA Aero, Brazil; L. G. M. Soltz¹; ¹Universidade Federal de Minas Gerais, 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 Yoshikawa¹, S Horishita², Y Hamada², T Ushio¹, V Chandrasekar, Colorado State University, United States; ¹The University of Osaka, Japan ;²Japan Aerospace Exploration Agency, 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. Klein¹, E. Arts¹, B. Atanasoaie¹, H. Meyer¹, F. Raddatz¹, Z. Daw, University of Stuttgart, Institute of Aircraft Systems, Germany; ¹German Aerospace Center (DLR), Germany
17. Sep 26 09:40 10:05 15.10.3
0244		 ACCELERATED EXPERIMENTAL INVESTIGATION OF ENVIRONMENTALLY ASSISTED CRACKING IN AA7085
J Rogers, RMIT University, Australia; I Field¹, N Tugwell¹, M Salagaras¹, B Dixon¹; ¹DSTG, 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. Zhu¹, J. Panta¹, R. Yang¹, S. Zhang, Univeristy of Technology Sydney , Australia; ¹Western 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
Dingxin Tang¹, Wenqing Yang¹, Jianlin Xuan¹; ¹Northwestern Polytechnical University, China

10:55 - 11:00CHANGEOVER BREAK

1.11AI 1
Chair(s): ,
Track 1
15 - Guest lectures
17. Sep 26 11:00 11:25 1.11.1
0990		 TOWARDS A FOUNDATIONAL AI MODEL FOR AIRCRAFT DESIGN: FROM HIGH-FIDELITY DATASETS TO SCALING LAWS
n. Ashton, United States
17. Sep 26 11:25 11:50 1.11.2
1018		 HYBRID AI-SIMULATION FOR AERODYNAMICS APPLICATIONS
Denis Gueyffier, ONERA, France
2.11Sharing the Air (Airspace)
Chair(s): ,
Track 2
15 - Guest lectures
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. BURKA¹, P. Smith¹; ¹Swinburne 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 10:35 11:00 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 11:00 11:25 3.11.2
0034		 MULTI-OBJECTIVE OPTIMISATION OF AERIAL VEHICLES USING REINFORCEMENT LEARNING
T Batty, Defence Science and Technology Group, Department of Defence, Australia
Presenter: Trevor Batty, Defence Science And Technology Group
17. Sep 26 11:25 11:50 3.11.3
0100		 INVERSE AEROELASTIC SIZING FOR STRUT-BRACED WINGS VIA PHYSICS-GUIDED GENERATIVE MODELING
Y.-Y. Ma, China; W.-Y. Wei, China; Y.-Q. Du, China; M. Abouhamzeh, Netherlands; Z.-H. Han, China
17. Sep 26 12:15 12:40 3.11.4
0609		 COMPARISON OF CONFIGRATIONS FOR FLEXIBLE AIRCRAFT USING AEROELASTIC ANALYSIS
N Okubo¹, N Morita, Velocity Aeroworks .Inc, Japan; T Tuchiya¹; ¹The 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
1022		 THE ROLE OF NEXT-GENERATION HPC AND MACHINE LEARNING IN ACHIEVING THE 2030 VISION GOALS
N. Ashton, NVIDIA, United States
17. Sep 26 12:15 12:40 4.11.4
0999		 CFD VISION 2030 LOOKING FORWARD: PANEL DISCUSSION
A. W. Cary, United States
5.11UAS and AAM Design Applications
Chair(s): Pezzella, G., 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 Jacinto¹, D. Skrna¹, M. Berens¹; ¹Technische Universität Wien, Austria
17. Sep 26 11:50 12:15 5.11.3
0280		 A COMPARATIVE STUDY OF THE AERODYNAMIC CHARACTERISTICS OF TWO CONFIGURATIONS
Kai You, China; Rongbo Zhu, China; Zhenli Chen, China
Presenter: Rongbo Zhu
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. Skrna¹, M. de Rosa Jacinto¹, Martin Berens¹; ¹Technische Universität Wien, Austria
Reserve Paper 5.11.R
0747		 RESEARCH ON AN AERODYNAMIC LOAD METHODOLOGY FOR FLAPPING WINGS BASED ON EXPERIMENTALLY ACQUIRED DEFORMATION
K.R. Yang¹, B.F. Song¹, D. Xue¹; ¹Northwestern Polytechnical University, China
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. FARCY¹, S. PRINCE², M. ALAM², G. TANGUY¹, N. VAUCHEL¹, A. PROENCA²; ¹ONERA, France ;²Cranfield University, United Kingdom
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
L. Malicki¹, M. Marciniuk¹, L. Kiszkowiak², P. Piskur, Polish Naval Academy of the Heroes of Westerplatte, Poland; S. Kachel²; ¹Wroclaw University of Science and Technology, Poland ;²Military University of Technology, Poland
Presenter: Łukasz Kiszkowiak, Military University of Technology
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. Domínguez¹, F. Parra¹, D. López¹, A. García-Gutiérrez¹; ¹Universidad de León, Spain
additional information (interactive) 6.11.R
0427		 DESIGN, MANUFACTURING, AND TESTING OF HUMPBACK WHALE-INSPIRED TUBERCLES FOR ENHANCED LOW-REYNOLDS WING PERFORMANCE.
Estela Barroso Barderas, instituto Nacional de Técnica Aeroespacial (INTA),, Spain; Rafael Bardera Mora¹, Juan Carlos Matías García¹, Jaime Fernández Antón¹, Ángel A. Rodríguez Sevillano, Universidad Politécnica de Madrid, Spain; ¹Instituto Nacional de Técnica Aeroespacial (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. Crase¹, S. Pywell¹, K. Rosser¹; ¹Defence Science and Technology Group, Australia
17. Sep 26 11:25 11:50 7.11.2
0204		 FAMILIARIZATION, OPERATION AND DEBRIEFING: AN ADAPTIVE AUGMENTED REALITY SUPPORT SYSTEM FOR UAV FLIGHT TESTING
M. Zintl¹, F. Holzapfel¹; ¹Technical University of Munich, 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
Minkyu Park, Changwon National Unviersity, 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. Thomessen¹, S. Schopferer¹, P. Nagarajan¹; ¹German Aerospace Center (DLR), Germany
8.11High-Temperature Materials/Structures
Chair(s): ,
Track 8
15 - Guest lectures
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-Rebassa¹, D. MacManus¹, R. Christie¹, J. Matesanz-Garcia¹, Y. Frey², C. Sheaf²; ¹Cranfield University, United Kingdom ;²Rolls-Royce plc., United Kingdom
17. Sep 26 11:25 11:50 10.11.2
0612		 RUBBER ENGINE INTEGRATED OPTIMIZATION STRATEGY FOR OVERALL AIRCRAFT DESIGN
J. Häßy¹, J. Schmeink¹, B. Fröhler¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 11:50 12:15 10.11.3
0111		 EFFECT OF INTAKE AERODYNAMICS AND FLOW DISTORTION ON FAN STALL INCEPTION
J. Hueso-Rebassa¹, D. MacManus¹, F. Tejero¹, T. Williams, Cambridge University, United Kingdom; Y. Frey², G. Thorne²; ¹Cranfield University, United Kingdom ;²Rolls-Royce plc., 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
M-X ZHANG¹, Y-S ZHANG, Chinese Flight Test Establishment, China; B-G MI¹, Y LIU¹, R-Q WANG¹; ¹Northwestern Polytechnical University, 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. Surmann¹, S. Myschik¹; ¹University 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. Alam¹, J. Renault¹, M. Hromcik², T. Hanis²; ¹Cranfield University, United Kingdom ;²Czech Technical University, Czech Republic
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
additional information (interactive) 11.11.R
0106		 AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE
R. Wang¹, Y. Liu¹, M. Zhang¹; ¹Northwestern Polytechnical University, 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 Zhang¹, L Wang¹, D.D Gu¹; ¹Nanjing 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. Yang¹, L.-K. Yang¹, L. Wei¹, S.-Y. Sun¹; ¹Dalian 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. Chen¹, D.-D. Gu¹; ¹Nanjing 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. D. Martins¹, C. C. D. Silva¹, D. A. Rade¹, J. M. G. Mello², A. V. S. Silva², A. P. C. Cuco²; ¹Aeronautics Institute of Technology, Brazil ;²Embraer S. A., Brazil
Presenter: Caroline Silva, Aeronautics Institute of Technology
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
Fangyi WU, China; Yingjie HE, China; Jiang Guo, China; YIkang WANG, China; Zhenyu GAO, 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
Sinan Abdulhak, University of Michigan, Industrial and Operations Engineering, United States; Ben Donaldson¹, Armaan Kamat¹, Karis Hu¹, Jason Huang¹, Max Z. Li, University of Michigan, United States; ¹University of Michigan, Aerospace Engineering, 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
Ziyan Chen¹, Yanpeng Zhao¹, Xinglong Wang¹, Wei Dai¹, Kin Huat Low¹; ¹Civil 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. Voth¹, J. Wade, UCSD, United States; O. Bertram¹, A. Bierig¹; ¹German Aerospace Center (DLR), Germany
17. Sep 26 11:25 11:50 14.11.2
0205		 COMMON ONTOLOGY FOR PROPULSION ARCHITECTURES - COPA
S. Reitenbach, German Aerospace Center (DLR), Germany
17. Sep 26 11:50 12:15 14.11.3
0479		 AUTOMATIC GENERATION OF PHYSICAL SYSTEM MODELS FOR AIRCRAFT SYSTEMS BASED ON LLMS
Y.-L. Ren¹, L.-F. You¹, X.-H. Gao¹, C.-Y. Chang¹, Z.-Q. Wang¹, Z.-Q. Guo¹; ¹Beihang 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
Z. Zengerling¹, A. Lau¹, M. Clococeanu¹, R. Kanitz¹, J. Schwengler², A. Vogel², K. Abu-Taa²; ¹German Aerospace Center (DLR), Germany ;²Rolls-Royce Deutschland, Germany
17. Sep 26 11:25 11:50 15.11.2
0611		 PROVIDING SENSOR INFORMATION FOR BORDING TIME PREDICTION
M. Schultz¹, S.B. Göppel¹, S. Reitmann, University of Technology Chemnitz, Germany; ¹University of the Bundeswehr Munich, 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
Naoise Barry¹, Conor Gallagher¹, Charles Stuart¹; ¹Trinity College Dublin, Ireland
17. Sep 26 12:15 12:40 15.11.4
0031		 ASSESSING AIRLINE PURCHASE MOTIVATION FOR HYDROGEN AIRCRAFT UNDER FUTURE CORSIA
Hiroko 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; 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 Aircraft Technical & Financial Consulting, Mexico; E Espinosa Juarez¹, A.M Zarate Villazon², B Ravikanti², H Szöke-Erös³, P Shiva Prakasha³, L Knöös Franzén¹; ¹Linköping University, Sweden ;²Georgia Institute of Technology, United States ;³German Aerospace Center (DLR), Germany

12:40 - 13:40LUNCH BREAK

1.12AI 2
Chair(s): ,
Track 1
15 - Guest lectures
2.12DPI workshop results
Chair(s): ,
Track 2
15 - Guest lectures
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. Swannet¹, N. A. K. Doan, Imperial College London, United Kingdom; C. Varriale¹; ¹Delft 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
W. Lin¹, C.-C. Nian¹, J.-C. Li¹; ¹Northwestern 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.-X Li¹, Z.-H Han¹, K. Song¹, K.-S Zhang¹; ¹Northwestern Polytechnical University, China
Reserve Paper 3.12.R
0254		 AN EFFICIENT TRANSITION PREDICTION METHOD USING NEURAL NETWORK SURROGATE MODELS
Jiahao Wu, China; Wenping Song, China; Han Nie, China; Chengpeng Liu, China
Reserve Paper 3.12.R
0458		 RESEARCH ON GENERALIZED REPRESENTATION OF FLYING-WING CONFIGURATIONS BASED ON DEEP LEARNING
X.-M. zhang, China; H. Zhao, China
Presenter: He He
4.12Propulsion/Propulsion-Integration
Chair(s): ,
Track 4
15 - Guest lectures
5.12Applied CFD Approaches
Chair(s): Bura, R., Imamura, T.
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
Haozhe Wang¹, Jialong Wang¹, Zhantao Li¹, Wenqing Yang¹, Xiaojun Yang¹; ¹Northwestern 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. Pirillo¹, R. Bianchini¹, D. Palma¹, F. Stella¹; ¹Sapienza University of Rome, 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. Avoni¹, M. Bronz¹, J.-M. Moschetta¹, J.-P. Condomines¹; ¹Fédération ENAC ISAE-SUPAERO ONERA, Université de Toulouse, France
17. Sep 26 14:55 15:20 5.12.4
0879		 FALCON: FRAMEWORK FOR AIRFOIL CFD AND ANALYSIS OPTIMIZATION
Prisha Desai, Manipal Insititute of Technology, Manipal, India; Anwak Manoj Kumar, Manipal Institute of Technology, Manipal, India; Manikandan Murugaiah, 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
H Mohsin¹, S.A. Prince¹, D Di Pasquale¹; ¹Cranfield University, United Kingdom
Presenter: Davide Di Pasquale, Cranfield University
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 Brown, RMIT university, Australia; J. McCarthy¹, C. Marshall¹, M Jones¹, I Maatz, Air Force Research Laboratory (AFRL), United States; ¹Defence Science and Technology Group (DSTG), 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. Hiemcke¹, R. Buth¹, C. Schneider¹, C. J. Jones¹; ¹General 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 13:15 13:40 7.12.1
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 13:15 13:40 7.12.2
0859		 VANE-LESS 3D WIND ESTIMATION FOR FIXED-WING UAVS: A TEMPORAL RESIDUAL NETWORK APPROACH WITH CHANNEL ATTENTION
Ziyang Zhang¹, Shaokun Li¹, XiaoPing Xu¹, Zhou Zhou¹; ¹Northwestern Polytechnical University, China
17. Sep 26 14:05 14:30 7.12.3
0454		 MPPI-BASED COMPUTATIONAL GUIDANCE FOR MOTION PLANNING OF A MULTIROTOR UAV USING DEPTH-CAMERA-BASED OBSTACLE REPRESENTATION
K.W Jang¹, Yangjae Jeong¹, G.G Kim¹; ¹Electronics and Telecommunications Research Institute, South Korea
8.12 Aircraft Electrification, Systems and Certification
Chair(s): ,
Track 8
15 - Guest lectures
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
Y. Pan¹, M. Alam¹; ¹Cranfield 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. Mueller¹, N. Singer¹, N. Moser¹, T. Siemer¹, F. Daoud¹; ¹Technical 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. Ma¹, H.-C. Yang¹, K. You¹, R.-B. Zhu¹, Z.-L. Chen¹; ¹Northwestern Polytechnical University, China
Presenter: Rongbo Zhu, Northwestern Polytechnical University
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. Song¹, H. Shi¹, Z. Huang¹, H. Xiao, China; ¹Northwestern 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
Q. T Dinh¹, D. L Chu¹, X. H Vu¹, C. A Pham¹; ¹Viettel Aerospace Institute, 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.B. Zhou¹, B.F. Song¹, Y.C. Liu¹, M.X. Chen, COMAC Shanghai Aircraft Manufacturing Co., Ltd., China; Q. Fu¹; ¹Northwestern Polytechnical University, 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. Kwiek¹, K. Kania¹; ¹Warsaw 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 Kock¹, BB Huyssen¹, RJ Huyssen, Council for Scientific and Industrial Research, South Africa; ¹University of Pretoria, South Africa
Presenter: Barbara Huyssen, University of Pretoria
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
LIXIA XI, China; Zhen Wang, China; Gu Dongdong, 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. Ravandi¹, G. Miris¹, P. Burka¹; ¹AIR Hub, Swinburne University Of Technology, 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
Ron Van Manen¹, Kjelt Van Rijswijk¹, Laura Veldenz¹; ¹Stichting 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. Murayama¹, Y. Murata¹, M. Kohzai¹, K. Yamamoto¹, Y. Ito¹, H. Ura¹, T. Takaishi¹; ¹Japan 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
14.12Aeronautical R&D in Australia
Chair(s): ,
Track 14
15 - Guest lectures
17. Sep 26 13:40 14:05 14.12.1
1021		 EVTOL AND PROPULSION R&D IN THE SYDNEY PROPULSION LAB
D. Verstraete, Australia
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 Filippatos¹, D Markatos¹, Th Kalampoukas¹, N Raptis¹, M Abouhamzeh², K Stamoulis², Sp Pantelakis¹; ¹Department of Mechanical Engineering & Aeronautics, University o, Greece ;²Faculty of Technology, Amsterdam University of Applied Sciences, Netherlands
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; K.P. Stamoulis, Amsterdam University of Applied Sciences, 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
Juliane 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
Z. Huang¹, D. Xiao¹, X. Guo¹, L. Zhao¹, C. Song¹; ¹Northwestern Polytechnical University, China
Presenter: Zilang Huang, Northwestern Polytechnical University
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
S.I. Hallstedt¹, P. Léonard¹, M. Aldèn¹, G. Dokter¹, O. Isaksson¹; ¹Chalmers 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