30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

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

Tuesday, 15. Sep 2020


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.1General Lecture 2 - Future needs you – the panel discussion of the skills for aeronautics
Chair: M. Kanerva ECSC Chair
15. Sep 20 08:00 09:00

0.2Interactive Presentations
Chair:
15. Sep 20 09:00 10:00

1.1Wing Design
Chair(s): Rinoie, K.
Track 1
01 - Aircraft Design and Integrated Systems
15. Sep 20 10:00 10:30 1.1.1 A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING
Y.K. Yin, Shanghai Jiao Tong University, China
15. Sep 20 10:30 11:00 1.1.2 VALUE ANALYSIS AND RISK ASSESSMENT FOR MORPHING LEADING AND TRAILING EDGE FOR VARIABLE CAMBER WING
W.Y.CHENG CHENG, Aviation Industry Development Research Center of China (ADR), China
15. Sep 20 11:00 11:30 1.1.3 EVALUATION AND VALIDATION OF AEROELASTIC ANALYSIS PROGRAM FOR AEROSTRUCT WING OPTIMIZATION PLATFORM
S.B. Ling, Northwestern Polytechnical University, China
15. Sep 20 11:30 12:00 1.1.4 ON WINGS WITH NON-ELLIPTIC LIFT DISTRIBUTIONS
E. Bragado Aldana¹, M. M. Lone¹; ¹Cranfield University, United Kingdom
Reserve Paper 1.1.R LOW SWEEP LAMINAR FLOW WING AT TRANSONIC SPEED
N. Qin, The University of Sheffield, United Kingdom
Reserve Paper 1.1.R ON THE FLIGHT MECHANICS OF A TRANSPORT AIRCRAFT FITTED WITH FLARED-HINGE FOLDING WINGTIPS
R Ajaj, Khalifa University, United Arab Emirates
2.1Cost Assessment
Chair(s): Bagassi, S.
Track 2
01 - Aircraft Design and Integrated Systems
15. Sep 20 10:00 10:30 2.1.1 FLEET LEVEL DIRECT OPERATING COST ASSESSMENT OF ADVANCED ALL NEW MID-RANGE TRANSPORT AIRCRAFT
J. Hartmann, DLR, Germany
15. Sep 20 10:30 11:00 2.1.2 STATISTICAL APPROACH TO INDIRECT COST ASSESSMENT FOR AN AIRCRAFT FLEET
G.-F. Ferrari, Politecnico di Torino, Italy
15. Sep 20 11:00 11:30 2.1.3 DEVELOPMENT OF A PARAMETRIC COST MODEL ASSESSING THE IMPACT OF NEW TECHNOLOGIES ON A REGIONAL AIRCRAFT
M. Fioriti, Politecnico di Torino, Italy
15. Sep 20 11:30 12:00 2.1.4 LIFECYCLE COST-BENEFIT ASSESSMENT OF SELECTED TECHNOLOGIES CONSIDERING UNCERTAINTIES
A.A. Pohya, DLR, Germany
Reserve Paper 2.1.R BASED ON THE CHARACTERISTIC PARAMETERS ESTIMATE MANUFACTURING COST FOR COMPOSITE STRUCTURES
H.-F. Feng, China
3.1Global Collaborative Digital Integration in Aviation / IFAR-X challenge
Chair(s): ,
Track 3
02 - Systems Engineering and Integration
4.1Aerodynamic Optimization
Chair(s): Wan, T., Gao, Z.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
15. Sep 20 10:00 10:30 4.1.1 FLOW CONTROL AT HIGH LIFT MISSION OF A CIVIL AIRCRAFTBY AN OPTIMUM MORPHING LEADING-EDGE DESIGN
alireza jahangirian, aerospace engineering departmen, Iran
15. Sep 20 10:30 11:00 4.1.2 OPTIMISATION OF VORTEX GENERATORS FOR STALL SPEED REDUCTION
C Bil, RMIT University, Australia
15. Sep 20 11:00 11:30 4.1.3 AERODYNAMIC DESIGN OOPTIMIZATION OF A CIVIL AIRCRAFT WINGLET USING MULTI-OBJECTIVE EVOLUTIONARY ALGORITHM AND CFD SOLVER
alireza jahangirian, aerospace engineering departmen, Iran
15. Sep 20 11:30 12:00 4.1.4 DESIGN AND OPTIMIZATION OF A HIGH-ALTITUDE LONG ENDURANCE UAV PROPELLER
K. Y. You, Northwestern Polytechnical University, China
Reserve Paper 4.1.R OPTIMAL DESIGN OF A NEXT GENERATION HIGH-LIFT REUSABLE RE-ENTRY VEHICLE
G. Pezzella, University of Campania, Italy
Reserve Paper 4.1.R MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF A CIVIL AIRCRAFT FUSELAGE
alireza jahangirian, aerospace engineering departmen, Iran
5.1Measurement Techniques & Data Analysis
Chair(s): Jujun, W., Xunmian, W.
Track 5
03.2 - Experimental Aerodynamics
15. Sep 20 10:00 10:30 5.1.1 AN OBJECTIVE APPROACH FOR MEASURING INTERMITTENCY IN THE TRANSITIONAL BOUNDARY LAYERS
D Veerasamy, City, University of London, United Kingdom
15. Sep 20 10:30 11:00 5.1.2 DYNAMIC TRAILING-EDGE FLAP MOVEMENT AS A NON-CONVENTIONAL LIFTING MECHANISM
M. Bremm, RWTH Aachen University, Germany
15. Sep 20 11:00 11:30 5.1.3 COMPUTATIONAL FLUID DYNAMIC STUDY ON LOW SPEED WIND TUNNEL DATA CORRECTIONS
W. S. Stryczniewicz, Lukasiewicz Research Network - Institute of Aviation, Poland
15. Sep 20 11:30 12:00 5.1.4 SKIN-FRICTION TOPOLOGY ON AXISYMMETRIC BOATTAIL MODELS BY AN OPTICAL-FLOW ALGORITHM WITH SUBGRID FUNCTION
T. H. Tran, Le Quy Don Technical University, Vietnam
Reserve Paper 5.1.R APPLIED RESEARCH ON SUPERVISED LEARNING IN THE JUDGMENT OF AIRFOIL TRANSITION
W.-B.B. Wei, China
6.1Developments in Modelling
Chair(s): Atkin, C., Mughal, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
15. Sep 20 10:00 10:30 6.1.1 EXPERIMENTAL INVESTIGATION, NUMERICAL AND MATHEMATICAL SIMULATION OF DISPERSE FLOWS IMPINGING ON AIRCRAFT SURFACE
Ivan Alexeevich: Amelyushkin, TsAGI, Russia
15. Sep 20 10:30 11:00 6.1.2 MODIFICATION OF TURBULENCE MODELS FOR PRESSURE-INDUCED SEPARATION ON SMOOTH SURFACES USING THE DLR VICTORIA EXPERIMENT
A. M. Krumbein, DLR - German Aerospace Center, Germany
15. Sep 20 11:00 11:30 6.1.3 A NETWORK-CENTROID BASED REDUCED-ORDER MODEL FOR A MIXING LAYER
H. Li, National University of Defense Technology, China
15. Sep 20 11:30 12:00 6.1.4 SINGULARITIES IN THE NEAR-WALL REGION OF 3D BOUNDARY LAYER AND ASYMPTOTIC FLOW STRUCTURE IN ITS VICINITY
V.I. Shalaev, Moscow Institute of Physics and Technology, Russia
Reserve Paper 6.1.R LOW ORDER MODELLING OF UNSTEADY AERODYNAMIC LIFT FORCES ON 2D FLAT-PLATE DURING SINUSOIDAL PITCHING
R. Zeng, Beihang University, China
7.1Propulsion Airframe Integration 1
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 20 10:00 10:30 7.1.1 PROPELLER WAKE - OBJECT INTERACTION USING A FREE WAKE MODEL UTILIZING LOCAL MESH REFINEMENT
M. Thiele, Technical University of Munich - Institute of Aircraft Design, Germany
15. Sep 20 10:30 11:00 7.1.2 AERODYNAMIC INVESTIGATION OF ROTOR-ROTOR INTERACTION FOR DISTRIBUTED-PROPELLER SYSTEMS
R. de Vries, Delft University of Technology, Netherlands
15. Sep 20 11:00 11:30 7.1.3 NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER SEVERE WEATHER
T. Wan, Tamkang University, Taiwan, China
15. Sep 20 11:30 12:00 7.1.4 MULTI-DISCIPLINARY FRAMEWORK FOR PROPELLER BLADE DESIGN
A. Kümmel, Germany
8.1Composite Materials and Structures
Chair(s): Fichera, S., Li, K.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
15. Sep 20 10:00 10:30 8.1.1 LIGHTWEIGHT DESIGN OF THERMAL PROTECTION STRUCTURES WITH EFFECTS OF MESO-PROPERTIES OF MATERIALS
S.-H.-A. You An, Computational Aerodynamic Institute(CAI), CARDC, China
15. Sep 20 10:30 11:00 8.1.2 ACCURATE MODELS FOR THE PREDICTION OF FREE-EDGE STRESSES OF COMPOSITE STRUCTURES UNDER THERMAL LOADS
E. Zappino, Italy
15. Sep 20 11:00 11:30 8.1.3 TEMPERATURE-INDUCED LOAD OF BOLTED HYBRID COMPOSITE/METAL JOINT
L.-K KAI, AVIC Aircraft Strength Research Institute, China
15. Sep 20 11:30 12:00 8.1.4 DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS
A. Shanygin, Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 8.1.R SEARCH OF RATIONAL LEVEL OF WING-FUSELAGE INTEGRATION TO INCREASE WEIGHT EFFICIENCY OF AIRCRAFT COMPOSITE STRUCTURES
I. Kondakov, Central Aerohydrodynamic Institute (TsAGI), Russia
Reserve Paper 8.1.R STRUCTURAL INDICES-BASED OPTIMIZATION METHODOLOGY FOR LIGHT AIRCRAFT COMPOSITE WINGS
M Nuño, RWTH Aachen University, Germany
9.1Multi Disciplinary Optimisation (MDO)
Chair(s): Mirzoyan, A.
Track 9
05 - Propulsion
15. Sep 20 10:00 10:30 9.1.1 KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND WEIGHT ESTIMATION OF RUBBER AERO ENGINES
J. Häßy, German Aerospace Center (DLR), Germany
15. Sep 20 10:30 11:00 9.1.2 RESEARCH OF PROPULSION-SYSTEM-SURROGATE-MODELING METHOD USING INFILL CRITERION SAMPLES
DC.W Wang, School of Aeronautics, Northwestern Polytechnical University, China
15. Sep 20 11:00 11:30 9.1.3 ELABORATION OF DISTRIBUTED MDAO SYSTEM FOR CONCEPTUAL DESIGN OF SCA PROPULSION SYSTEM IN INTEGRATED DEVELOPMENT ENVIRONM
L.A. Mirzoyan, CIAM, Russia
15. Sep 20 11:30 12:00 9.1.4 AERODYNAMIC PROPULSION SYSTEM OPTIMIZATION: TOWARDS TO AGILE 4.0
K.S. Anisimov, Federal State Unitary Enterprise Central Aerohydrodynamic Instit, Russia
10.1Virtual Testing
Chair(s): Stumpf, E., Peters, M.
Track 10
07 - Systems, Subsystems and Equipment
15. Sep 20 10:00 10:30 10.1.1 VIRTUAL TESTING IN LANDING GEAR SHOCK ABSORBER DESIGN USING AN EQUIVALENT CFD-MODEL
R. Springmann, Hamburg University of Technology, Germany
15. Sep 20 10:30 11:00 10.1.2 VIRTUAL TESTING OF A MULTIFUNCTIONAL POWER CONTROL UNIT FOR HYDRAULIC SUPPLY AND HIGH LIFT ACTUATION
L. Nordmann, Germany
15. Sep 20 11:00 11:30 10.1.3 RESEARCH AND VALIDATION OF SYSTEM MODELING AND SIMULATION OF INTAKE AIR MIXER ALTITUDE TEST BED
Feng-Wu: F. -W. Wu, AECC Sichuan Gas Turbine Establishment, China
15. Sep 20 11:30 12:00 10.1.4 DESIGN AND DEVELOPMENT OF A MODULAR IRON BIRD TO TEST MOVABLE SURFACE ACTUATORS OF GENERAL AVIATION AIRCRAFT AND UAVS
M. Mattei, Università della Campania "Luigi Vanvitelli", Italy
11.1UAV Dynamics and Control 1
Chair(s): Rui, W., Götzendorf Grabowski, T.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 20 10:00 10:30 11.1.1 RESEARCH ON DYNAMIC MODELING AND TRANSITION FLIGHT STRATEGY OF INDUCED-LIFT VTOL UAV
C.W Wang, Northwestern Polytechniacl University, China
15. Sep 20 10:30 11:00 11.1.2 COMPARATIVE ANALYSIS OF METHODS USED TO ACTIVE CONTROL OF MICRO AERIAL VEHICLE
K.-S. Sibilski, Warsaw University of Technology, Poland
15. Sep 20 11:00 11:30 11.1.3 PERCHING PRINCIPLES ANALYSIS OF POST-STALL PERCHING UNMANNED AERIAL VEHICLE
S.-Y Yang, NWPU, China
15. Sep 20 11:30 12:00 11.1.4 DEVELOPMENT TOWARDS A TOOLCHAIN FOR ESTIMATING UAV FLIGHT DYNAMIC MODELS IN EARLY DESIGN
S. Koeberle, Institute of Aircraft Design/Technical University of Munich, Germany
Reserve Paper 11.1.R STUDY OF SMALL UAVS DISTURBED MOTION NATURAL FREQUENCIES USING EXTENDED EXPERIMENTAL DATASETS
M. E. El-Salamony, Peking University, China
12.1Composite Characterization and Fabrication
Chair(s): Pinto, L., Wallin, M.
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
15. Sep 20 10:00 10:30 12.1.1 A DEEP-LEARNING-BASED METHOD FOR DAMAGE IDENTIFICATION OF COMPOSITE LAMINATES
Y Yu¹, W Binwen¹, L Shuaishuai¹, Z Yuxi, Peking University, China; W Li¹, L Guoqiang¹; ¹Aircraft Strength Research Institute of ChinaAffiliation, China
15. Sep 20 10:30 11:00 12.1.2 IN-SITU LASER ASSISTED DIRECT IMPREGNATION, LAMINATION AND PLACEMENT OF CFRTP
T. Ikeda, Chubu University, Japan
15. Sep 20 11:00 11:30 12.1.3 MOISTURE ABSORPTION BEHAVIOR OF COMPOSITE STIFFENED PANELS IN HYGROTHERMAL ENVIRONMENT
B-L Ma, China
15. Sep 20 11:30 12:00 12.1.4 A TWO PHASES COUPLING FREE AND POROUS FLOW NUMERICAL SIMULATION METHOD OF LCM PROCESS
C. Li, BASTRI of COMAC, China
Reserve Paper 12.1.R RESEARCH OF THE MECHANICAL PROPERTIES OF CFRP OF THE HIGH THICKNESS
A.A. Sviridov, The Central Aerohydrodynamic Institute, Russia
Reserve Paper 12.1.R DESIGN FOR MANUFACTURING APPROACH AND LOW COST METAL STRUCTURE
LP PINTO, AIRBUS, France
13.1ATC, Pilot & Controller
Chair(s): ,
Track 13
10 - Safety and Security
15. Sep 20 10:00 10:30 13.1.1 ATTENTION: TARGET AND ACTUAL – THE CONTROLLER FOCUS
J. Rataj, DLR, Germany
15. Sep 20 10:30 11:00 13.1.2 ANALYSIS OF PILOT OPERATIONAL STRATEGY DIFFERENCE USING NEURAL NETWORK
R. Mori, Electronic Navigation Research Institute, Japan
15. Sep 20 11:00 11:30 13.1.3 WORKLOAD EVALUATION USING OBJECTIVE AND SUBJECTIVE DATA MEASURED DURING SIMULATED FLIGHT
C. Orlando, Kore University of Enna, Italy
15. Sep 20 11:30 12:00 13.1.4 ENSURING HIGH NAVIGATION INTEGRITY FOR URBAN AIR MOBILITY USING TIGHTLY COUPLED GNSS/INS SYSTEM
S.-Z Wang, Shanghai Jiao Tong University, China
Reserve Paper 13.1.R OBJECTIVE MEASUREMENT OF HUMAN FACTORS FOR SUPPORTING THE OPERATOR’S LOAD SIMULATION AND MANAGEMENT
U. Kale, Budapest University of Tech. and econ.;, Hungary

12:00 - 13:00Lunch

0.3ICAS Lecture for Innovation in Aeronautics - Electrification - The third revolution in aviation, Cory Combs, USA
Chair:
15. Sep 20 13:00 13:45

1.2Hybrid/Electric & Unconventional Aircraft 1
Chair(s): Prakasha, P.
Track 1
01 - Aircraft Design and Integrated Systems
15. Sep 20 14:00 14:30 1.2.1 CONCURRENT OPTIMIZATION OF AIRFRAME AND ENERGY STORAGE AND CONVERSION SYSTEMS FOR HYBRID ELECTRIC PROPULSION AIRCRAFT
A. Elham, TU Braunschweig, Germany
15. Sep 20 14:30 15:00 1.2.2 PRELIMINARY DESIGN AND EXPERIMENTAL INVESTIGATION OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
Y.-M. Ma, Northwestern Polytechnical University, China
15. Sep 20 15:00 15:30 1.2.3 UNMANNED FIRE-FIGHTING AMPHIBIOUS AIRCRAFT WITH DISTRIBUTED TURBOELECTRIC PROPULSION SYSTEM
A.N. Varyukhin, CENTRAL INSTITUTE OF AVIATION MOTORS (CIAM), Russia
Reserve Paper 1.2.R MULTIFIDELITY OPTIMISATION OF A BLENDED WING BODY MARTIAN GLIDER
D. Verstraete, The University of Sydney, Australia
2.2Shape Optimization
Chair(s): Rinoie, K.
Track 2
01 - Aircraft Design and Integrated Systems
15. Sep 20 14:00 14:30 2.2.1 MULTI-FIDELITY AND MULTI-POINT SIMULTANEOUS SHAPE AND SIZING OPTIMISATION FOR MAXIMUM AIRCRAFT PERFORMANCE
A. Gastaldi, Airbus Defence and Space, Germany
15. Sep 20 14:30 15:00 2.2.2 BWB CONFIGURATION’S AERODYNAMIC OPTIMIZATION DESIGN AND SHAPE PARAMETERIZATION BASED ON GRADIENT METHOD
W.zy Wang, The First Aircraft Institute, China
15. Sep 20 15:00 15:30 2.2.3 MULTIFIDELITY AERODYNAMIC/STEALTH SHAPE DESIGN OPTIMIZATION METHOD FOR FLYING WING AIRCRAFT
Z.-Q. Liu, School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 2.2.R A GRADIENT-BASED AERO-STEALTH OPTIMIZATION DESIGN METHOD FOR THE LONG-ENDURANCE UAV SHAPE DESIGN
L.-M. Ming, Northwestern Polytechnical University, China
3.2System Architecture
Chair(s): Limouzy, J.C., Pan, D.P.
Track 3
02 - Systems Engineering and Integration
15. Sep 20 14:00 14:30 3.2.1 ARCHITECTURE INTEGRATION OF FUTURE ATM SYSTEM BASED ON META MODEL
JY Wang, China Aeronautical Radio Electronics Research Institute, China
15. Sep 20 14:30 15:00 3.2.2 TECHNOLOGY ROADMAPS FOR THE DEVELOPMENT OF FUTURE HIGH-SPEED TRANSPORTATION SYSTEMS
N. Viola, Politecnico di Torino, Italy
15. Sep 20 15:00 15:30 3.2.3 ARCHITECTURE OF PRODUCT RESEARCH AND DEVELOPMENT SYSTEM
L. Su, Aero-Engine Academy of China, China
Reserve Paper 3.2.R GREENER ATM SYSTEM ARCHITECTURE RESEARCH BASED ON COMPLEX SYSTEM ENGINEERING METHOD
H. Hu, China Aeronautical Radio Electronics Research Institute, China
4.2Ice Accretion
Chair(s): Gao, Z., Santos, L.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
15. Sep 20 14:00 14:30 4.2.1 DEVELOPMENT OF ANTI-ICING SIMULATION CODE USING THE CONJUGATE HEAT TRANSFER BASED ON ICEPAC
YH KIM, SNU, South Korea
15. Sep 20 14:30 15:00 4.2.2 NUMERICAL STUDY ON THE STALL CHARACTERISTICS AND SEPARATED FLOW AROUND ICED AIRFOILS USING LATTICE BOLTZMANN METHOD
H.Y.G Gu, Northwestern Polytechnical University, China
15. Sep 20 15:00 15:30 4.2.3 EFFECT OF DROPLET SIZE ON ICING RANGE FOR HELICOPTER BLADE
Li Weibin, China
Reserve Paper 4.2.R THREE-EQUATION TTURBULENCE MODEL FOR SEPARATION PREDICTION OF ICE-ACCRETION AIRFOIL
H.-L Li, Tsinghua University, China
5.2Aeroacoustics & Noise
Chair(s): Bao, C., Rasuo, B.
Track 5
03.2 - Experimental Aerodynamics
15. Sep 20 14:00 14:30 5.2.1 WAVE AND SOUND ATTENUATION EFFECT OF BIO-INSPIRED SMALL TUBERCLES
Y Inada, Tokai University, Japan
15. Sep 20 14:30 15:00 5.2.2 FEASIBILITY OF DETERMINING AIRCRAFT CERTIFICATION NOISE LEVELS USING GROUND PLANE MICROPHONE MEASUREMENTS
V.-P. Blandeau, Airbus, France
15. Sep 20 15:00 15:30 5.2.3 INVESTIGATION OF A NOISE REDUCTION PROPELLER GEOMETRY BASED ON AERODYNAMIC AND AEROACOUSTIC OPTIMIZATION
X GENG, BEIHANG UNIVERSITY, China
Reserve Paper 5.2.R MICROPHONE ARRAY TECHNIQUES FOR TRAILING EDGE NOISE BASED ON CONVOLUTIONAL NEUTRAL NETWORK
ZC Song, BeiHang Univerisity, China
6.2Turbulent Flows
Chair(s): Breitsamter, C., Fu, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
15. Sep 20 14:00 14:30 6.2.1 NUMERICAL SIMULATION OF BOUNDARY LAYER FLOW ON MICROSTRUCTURE SURFACE
R.P. Pang, Northwestern Polytechnical University , China
15. Sep 20 14:30 15:00 6.2.2 SUBSONIC WIND TUNNEL SMALL RIBLETS DRAG REDUCTION TEST ON C919 FUSELAGE MODEL
H.W. Wang, China Academy of Aerospace Aerodynamics, China
15. Sep 20 15:00 15:30 6.2.3 THE EFFECTS OF ADVERSE PRESSURE GRADIENT ON THE BEHAVIORS OF RESOLVENT MODE IN TURBULENT CHANNEL FLOWS
Cheng Chen, CARDC, China
Reserve Paper 6.2.R DIRECT SIMULATION OF THE HYPERSONIC SHOCK WAVE/BOUNDARY LAYER INTERACTION AND ITS HEATING LOAD CONTROL BY MICRO-RAMP VOR
D. Sun, State Key Laboratory of Aerodynamics, China
Reserve Paper 6.2.R FLOW AND HEAT TRANSFER MECHANISMS OF SINGLE CIRCULAR JET IMPINGEMENT USING LARGE EDDY SIMULATION
Q.-L. Li, China
7.2Propulsion Airframe Integration 2
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 20 14:00 14:30 7.2.1 AERODYNAMIC ANALYSIS OF AN AIR DRIVE EJECTOR FOR USE IN ENGINE TEST FACILITIES
F. R. Rasi, NRC, Canada
15. Sep 20 14:30 15:00 7.2.2 LOW PARAMETRIZED MODELLING METHODOLOGY TO OPTIMIZE THE WING SURFACE OF AN AIRCRAFT WITH OVER_WING MOUNTED ENGINES
PW WEGENER, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
15. Sep 20 15:00 15:30 7.2.3 AERODYNAMIC INTERFERENCE OPTIMIZATION OF THE FUSELAGE-PUSHING PROPELLER CONFIGURATION
V. Gubskiy, TsAGI, Russia
8.2Fluid Structure Interaction
Chair(s): Schmidt, H., Zheng, J.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
15. Sep 20 14:00 14:30 8.2.1 OPTIMAL DESIGN OF FLUID-CONVEYING PIPE SUPPORT FOR CONTROLLING REACTION FORCE DURING VIBRATION
R.T. tian, Aviation Industry Aircraft Strength Research Institute, China
15. Sep 20 14:30 15:00 8.2.2 OPERATIONAL MODAL ANALYSIS AND ESTIMATION OF AERODYNAMIC PARAMETERS OF A FLEXIBLE AIRCRAFT
L. Goes, ITA, Brazil
15. Sep 20 15:00 15:30 8.2.3 PRELIMINARY DESIGN AND OPTIMIZATION OF A REFERENCE AIRCRAFT UNDER DYNAMIC LOADS
H. Schmidt, RWTH University, Germany
9.2More / Hybrid / Electric Propulsion
Chair(s): Fioriti, M.
Track 9
05 - Propulsion
15. Sep 20 14:00 14:30 9.2.1 CONCEPTUAL STUDIES OF DIFFERENT TYPE OF HYBRID ELECTRIC PROPULSION SYSTEMS FOR COMMUTER AIRLINERS
V.S. Zakharchenko, CENTRAL INSTITUTE OF AVIATION MOTORS, Russia
15. Sep 20 14:30 15:00 9.2.2 THERMAL MANAGEMENT FOR GASOLINE ENGINE-BATTERY HYBRID PROPULSION SYSTEM OF SMALL UAV PLATFORM
H.R. Gwon, Korean Air R&D Center, South Korea
15. Sep 20 15:00 15:30 9.2.3 COMPARATIVE ANALYSIS OF THE HWB WITH MECHANICAL AND ELECTRICAL DRIVEN
M. Fioriti, Politecnico di Torino, Italy
Reserve Paper 9.2.R DIGITAL SIMULATION OF STARTER/GENERATOR CONTROL FOR MORE ELECTRIC ENGINE
J XU, AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD., China
Reserve Paper 9.2.R IMPLEMENTATION OF DISTRIBUTED ELECTRIC PROPULSION ON A GENERAL AVIATION AIRCRAFT
M Gallani, EMBRAER, Brazil
10.2Boundary Control
Chair(s): Itoh, E.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 20 14:00 14:30 10.2.1 INFLUENCE OF STABILITY AND CONTROL DERIVATIVES IN PIO PHENOMENON
G.D.A.N. Daher de Alencar Neves, Escola de Engenharia de São Carlos, Brazil
15. Sep 20 14:30 15:00 10.2.2 AIRCRAFT GROUND MOTION SIMULATION ORIENTED 6 DEGREE OF FREEDOM MODEL
N. Bai Bai, Beihang University, China
15. Sep 20 15:00 15:30 10.2.3 RE-ENTRY TRAJECTORY TRACKING CONTROL OF A MICRO-SATELLITE SYSTEM WITH A DEPLOYABLE FRONT STRUCTURE
M. Mattei, Università della Campania "Luigi Vanvitelli", Italy
Reserve Paper 10.2.R INFLUENCE OF AERODYNAMIC ASYMMETRY ON SPIN PARAMETERS OF THE COMMON RESEARCH MODEL
M. Sidoryuk, Central Aerohydrodynamic Institute (TsAGI) , Russia
11.2UAV Conflict Avoidance 1
Chair(s): Sabatini, R., Goraj, Z.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 20 14:00 14:30 11.2.1 IMPLEMENTATION OF VELOCITY OBSTACLE METHOD ON A QUADROTOR UNMANNED AERIAL VEHICLE FOR DYNAMIC CONFLICT AVOIDANCE
Y.I. Jenie, FTMD - Institut Teknologi Bandung, Indonesia
15. Sep 20 14:30 15:00 11.2.2 MPC BASED PARTIAL TRAJECTORY PLANNING FOR MULTIROTOR WITH POINT CLOUD OBSTACLES
H. Ahn, KAIST, South Korea
15. Sep 20 15:00 15:30 11.2.3 VELOCITY OBSTACLE METHOD IN OPTICAL FLOW FRAMEWORK FOR AUTOMATIC CONFLICT DETECTION AND RESOLUTION IN UAVS
Y.I. Jenie, Faculty of Mechanical and Aerospace Engineering, ITB, Indonesia
Reserve Paper 11.2.R MOTHERSHIP PLANE WITH SENSING DRONES SYSTEM FOR 3D MAPPING APPLICATIONS
M.J. Modzelewski, Warsaw University of Technology, Poland
12.2Dynamics and Noise
Chair(s): Jokinen, J., Bayandor, J.
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
15. Sep 20 14:00 14:30 12.2.1 THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE
P-H Hou, Shenyang Aeroengine Research Institute, China
15. Sep 20 14:30 15:00 12.2.2 DYNAMIC RESPONSE AND DAMAGE OF THE FAN BLADES DURING UAV INGESTION INTO AN AERO-ENGINE
N.D Hou, China
15. Sep 20 15:00 15:30 12.2.3 EXPERIMENTAL AND NUMERICAL STUDY ON BALLISTIC IMPACT OF ARAMID FABRIC
H. Pei, China
Reserve Paper 12.2.R ANALYSIS OF THE DYNAMIC RESPONSE AND FAILURE OF FABRIC SUBJECTED TO BLAST LOADING
J.C Jiang, Civil Aviation University of China, China
13.2Systems & Components Safety
Chair(s): ,
Track 13
10 - Safety and Security
15. Sep 20 14:00 14:30 13.2.1 AIRCRAFT INFLIGHT ICING DETECTION AND DIAGNOSIS METHODS
D. D. Ding, China Aerodynamics Research and Development Center, China
15. Sep 20 14:30 15:00 13.2.2 DESIGN AND RESEARCH ON SAFETY ANALYSIS TOOL FOR AVIONICS SYSTEM
Yu Liu, Shanghai Aircraft Design and Research Institute, China
15. Sep 20 15:00 15:30 13.2.3 A PROTOTYPE WHIRL TOWER FOR TESTING INSOLATED ROTOR SYSTEMS IN HOVER
M. Wojtas, ?ukasiewicz Research Network - Institute of Aviation, Poland
Reserve Paper 13.2.R EXPERIMENTAL STUDY ON CRITICAL HEAT FLUX CHARACTERISTICS OF R134A FOLW BOILING IN HORIZONTAL 2.1MM TUBE UNDER HYPERGRAVI
H.JJ Jianjun, Nanjing engineering Institute of Aircraft System, Jincheng, AVIC, China

15:30 - 16:00Break

1.3Design Optimization under Uncertainty
Chair(s): Padulo, M.
Track 1
01 - Aircraft Design and Integrated Systems
15. Sep 20 16:00 16:30 1.3.1 ON ROBUST MULTI DISCIPLINARY ANALYSIS AND OPTIMISATION FOR NEW GENERATION FLEXIBLE AIRCRAFT
M. Saporito, University of Southampton, United Kingdom
15. Sep 20 16:30 17:00 1.3.2 APPLICATION OF ARTIFICIAL NEURAL NETWORKS FOR EFFICIENT RELIABILITY-BASED DESIGN OPTIMIZATION
X. Chen, Cranfield University, United Kingdom
15. Sep 20 17:00 17:30 1.3.3 VALIDATING SURROGATE MODELS AND ICORPORATING UNCERTAINTY QUANTIFICATION IN MULTI-ELEMENTS AIRFOIL DESIGN OPTIMISATION
C. Bolart, Cranfield University, United Kingdom
15. Sep 20 17:30 18:00 1.3.4 A SET-BASED DESIGN APPROACH FOR EVOLVABILITY EXPLORATION
A.S.J. van Heerden, Cranfield University, United Kingdom
Reserve Paper 1.3.R EFFICIENT ADAPTIVE SURROGATE-BASED OPTIMIZATION USING FUZZY CLUSTERING FOR COMPLEX SYSTEM OPTIMIZATIONS
C.-N. Li, Northwestern Polytechnical University, China
2.3Hypersonics
Chair(s): Kimmel, B.
Track 2
01 - Aircraft Design and Integrated Systems
15. Sep 20 16:00 16:30 2.3.1 H2020 STRATOFLY PROJECT FROM EUROPE TO AUSTRALIA IN LESS THAN 3 HOURS
N. Viola, Politecnico di Torino, Italy
15. Sep 20 16:30 17:00 2.3.2 THERMAL PROTECTION SYSTEM PRELIMINARY DESIGN OF STRATOFLY HIGH-SPEED PROPELLED VEHICLE
R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy
15. Sep 20 17:00 17:30 2.3.3 HEXAFLY-INT HYPERSONIC VEHICLE THERMAL PROTECTION SYSTEM DESIGN
R. SCIGLIANO, Italian Aerospace Research Centre (CIRA), Italy
15. Sep 20 17:30 18:00 2.3.4 AERODYNAMIC DESIGN THEORY AND METHODOLOGY FOR AN AIRFRAME-INLET INTEGRATED FULL-WAVERIDER VEHICLE
F. D. Ding, National University of Defense Technology, China
Reserve Paper 2.3.R NOVEL OSCULATING AXISYMMETRIC DESIGN METHOD FOR A HYPERSONIC WAVERIDER VEHICLE DERIVED FROM A POINTED VON KARMAN OGIVE
F. D. Ding, National University of Defense Technology, China
3.3Digital Pioneering - Where will MDO, MBSE, Digital Twins and AI bring engineering in 20 years?
Chair(s): ,
Track 3
4.3Turbulence Modeling
Chair(s): Bigarella, E., Wolf, W.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
15. Sep 20 16:00 16:30 4.3.1 ON THE ASSESSMENT OF TURBULENCE MODELS FOR THE SIMULATION OF VORTICAL FLOWS
R. C. Gonzalez, Cranfield Unversity, United Kingdom; S. A. Prince, Cranfield University, United Kingdom
15. Sep 20 16:30 17:00 4.3.2 COMPARISON OF DIFFERENT TURBULENCE MODELS FOR PREDICTING IMPINGING JET FLOWS
X.C Cai¹, W Dong¹; ¹Shanghai Jiao Tong University, China
15. Sep 20 17:00 17:30 4.3.3 RESEARCH OF TURBULENCE MODELING BASED ON MACHINE LEARNING
Y. Y. Yin, Tsinghua University, China
15. Sep 20 17:30 18:00 4.3.4 RESEARCH ON MACHINE LEARNING RECONSTRUCTION OF TURBULENCE MODEL DRIVEN BY EXPERIMENTAL DATA
Y.-F. Wang, BUAA, China
Reserve Paper 4.3.R TURBULENCE MODEL ASSESSMENT OF THE SEPARATED FLOW IN THE STANFORD DIFFUSER
M. Bonnici¹, S. A. Prince¹, K. P. Garry¹; ¹Cranfield University, United Kingdom
5.3Turbomechanics
Chair(s): Hui, D., Heng, L.
Track 5
03.2 - Experimental Aerodynamics
15. Sep 20 16:00 16:30 5.3.1 EXPERIMENT AND THEORETICAL ANALYSIS OF A TYPE OF NON-SYNCHRONOUS VIBRATION IN A HIGH PRESSURE COMPRESSOR
GAO Fei-Long, Shenyang Engine Research Institute, China
15. Sep 20 16:30 17:00 5.3.2 COMMISSIONING A NEW VIGV WIND TUNNEL
R.G. Frank, Institute of Jet Propulsion, Bundeswehr University Munich, Germany
15. Sep 20 17:00 17:30 5.3.3 TSAGI’S EXPERIENCE IN THE DEVELOPMENT OF SIX-COMPONENT ROTATING SHAFT BALANCES
V.S. Manvelyan, Central Aerohydrodynamic Institute (TsAGI), Russia
15. Sep 20 17:30 18:00 5.3.4 JET FLAME RESEARCH BASED ON PHOSPHORESCENT IMAGING TECHNIQUE AND HILBERT-HUANG TRANSFORM METHOD
P Tian, Shanghai Jiao Tong University, China
Reserve Paper 5.3.R MEASUREMENT AND ANALYSIS OF INTER-STAGE FLOW FIELD IN A HIGH-LOAD AXIAL MULTISTAGE COMPRESSOR
Z.-Z. Zhang, AECC Shenyang Engine Research Institute, China
6.3Flow Control Applications 1
Chair(s): Gowree, E., Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
15. Sep 20 16:00 16:30 6.3.1 HYBRID LAMINAR FLOW CONTROL (HLFC) RESEARCH AT AIRCRAFT RESEARCH ASSOCIATION (ARA), PAST, PRESENT AND FUTURE
P.W.C. Wong, Aircraft Research Association, United Kingdom
15. Sep 20 16:30 17:00 6.3.2 INVESTIGATION OF LAMINARIZATION EFFICIENCY OF THE SECTIONED SUCTION SYSTEM ON THE SWEPT WING IN FAILURE CASE
S.N. Tolkachev, Central Aerohydrodynamic Institute (TsAGI), Russia
15. Sep 20 17:00 17:30 6.3.3 ENERGY HARVESTING FROM PIEZOELECTRIC FRINGES AT THE TRAILING EDGE OF A FINITE WING WITH LEADING-EDGE TUBERCLES
M. Melo de Sousa, Instituto Superior Tecnico, Portugal
15. Sep 20 17:30 18:00 6.3.4 HIGH-LIFT NOISE REDUCTION USING PLASMA ACTUATORS
G. P. G. Silva, University of Sao Paulo, Brazil
Reserve Paper 6.3.R INVESTIGATION OF ROLL ATTENUATION MECHANISM OF LOW-ASPECT-RATIO WINGS USING BIONIC FLOW CONTROL APPROACHES
T. Hu, Beihang University, China
7.3Flapping Wing/MAV
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
15. Sep 20 16:00 16:30 7.3.1 INVESTIGATION AERODYNAMICS FLAPPING FLIGHT ROBOTIC BIRD
H.W.M. Hoeijmakers, University of Twente, Netherlands
15. Sep 20 16:30 17:00 7.3.2 DEFORMATION AND FLOWFIELD INVESTIGATION OF A FLAPING-WING MAV IN GROUND EFFECT
J WANG, Northwestern Polytechnical University, China
15. Sep 20 17:00 17:30 7.3.3 EFFECTS OF SPANWISE AREA DISTRIBUTION ON AERODYNAMIC PERFORMANCE OF FLAPPING WINGS IN HOVER
Z CAO, Northwestern Polytechnical University, China
15. Sep 20 17:30 18:00 7.3.4 THE INFLUENCE OF SWEEPING MOTION ON THREE-DIMENSIONAL FLOW PATTERNS AND AERODYNAMIC PERFORMANCE OF FLAPPING WINGS
T.-W. Wu, Northwestern Polytechnical University, China
Reserve Paper 7.3.R NEURAL MODEL OF FIXED WINGS MICRO AERIAL VEHICLE AERODYNAMICS
K.-S. Sibilski, Warsaw University of Technology, Poland
Reserve Paper 7.3.R NUMERICAL SIMULATION OF SPANWISE FOLDING EFFECTS ON A BIRD-SCALE FLAPPING WING
X.Y. Lang, School of Aeronautics, Northwestern Polytechnical University, China
Reserve Paper 7.3.R BIO-INSPIRED AERODYNAMIC OPTIMISATION OF BLUFF-BODIES
E.R.G Gowree, ISAE-SUPAERO, France
8.3Buckling and Instability
Chair(s): Juracka, J., Cestino, E.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
15. Sep 20 16:00 16:30 8.3.1 ACHIEVEMENTS IN THE BUCKLING OF THIN-WALLED COMPOSITE LAUNCHER STRUCTURES
RD Degenhardt, DLR, Germany
15. Sep 20 16:30 17:00 8.3.2 THE VIBRATION CORRELATION TECHNIQUE – A RELIABLE NONDESTRUCTIVE METHOD TO PREDICTBUCKLING LOADS
- Abramovich, Technion, I.I.T.,, Israel
15. Sep 20 17:00 17:30 8.3.3 INVESTIGATION OF BUCKLING RESPONSE OF CYLINDRICAL SHELLS USING 3D-PRINTING TECHNOLOGY
C. Bisagni, Delft University of Technology, Netherlands
15. Sep 20 17:30 18:00 8.3.4 KINEMATIC MODEL OF REFINED THEORY AND EXACT ANALYTICAL SOLUTIONS OF STATIC AND BUCKLING PROBLEMS OF STRUCTURALLY-ANISOTR
L M Liubov, Moscow Aviation Institute (NRU), Russia
Reserve Paper 8.3.R OPTIMIZATION AND STRENGTH TESTS OF COMPRESSED COMPOSITE TUBE AS A MAIN ELEMENT OF MECHANICAL FLIGHT CONTROL SYSTEM.
W. Grendysa, Warsaw University of Technology, Poland
9.3Transition Physics 1
Chair(s): Atkin, C., Sousa, J.
Track 9
03.3 - Basic Fluid Dynamics and Flow Control
15. Sep 20 16:00 16:30 9.3.1 EVOLUTION OF TOLLMIEN-SCHLICHTING DISTURBANCES OVER NATURALLY DISTRIBUTED ROUGH SURFACES
S. Mughal, Imperial College London, United Kingdom
15. Sep 20 16:30 17:00 9.3.2 VIBRATION INDUCED EXCITATION AND CONTROL OF TOLLMIEN-SCHLICHTING WAVES
E.R.G Gowree, ISAE-SUPAERO, France
15. Sep 20 17:00 17:30 9.3.3 NON-LINEAR BOUNDARY LAYER RECEPTIVITY TO FREE-STREAM TURBULENCE
D. Sboev, Central Aerohydrodynamic Institute (TsAGI), Russia
15. Sep 20 17:30 18:00 9.3.4 STABILITY ANALYSIS OF STREAMWISE CORNER FLOW
D Xu, Tsinghua University, China
10.3Decoupling Control
Chair(s): Wang, Q.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
15. Sep 20 16:00 16:30 10.3.1 LANDING PERFORMANCE OF BOX-WING AIRCRAFT USING DIRECT LIFT CONTROL IN TURBULENT ATMOSPHERE
C. Varriale, Delft University of Technology, Netherlands
15. Sep 20 16:30 17:00 10.3.2 DECISION-MAKING MODELLING: APPLICATION TO APPROACH PHASE IN AUTONOMOUS AIR TO AIR REFUELLING
I Romo, Airbus, Spain
15. Sep 20 17:00 17:30 10.3.3 ADVANCED REFUELING BOOM SYSTEM (ARBS) AUTOMATIC AIR TO AIR REFUELING FLIGHT CONTROL LAWS
A. Sanz de Blas, Airbus Defence & Space, Spain
15. Sep 20 17:30 18:00 10.3.4 DECOUPLING CONTROL LAW DESIGN FOR AN OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING
L Qiu, Chinese Flight Test Establishment, China
Reserve Paper 10.3.R GAIN SCHEDULING BY FREQUENCY SHAPED LINEAR QUADRATIC CONTROL OF FIXED-WING AIRCRAFT LONGITUDINAL MOTION.
L.S. Kim, Korea Advanced Institute of Science and Technology, South Korea
11.3UAV Dynamics and Control 2
Chair(s): Bai, J., Krus, P.
Track 11
06.2 - Flight Dynamics and Control (UAV related)
15. Sep 20 16:00 16:30 11.3.1 A VARIABLE-FIDELITY METHOD FOR UNMANNED AIRCRAFT WAKE VORTEX SAFETY AND CONTROL ANALYSIS
V. Golubev, ERAU, United States
15. Sep 20 16:30 17:00 11.3.2 MULTIROTOR VEHICLES DESIGN BASED ON DYNAMIC MANIPULABILITY FOR UNDERACTUATED FLYING SYSTEMS
S. Hokamoto, Kyushu Univ., Japan
15. Sep 20 17:00 17:30 11.3.3 LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV
S Ishioka, Nihon university, Japan
15. Sep 20 17:30 18:00 11.3.4 MPPC OF MULTICOPTER WITH FAULT ROTOR IN COLLISION SITUATION
Y Shimizu, Univerisity of Tokyo, Japan
Reserve Paper 11.3.R AUTONOMOUS CONTROL OF FIXED-WING UNMANNED AERIAL SYSTEMS(UASS) BY REINFORCEMENT LEARNING
H. Wang, AVIC Xi'an Flight Automatic Control Research Institute, China
12.3Fatigue Assessment
Chair(s): van Doeselaar, J., Blom, A.
Track 12
04.1 - Material Issues, Fatigue and Damage Tolerance
15. Sep 20 16:00 16:30 12.3.1 TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES
I. Rivero Arevalo, Airbus, Spain
15. Sep 20 16:30 17:00 12.3.2 STUDY OF COMPOSITE SKIN-STRINGER FATIGUE BEHAVIOR UNDER BROADBAND RANDOM VIBRATION
F. Sevastyanov, The Central Aerohydrodynamic Institute named after N.E.Zhukovsky, Russia
15. Sep 20 17:00 17:30 12.3.3 APPROACH OF THE STATIC AND FATIGUE STRENGTH ESTIMATION OF THE COMPOSITE JOINTS
A.A. Sviridov, The Central Aerohydrodynamic Institute, Russia
15. Sep 20 17:30 18:00 12.3.4 FAILURE CRITERION OF CFRP FOR OPEN-HOLE FATIGUE TESTING
A.G. Kalinin, TsAGI, Russia
Reserve Paper 12.3.R MODEL CURVES: A SIMPLE WAY TO ACCOUNT FOR COMPLEX EFFECTS
A.A. Bautin, TsAGI, Russia
13.3Safety and Security Analysis
Chair(s): ,
Track 13
10 - Safety and Security
15. Sep 20 16:00 16:30 13.3.1 RESEARCH ON SAFETY ASSESSMENT APPROACH FOR UAS OPERATIONS OVER UNINHABITED AREAS
ZQ Zhang, Northwestern Polytechnical University, China
15. Sep 20 16:30 17:00 13.3.2 END TO END CYBERSECURITY IN CIVIL AVIATION ECO SYSTEM
JC Jean-Claude, Airbus, France
15. Sep 20 17:00 17:30 13.3.3 STUDY ON DYNAMIC RESPONSE AND INJURY OF FRONT ROW OCCUPANT UNDER HORIZONTAL IMPACT
M.S.C. MA, Civil Aviation University of China, China
15. Sep 20 17:30 18:00 13.3.4 STATISTICAL ANALYSIS OF AIRCRAFT INCIDENTS M-28 BRYZA
J. Tomaszewska, Polish Air Force University, Poland
Reserve Paper 13.3.R FIRE AND EXPLOSION ANALYSIS OF AIRCRAFT FUEL TANK BASED ON TNT EQUIVALENT METHOD AND FIREBALL EXPLOSION MODEL
W K KAI, AVIC XI'AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD, China