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

Tuesday, 15. Sep 2026

0.3ICAS 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 IFAR 2025 PERSPECTIVES ON NOISE REDUCTION FOR EMERGING AND CONVENTIONAL AIR TRANSPORT
K. Benameur, ONERA, France
15. Sep 26 09:20 09:45 1.4.2 CHALLENGES IN ADVANCED AIR MOBILITY NOISE PREDICTION - FROM SOURCE TO PERCEPTION
B.I. Schuchard, German Aerospace Center (DLR, Germany
15. Sep 26 09:45 10:10 1.4.3 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 RECENT ADVANCES IN AEROACOUSTIC DESIGN OF ADVANCED AIR MOBILITY VEHICLES
AS Sieradzki, ?ukasiewicz - Institute of Aviation, Poland
Presenter: Witold Klimczyk, Lukasiewicz Research Network - Institute of Aviation
2.4Aircraft Electrification, Innovation & Certification Perspectives & Challenges
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
3.4Propulsion 1
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 08:55 09:20 3.4.1 IMPACT OF SERIAL-PARALLEL POWERTRAIN SIZING STRATEGIES ON HYBRID-ELECTRIC AIRCRAFT PERFORMANCE
G. Palaia, Polytechnic of Turin, Italy
15. Sep 26 09:20 09:45 3.4.2 IMPLEMNTATION OF PROPELLER-WING INTERFERENCE MODEL AND HORIZONTAL TAIL ANALYSIS INTO A VISCOUS FULL POTENTIAL FLOW SOLVER FRAMEWORK FOR AIRCRAFT DESIG
D.D.P. Di Pasquale, Cranfield University, United Kingdom
15. Sep 26 09:45 10:10 3.4.3 IMPACT OF DIFFERENT PROPELLER CONFIGURATIONS ON THE FLIGHT DYNAMICS AND STABILITY OF A SMALL REGIONAL ELECTRIC AIRCRAFT
A. H Hammad, Germany
15. Sep 26 10:10 10:35 3.4.4 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
Reserve Paper 3.4.R RESONANT ELASTIC SHAFT THRUST VECTORING: IMPLICATIONS FOR UAV DESIGNS
HF.G. Guan, Australia
4.4Hydrogen in design
Chair(s): Verstraete, D.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 08:55 09:20 4.4.1 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 CHALLENGES AND SOLUTIONS FOR LIQUID HYDROGEN-POWERED UAVS: REGULATIONS AND CASE STUDY INSIGHTS
B. Legrand, ISAE-SUPAERO, France
15. Sep 26 09:45 10:10 4.4.3 ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035
M. Kotzem, German Aerospace Center (DLR), Germany
15. Sep 26 10:10 10:35 4.4.4 AN INTEGRATED SYSTEM-LEVEL AND MULTIPHYSICS APPROACH FOR AIRCRAFT LH2 FUEL SYSTEM DESIGN
A. Tramposch, University of Applied Sciences FH JOANNEUM GesmbH, Austria
5.4Supersonic and Hypersonic Flows
Chair(s): Pezzella, G., Kiszkowiak, L.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 08:55 09:20 5.4.1 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 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 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 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 NUMERICAL INVESTIGATION OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH 2.5 OVER A COMPRESSION RAMP
Z.A. Rana, Prince Mohammad bin Fahd University, Saudi Arabia
6.4Rotor aerodynamics and acoustics
Chair(s): Azarpeyvand, M., Gowree, E.
Track 6
03.2 - Experimental Aerodynamics
15. Sep 26 08:55 09:20 6.4.1 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 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 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 MISSION-WIDE SEMI-EMPIRICAL AEROACOUSTIC NOISE MODELING OF A CARGO EVTOL UAV WITH CONSIDERATION OF A SIMPLE URBAN FLYOVER
I. Peleshok, Technical University of Munich, Germany
7.4Boundary Layer Control and Stall Mitigation
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 26 08:55 09:20 7.4.1 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 INFLUENCE OF ZIGZAG TAPE–INDUCED TRANSITION ON THE DU89-134 AIRFOIL PERFOMANCE AT LOW REYNOLDS NUMBER
M. Avirovic, Royal Military Academy, Belgium
15. Sep 26 09:45 10:10 7.4.3 EXERGY AND INTEGRAL BOUNDARY LAYER PARAMETERS CHARACTERISTIC CURVES FOR AERODYNAMIC DESIGN
G. Bourreau-Tirel, AURA AERO/ISAE-SUPAERO, France
15. Sep 26 10:10 10:35 7.4.4 PARAMETRIC AERODYNAMIC STUDY OF LEADING-EDGE SERRATIONS ON WING SECTIONS ACROSS REYNOLDS NUMBERS
J.J Whittaker, Australia
additional information (interactive) 7.4.R 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 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 COMPOSITE PLATE OPTIMIZATION UNDER COMBINED COMPRESSION AND SHEAR BUCKLING LOAD
R.P Pereira da Silva, Boeing, Brazil
15. Sep 26 09:45 10:10 8.4.3 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 10:10 10:35 8.4.4 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 ENERGY ABSORPTION OF THIN-WALLED CONCENTRIC SPHERES FOR CARGO AIRDROP
A.E. Lloyd, The University of Sydney, Australia
15. Sep 26 09:20 09:45 9.4.2 GROUND VIBRATION TEST ANALYSIS OF A PC-9 AIRCRAFT USING DELAY-EMBEDDED DYNAMIC MODE DECOMPOSITION WITH CONTROL
A. Das, RMIT University, Australia
15. Sep 26 09:45 10:10 9.4.3 NUMERICAL PREDICTION OF CABIN NOISE FOR FUTURE SHORT-HAUL AIRCRAFT IN EARLY AIRCRAFT DESIGN
C. Hesse, DLR e.V., Germany
15. Sep 26 10:10 10:35 9.4.4 DATA-DRIVEN MULTI-MODAL PREDICTION OF IMPACT RESPONSE IN COMPOSITE LAMINATES: FORCE–TIME HISTORIES AND INTERLAMINAR DELAMINATION
G.J.-Zh Zhang, China
10.4Advanced vehicle concepts
Chair(s): ,
Track 10
05 - Propulsion and Energy
15. Sep 26 08:55 09:20 10.4.1 ASSESSMENT OF ENGINE-OUT ATMOSPHERIC EMISSIONS FROM COCONUT-OIL-DERIVED BIOJET FUEL
S. Ogawa, Osaka Metropolitan University, Japan
15. Sep 26 09:20 09:45 10.4.2 MAGNETOPLASMAIONIC (MPI) ENGINE
N. K. Chaudhary, Australia
15. Sep 26 09:45 10:10 10.4.3 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 SYSTEM-LEVEL MODELLING OF TURBOFAN NOISE SUPPRESSION AND ACOUSTIC LINER ATTENUATION
X Zhao, Chalmers University of Technology, Sweden
Reserve Paper 10.4.R EVALUATION OF LIQUID HYDROGEN CONDITIONING CONCEPTS FOR AIRCRAFT ENGINES EMPLOYING EXHAUST GAS WASTE HEAT RECOVERY
P. Kirschnek, FH JOANNEUM GesmbH, Austria
11.4Guidance and flight trajectory control 1
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 08:55 09:20 11.4.1 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 SENSITIVITY-BASED REFERENCE TRAJECTORY UPDATES FOR AIRCRAFT PATH-FOLLOWING MODEL PREDICTIVE CONTROL
S. Fuchsgruber, Technische Universität München, Germany
15. Sep 26 09:45 10:10 11.4.3 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 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 CONVEX OPTIMIZATION-BASED EMERGENCY LANDING TRAJECTORY GENERATION FOR UAM VEHICLES
Y. Jung, Korea Aerospace Research Institute, South Korea
12.4Concent design/MBSE
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
15. Sep 26 08:55 09:20 12.4.1 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 WEATHER, AVIATION, AND CLIMATE: CURRENT TOPICS IN AIRBORNE RESEARCH
Z. R. Milani, National Research Council of Canada, Canada
15. Sep 26 09:45 10:10 12.4.3 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 AUTOMATING SYSTEM MODELING USING LARGE LANGUAGE MODELS
I. S. Rehder, Brazil
Reserve Paper 12.4.R A RELIABLE AND COST-EFFICIENT DATA ACQUISITION SYSTEM FOR MIL-1763 STATIC EJECTION TESTING OF AIRCRAFT EXTERNAL STORES
N.-V. Nguyen, Viettel Aerospace, Vietnam
additional information (interactive) 12.4.R 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 VALUE DRIVEN CO-ARCHTIECTING AND TRADESPACE EXPLORATION: AN AERONAUTICAL CASE STUDY INVOLVING INDUSTRIAL SYSTEMS
G. Donelli, German Aerospace Center DLR, Germany
15. Sep 26 09:20 09:45 13.4.2 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 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 AIRCRAFT AND INDUSTRIAL SYSTEMS CO-ARCHITECTING BASED ON VALUE-DRIVEN MBPLE APPROACH
G. Donelli, German Aerospace Center DLR, Germany
14.4UAV Design
Chair(s): , , Bil, C.
Track 14
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 26 08:55 09:20 14.4.1 DISCRIMINATORY AUTONOMY: OPERATING FASTER, SMARTER, AND WITH PURPOSE
J. Garth, Australia
15. Sep 26 09:20 09:45 14.4.2 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 SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION
B. Kunwar, Auburn University, United States
15. Sep 26 10:10 10:35 14.4.4 A WORKFLOW FOR RAPID DESIGN, SIMULATION, FABRICATION, AND SUBSCALE FLIGHT-TESTING OF NOVEL AIRCRAFT CONCEPTS
I Chakraborty, Auburn University, United States
Reserve Paper 14.4.R 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 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 EVALUATION OF THE USE OF THE EYE TRACKER IN AERONAUTICAL PRODUCT DEVELOPMENT AS A HUMAN FACTORS METHOD
G. Cicelini, Brazil
15. Sep 26 09:45 10:10 15.4.3 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 10:10 10:35 15.4.4 SUBSCALE FLIGHT TRAINING EFFECTS ON PILOT WORKLOAD AND PERFORMANCE DURING VTOL HQTES
A.M. Comer, Oklahoma State University, United States

10:35 - 11:00COFFEE BREAK

1.5GSA2: Perspectives and Progress on Airliners for 2050+ Energy Landscapes
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
15. Sep 26 11:00 11:25 1.5.1 ECONOMIC, ENVIRONMENTALLY SUSTAINABLE AVIATION ENERGY
J.I. Hileman, Boeing, United States
15. Sep 26 11:25 11:50 1.5.2 AIRBUS\' PERSPECTIVES & PROGRESS ON AIRLINERS FOR 2050+ ENERGY LANDSCAPES
F Haselbach, Airbus, France
15. Sep 26 11:50 12:15 1.5.3 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 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 (by personal invitation only)
15. Sep 26 11:00 11:25 2.5.1 AI-ASSISTED DESIGN OF HOLISTICALLY SUSTAINABLE AEROSTRUCTURES
A. Filippatos, University of Patras, Greece
15. Sep 26 11:25 11:50 2.5.2 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 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 OVERVIEW OF CRITICAL ISSUES AND OPPORTUNITIES FOR NEW A/C WITH HYBRID AND FULL-ELECTRIC POWERTRAIN
F. Nicolosi, University of Naples Federico II, Italy
3.5Propulsion 2
Chair(s): ,
Track 3
01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
15. Sep 26 11:00 11:25 3.5.1 A HYBRID 0D–2D WHOLE-ENGINE MATCHING FRAMEWORK FOR TURBOJET ENGINE PERFORMANCE SIMULATION
Q.-H.-T.-X. Hoang Thi Xuan, Viettel Aerospace Institute, Vietnam
15. Sep 26 11:25 11:50 3.5.2 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 MIXED-FIDELITY, NONLINEAR AIRCRAFT MISSION MODELING FOR HYBRID REGIONAL AIRCRAFT DESIGN VERIFICATION
Agostino: A. De Marco, University of Naples Federico II, Italy
15. Sep 26 12:15 12:40 3.5.4 EFFECT OF ENGINE RESPONSE TIME IN AIRCRAFT CONCEPTUAL DESIGN
A.P.S. Inderawan, Delft University of Technology, Netherlands
4.5Application of advanced propulsion concepts
Chair(s): Ying, A.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 11:00 11:25 4.5.1 INTEGRATION OF A SOLID OXIDE FUEL CELL PROPULSION SYSTEM: A TECHNOLOGY DEVELOPMENT GOAL FOR REGIONAL AIRCRAFT
N. Schneiders, German Aerospace Center (DLR), Germany
15. Sep 26 11:25 11:50 4.5.2 HYBRID-ELECTRIC AND HYDROGEN-FUEL-CELL PROPULSION AS ALTERNATIVES TO KEROSENE FOR REGIONAL AIRCRAFT
F. Nicolosi, UNIVERSITY OF NAPLES , Italy
15. Sep 26 11:50 12:15 4.5.3 EXPLORATION OF ALTERNATIVE PROPULSION ARCHITECTURES FOR BUSINESS AVIATION
M. Bouchard¹, M. Bashir², D. Rancourt¹, S. Liscouët-Hanke², F. Sirois, Polytechnique Montréal, Canada; A. Tfaily³, M. Mark³, R. Freer, Pratt & Whitney Canada, Canada; J. Moriot, Calogy Solutions, Canada; S. Lloyd²; 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 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 PROPULSION SYSTEM MODELING AND OPTIMIZATION FOR CONCEPTUAL DESIGN OF HYBRID-ELECTRIC VTOL AIRCRAFT
D. E. Lampl, Technical University of Munich, Germany
Reserve Paper 4.5.R PRELIMINARY SIZING METHODOLOGY FOR HYBRID-ELECTRIC PROPULSION SYSTEM IN CARGO AIRSHIPS
S. Trivedi, Indian Institute Technology Bombay, Mumbai, India, India
5.5CFD Applications
Chair(s): Marzocca, P., Imamura, T.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 11:00 11:25 5.5.1 NUMERICAL REBUILDING OF AERODYNAMIC WIND TUNNEL ANALYSES OF A CREW RETURN VEHICLE
N. Montella, CIRA (Centro Italiano Ricerche Aerospaziali), Italy
15. Sep 26 11:25 11:50 5.5.2 NUMERICAL BOUNDARY LAYER VALIDATION TECHNIQUE USING RAE M2155 SWEPT WING
M.H. Mohsin, Cranfield University, United Kingdom
15. Sep 26 11:50 12:15 5.5.3 SIMULATION OF FIFTH-GENERATION HIGH-PERFORMANCE AIRCRAFT USING VISCOUS SURFACE-VORTICITY PANEL METHOD
S Shahjahan, 1Siemens Digital Industries Software Inc., United States
15. Sep 26 12:15 12:40 5.5.4 EXERGY-BASED AERODYNAMIC CHARACTERISTICS ANALYSIS OF THE NASA COMMON RESEARCH MODEL AND BWB CONFIGURATION CIVIL AIRCRAFT
H.C. Yang, Northwestern Polytechnical University, China
Reserve Paper 5.5.R 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 INVESTIGATING A STABLE LIFTING FUSELAGE FOR A TWO SEAT SAILPLANE OF THE GULL WING CONFIGURATION
B Huyssen, University of Pretoria, South Africa
additional information (interactive) 5.5.R 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 STUDY ON THE INJECTOR JETTING CHARACTERISTICS FOR VENTILATION EFFICIENCY OPTIMIZATION IN AIRCRAFT ENGINE LUBRICATION SYSTEMS?
X.-T XIE, Northwestern Polytechnical University, China
6.5Complex flow phenomena
Chair(s): Coder, J., Gowree, E.
Track 6
03.2 - Experimental Aerodynamics
15. Sep 26 11:00 11:25 6.5.1 EVALUATING THE LAMINAR FLOW ON A SLOTTED, NATURAL-LAMINAR-FLOW WING IN THE NASA AMES 11-FOOT TRANSONIC WIND TUNNEL
J. G. Coder, Penn State University, United States
15. Sep 26 11:25 11:50 6.5.2 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 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 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 EFFECTS OF SLOT LOCATION ON FLOW AND HEAT TRANSFER IN A LATTICEWORK COOLING CHANNEL: AN MRV EXPERIMENT AND NUMERICAL STUDY
Y. Jia, Xian Jiaotong University, China
7.5Transonic and Supersonic Aerodynamics for Advanced Configurations
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 26 11:00 11:25 7.5.1 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 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 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 FLOW SOLUTIONS AROUND VON KARMAN NOSES AT SUPERSONIC SPEEDS USING PHYSICS INFORMED NEURAL NETWORKS AND PRESSURE-SENSITIVE PAINT
MAE Escudero, Cranfield University, United Kingdom
8.5Fatigue & Progressive Damage
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 11:00 11:25 8.5.1 FEASIBILITY OF ELECTROPULSING-INDUCED FATIGUE CRACK CLOSURE IN AEROSPACE METALLIC MATERIALS
H. Park, Korea Institute of Materials Science, South Korea
15. Sep 26 11:25 11:50 8.5.2 LABORATORY METHOD FOR REPLICATING FASTENER HOLE CORROSION IN AA 7085
NB Tugwell, Defence Science and Technology Group, Australia
15. Sep 26 11:50 12:15 8.5.3 NEW INSIGHTS INTO AA7085 ENVIRONMENTALLY ASSISTED CRACKING THROUGH HIGH RESOLUTION FRACTOGRAPHY
I.C.W. Field, DSTG, Australia
15. Sep 26 12:15 12:40 8.5.4 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 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 VALIDATION OF A LOW-COST DATA COLLECTION SYSTEM FOR AIRCRAFT VIBRATION TESTING
G Dessena, Universidad Carlos III de Madrid, Spain
15. Sep 26 11:50 12:15 9.5.3 IMPACT RESISTANCE ENHANCEMENT IN FIBER-REINFORCED COMPOSITES USING CARBON/BASALT HYBRIDIZATION APPROACHES
A.H. Baluch¹, Z. Sajid¹, T. Rehman¹; ¹King Fahd University of Petroleum & Minerals, Saudi Arabia
Presenter: Abrar Ul Haq Khan Baluch, King Fahd University of Petroleum & Minerals
10.5Hybrid Electric UAVs
Chair(s): ,
Track 10
05 - Propulsion and Energy
15. Sep 26 11:00 11:25 10.5.1 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 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 TOWARDS A DATABASE OF MICRO-ELECTRIC MOTORS AND ELECTRONIC SPEED CONTROLLERS FOR SMALL UNCREWED AERIAL SYSTEMS
B.P. van Magill, The University of Sydney, Australia
15. Sep 26 12:15 12:40 10.5.4 IN-FLIGHT LOW-COST THRUST MEASUREMENT SYSTEM FOR SMALL UNMANNED AERIAL VEHICLES
C. Rieger, Technical University of Munich - Chair of Aircraft Design, Germany
Reserve Paper 10.5.R HIGH-FIDELITY NUMERICAL INVESTIGATION OF ROTOR-WING INTERACTIONS IN A MULTI-ROTOR DISTRIBUTED ELECTRIC PROPULSION CONFIGURATION
H A Abid, Queen Mary, University of London, United Kingdom
11.5System modeling
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 11:00 11:25 11.5.1 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 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 FLIGHT DYNAMICS AND GUIDANCE CONTROL FOR AERCRAFT IN TYPHOON ENVIRONMENT FOR DELIVERLY OF TYPHOON CONTROL SUBSTANCE
T. Sakurai, Yokohama National University, Japan
15. Sep 26 12:15 12:40 11.5.4 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 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 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 HARDWARE-IN-THE-LOOP VERIFICATION OF A SAFETY-CRITICAL MULTILEVEL BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIRCRAFT
P Panchal, University of the Bundeswehr Munich, Germany
15. Sep 26 12:15 12:40 12.5.4 AN EMBEDDED PHYSICS-INFORMED NEURAL NETWORK (PINN) FRAMEWORK FOR HIGH-FIDELITY REAL-TIME SIMULATION OF A FLIGHT CONTROL SURFACE ACTUATION SYSTEM
D.C. Lyu, China
Reserve Paper 12.5.R NEUROMORPHIC ASCENT: REVOLUTIONISING AIRCRAFT STORES COMPATIBILITY AND AUTONOMOUS SYSTEMS
M.G. Tutty, JAIME AMERICA, LLC, United States
additional information (interactive) 12.5.R 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 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 SYSTEM OF SYSTEMS ENGINEERING ROADMAP FOR INTEGRATING SUSTAINABLE AVIATION FUEL INTO MEXICO\'S AIRPORT FUEL INFRASTRUCTURE
G.-L. Gomez Falcon, UNIVERSIDAD AUTÓNOMA DE BAJA CALIFORNIA, Mexico
15. Sep 26 11:50 12:15 13.5.3 SOFTWARE ARCHITECTURE FOR A RECONFIGURABLE BATTERY SYSTEM FOR USE IN AN ELECTRIC AIRCRAFT
W. Bliemetsrieder, UniBw Munich, Germany
15. Sep 26 12:15 12:40 13.5.4 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 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 RAPID FLIGHT DYNAMICS EVALUATION OF STRONGLY COUPLED DISTRIBUTED PROPULSION
Y. Zhu, Northwestern Polytechnical University, China
15. Sep 26 11:50 12:15 14.5.3 ENSEMBLE MACHINE LEARNING FOR UAV PROPELLER PERFORMANCE PREDICTION WITH UNCERTAINTY QUANTIFICATION
M. I. Alam, King Fahd University of Petroleum and Minerals (KFUPM), Saudi Arabia
15. Sep 26 12:15 12:40 14.5.4 STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION
T. Goetzendorf-Grabowski, Warsaw University of Technology Institute of Aeronautics and App, Poland
Reserve Paper 14.5.R 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 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 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 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 EVALUATION OF METHODS FOR ANOMALY DETECTION IN THE APPROACH PHASE OF OPERATIONAL FLIGHT DATA
Robin Hähnel, German Aerospace Centre (DLR), Germany
15. Sep 26 12:15 12:40 15.5.4 PRELIMINARY SAFETY AND CERTIFICATION RISK ASSESSMENT FOR AN INNOVATIVE REGIONAL HYBRID AIRCRAFT CONFIGURATION
G. B Buzzo, CIRA - Italian Aerospace Research Centre, Italy
Reserve Paper 15.5.R EVALUATION OF A MULTI-SENSOR OBSTACLE TRACKING SYSTEM FOR AIRCRAFT USING REAL-WORLD DATA
K.D. Theuma, MCAST, Malta
additional information (interactive) 15.5.R CONTEXT-AWARE FLIGHT SAFETY EVENT DETECTION AND CLASSIFICATION USING A TWO-STAGE HYBRID MACHINE LEARNING MODEL
T. Asghar, National University of Sciences and Technology (NUST), Pakistan

12:40 - 13:40LUNCH BREAK

1.6GSA2: Regional Airliners: Electrified/H2 Prospects and Demonstrations
Chair(s): ,
Track 1
15 - Guest lectures (by personal invitation only)
15. Sep 26 13:40 14:05 1.6.1 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 (by personal invitation only)
15. Sep 26 13:40 14:05 2.6.1 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 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 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 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 A SINGLE-LOOP OPTIMIZATION METHOD FOR MULTIDISCIPLINARY DESIGN UNDER UNCERTAINTY
B Wang, The University of Sydney, Australia
15. Sep 26 14:05 14:30 3.6.2 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 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 A MIXED-FIDELITY VISCOUS-INVISCID INTERACTION APPROACH FOR THE DESIGN OPTIMIZATION OF NOVEL AIRCRAFT CONCEPTS
S.A. Bakhshi, University of Michigan, United States
Reserve Paper 3.6.R METHODOLOGICAL APPROACH TO MULTI-CRITERIA OPTIMISATION OF PRODUCT FAMILY ARCHITECTURES UTILISING SYSTEM MODELS
F. H. Christiansen, Hamburg University of Technology, Germany
4.6UAVs and advanced air mobility
Chair(s): Kanazaki, M.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 13:40 14:05 4.6.1 ENDURANCE EVALUATION OF DIFFERENT UAV CONFIGURATIONS AND POWERTRAIN ARCHITECTURES
A. Orgiu, Concordia University, Canada
15. Sep 26 14:05 14:30 4.6.2 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 COMMON RESEARCH MODELS FOR SMALL UNCREWED AERIAL VEHICLES
J.-A. Rasines Mazo, The University of Sydney, Australia
15. Sep 26 14:55 15:20 4.6.4 DESIGN AND TESTING OF A BUOYANT UAV FOR AGRICULTURAL SURVEILLANCE
P.-P. Kapoor, University of Hull, United Kingdom
Reserve Paper 4.6.R 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 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 DATA-DRIVEN RANS CLOSURES USING AN ADAPTIVE CURVATURE-BASED CLASSIFIER FOR VORTEX FLOWS
P West, Williams F1 team, United Kingdom
15. Sep 26 14:05 14:30 5.6.2 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 AN EVALUATION OF NONLINEAR EDDY-VISCOSITY MODELS FOR HIGH REYNOLDS NUMBER TURBULENT FLOW SIMULATIONS
T. Chagas Silva, Instituto Tecnologico de Aeronautica, Brazil
15. Sep 26 14:55 15:20 5.6.4 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
Reserve Paper 5.6.R CFD ANALYSIS OF MMRTG THERMAL PLUME ON THE EXTERNAL AERODYNAMICS OF A MARS ROVER
J. Fernandez Anton, Instituto Nacional de Técnica Aeroespacial, Spain
additional information (interactive) 5.6.R 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 MIDAS: A MODULAR SOFTWARE FOR INTAKE FLOW DISTORTION ANALYSIS
T. Piovesan, Cranfield University, United Kingdom
15. Sep 26 14:05 14:30 6.6.2 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 LOW-SPEED EXPERIMENTAL INVESTIGATION OF PODDED ENGINE INTEGRATION OF FLYING V AIRCRAFT
A. Kumar, TU Delft Faculty of Aerospace Engineering, Netherlands
15. Sep 26 14:55 15:20 6.6.4 WHEN ROTOR WAKE MEETS THE GROUND: INFLUENCE OF BLADE COUNT AND BLADE PITCH ON ROTOR OUTWASH
- Pradyumna, The University of Sydney, Australia
Reserve Paper 6.6.R 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 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 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 AERODYNAMIC OPTIMISATION OF BIOINSPIRED CORRUGATED WINGS FOR HIGH-EFFICIENCY MAV GLIDING
M Krasniqi, Flat 63 Nottingwood House, United Kingdom
15. Sep 26 14:30 14:55 7.6.3 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 THREE-DIMENSIONAL FLOW STRUCTURES OVER A LOW-ASPECT-RATIO PLUNGING WING
B. Anilir, METU Aerospace Engineering Department, Turkey
Reserve Paper 7.6.R 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 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 INVESTIGATION ON THE HIGH-EFFICIENCY PROPULSION MECHANISMS OF DUCK-WEBBED PADDLING FOR BIOINSPIRED AIRCRAFT APPLICATION
C. Cao, Northwestern Polytechnical University, China
8.6Structural Optimization
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 13:40 14:05 8.6.1 TOPOLOGY-OPTIMIZATION OF INTERCONNECTED 3D-PRINTED STRUCTURES FOR COST-EFFICIENT UAVS
A.M. Comer, Oklahoma State University, United States
15. Sep 26 14:05 14:30 8.6.2 TRACING MATERIAL PROPERTIES TO SYSTEM-LEVEL PERFORMANCE: A NORMALISED SENSITIVITY ANALYSIS FOR A BOEING 737 CLASS AIRCRAFT
S Stekovic, Linköping University, Sweden
15. Sep 26 14:30 14:55 8.6.3 GRADIENT-BASED STRUCTURAL OPTIMISATION OF COMPOSITE WING STRUCTURES USING HIGH-ORDER BEAM MODELS
D. Cardone, Universidad Carlos III de Madrid, Spain
15. Sep 26 14:55 15:20 8.6.4 THE STUDY ON STIFFNESS OPTIMIZATION ANALYSIS OF CIVIL AIRCRAFT FUSELAGE DOOR OPENINGS
Kaijun Yin, China
Reserve Paper 8.6.R SENSITIVITY ANALYSIS OF THE JOHNSON-COOK MODEL PARAMETERS FOR AL2024-T3 IN BIRD STRIKE ANALYSIS ON FIXED LEADING EDGES
R. Martins Martins, Boeing, Brazil
9.6Testing & Demonstrator
Chair(s): ,
Track 9
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
15. Sep 26 13:40 14:05 9.6.1 A FULL-SCALE DEMONSTRATOR FOR RAPID TESTING OF HELICOPTER AIRFRAMES USING ADVANCED CONTROL SYSTEM METHODOLOGIES
G. Swanton, Defence Science and Technology Group, Australia
15. Sep 26 14:05 14:30 9.6.2 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 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 EFFECT OF MORPHOLOGICAL CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF THE WING AND TAIL FEATHERS OF A TAXIDERMY BLACK-TAILED GULL
N. Kishimoto, Kwansei Gakuin University, Japan
10.6Supersonic
Chair(s): ,
Track 10
05 - Propulsion and Energy
15. Sep 26 13:40 14:05 10.6.1 NUMERICAL INVESTIGATION OF GEOMETRIC EFFECT ON INFRARED CHARACTERISTICS OF MULTI-STREAM SERPENTINE NOZZLES
Y. Wu, Northwestern Polytechnical University, China
15. Sep 26 14:05 14:30 10.6.2 COMPARATIVE ASSESSMENT OF PROPULSION SYSTEM ARCHITECTURES TAILORED FOR SUPERSONIC APPLICATIONS
L. Carrea, Mälardalen University, Sweden
15. Sep 26 14:30 14:55 10.6.3 SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET
H. Miki, JAXA, Japan
15. Sep 26 14:55 15:20 10.6.4 NUMERICAL STUDY OF UNSTEADY DISTORTION IN AN S-DUCT INTAKE SUBJECTED TO BLAST SHOCK WAVES
L. Shi, China
Reserve Paper 10.6.R TOWARDS SUSTAINABLE SUPERSONIC PROPULSION: INTEGRATED PROPULSIVE-EMISSIONS MODEL FOR MACH-2 MIXED-FLOW TURBOFAN ENGINES
Fabrizio Borgna¹, Roberta Fusaro¹, Davide Ferretto¹, Nicole Viola¹, Marco Marini, Italian Aerospace Research Centre (CIRA), Italy; ¹Politecnico di Torino, Italy
11.6Optimization
Chair(s): ,
Track 11
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 26 13:40 14:05 11.6.1 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 OPTIMAL GUIDANCE ALGORITHM FOR BOOST-BACK OF REUSABLE LAUNCH VEHICLES
J. Shim, Korea Advanced Institute of Science and Technology, South Korea
15. Sep 26 14:30 14:55 11.6.3 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 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 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 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 MODAL-BASED FUEL LEVEL ESTIMATION OF CRYOGENIC PROPELLANT TANKS
S Pfeifer, FH JOANNEUM Ges.mbH, Austria
15. Sep 26 14:30 14:55 12.6.3 SIZING OF LINEAR ACTUATORS FOR SPAN EXTENSION OF HALE UAV
T Prakash, India
15. Sep 26 14:55 15:20 12.6.4 DYNAMIC PERFORMANCE DEGRADATION OF FLIGHT CONTROL EHA UNDER HIGH-TEMPERATURE CONDITIONS
M. -W. Sun, Beihang University, China
Reserve Paper 12.6.R NONLINEAR FRICTION MODELING OF HELIX SWING HYDRAULIC CYLINDERS FOR MORPHING AIRCRAFT USING PHYSICS-INFORMED NEURAL NETWORKS
S. Chen, Beihang University, China
Reserve Paper 12.6.R LIGHTWEIGHT BIMETALLIC GEARS FOR AEROSPACE TRANSMISSIONS ENABLED BY OPEN-AIR DIFFUSION BONDING
J Jiang, Imperial College London, United Kingdom
additional information (interactive) 12.6.R 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 APPROPRIATE ATC GO-AROUND INSTRUCTION TIMING TO PREVENT RUNWAY COLLISIONS
S. Kontani, Graduate School of Maritime Sciences, Kobe University, Japan
15. Sep 26 14:05 14:30 13.6.2 COMPARATIVE VALIDATION OF TRADITIONAL COMPETENCY-BASED ASSESSMENT AND EXPERIENCE-BASED AUTHORISATION FOR AIR TRAFFIC CONTROLLERS
J. Meier, German Aerospace Center (DLR), Germany
15. Sep 26 14:30 14:55 13.6.3 FLIGHT CENTRIC ATC – HOW TO SOLVE CONFLICTS WITHOUT COMMUNICATION AND COORDINATION OVERLOADS?
T. Finck, German Aerospace Center, Germany
15. Sep 26 14:55 15:20 13.6.4 AUGMENTED REALITY SAFETY NETS FOR INCREASED AIRPORT SAFETY
T. Fadda, University of Bologna - Italy, Italy
Reserve Paper 13.6.R 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 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 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
15. Sep 26 14:30 14:55 14.6.3 REINFORCEMENT LEARNING-BASED ADAPTIVE WEIGHTING OF SWARM GUIDANCE LAWS FOR SMALL FIXED-WING UAVS
C Kang, Hanseo University, South Korea
15. Sep 26 14:55 15:20 14.6.4 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 IMPLEMENTATION OF DISTRIBUTED SWARM GUIDANCE ALGORITHMS ON LOW-COST UAVS
J.L. McGuire, DSTG, Australia
additional information (interactive) 14.6.R 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 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 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 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 PROBABILISTIC VALIDATION OF A NUMERICAL MODEL FOR RUN-BACK ICE SHAPES PREDICTION
M. Gallia, TU Braunschweig, Germany
15. Sep 26 14:30 14:55 15.6.3 EARLY WARNING FOR POTENTIAL BIRD STRIKES: STRATEGIC OPTIMIZATION OF PAN-TILT-ZOOM SENSOR NETWORKS FOR BIRD HAZARD DECREASE IN AIRPORT ENIRONMENT
- Mei, The University of Sydney, Australia
15. Sep 26 14:55 15:20 15.6.4 REAL-TIME AIRPORT BIRD-STRIKE PROTECTION WITH IMPROVED EDGE DEVICE DETECTION METHOD
J Gao, The University of Sydney, Australia

15:20 - 15:25CHANGEOVER BREAK

0.4GENERAL 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 (by personal invitation only)
15. Sep 26 16:40 17:05 1.7.1 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 JET ZERO: ATJ SAF PROJECT DEVELOPER
J Mason, Jet Zero Australia, Australia
15. Sep 26 17:30 17:55 1.7.3 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 PANEL DISCUSSION Q&A WITH THE SPEAKERS
P Panel,
2.7GARTEUR 1
Chair(s): ,
Track 2
15 - Guest lectures (by personal invitation only)
15. Sep 26 16:40 17:05 2.7.1 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 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 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 COMPARING DIFFERENT SEMI-EMPIRICAL AERODYNAMIC TOOLS FOR ANALYSING NOVEL AIRCRAFT CONFIGURATIONS
J.C Chan, Cranfield University, United Kingdom
15. Sep 26 17:05 17:30 3.7.2 DEEP LEARNING-BASED INVERSION OF NEAR-FIELD OVERPRESSURE SIGNATURES FOR LOW-BOOM SUPERSONIC TRANSPORT
Y.-P. Peng, Northwestern Polytechnical University, China
15. Sep 26 17:30 17:55 3.7.3 EASIBILITY-AWARE MULTISOURCE DESIGN METHODOLOGIES FOR HYDROGEN-POWERED SUSTAINABLE AVIATION
R Obasa, Imperial College London, United Kingdom
15. Sep 26 17:55 18:20 3.7.4 AN INCREMENTAL MODULAR MDO FRAMEWORK FOR HYDROGEN-ELECTRIC POWERTRAIN SIZING AND INTEGRATION IN GENERAL AVIATION AIRCRAFT
Pablo Moreno-Escolástico, Universidad Carlos III de Madrid, Spain
4.7Optimization in design
Chair(s): Gerhards, R.
Track 4
01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
15. Sep 26 16:40 17:05 4.7.1 A MULTI-SCALE COMPUTATIONAL FRAMEWORK FOR EVALUTATING TECHNOLOGY IMPACTS ON FUTURE AIRCRAFT FLEETS
ES Cassidy, University of Michigan, United States
15. Sep 26 17:05 17:30 4.7.2 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 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 TOP-LEVEL AIRCRAFT REQUIREMENT TRADE STUDIES FOR HYDROGEN FUEL CELL REGIONAL AIRCRAFT
M. Di Stasio, University of Naples Federico II, Italy
Reserve Paper 4.7.R MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY
G. Shen, Northwestern Polytechnical University, China
5.7Aeroacoustics and Noise Predictions
Chair(s): Thomber, B., Lawson, N.
Track 5
03.1 - Aerodynamics – CFD Methods and Validation
15. Sep 26 16:40 17:05 5.7.1 THE NUMERICAL SIMULATIONS OF THE ACOUSTIC SHIELDING EFFECTS ON THE BLADE-VORTEX INTERACTION NOISE OF THE HART-II MODEL
T. Ikeda, Japan Aerospace Exploration Agency, Japan
15. Sep 26 17:05 17:30 5.7.2 NOISE-OPTIMIZED HOVER PROPELLER DESIGN FOR VTOL CARGO DRONES IN TRANSIENT FLIGHT CONDITIONS
T. Moses, Technical University of Munich, Germany
15. Sep 26 17:30 17:55 5.7.3 HIGH-FIDELITY AEROACOUSTIC AND UNSTEADY FLOW ANALYSIS OF WIND TURBINE BLADES
H A Abid, King Fahd University of Petroleum and Minerals, Saudi Arabia
15. Sep 26 17:55 18:20 5.7.4 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 PRACTICAL ASPECTS OF ROTOR AERODYNAMIC AND AEROACOUSTIC DESIGN OPTIMIZATION
W. A. Klimczyk, Lukasiewicz Research Network - Institute of Aviation, Poland
6.7Morphing and shape adaptation
Chair(s): Imamura, T., Allen, N.
Track 6
03.2 - Experimental Aerodynamics
15. Sep 26 16:40 17:05 6.7.1 EXPERIMENTAL STUDY OF LOAD ALLEVIATION WITH PASSIVE ADAPTIVE CAMBER AIRFOILS
A. Sumi, Tokyo University of Agriculture and Technology, Japan
15. Sep 26 17:05 17:30 6.7.2 EVALUATION OF MORPHOUS WING CHARACTERISTICS IN WATER AND WIND TUNNEL IN THE CONTEXT OF UAV OPERATIONAL FLEXIBILITY
M. A. Marciniuk, Wroc?aw University of Science and Technology, Poland
15. Sep 26 17:30 17:55 6.7.3 GUST RESILIENCE: PASSIVE GUST MITIGATION MECHANISMS USED BY GLIDING KESTRELS
D Penn, RMIT University, Australia
15. Sep 26 17:55 18:20 6.7.4 AERODYNAMIC PERFORMANCE INCREASE OF AN A320 MORPHING WING IN SUBSONIC REGIME AT REYNOLDS NUMBER OF 1 MILLION
J.A.K. Abu Kalil, ICUBE/IMFT, France
Reserve Paper 6.7.R WIND-TUNNEL FORCE BALANCE AND MOUNTING SYSTEM FOR INFLATABLE WINGS
B Desale, IITB-Monash Research Academy, India
additional information (interactive) 6.7.R EFFECTS OF MOLTING ON THE AERODYNAMIC CHARACTERISTICS OF BLACK-TAILED GULLS
Y Tanahashi, Chubu University, Japan
7.7Data-Driven Design, Optimization and Reduced-Order Modeling
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 26 16:40 17:05 7.7.1 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 SUPERVISED DIMENSIONALITY-REDUCED MULTI-FIDELITY SURROGATE MODEL ASSISTED HIGH-DIMENSIONAL NATURAL LAMINAR FLOW OPTIMIZATION
Y. Gan, Northwestern Polytechnical University, China
15. Sep 26 17:30 17:55 7.7.3 AIRFOIL DESIGN OPTIMIZATION FOR HIGH-LIFT AND HIGH-EFFICIENCY APPLICATIONS USING DEEP REINFORCEMENT LEARNING
P Scavella, UNIVERSITY OF NAPLES FEDERICO II, Italy
Presenter: Gerardo Paolillo, UNIVERSITY OF NAPLES FEDERICO II
15. Sep 26 17:55 18:20 7.7.4 UNSTEADY AERODYNAMIC OPTIMIZATION OF THIN ANGULAR AIRFOIL USING CARTESIAN MESH CFD WITH LEVEL SET METHOD
D Sasaki, Osaka Metropolitan University, Japan
Reserve Paper 7.7.R MULTI-SCALE LINEAR FEATURE MODULATION DEEP NEURAL OPERATOR FOR RAPID PRESSURE COEFFICIENT PREDICTION
ZWF Zhang, NWPU, China
8.7Damage Tolerance
Chair(s): ,
Track 8
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
15. Sep 26 16:40 17:05 8.7.1 ARCHITECTED LATTICE SANDWICH STRUCTURES FOR LIGHTWEIGHT IMPACT AND ENERGY ABSORPTION APPLICATIONS
George Catalin: Cristea, INCAS, Romania
15. Sep 26 17:05 17:30 8.7.2 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 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 MULTIPHYSICS COUPLING EFFECT ON INTERFACIAL PROPERTIES OF CNT/GFRP/CFRP COMPOSITES FOR ELECTROTHERMAL AI/DI APPLICATIONS
X. Yao, Northwestern Polytechnical University, China
Reserve Paper 8.7.R 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 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 COMBINED TOPOLOGY AND COMPOSITE LAMINATE OPTIMIZATION OF A STRUT-BRACED DRY WING FOR A HYDROGEN AIRCRAFT
LEM Vertonghen, France
15. Sep 26 17:05 17:30 9.7.2 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 AN AUTOMATED PARAMETRIC FRAMEWORK FOR EARLY-STAGE STRUCTURAL DESIGN AND OPTIMIZATION OF COMPOSITE AIRFRAMES
N Ziakos, Universidad Carlos III de Madrid, Spain
15. Sep 26 17:55 18:20 9.7.4 DYNAMIC BUCKLING ANALYSIS OF VARIABLE STIFFNESS COMPOSITE CYLINDRICAL SHELLS
Y. Guo, Nanjing University of Aeronautics and Astronautics, China
Reserve Paper 9.7.R 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 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 DESIGN CONCEPT FOR STRUCTURAL ELEMENTS MANUFACTURED FROM THICK LAMINATED COMPOSITE MATERIALS
G. C. Fonseca, Embraer Minas Gerais, Brazil
10.7Hypersonic
Chair(s): ,
Track 10
05 - Propulsion and Energy
15. Sep 26 16:40 17:05 10.7.1 PROPULSION-AIRFRAME INTEGRATED AERODYNAMIC PREDICTION METHOD USING FASTAR FOR SPACEPLANE CONCEPTUAL DESIGN
K. Tsukuda, Osaka Metropolitan University, Japan
15. Sep 26 17:05 17:30 10.7.2 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 REPRESENTATIVE THERMO-STRUCTURAL TESTING OF SCRAMJETS USING COMMERCIAL ROCKET ENGINE TEST
A Lockley, Australia
Presenter: Alison Roco
15. Sep 26 17:55 18:20 10.7.4 GREEN PROPULSION VIA SUSTAINABLE 3D-PRINTED METAL-DOPED PLA HYBRID ROCKET FUELS
N. Binti Abd Razak, Malaysia
Reserve Paper 10.7.R 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 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 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 HPC-BASED PARAMETER SPACE EXPLORATION FOR DENSE PICOSAT FORMATION FLYING TOWARD DIRECT-TO-DEVICE COMMUNICATIONS
S. Joshin, The University of Osaka, Japan
15. Sep 26 17:55 18:20 11.7.4 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 HYPERSONIC VEHICLE FLIGHT SIMULATION AND FLIGHT CONTROL
Hyoung Sik Choi, KARI, South Korea
Reserve Paper 11.7.R A FRAMEWORK FOR VIRTUAL CERTIFICATION OF AIRCRAFT IN ICING CONDITIONS: WORKFLOW IMPLEMENTATION AND ASSESSMENT
H. P. Heramarwan, Politecnico di Milano, Italy
12.7Informatic modeling
Chair(s): ,
Track 12
07 - Systems, Subsystems and Equipment
15. Sep 26 16:40 17:05 12.7.1 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 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 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 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 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 A PRELIMINARY STUDY ON DYNAMIC AIRSPACE CONFIGURATION USING FLEXIBLE VERTICAL BOUNDARIES IN DOUBLE-LAYER AIRSPACE
H Suizu, Electronic Navigation Research Institute, Japan
15. Sep 26 17:30 17:55 13.7.3 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 UNDERSTANDING THE IMPACT OF OPERATIONAL VARIABLES ON ELECTRIC AIRCRAFT BATTERY PERFORMANCE VIA REAL-FLIGHT DATA ANALYSIS
J.H. Kim, Sejong University, South Korea
Reserve Paper 13.7.R 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 QUANTIFYING LAND AERIAL RESCUE DEMAND INTENSITY: A DATA-DRIVEN MODELING APPROACH FOR DEFINING THE AIR-GROUND OPERATIONAL BOUNDARY
G. Wang, Aerial Industry Development Research Center of China, China
14.7ICAS Council Meeting
Chair(s): ,
Track 14
15.7Design challenges and Training enablers
Chair(s): ,
Track 15
14 - Education and Training
15. Sep 26 16:40 17:05 15.7.1 DESIGN, BUILD AND TEST A FULLY AUTONOMOUS UAV FOR HUMANITARIAN AID DELIVERY
B. Sebastiani, University of Bologna, Italy
15. Sep 26 17:05 17:30 15.7.2 A STRUCTURED CONCEPTUAL AND PRELIMINARY DESIGN FOR A SMALL-SCALE ELECTRICALLY POWERED FIXED-WING AIRCRAFT
N.A Azmitia, Universidad Panamericana, Mexico
15. Sep 26 17:30 17:55 15.7.3 EVALUATING LEARNING EFFECTIVENESS THROUGH A MIXED REALITY TRAINING FRAMEWORK FOR AEROSPACE MAINTENANCE TASKS
MA Higinio, RMIT UNIVERSITY, Australia
15. Sep 26 17:55 18:20 15.7.4 FROM DATA TO DEBRIEF: A FRAMEWORK FOR PILOT PERFORMANCE ASSESSMENT
P. B. Kurka, ITA, Brazil
Reserve Paper 15.7.R 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 TOWARDS AN ECOSYSTEM FOR AERONAUTICAL RESEARCH IN MEXICO
A. M. Zarate Villazon, Georgia Institute of Technology - Aerospace Systems Design Lab, United States