35th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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

Wednesday, 16. Sep 2026

0.6ICAS LECTURE FOR INNOVATION IN AERONAUTICS Veronique Roca – Airbus Beluga X
Chair: A. Andreeva-Mori ICAS EC Member
16. Sep 26 08:00 08:50

08:50 - 09:15COFFEE BREAK

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

10:45 - 10:50CHANGEOVER BREAK

1.7GSA2: Super Panel: Pathways to Global Sustainable Aviation
Chair(s): Madavan, N., Fischer, M.
Track 1 Pyrmont Theatre
15 - Guest lectures
16. Sep 26 10:50 11:15 1.7.1 GLOBAL SUSTAINABLE AVIATION PANEL DISCUSSION WITH VERONIQUE ROCA, ALAN NEWBY, JIM HILEMAN, CHRISTINE ANDREWS, RICH WAHLS AND CLAIRE WAGHORN (DURATION 100 MINUTES)
R.A. Wahls, NASA, Retired, United States
2.7GARTEUR 2
Chair(s): Hammer, B.
Track 2 C4.1
15 - Guest lectures
16. Sep 26 10:50 11:15 2.7.1 MULTIFUNCTIONAL METAMATERIALS FOR AEROSPACE APPLICATIONS
F.J. San Millán¹, J. Garcia-Martinez¹, P. Pflueger Tejero¹, I. Martinez Teres¹, U. Dincer², M. Misol, Germany; P. Wierach², A. Riccio³, A. Garofano³, M. Battaglia³, J. Berthe*, R. Ortiz*, J. Germain*, F. Roudolff*, W.W. Witsº, B. Noordmanº, O. Erartsinº, J. de Kruijk, Netherlands; ¹INTA, Spain ;²DLR, Germany ;³University of Campania, Italy ;*ONERA, France ;ºNLR, Netherlands
Presenter: Francisco Javier San Millan Fiel, INTA- Spanish National Institute for Aerospace Research
16. Sep 26 11:15 11:40 2.7.2 ADDITIVE MANUFACTURING OF NOVEL HIGH STRENGTH ALUMINIUM ALLOYS
M.L. Montero-Sistiaga¹, M. de Smit¹, A. Pastor Muro², N. Redondo Torrico², M. Thomas³, A. Morel³, S. Drawin³, F. Palm, Airbus, Central Research & Technology (CRT), Germany; ¹Royal NLR-Netherlands Aerospace Centre, Netherlands ;²National Institute of Aerospace Technology (INTA), Spain ;³DMAS, ONERA, France
Presenter: Francisco Javier San Millan Fiel, INTA- Spanish National Institute for Aerospace Research
16. Sep 26 11:40 12:05 2.7.3 CHARACTERIZATION AND MODELLING OF CERAMIC MATRIX COMPOSITES SUBMITTED TO SEVERE THERMO-MECHANICAL LOADING
F. Laurin¹, Y. Delgado González, NLR, Netherlands; S. Reh, DLR, Germany; A. Russo, 4Università degli Studi della Campania , Italy; C. Footer, QINETIQ, United Kingdom; F. Roudolff¹; ¹ONERA, France
16. Sep 26 12:05 12:30 2.7.4 AI IN AVIATION CYBERSECURITY RISK ASSESSMENT: OPPORTUNITIES AND CHALLENGES
R. Elia, Univesity of Campania Luigi Vanvitelli, Italy; P. Bieber¹, D. Pascarella, CIRA, Italy; M. Rak, University of Naples Federico II, Italy; C. Döll¹; ¹ONERA, France
3.7Case Studies 1
Chair(s): Gibson, T.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
16. Sep 26 10:50 11:15 3.7.1 SWIFT: AN ULTRA HIGH ASPECT RATIO STRUT-BRACED DRY WING HYDROGEN-POWERED AIRCRAFT
E. Stragiotti¹, E. Nguyen Van¹, R. Parello¹, S. Defoort¹, D. Losada Costoso², C. Mollet², M. Méheut², O. Atinault², F. Moëns², L. Vertonghen³, C. Julien³, A. Lannoo*, V. 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 3.7.2 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 3.7.3 A BILEVEL STRATEGY FOR ON-DESIGN EVTOL SIZING AND OFF-DESIGN STRUCTURAL WEIGHT OPTIMIZATION
L. Liu¹, Y. Wu¹, M.A. Hariansyah¹, R.P. Liem, ICL, Department of Aeronautics, United Kingdom; ¹HKUST, Department of Mechanical and Aerospace Engineering, Hong Kong SAR of China
Presenter: Yiran Wu, HKUST,Department of Mechanical and Aerospace Engineering
16. Sep 26 12:05 12:30 3.7.4 OPTIMAL CONCEPTUAL DESIGN AND UPGRADE STRATEGIES FOR EVTOL AIRCRAFT UNDER EVOLVING TECHNOLOGIES
M.A. Hariansyah¹, C. Reyner¹, R.P. Liem, Imperial College London, United Kingdom; P.S. Palar, Institut Teknologi Bandung, Indonesia; ¹The Hong Kong University of Science and Technology, Hong Kong SAR of China
Reserve Paper 3.7.R THREE-DIMENSIONAL AERODYNAMIC ANALYSIS OF A WING–ROTOR CONFIGURATION FOR A FOLDING WING UAV
S. Choi¹, Y. Lee¹, H. Choi¹, B. Cho¹, Y. Kim¹, D. Jung¹; ¹Korea Aerospace University, South Korea
Presenter: Byeonggeun Cho, Korea Aerospace University
4.7Unconventional Configurations - 1
Chair(s): Gerhards, R.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
16. Sep 26 10:50 11:15 4.7.1 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 4.7.2 COMPARATIVE DESIGN OF SBW AIRCRAFT WITH AERODYNAMIC SHAPE OPTIMIZATION FOR THREE DIFFERENT PROPULSION LAYOUTS
L. Li¹, M. Chao¹, L. Wang, AVIC (CHENGDU) UAS CO., LTD., China; J. Zhong, School of Aeronautics, Northwestern Polytechnical University, China; F. Li, Xinjiang Institute of Intelligent Equipment, China; ¹School of Future Transportation, Chang’an University, China
16. Sep 26 11:40 12:05 4.7.3 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
16. Sep 26 12:05 12:30 4.7.4 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
5.7Machine Learning Applications
Chair(s): , , Halila, G.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 10:50 11:15 5.7.1 EFFICIENT ROTOR AERODYNAMIC SHAPE DESIGN USING A MULTI-FIDELITY NEURAL NETWORK-BASED GLOBAL OPTIMIZATION METHOD
S. Li¹, W.P. Song¹, Z.Q. Shen¹; ¹ Northwestern Polytechnical University, China
16. Sep 26 11:15 11:40 5.7.2 MACHINE LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION OF NACA AIRFOILS UNDER GEOMETRIC DESIGN CONSTRAINTS
M.S. Abulela¹, M.I. Alam¹; ¹King Fahd University of Petroleum and Minerals, Saudi Arabia
16. Sep 26 11:40 12:05 5.7.3 PHYSICS-INFORMED NEURAL OPERATORS FOR DISTURBANCE FIELD PREDICTION IN NONPARALLEL BOUNDARY-LAYER STABILITY ANALYSIS
G. Dalinajara Abreu Smith Borges¹, V. Silva Figueredo¹, G.L. Olichevis Halila¹, J. Messias Magalhães Júnior, Georgia Institute of Technology, United States; J.L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
16. Sep 26 12:05 12:30 5.7.4 EXPLAINABLE KNOWLEDGE DRIVEN LLM AGENTS FOR TRUSTWORTHY AIRFOIL AERODYNAMIC OPTIMIZATION DESIGN
Y. Fan¹, Y. Sun¹, J. Xue¹, Y. Wang¹, B. Mi¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
6.7High Speed Flight: High-Temperature Materials/Structures
Chair(s): Bowcutt, K., Neely, A.
Track 6 C4.5
15 - Guest lectures
16. Sep 26 10:50 11:15 6.7.1 PREDICTING THE RESPONSE OF HIGH-TEMPERATURE STRUCTURE FOR HIGH-SPEED VEHICLES THROUGH SIMULATION AND MEASUREMENT
A. Neely, UNSW, Australia
16. Sep 26 11:15 11:40 6.7.2 FROM HIGH-TEMPERATURE MATERIALS TO HIGH-RATE PRODUCTION: OVERVIEW OF EXISTING RESEARCH EFFORTS AND OUTLOOK
M. Heitzmann, University of Queeensland, Australia
16. Sep 26 11:40 12:05 6.7.3 PANEL DISCUSSION (TIL END OF THE BLOCK)
P. Panel
7.7Configuration Aerodynamics and Coupled Flight Behaviour
Chair(s): Lawson, N.
Track 7 C4.6
03.4 - Applied Aerodynamics
16. Sep 26 10:50 11:15 7.7.1 FLIGHT-TEST DATA-DRIVEN HIGH-ANGLE-OF-ATTACK DYNAMICS MODELING VIA LSTM-POLYNOMIAL HYBRID APPROACH
Z. Zhang¹, H. Zhao¹, W. Zhang¹, J. He¹, Z. Gao¹; ¹Northwestern Polytechnical University, China
16. Sep 26 11:15 11:40 7.7.2 MULTI-OBJECTIVE SHAPE OPTIMIZATION OF A LAUNCH VEHICLE FAIRING ACROSS MULTIPLE FLOW 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 7.7.3 STUDY ON THE IMPACT OF TRIM CONDITION ON LATERAL AND DIRECTIONAL STABILITY FOR A TAILLESS AIRCRAFT
K. Kania, Warsaw University of Technology, Poland
Presenter: Agnieszka Kwiek, Warsaw University of Technology
16. Sep 26 12:05 12:30 7.7.4 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 7.7.R NUMERICAL CHARACTERISATION OF SHIP-AIRWAKE EFFECTS ON MEDIUM-WEIGHT UAV APPROACH AND GO-AROUND OPERATIONS TO CANBERRA-CLASS LHDS
M.J. Ericksen¹, N.J. Lawson¹; ¹The University of Sydney, Australia
8.7Additive Manufacturing
Chair(s): Denquin, A, Gliszcynski, A.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
16. Sep 26 10:50 11:15 8.7.1 ELECTROMAGNETISM FOR SMART MANUFACTURING OF POLYMER COMPOSITES
S.H. Vattathurvalappil, King Fahd University of Petroleum and Minerals, Saudi Arabia
16. Sep 26 11:15 11:40 8.7.2 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
16. Sep 26 11:40 12:05 8.7.3 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
16. Sep 26 12:05 12:30 8.7.4 FLYING BY THE THREAD OF MY PANTS: USING HOUSEHOLD TEXTILES COMPOSITES FOR ACCESSIBLE UAV AIRFRAMES
C. Koutsambasis¹, M. Marino¹, N.J. Brown¹, W. Wu¹; ¹RMIT University, Australia
9.7Flutter
Chair(s): Tsushima, N., Candon, M.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
16. Sep 26 10:50 11:15 9.7.1 A FLUTTER VERIFICATION METHOD FOR ALL-MOVABLE CONTROL SURFACE CONSIDERING FREE-PLAY NONLINEARITY
W. 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 9.7.2 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 11:40 12:05 9.7.3 TIME-VARYING AEROELASTIC MODELING AND FLUTTER ANALYSIS OF TELESCOPIC WINGS
C.-Y. Li¹, S. He¹, Z.-C. Yang¹; ¹Northwestern Polytechnical University, China
additional information (interactive) 9.7.R FLUTTER ANALYSIS OF A DYNAMIC VARIABLE-SWEEP WING
Z.Y. Xi¹, Y.T. Dai¹, C. Yang¹; ¹Beihang University, China
additional information (interactive) 9.7.R MODELING AND ANALYSIS OF ACTIVE FLUTTER SUPPRESSION OF THE PREPOSITIVE ELLIPTICAL WING-MAIN WING COMPOSITE CONFIGURATION
C.Y. Zhao, China; B.G. Mi, China; X. Bai, China
10.7Propellers, Compressors and Turbines 1
Chair(s): Haselbach, F.
Track 10 C4.9
05 - Propulsion and Energy
16. Sep 26 10:50 11:15 10.7.1 CONCEPTUAL PERFORMANCE AND MASS ASSESSMENT OF AN OPEN FAN ENGINE FOR THE DLR-F25 AIRCRAFT
P. Wehrel¹, J. Häßy¹, R. Schnell¹, S. Wöhler¹; ¹German Aerospace Center (DLR)), Germany
16. Sep 26 11:15 11:40 10.7.2 SURROGATE-BASED OPTIMIZATION OF AIRCRAFT PROPELLER PERFORMANCE USING A HIGH-FIDELITY AND EFFICIENT RANS FRAMEWORK
A. Stuermer¹, M. Hepperle¹, P. Wegener¹; ¹DLR, Germany
16. Sep 26 11:40 12:05 10.7.3 FEASIBILITY OF ELECTRIC DUCTED FANS TO REPLACE OPEN PROPELLERS ON AN ELECTRIFIED TRAINING AIRCRAFT
G. Braggett¹, K.F. Joiner¹, A. Somerville¹, D. Hill, Altavia Aerospace, Australia; ¹University of New South Wales, Australia
Presenter: Georgia Braggett, University of New South Wales
16. Sep 26 12:05 12:30 10.7.4 FLIGHT-DATA-DRIVEN PHYSICS-INFORMED COMPONENT MAP DERIVATION WITH STRUCTURAL COMPLIANCE
Y. Liu¹, L. Gou¹, Y. Huang, Shenzhen Research Institute of Northwestern Polytechnical Univer, China; ¹School of Power and Energy, Northwestern Polytechnical Universit, China
additional information (interactive) 10.7.R STUDY ON OIL CAVITATION AND PUMPING CHARACTERISTICS OF SURFACE MICROTOPOGRAPHY GRAPHITE SEALS
Y.P. Li, China; J.P. Hu, China; G.L. Li, China; H.L. Zhao, China; S. Li, China
Presenter: Shu Li
11.7System Identification
Chair(s): Kim, S., Wan, T.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 26 10:50 11:15 11.7.1 SYSTEM IDENTIFICATION OF SMALL-SCALE HELICOPTER VIA EKF WITH DATA-DRIVEN NOISE COVARIANCE DETERMINATION
E.J. Kim¹, B. Seo¹, S.K. Kim¹, J.Y. Suk¹; ¹Chungnam National University, South Korea
16. Sep 26 11:15 11:40 11.7.2 ATTITUDE CONTROL TECHNIQUES FOR A MICRO-SCALE FLAP-BASED AERODYNAMIC DECELERATOR SYSTEM
J. Clarendon¹, T. Fields¹, J. Nguyen¹, A. Chance¹, O. Yakimenko, Naval Postgraduate School, United States; ¹University of Missouri-Kansas City, United States
16. Sep 26 11:40 12:05 11.7.3 GUST ERROR METHOD (GEM): PARAMETER IDENTIFICATION FOR AIRCRAFT SUBJECT TO VON KÁRMÁN PROCESS NOISE
J. Cox¹, K.C. Wong¹, G. Chamitoff, Texas A&M University College of Engineering, United States; ¹The University of Sydney, Australia
16. Sep 26 12:05 12:30 11.7.4 WIND FIELD PERCEPTION AND FEATURE PREDICTION FOR LOW-ALTITUDE SMALL FIXED-WING UAVS TOWARDS ENERGY HARVESTING
Y.L. He, China; X.P. Xu, China; Z. Zhou, China; S. Song, China
Presenter: Shiqi Song
Reserve Paper 11.7.R AFFINE-INVARIANT ELLIPTICAL STATE ESTIMATION FOR ROBUST EXTENDED OBJECT TRACKING
I.H. Lee, Korea Institute of Industrial Technology, South Korea
Presenter: inho lee
12.7CRM-HL 1
Chair(s): , , Imamura, T.
Track 12 C2.3
03.2 - Experimental Aerodynamics
16. Sep 26 10:50 11:15 12.7.1 ECOSYSTEM UPDATES AND PLANS
M. Rivers, NASA, United States
16. Sep 26 11:15 11:40 12.7.2 AERODYNAMIC CHARACTERISTICS OF 8% SCALE SEMI-SPAN HIGH-LIFT COMMON RESEARCH MODEL AT THE JAXA 6.5M X 5.5M LOW SPEED WIND TUNNEL
M. Kohzai¹, M. Murayama¹, A. Sansica¹, D. Lusher¹, T. Takaishi¹, H. Abe¹; ¹Japan Aerospace Exploration Agency, Japan
16. Sep 26 11:40 12:05 12.7.3 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
16. Sep 26 12:05 12:30 12.7.4 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
13.7Optimizing AAM Networks
Chair(s): Wickramasinghe, N.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
16. Sep 26 10:50 11:15 13.7.1 RECIPROCITY-GUIDED JOINT BASE STATION PLACEMENT AND FLIGHT CORRIDOR PLANNING FOR URBAN AIR MOBILITY
Y. He¹, Y. Wang¹, F. Wu¹, J. Guo¹, Z. Gao¹; ¹HKUST, Hong Kong SAR of China
16. Sep 26 11:15 11:40 13.7.2 SIMULATION-BASED EVALUATION OF SIGNALISED INTERSECTIONS FOR EMERGENCY SAFETY LANDINGS IN URBAN AIR MOBILITY
P. Sathya Kumar¹, M. Schultz¹, E. Asadi¹; ¹Universität der Bundeswehr München, Germany
16. Sep 26 11:40 12:05 13.7.3 SCHEDULING AND ROUTING FOR TIMETABLE-BOUND URBAN AIR MOBILITY OPERATIONS
A. Edsel¹, W.A. Crossley¹, D.A. DeLaurentis¹; ¹Purdue University, United States
16. Sep 26 12:05 12:30 13.7.4 ESTIMATION AND ANALYSIS OF RNP REQUIREMENTS FOR HETEROGENEOUS UAM CONFIGURATIONS: INSIGHTS FROM OPPAV DEMONSTRATION
J.S. Lee¹, K.R. Oh¹; ¹Korea Aerospace Research Institute, South Korea
additional information (interactive) 13.7.R OPTIMISATION OF OPERATING RADII FOR DRONE WAREHOUSES
A. Tiwari¹, R.S. Pant¹; ¹Indian Institute of Technology Bombay, India
14.7Multidisciplinary Advances in Aerodynamics, Aeroacoustics, and Aeroelasticity (by IFAR)
Chair(s): Schuchardt, B.
Track 14 C2.5
15 - Guest lectures
16. Sep 26 10:50 11:15 14.7.1 AERODYNAMIC AND AEROACOUSTIC ASSESSMENT OF 3D PRINTED AAM PROPELLER BLADES WITH SURFACE TREATMENTS
D. Skrna¹, M. de Rosa Jacinto¹, L. Frei¹, B. Mittenecker¹, J. Nagl¹, H. Mad¹, M. Berens¹; ¹Technische Universität Wien, Austria
16. Sep 26 11:15 11:40 14.7.2 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 11:40 12:05 14.7.3 UNDERSTANDING HYPERSONIC BOUNDARY LAYER LAMINAR TO TURBULENT TRANSITION IN WIND TUNNEL ENVIRONMENT
M. Lugrin, ONERA, France
Presenter: Mathieu Lugrin, ONERA
16. Sep 26 12:05 12:30 14.7.4 PANEL DISCUSSION AND Q&A
1 Q,
15.7Education Enablers
Chair(s): Corsi, M.
Track 15 C2.6
14 - Education and Training
16. Sep 26 10:50 11:15 15.7.1 PREPARING AERONAUTICAL ENGINEERING UNDERGRADUATES FOR WORKING IN GLOBAL TEAMS
J. Abulawi, HAW Hamburg, Germany; P. Raj, Virginia Tech, United States
16. Sep 26 11:15 11:40 15.7.2 REFLECTIONS ON THE AEROSPACE ENGINEERING DEVELOPMENT PROGRAMME AT THE CSIR
K. Ramotsabi¹, L. Strydom¹, L. Zwane¹; ¹CSIR, South Africa
16. Sep 26 11:40 12:05 15.7.3 AN INDIVIDUALISED, SCALABLE PROJECT-BASED LEARNING FRAMEWORK FOR STRUCTURE DESIGN COURSES ESTABLISHED IN A LARGE AEROSPACE STUDY PROGRAMME
N. Moser¹, N. Singer¹, V. N. Mueller¹, T. Siemer¹, F. Daoud¹; ¹TU Munich, Germany
Presenter: Valentin Müller
16. Sep 26 12:05 12:30 15.7.4 AN MBSE-ORIENTED FRAMEWORK FOR AEROSPACE SYSTEMS EDUCATION: THE CEA-UFMG LIGHT-AIRCRAFT DESIGN-BUILD-TEST TRADITION
L.H.J. Machado¹, J.L.C. Reis¹, M. Lott², R. Carlana²; ¹Universidade Federal de Minas Gerais, Brazil ;²Boeing, Brazil
additional information (interactive) 15.7.R INTERACTIVE NOTEBOOKS TO BRIDGE THE DIDACTIC GAP BETWEEN CALCULUS AND FLIGHT PERFORMANCE OPTIMIZATION
C. Varriale¹, F. Angioni¹; ¹Delft University of Technology, Netherlands

12:30 - 13:30LUNCH BREAK

0.8GENERAL LECTURE 4 Aeronautics Outlook - Directors Cut (Michael Edwards, Boeing, Veronique Roca, Airbus, Dimitri Mavris, Georgia Tech, Alan Newby, Rolls-Royce, Per Olof Marklund, SAAB. Markus Fischer, DLR
Chair: S.Bagassi/A.Krein ICAS EC Members
16. Sep 26 13:30 15:15

15:15 - 15:40AFTERNOON BREAK

1.8ECSC Pitch Session (10 Minute Talks with Q&A afterwards)
Chair(s): Citron, T.
Track 1 Pyrmont Theatre
15 - Guest lectures
16. Sep 26 15:40 16:05 1.8.1 DETECTION OF SURFACE DISCONTINUITIES IN ADDITIVELY MANUFACTURED ALSI10MG USING THERMOELASTIC STRESS ANALYSIS (PITCH SESSION)
J. Rodrigues, RMIT, Australia
16. Sep 26 16:05 16:30 1.8.2 AN OPTIMAL POWER MANAGEMENT POLICY FOR HYDROGEN BASED HYBRID AERO ENGINES (PITCH SESSION)
P. Faezeh, Eindhoven University of Technology, Netherlands
16. Sep 26 16:30 16:55 1.8.3 ONBOARD MISSION MANAGEMENT FOR A DECENTRALIZED MULTI-UAV SYSTEM USING BEHAVIOR TREES (PITCH SESSION)
K. Thomessen, DLR, Germany
16. Sep 26 16:55 17:20 1.8.4 NONLINEAR FRICTION MODELING OF HELIX SWING HYDRAULIC CYLINDERS FOR MORPHING AIRCRAFT USING PHYSICS-INFORMED NEURAL NETWORKS (PITCH SESSION)
S. Chen, Beihang University, China
Reserve Paper 1.8.R SENSITIVITY STUDY OF DEPARTURE TIME ACCURACY FOR AIRPORT COLLABORATIVE DECISION MAKING USING FAST-TIME SIMULATION (PITCH SESSION)
Y. Iwatsuki, Mitsubishi Research Institute, Inc., Japan
2.8Shaping Aviation for Society ETF with Introduction and Panel Discussion at the End
Chair(s): Holmberg, G., Collier, F.
Track 2 C4.1
15 - Guest lectures
16. Sep 26 15:40 16:05 2.8.1 THE COLLABORATIVE NATURE OF AVIATION INDUSTRY
B. Stoufflet, France
16. Sep 26 16:05 16:30 2.8.2 PRACTICAL INNOVATION IN AEROSPACE
William Dean Donovan, DiamondStream Partners, United States
16. Sep 26 16:30 16:55 2.8.3 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 2.8.4 A MULTI-FUEL PROPULSION SYSTEM STRATEGY FOR AVIATION TRANSPORT RESILIENCE
A. Murphy, United States
3.8Case Studies 2
Chair(s): Gibson, T.
Track 3 C4.2
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
16. Sep 26 15:40 16:05 3.8.1 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 16:05 16:30 3.8.2 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 16:30 16:55 3.8.3 STUDY ON INDUCED DRAG CALCULATION FOR BIRD-LIKE WINGTIP SLOTS USING WAKE-PLANE INTEGRATION
X. Liu, China; T. Yu, China; B. Song, China; D. Xue, China
16. Sep 26 16:55 17:20 3.8.4 MULTIDISCIPLINARY DESIGN OF COMPLIANT DEFORMABLE WINGS FOR IMPROVED AIRCRAFT EFFICIENCY: INTRODUCING AN ARCHITECTURE-AWARE OPTIMIZATION STRATEGY
B. Blaxall¹, F. Di Fiore¹, D. Venetsanos¹, L. Mainini¹; ¹Imperial College London, United Kingdom
4.8Unconventional Configurations - 2
Chair(s): Melkert, J.
Track 4 C4.3
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
16. Sep 26 15:40 16:05 4.8.1 MODELING & PRELIMINARY ANALYSIS OF AN ECOFRIENDLY AIRBORNE GLOBAL LUXURY EKRANOPLAN
M. Sankrithi, RIC Enterprises, United States; D. Mavris¹, R. Sundar¹; ¹Georgia Institute of Technology, United States
16. Sep 26 16:05 16:30 4.8.2 LIFT-AND-CRUISE EVTOL BOX-WING CONFIGURATION FOR THE LOW ALTITUDE ECONOMY
A. Frediani¹, E. Rizzo¹, G. Palaia, Politecnico di Torino, Italy; K. Abu Salem, University of Trento, Italy; M. Martini¹; ¹SkyBox Engineering, Italy
16. Sep 26 16:30 16:55 4.8.3 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
16. Sep 26 16:55 17:20 4.8.4 EFFECTS OF LIFT DISTRIBUTION AND WING POSTURE ON THE STABILITY AND CONTROL OF TAILLESS AIRCRAFT
M.R. de Kock¹, B.B. Huyssen¹, R.J. Huyssen, Council for Scientific and Industrial Research, South Africa; ¹University of Pretoria, South Africa
Presenter: Barbara Huyssen, University of Pretoria
5.8Aerodynamic Optimization
Chair(s): , , Zingg, D.
Track 5 C4.4
03.1 - Aerodynamics – CFD Methods and Validation
16. Sep 26 15:40 16:05 5.8.1 HIGH-FIDELITY AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINES USING A DISCRETE ADJOINT APPROACH
L. Rodrigues Arnaud¹, F. Maia Nunes Celestino¹, G.L. Olichevis Halila¹, J.L. F. Azevedo, Instituto Tecnológico de Aeronáutica, Brazil; ¹Pontifícia Universidade Católica do Paraná, Brazil
16. Sep 26 16:05 16:30 5.8.2 CONTINUOUS UNSTEADY ADJOINT VARIATIONAL MULTISCALE METHOD FOR AIRFOILS SHAPE OPTIMIZATION
C. Brunelli¹, M. Avirovic¹, B. Janssens¹, B.G. Marinus¹; ¹Royal Military Academy, Belgium
16. Sep 26 16:30 16:55 5.8.3 SIMULATION OF AERODYNAMIC GROUND EFFECT FOR TILTED PROPELLERS USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S. 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 5.8.4 A MACHINE-LEARNING-DRIVEN AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK USING FREE-FORM DEFORMATION AND DEEP NEURAL NETWORKS
G. 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
additional information (interactive) 5.8.R LEAKAGE PREDICTION AND GEOMETRIC PARAMETER OPTIMIZATION OF STEPPED LABYRINTH SEALS BASED ON DATA-DRIVEN SURROGATE MODELS
X. Li¹, L. Yang¹, Y. Wei¹; ¹Beijing Jiaotong University, China
6.8Certification by Analysis - Accelerating Momentum and Impact
Chair(s): Slotnick, J., van Dam, C.P.
Track 6 C4.5
15 - Guest lectures
16. Sep 26 15:40 16:05 6.8.1 PANEL DISCUSSION WITH J. SLOTNICK, B.APONSO, D.PETERSON, T.ISHIDA, H.SCKLICKENMAIER (DURATION 100 MINUTES)
J. Slotnick, United States
7.8Aerodynamics of Unconventional Aircraft Configurations
Chair(s): Jagadeesh, C.
Track 7 C4.6
03.4 - Applied Aerodynamics
16. Sep 26 15:40 16:05 7.8.1 AERODYNAMIC OPTIMIZATION DESIGN OF FULL-WING SOLAR-POWERED UAV FOR FLOW SEPARATION CONTROL
J. Wang¹, Z. Zhou¹, K. Wang¹, M. Li¹; ¹Northwestern Polytechnical University, China
16. Sep 26 16:05 16:30 7.8.2 STATIC GROUND EFFECT OF HIGH-ASPECT-RATIO WINGS
C. Zheng¹, Q. Qu¹, P. Liu¹, T. Hu¹; ¹Beihang University, China
16. Sep 26 16:30 16:55 7.8.3 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 7.8.4 AERODYNAMIC FEASIBILITY OF A NOVEL SWIVEL ROTOR ARCHITECTURE
B.I. Soemarwoto, Royal Netherlands Aerospace Centre NLR, Netherlands
Reserve Paper 7.8.R DEVELOPMENT OF HYDROPHILIC COATINGS FOR PRACTICAL APPLICATION OF LAMINAR FLOW WINGS
H. Iijima¹, Y. Iijima¹, N. Tokugawa¹; ¹JAXA, Japan
additional information (interactive) 7.8.R FLUTTER FEATURES AND AERODYNAMIC DAMPING CALCULATION METHODS FOR PLATE-HEAT EXCHANGERS IN HIGH-SPEED TURBINE ENGINES
K. Qiao, China; D. Wei, China; L. Han, China; Z. Chen, China; Z. Yan, China; Y. Qin, China; G. Xu, China; H. Tang, China
additional information (interactive) 7.8.R UNCONTROLLED TAILLESS GLIDING: PAPER AEROPLANES GEOMETRY, AERODYNAMICS AND FLIGHT DURATION ANALYSIS
J. Guo¹, Y. Sun¹; ¹Cranfield University, United Kingdom
8.8Structural Optimization
Chair(s): Gliszcynski, A.
Track 8 C4.7
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
16. Sep 26 15:40 16:05 8.8.1 HIERARCHICAL HIGH-ORDER BEAM MODELS FOR OPTIMISATION-ORIENTED ANALYSIS OF COMPOSITE WING-LIKE STRUCTURES
D. Cardone¹, R. Cavallaro, Barcelona Supercomputing Center, Spain; A. Cini¹; ¹Universidad Carlos III de Madrid, Spain
16. Sep 26 16:05 16:30 8.8.2 DESIGN ASSESSMENT OF A HELICOPTER BLADE
C. Pagwiwoko¹, K. Warnakula¹, M. Silla¹, C. Barber¹, T. Hallwright¹, O. Kaleagasi¹, D. Schoemaker, Gyro Technic Inc., United States; ¹SYOS Aerospace, New Zealand
Presenter: Cosmas Pagwiwoko, SYOS Aerospace
16. Sep 26 16:30 16:55 8.8.3 ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS
G.C. Cristea¹, M. Pop¹, A. Stefan¹, M. Botan¹, A. Dragomirescu¹; ¹INCAS, Romania
16. Sep 26 16:55 17:20 8.8.4 OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR UAVS
C.D. Scott¹, A.M. Comer¹, J.C. Hanan¹, A. Nunley¹; ¹Oklahoma State University, United States
9.8Aeroelastic Analysis & Design 1
Chair(s): Han, J., Muscarello, V.
Track 9 C4.8
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
16. Sep 26 15:40 16:05 9.8.1 AEROELASTIC TAILORING FOR COMPOSITE ADAPTIVE WINGLETS
N. Tsushima, Kyushu University, Japan; R. Higuchi¹, T. Yokozeki¹; ¹The University of Tokyo, Japan
16. Sep 26 16:05 16:30 9.8.2 PARAMETRIC AEROELASTIC STUDY OF WINGLET GEOMETRY USING VORTEX LATTICE METHOD FOR FUTURE PASSIVE MORPHING APPLICATIONS
M. Kouchlef¹, N. Tsushima¹, T. Yokozeki¹; ¹The University of Tokyo, Japan
16. Sep 26 16:30 16:55 9.8.3 AEROELASTIC DESIGN OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT IN AN MDO FRAMEWORK
C. Mollet¹, L. Vertonghen¹, C. Julien¹; ¹ONERA, France
16. Sep 26 16:55 17:20 9.8.4 MANEUVER LOAD ALLEVIATION OF THE DRY WING FOR HYDROGEN AIRCRAFT
F. Yu¹, M. Hornung¹; ¹Technical University of Munich, Germany
10.8Propellers, Compressors and Turbines 2
Chair(s): Haselbach, F
Track 10 C4.9
05 - Propulsion and Energy
16. Sep 26 15:40 16:05 10.8.1 MODULAR JET AND PROPELLER ENGINE – PART I: INITIAL STUDIES
T. Otten¹, T. Matuschek¹, J. Häßy¹, J. Frank¹, R.G. Brakmann¹; ¹German Aerospace Center (DLR), Germany
16. Sep 26 16:05 16:30 10.8.2 MODULAR JET AND PROPELLER ENGINE – PART II: INTEGRATED DESIGN PROCESS AND DESIGN SPACE ASSESSMENT
T. Matuschek¹, T. Otten¹, J. Häßy¹, R. Brakmann¹, J. Frank¹, P. Wehrel¹; ¹German Aerospace Center (DLR), Germany
16. Sep 26 16:30 16:55 10.8.3 INVESTIGATION OF GENERIC SWIRL DISTORTION AND ITS EFFECTS ON COMPRESSOR PERFORMANCE AND FLOW STABILITY
L. 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 10.8.4 INITIAL GEOMETRIC UNCERTAINTY ASSESSMENT IN COMPRESSOR AIRFOILS USING PHYSICS-BASED DIRECT MANIPULATED FFD
K. Omoto¹, D. Sasaki¹, K. Matsui², M. Yamagami²; ¹Osaka Metropolitan University, Japan ;²IHI Corporation, Japan
11.8Guidance and Flight Trajectory Control 2
Chair(s): Drupka, G., Rohacs, D.
Track 11 C4.10
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 26 15:40 16:05 11.8.1 TRAJECTORY OPTIMIZATION OF HIT-TO-KILL INTERCEPTORS VIA SEQUENTIAL CONVEX PROGRAMMING APPROACH
S.-J. Im¹, C.-H. Lee¹, J.-H. Jin, Sunchon National University, South Korea; H.-C. Bang¹; ¹Korea Advanced Institute of Science and Technology, South Korea
16. Sep 26 16:05 16:30 11.8.2 DUAL BEZIER SPACE-TIME OPTIMIZATION UNDER HARD OBSERVATION-WINDOW CONSTRAINTS: A FEASIBILITY-ORIENTED JERK-CAP COMPARISON
H. Kim¹, S. Lee¹; ¹Kookmin University, South Korea
16. Sep 26 16:30 16:55 11.8.3 OFFLINE REINFORCEMENT LEARNING FOR INFRARED IMAGE-BASED MISSILE GUIDANCE AND CONTROL
S. Kim¹, J. Shin¹, H.-G. Kim, Konkuk University, South Korea; ¹Chungbuk National University, South Korea
12.8Robot Manufacturing and Assembly Technology
Chair(s): Guevara, E., Zhang, H.
Track 12 C2.3
08 - Manufacturing and Supply Chain Management
16. Sep 26 15:40 16:05 12.8.1 GAP OPTIMIZATION ADAPTIVE TOOL FOR LARGE SCALE FLEXIBLE STRUCTURE ASSEMBLY
M. Tatar¹, L. Branko¹, R.W. Grube¹, R. Noll¹, G.M. Buckus¹, O. Wagner¹; ¹Boeing, United States
16. Sep 26 16:05 16:30 12.8.2 EVALUATION OF TRUST AS A HUMAN FACTOR IN COLLABORATIVE ROBOTICS ASSOCIATED WITH ARTIFICIAL INTELLIGENCE APPLIED TO THE AERONATUCAL INDUSTRY
I. Ali¹, C. Silva², E. Villani², J.M. Mello¹, W. Oliveira²; ¹Embraer, Brazil ;²ITA, Brazil
16. Sep 26 16:30 16:55 12.8.3 VIRTUAL COMMISSIONING APPLIED TO ROS AIRCRAFT ROBOTIC CELL
A.T. Ferraz¹, C.C.D. Silva¹, J.M.G. Mello, EMBRAER, Brazil; E. Villani¹; ¹ITA, Brazil
Presenter: Emilia Villani, ITA
16. Sep 26 16:55 17:20 12.8.4 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
13.8Strategic Planning for AAM
Chair(s): Enea, G.
Track 13 C2.4
09 - Crewed and Uncrewed Aircraft Operations and Traffic Management
16. Sep 26 15:40 16:05 13.8.1 VERTIPORT FINAL APPROACH AND TAKEOFF AREA ORIENTATION IDENTIFICATION USING COUPLED MICROSCALE WIND AND FLIGHT DYNAMICS ANALYSIS
D.S. Nithya¹, F. Monteleone¹, V. Muscarello, RMIT University, Australia; G. Quaranta¹; ¹Politecnico di Milano, Italy
16. Sep 26 16:05 16:30 13.8.2 LOW-NOISE VERTIPORT PROCEDURE PLANNING USING 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 13.8.3 IMPACT OF BOOKING LEAD TIME ON FLEET AND INFRASTRUCTURE IN URBAN AIR MOBILITY
M. Swaid, German Aerospace Center (DLR), Germany
16. Sep 26 16:55 17:20 13.8.4 ADVANCING TRAFFIC MANAGEMENT SERVICES FOR VERTIPORT OPERATIONS IN EUROPE: INSIGHTS FROM THE EUREKA PROJECT
M. Corsi, 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) 13.8.R A BIONIC-INSPIRED COLLABORATIVE SYSTEM FOR MANNED AND UNMANNED AERIAL VEHICLES IN EMERGENCY RESCUE MISSIONS
M. Xu¹, L. Wang, School of Reliability and Systems Engineering, Beihang universi, China; T. Ma¹, X. Wang, School of Reliability and Systems Engineering, Beihang universit, China; J. Fu¹; ¹Institute of Unmanned System, Beihang University, China
14.8Emerging Technologies for Future Air Operations (by IFAR)
Chair(s): Kramar, V., Kopardakar, P.
Track 14 C2.5
15 - Guest lectures
16. Sep 26 15:40 16:05 14.8.1 ADVANCED AIR MOBILITY: THE CURRENT STATE OF DEVELOPMENT AND THE CHALLENGES
V. Kramar, VTT Technical Research Centre of Finland (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.H. 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 14.8.2 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 14.8.3 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
Presenter: Petter Krus, Linköping University
16. Sep 26 16:55 17:20 14.8.4 A SEMI-AUTONOMOUS DECISION SUPPORT TOOL FOR ATC IN EN-ROUTE REROUTING OPERATIONS
R. Fernandes Viana¹, C. Rutili de Lima¹, V. Abrão S. Marques, Federal University of Triângulo Mineiro, Brazil; M. Condé Rocha Murça¹, M. R. O. A. Maximo¹, Q.F. Carlos Henrique¹; ¹Aeronautics Institute of Technology, Brazil
Presenter: Vinicius Abrão da Silva Marques, Federal University Of Triângulo Mineiro
15.8Condition Based Maintenance
Chair(s): Koschlik, A.K., Scott, M.
Track 15 C2.6
11 - Operations and Sustainment
16. Sep 26 15:40 16:05 15.8.1 EXPLAINABLE NATURAL LANGUAGE PROCESSING FOR AIRCRAFT STRUCTURAL INTEGRITY DEFECT CLASSIFICATION
V. Kekoc, Defence Science and Technology Group, Australia; M. Scott¹, W.J.C. Verhagen¹, P. Marzocca¹; ¹RMIT University, Australia
16. Sep 26 16:05 16:30 15.8.2 AI-BASED MAINTENANCE CODE CORRECTION FOR RELIABLE MTBF ANALYSIS
M. Kim¹, S.-H. Jeong¹, I. Lee¹, B. Shim¹; ¹Korea Aerospace Industries, LTD, South Korea
16. Sep 26 16:30 16:55 15.8.3 PHYSICS-INFORMED NEURAL NETWORKS FOR ULTRASONIC LAMB WAVE RECONSTRUCTION IN NON-DESTRUCTIVE TESTING
L. 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 15.8.4 DATA-DRIVEN TECHNOLOGY INTELLIGENCE: AN APPLICATION TO AIRCRAFT ENGINE MAINTENANCE
A. Dadashi, DLR, Germany
additional information (interactive) 15.8.R REBUILDING AGRICULTURAL STATISTICS IN POST-WAR SUDAN: A STRATEGIC FRAMEWORK FOR RECOVERY AND RESILIENCE
N. Ahmed, Sudan
additional information (interactive) 15.8.R PARAMETER INVERSION ALGORITHM FOR AERO-ENGINE ? -PHOTON FLOW FIELD IMAGES BASED ON UNET-GAN ARCHITECTURE
L.Y. Hou¹, J.T. Liu¹, Y.L. Song¹, H. Xiao¹; ¹Nanjing University of Aeronautics and Astronautics, China

0.9SPEED MENTORING
Chair: The Speed Mentoring initiative aims to create meaningful interactions between students, early-career researchers, and experienced professionals from academia, industry, and government sectors through structured discussions and networking opportunities
16. Sep 26 17:20 19:00