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.

Wednesday, 16. Sep 2020


7:30-8:00 Briefing for presenters and chairpersons in each day at each presentation room
0.1General Lecture 3 - Trends in Aircraft Propulsion: Reflections on ISABE 2019
Chair: Ric Parker President ISABE
16. Sep 20 08:00 09:00
Ric Parker, President ISABE

09:00 - 09:30Break

1.1Design Methods
Chair(s): Cestino, E.
Track 1
01 - Aircraft Design and Integrated Systems
16. Sep 20 09:30 10:00 1.1.1 IMPACT OF NEW TECHNOLOGIES ON AIRCRAFT SYSTEMS
A. Berres, German Aerospace Center, Germany
16. Sep 20 10:00 10:30 1.1.2 APPLICATIONS OF FAST: AN OPEN SOURCE TOOL FOR AIRCRAFT CONCEPTUAL AND PRELIMINARY DESIGN
S. M. Delbecq, ISAE-SUPAERO, France
16. Sep 20 10:30 11:00 1.1.3 MICLADO – LAMINAR AIRCRAFT DESIGN WITH MICADO
F. Schueltke, RWTH Aachen University, Institute of Aerospace Systems, Germany
16. Sep 20 11:00 11:30 1.1.4 LAMBDA: A KNOWLEDGE-BASED MODULAR, MULTIFIDELITY AND MULTIDISCIPLINARY AIRCRAFT CONCEPTUAL DESIGN ENVIRONMENT
S. Hosseini, Amirkabir University of Technology, Iran
16. Sep 20 11:30 12:00 1.1.5 IMPROVED LINEAR METHOD FOR SONIC BOOM PREDICTION OF SUPERSONIC TRANSPORTS
Y.-L. Ding, Northwestern Polytechnical University, China
Reserve Paper 1.1.R AERODYNAMIC SHAPE OPTIMIZATION PLATFORM ASSISTED WITH SURROOPT AND CPACS TECHNIQUE
C.-Y. Ma, Northwestern Polytechnical University, China
2.1UAS 1
Chair(s): Gerhards, R.
Track 2
01 - Aircraft Design and Integrated Systems
16. Sep 20 09:30 10:00 2.1.1 MULTIDISCIPLINARY OPTIMISATION OF A FUEL-CELL-POWERED EVTOL FIXED-WING CARGO UAV
D. Verstraete, The University of Sydney, Australia
16. Sep 20 10:00 10:30 2.1.2 CONCEPTUAL DESIGN FOR LONG-ENDURANCE CONVERTIBLE UNMANNED AERIAL SYSTEM
Y Leng, ISAE, France
16. Sep 20 10:30 11:00 2.1.3 DESIGN OF A HYBRID-POWER VTOL LOGISTICS UAV SYSTEM INTEGRATED INTO THE CIVIL AVIATION AIR TRAFFIC MANAGEMENT SYSTEM
H.-J. Jiang, Xi'an Tangyan Aviation Technology CO. LTD, China
16. Sep 20 11:00 11:30 2.1.4 SURROGATE-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION OF MULTIROTOR DRONES
S. M. Delbecq, ISAE-SUPAERO, France
16. Sep 20 11:30 12:00 2.1.5 AERODYNAMIC ANALYSIS ON TAIL-SITTER UAV HOVERING UNDER CROSSWIND
Chen Jiaojiao Jiaojiao, Northwestern Polytechnical University, China
Reserve Paper 2.1.R LIGHTWEIGHT UAV FOR EMERGENCY MEDICAL SERVICE
T. Goetzendorf-Grabowski, Warsaw University of Technology, Poland
Reserve Paper 2.1.R CONCEPTUAL DESIGN AND IMPLEMENTATION OF A NOVEL TRICOPTER FIXED-WING VTOL UAV CONFIGURATION
P. Stahl, Technical University of Munich, Germany
3.1Model Based Systems Engineering
Chair(s): Vijgen, P., Müller Wiesner, D.
Track 3
02 - Systems Engineering and Integration
16. Sep 20 09:30 10:00 3.1.1 MODEL-BASED ENGINEERING OF A SYSTEM DIAGNOSTIC ENGINE FOR AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
F. Mardt, Hamburg University of Technology, Germany
16. Sep 20 10:00 10:30 3.1.2 A MBSE DESIGN ARCHITECTURE FOR CONTROL SYSTEM BASED ON DEMAND ELEMENT TRANSFER
P.J. Wang, Tsinghua University, China
16. Sep 20 10:30 11:00 3.1.3 A DOCUMENT-BASED VS. MODEL-BASED APPLICATION OF THE NASA SYSTEMS ENGINEERING PROCESS
L. Boggero, German Aerospace Center (DLR), Germany
16. Sep 20 11:00 11:30 3.1.4 TOWARDS THE NEXT GENERATION OF COMPLEX SYSTEMS ARCHITECTING: A MBSE FRAMEWORK TO AIRCRAFT DEVELOPMENT
P. D. Ciampa, DLR, Germany
16. Sep 20 11:30 12:00 3.1.5 HYBRID MODELLING FOR FULL MISSION SIMULATION
P Krus, Linköping university, Sweden
Reserve Paper 3.1.R MODEL-BASED STAKEHOLDER REQUIREMENTS DEFINITION FOR JOINT MISSION PLANNING SYSTEM
D.-Z. Du, Aviation Industry Development Research Center of China, China
Reserve Paper 3.1.R SOS BEHAVIOR MODEL TRANSFORMATION FOR AIRCRAFT TOP-LEVEL DEMONSTRATION
J Zang, Aviation Industry Development Research Center of China, China
4.1Applied CFD 1
Chair(s): Wei, S., Azevedo, J.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
16. Sep 20 09:30 10:00 4.1.1 EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION
L. P. Ruiz Calavera, Airbus Defence & Space, Spain
16. Sep 20 10:00 10:30 4.1.2 FLOW STRUCTURE INVESTIGATION OF CONTRA-ROTATING WIND TURBINES BY CFD AND EXPERIMENTAL METHODS
K You, Northwestern Polytechnical University, China
16. Sep 20 10:30 11:00 4.1.3 STATIC AEROELASTIC COMPUTATIONS OF WING CONFIGURATIONS IN TRANSONIC FLOWS AT HIGH REYNOLDS NUMBERS
J. A. A. Lyrio, Instituto Tecnológico de Aeronáutica, Brazil
16. Sep 20 11:00 11:30 4.1.4 NUMERICAL INVESTIGATION OF WING ROCK PHENOMENON ON LOW ASPECT RATIO RECTANGULAR WINGS AT LOW REYNOLDS NUMBER
N/A Maqsood, Pakistan
16. Sep 20 11:30 12:00 4.1.5 A COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF A HISTORICAL SEAPLANE CRUISE AND TAKE OFF PERFORMANCE
E. Cestino, Politecnico di Torino, Italy
Reserve Paper 4.1.R ADVANCED AIRCRAFT FIRE EXTINGUISHING NUMERICAL SIMULATION
Y. SOMMERER, AIRBUS, France
Reserve Paper 4.1.R FLUID STRUCTURE INTERACTION OF RAM-AIR PARACHUTE TRAILING EDGE DEFLECTION
Gao XL Gao, China Aerodynamics Research and Development Center, China
5.1Transonic/Supersonic
Chair(s): Prince, S., Dehua, C.
Track 5
03.2 - Experimental Aerodynamics
16. Sep 20 09:30 10:00 5.1.1 NEW INVESTIGATION METHOD OF THE SHOCK WAVE/BOUNDARY LAYER INTERACTION PATTERN AT TRANSONIC SPEEDS
M.A. Brutyan, TsAGI, Russia
16. Sep 20 10:00 10:30 5.1.2 INFLUENCE OF VARIABLE WALL PERFORATION RATIO ON BOUNDARY LAYER PARAMETERS AT TRANSONIC SPEEDS
S.L. Osipova, Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia
16. Sep 20 10:30 11:00 5.1.3 RESEARCH OF HYBRID LAMINAR FLOW CONTROL TECHNOLOGY FOR CIVIL AIRCRAFT WING
C. Shao, Shanghai Aircraft Design and Research Institute, COMAC, China
16. Sep 20 11:00 11:30 5.1.4 STUDY OF SHOCK WAVE / LAMINAR BOUNDARY LAYER INTERACTION AREA BY PIV TECHNIQUE
Oleg: O. Vishnyakov, Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia
16. Sep 20 11:30 12:00 5.1.5 DEVELOPMENT OF THE MODEL NEAR-FIELD STUDY TECHNIQUES INTHE SUPERSONIC WIND TUNNELS AIMED AT THE SONIC BOOM PREDICTION
A.I. IVANOV, TSAGI, Russia
Reserve Paper 5.1.R THE EXPERIMENTAL INVESTIGATION OF THE THROTTLING SECOND THROAT INFLUENCE ON TRANSONIC WIND TUNNEL FLOW QUALITY
Z HaiYang, China Aerodynamics Research and Development Center, Facility des, China
6.1Unsteady Flow Phenomena
Chair(s): Breitsamter, C., Wong, P.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
16. Sep 20 09:30 10:00 6.1.1 INVESTIGATIONS OF AERODYNAMIC CHARACTERISTICS AND LAMINAR-TURBULENT TRANSITION ON LARGE-SCALE TRANSONIC AIRFOIL
V.G. Soudakov, TsAGI, Russia
16. Sep 20 10:00 10:30 6.1.2 TYPES OF TRANSONIC BUFFET FOR A LAMINAR AIRFOILS
P.A. Polivanov, Khristianovich Institute of Theoretical and Applied Mechanics SB, Russia
16. Sep 20 10:30 11:00 6.1.3 BUFFET CONTROL ON STRUCT-BRACED WING AIRCRAFT USING TANGENTIAL BLOWING
S Li, School of Aerospace Engineering, Tsinghua University, China
16. Sep 20 11:00 11:30 6.1.4 HIGH-FIDELITY ANALYSIS OF ROBUST NONLINEAR 2-DOF AIRFOIL LCO CONTROL
V. Golubev, ERAU, United States
16. Sep 20 11:30 12:00 6.1.5 ANALYSIS AND CONTROL OF DYNAMIC STALL CHARACTERISTICS OF S809 AIRFOIL
L-S Hao, Northwestern Polytechnical University, China
Reserve Paper 6.1.R NUMERICAL STUDY ON HIGH-FREQUENCY RESPONSE OF WALL JETS FOR GUST LOAD CONTROL
X. C. Xue, Nanjing University of Aeronautics and Astronautics, China
Reserve Paper 6.1.R PHISICAL AND MATHEMATICAL MODELS OF THE BUFFET ONSET
A.M. Lipanov, Institute of Applied Mathematics, Russia
7.1Optimization 1
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
16. Sep 20 09:30 10:00 7.1.1 SPARSE POLYNOMIAL CHAOS EXPANSION BASED ON FULLY ADAPTIVE FORWARD-BACKWARD SELECTION METHOD
Huan Zhao, China
16. Sep 20 10:00 10:30 7.1.2 ON IMPROVING GRADIENT-ENHANCED KRIGING MODEL FOR AERODYNAMIC DESIGN OPTIMIZATION
D.H.D. Dang, Northwestern Polytechnical University, China
16. Sep 20 10:30 11:00 7.1.3 FAR-FIELD WAVEFORM DESIGN OPTIMIZATION BASED ON SONIC BOOM NOISE LEVEL
J.-L. Qiao, Northwestern Polytechnical University, China
16. Sep 20 11:00 11:30 7.1.4 PREDICTION OF FLIGHT DYNAMICS IN WAKE SURFING SCENARIOS
MML Lone, Cranfield University, United Kingdom
16. Sep 20 11:30 12:00 7.1.5 IMPROVED WEIGHTED GRADIENT-ENHANCED KRIGING MODEL FOR HIGH-DIMENSIONAL AERODYNAMIC DESIGN OPTIMIZATION PROBLEMS
C.-Z. Xu, China
Reserve Paper 7.1.R AERODYNAMIC EVALUATION OF FORWARD-SWEPT AND SWEPTBACK WING WITH OPTIMIZED PLANEFORMS
Sei-ichiro Morizawa, National Institute of Technology, Okinawa College, Japan
Reserve Paper 7.1.R AERODYNAMIC DESIGN OPTIMIZATION OF WAVERIDER-DERIVED VEHICLE
W. Su, Beijing Institute of Space Long March Vehicle, China
8.1Design of Aircraft Structures
Chair(s): Cestino, E., Alaimo, A.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
16. Sep 20 09:30 10:00 8.1.1 AN INVERSE APPROACH BASED ON EUCLIDEAN SPACE FOR DETERMINING STRUCTURAL LOAD DISTRIBUTION FROM STRAIN MEASUREMENTS
H.N. Dui, AVIC, Chengdu Aircraft Design & Research Institute, China
16. Sep 20 10:00 10:30 8.1.2 DESIGN OF EXPERIMENTS TECHNIQUES TO INVESTIGATE LOAD SHARE STRATEGIES BETWEEN AERO ENGINE, NACELLE AND POWERPLANT COMPONENTS
C.-M MARTIN , Queens University Belfast, United Kingdom
16. Sep 20 10:30 11:00 8.1.3 THERMOPLASTIC APPLICATIONS FOR AEROSTRUCTURES: TOWARDS SUSTAINABLE AND WEIGHT EFFICIENT APPLICATIONS
M HERMAN, Airbus, France
16. Sep 20 11:00 11:30 8.1.4 RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME
A.V. Bezuevsky, TsAGI, Russia
16. Sep 20 11:30 12:00 8.1.5 AIRCRAFT ENGINE ROTOR DYNAMICS ANALYSIS AFTER FAN BLADE-OUT WITH ACCOUNT OF ROTOR-CASING CONTACT INTERACTIONS
V. Myasnikov, Central Institute of Aviation Motors, Russia
Reserve Paper 8.1.R THE METHOD OF AIRCRAFT MATHEMATICAL MODEL STIFFNESS PROPERTIES CORRECTION BASED ON EXPERIMENTAL RESEARCH RESULTS
M.A. Pronin, Central Aerohydrodynamic Institute n.a. prof. N.E.Zhukovsky, Russia
Reserve Paper 8.1.R STRUCTURAL HEALTH MONITORING OF SANDWICH STRUCTURES WITH LATTICE CORES IN AIRCRAFT DESIGN: CHALLENGES AND POTENTIAL
T. Huang, RWTH Aachen University, Germany
9.1Advanced Manufacturing
Chair(s): Rupeng, L.
Track 9
08 - Manufacturing and Supply Chain Management
16. Sep 20 09:30 10:00 9.1.1 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF POST-MACHINING DISTORTION FOR LARGE AEROSPACE MONOLITHIC COMPONENTS
BS SHI, National Research Council Canada, Canada
16. Sep 20 10:00 10:30 9.1.2 RESEARCH ON THE DEVELOPMENT AND PERFORMANCE OF THE OBSTACLE-PASSING STRUCTURE OF THE CRAWLER INSPECTION ROBOT
Pu Zhang¹, Jin Sun¹; ¹Beihang University, China
16. Sep 20 10:30 11:00 9.1.3 SOFTWARE-BASED IMPROVING THE QUALITY OF HIGH-SPEED MACHINING
S. Zietarski, Military University of Technology, Poland
16. Sep 20 11:00 11:30 9.1.4 RESEARCH ON MANUFACTURING PROCESS AND MICROSTRUCTURE OF SIC/ALSI7MG COMPOSITE FABRICATED BY SELECTIVE LASER MELTING
H Zhu, China
16. Sep 20 11:30 12:00 9.1.5 EXPERIMENTAL STUDY ON PATH PLANNING OF BELT GRINDING FOR BIOMIMETIC SURFACE ON AERO-ENGINE BLADE
Chongqing Univer Xiao, China
Reserve Paper 9.1.R AUTOMATIC DETECTION TECHNOLOGYOF LARGE CIVIL AIRCRAFT BASED ON IMAGE RECOGNITION
T.-L. SHEN, China
Reserve Paper 9.1.R ???????????????????????????
M.B.L ??, ????????, China
Reserve Paper 9.1.R RESEARCH ON SOLVING PROBLEM OF AIRCRAFT ASSEMBLY COORDINATION BASED ON 3D LASER SCANNING MEASUREMENT TECHNOLOGY
W J JIAN, China
10.1Flight Dynamics
Chair(s): Götzendorf Grabowski, T.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 20 09:30 10:00 10.1.1 VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL
B.W. NIE, National University of Defense Technology, China
16. Sep 20 10:00 10:30 10.1.2 INVESTIGATION INTO FLIGHT DYNAMICS OF A BLENDED-WING-BODY AIRCRAFT
F. CEN, China
16. Sep 20 10:30 11:00 10.1.3 BAYESIAN APPROACH TO SIMULTANEOUS STATIC AND DYNAMIC FLIGHT CHARACTERISTICS MODELING
M. Naruoka, Japan Aerospace Exploration Agency, Japan
16. Sep 20 11:00 11:30 10.1.4 THE ANALYSIS OF TAKEOFF ROTATION OF SUBSCALE FREE-FLIGHT TESTS
K.-M. MA, Xi’an Aircraft Design Institute, China
16. Sep 20 11:30 12:00 10.1.5 SIMULTANEOUS ESTIMATION OF DERIVATIVES, TRIM STATES, AND WIND
Yoshimasa: Y. Ochi, National Defense Academy, Japan
Reserve Paper 10.1.R IDENTIFICATION OF AIRCRAFT MODEL CONSIDERING FREQUENCY CHARACTERISTICS OF MAXIMAL LENGTH SEQUENCE INPUT
A. Fujimori, University of Yamanashi, Japan
Reserve Paper 10.1.R SEPARATE IDENTIFICATION OF AIRCRAFT THRUST AND DRAG FORCES THROUGH FLIGHT TEST DATA
O. N. Korsun, Moscow Aviation Institute (National Research University), Russia
11.1Actuator design & Analysis
Chair(s): Mare, J., Fu, Y.
Track 11
07 - Systems, Subsystems and Equipment
16. Sep 20 09:30 10:00 11.1.1 LIEBHERR-AEROSPACE EHA TECHNOLOGY FOR FUTURE FLIGHT CONTROL APPLICATION
T. Röben, Liebherr-Aerospace, Germany
16. Sep 20 10:00 10:30 11.1.2 THE DEVELOPMENT OF ALGORITHMS FOR EMA FAULT EARLY DETECTION SYSTEM
A.V. Skryabin, 1. Central Aerohydrodynamic Institute of Russia, Russia
16. Sep 20 10:30 11:00 11.1.3 CONCEPTUAL STUDY OF THE DIGITAL HYDRAULIC ACTUATOR WITH PROPORTIONAL CONTROL FOR FLIGHT CONTROL ACTUATION SYSTEMS
A. Dell'Amico, Saab AB, Sweden
16. Sep 20 11:00 11:30 11.1.4 VIRTUAL PROTOTYPING OF ELECTRICAL THS ACTUATOR FOCUSED ON MECHANICAL POWER TRANSMISSION FUNCTIONS
J. FU FU, BEIHANG UNIVERSITY, China
16. Sep 20 11:30 12:00 11.1.5 DYNAMIC ANALYSIS AND CONTROL DESIGN OF A FAULT-TOLERANT ELECTRO-MECHANICAL ACTUATOR WITH DIFFERENTIAL BALL SCREWS
G. Di Rito, Università di Pisa - Dipartimento di Ing. Civile ed Industriale, Italy; N. Borgarelli¹, M. Nardeschi¹, B. Luciano, AESIS s.r.l., Italy; ¹Umbra Group S.p.A., Italy
Reserve Paper 11.1.R DESIGN AND CHARACTERIZATION OF A NOVEL DUAL REDUNDANCY ELECTRO-HYDROSTATIC ACTUATOR SYSTEM
H.-Q. QI, Beihang University, China
Reserve Paper 11.1.R A RESEARCH ON POSITION CONTROL ACTUATORS FOR FIXEDWINGED RESEARCH UAVS
D.T. Teubl, Institute of Aircraft Design TUM, Germany
12.1Air Traffic Efficiency
Chair(s): Nguyen, D.
Track 12
09 - Air Transport System Efficiency
16. Sep 20 09:30 10:00 12.1.1 IMPACT OF ENROUTE TIME-BASED METERING ON EQUITY IN DELAY DISTRIBUTION
A. Andreeva-Mori, JAXA, Japan
16. Sep 20 10:00 10:30 12.1.2 SPATIO-TEMPORALLY CORRELATED WIND MODELING AND PROBABILISTIC TRAJECTORY PREDICTION USING ENSEMBLE WEATHER FORECASTS
Y Matsuno, Japan Aerospace Exploration Agency, Japan
16. Sep 20 10:30 11:00 12.1.3 IMPACT ASSESSMENT OF ENHANCED AIR TRANSPORT CONCEPTS ON AIRLINE OPERATIONAL SCHEDULES
J. Michelmann, Institute of Aircraft Design, Technical University of Munich, Germany
16. Sep 20 11:00 11:30 12.1.4 COGNITIVE HUMAN-MACHINE INTERFACES FOR ENROUTE AIR TRAFFIC FLOW MANAGEMENT
A. Gardi, RMIT University, Australia
16. Sep 20 11:30 12:00 12.1.5 RESEARCH ON TRAJECTORY OPTIMIZATION TECHNOLOGY CONSIDERING METEOROLOGICAL INFORMATION PREDICTION
G.-W Guo, China National Aeronautical Radio Electronics Research Institute, China
Reserve Paper 12.1.R STANDARD TERMINAL AUTOMATION REPLACEMENT SYSTEM ENHANCEMENT 2 - BENEFITS ANALYSIS THROUGH FAST-TIME MODELING
R. Dean, Regulus Group, United States
13.1Fan / Nacelle & Propeller
Chair(s): Pankov, S.
Track 13
05 - Propulsion
16. Sep 20 09:30 10:00 13.1.1 GEARED FANS AND VARIABLE PITCH FANS - NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF THEIR AERODYNAMICS
S.V. Pankov, Central Institute of Aviation Motors (CIAM), Russia
16. Sep 20 10:00 10:30 13.1.2 ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF PROPELLERS AT LOW ADVANCE RATIO USING A WHIRLING ARM
Y.I. Itoh, Iwate university, Japan
16. Sep 20 10:30 11:00 13.1.3 EXPERIMENTAL STUDIES OF SLOT-TYPE CASING TREATMENTS FOR MODEL FANS WITH THE AIM OF AERODYNAMIC AND ACOUSTIC IMPROVEMENTS
V.I. Mileshin, Central Institute of Aviation Motors, Russia
16. Sep 20 11:00 11:30 13.1.4 ANALYSIS OF THRUST-SCALED PROPELLER NOISE AND ITS TRADE-OFF WITH PROPELLER EFFICIENCY
T. Sinnige, Netherlands
16. Sep 20 11:30 12:00 13.1.5 MODELING OF COUNTER-ROTATING LIFT FAN/MAIN ENGINE COMBINED PROPULSION SYSTEM AND LIFT FAN AERODYNAMIC DESIGN
H.-L JIN, AECC Hunan Aviation Powerplant Research Institute, China
Reserve Paper 13.1.R AERODYNAMICS DESIGN, OPTIMIZATION AND FLOW FIELD INVESTIGATION OF A CONTRA-ROTATING PROPFAN AT HIGH FLIGHT MACH NUMBERS
T Wu¹, W Dong¹; ¹Shanghai Jiao Tong University, China
Reserve Paper 13.1.R STUDY OF NON-ROTATING MICROPHONE ARRAY FOR SPINNING DUCT MODE DETECTION
Y. Jiyong, AECC Commercial Aircraft Engine Co., Ltd., China

12:00 - 13:00Lunch

0.2General Lecture 4 - Virtual Aircraft Technology Integration Platform – Results of DLR’s Project VicToria
Chair: Björn Nagel DLR
16. Sep 20 13:00 13:55

1.2Hybrid/Electric & Unconventional Aircraft 2
Chair(s): Melkert, J.
Track 1
01 - Aircraft Design and Integrated Systems
16. Sep 20 14:00 14:30 1.2.1 PRELIMINARY FEASIBILITY STUDY OF A HYBRID TURBOPROP
R. Martínez-Val, Univ. Politécnica Madrid, Spain
16. Sep 20 14:30 15:00 1.2.2 EXPERIMENTAL RESEARCH ON PROPULSION AND AERODYNAMIC CHARACTERISTICS OF A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT
X.-Y. ZHANG, Northwestern Polytechnical University, China
16. Sep 20 15:00 15:30 1.2.3 PROPULSIVE FUSELAGE AIRCRAFT CONCEPT – A SUMMARY OF STRUCTURE ANALYSIS BASED ON CENTRELINE H2020
Z. Goraj, Warsaw University of Technology, Poland
2.2Education & Knowledge Management
Chair(s): Fusaro, R.
Track 2
01 - Aircraft Design and Integrated Systems
16. Sep 20 14:00 14:30 2.2.1 TEAM S55: 1:8 SCALE “REPLICA” OF THE SIAI-MARCHETTI S55X
L. Di Ianni, Politecnico di Torino, Italy
16. Sep 20 14:30 15:00 2.2.2 INTERNATIONAL VIRTUAL COLLABORATION IN UNDERGRADUATE AERONAUTICAL ENGINEERING EDUCATION – CHALLENGES AND EXPERIENCES
J. Abulawi, HAW Hamburg, Germany
16. Sep 20 15:00 15:30 2.2.3 OPEN SCIENCE IN AVIATION RESEARCH: THE INDIVIDUAL ADVANTAGE OF SHARING KNOWLEDGE
M. Spieck, Thelsys GmbH, Germany
3.2UAV Conflict Avoidance 2
Chair(s): Bang, H., Bil, C.
Track 3
06.2 - Flight Dynamics and Control (UAV related)
16. Sep 20 14:00 14:30 3.2.1 A RECURRENT PLANNING STRATEGY FOR UAV PATH IDENTIFICATION IN A DYNAMIC ENVIRONMENT BASED ON BIT-CODED FLIGHT MANOEUVRES
L. BLASI, UNIVERSITA' DELLA CAMPANIA "LUIGI VANVITELLI", Italy
16. Sep 20 14:30 15:00 3.2.2 A NOVEL DETECT-AND-AVOID SYSTEM OF UAS IN URBAN ENVIRONMENT
L.N. Nurhakim, RMIT University, Australia
16. Sep 20 15:00 15:30 3.2.3 AUTONOMOUS CONFLICT RESOLUTION ALGORITHM BASED ON ELLIPTIC GEOMETRY
R.A. Sasongko, Institut Teknologi Bandung, Indonesia
Reserve Paper 3.2.R HYDRO ENVIRONMENTAL MAPPING TOOL USING SWARMS AND MACHINE LEARNING, UAV & USV
R.K.R. Kuntz, Brazil
4.2Numerical Methods 2
Chair(s): Viviani, A., Moura, R.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
16. Sep 20 14:00 14:30 4.2.1 VALIDATION OF A DISCONTINUOUS GALERKIN BASED DES SOLVER IN FLOW PROBLEMS USING HIGH PERFORMANCE COMPUTING
A.V. Wolkov, TsAGI, Russia
16. Sep 20 14:30 15:00 4.2.2 ADVANCED WEEK SOLUTIONS IN FLUID DYNAMICS AND THEIR NUMERICAL COMPUTATIONS WITH AERODYNAMIC HEATING
M.Ja. Ivanov, Central Institute of Aviation Motors, Russia
16. Sep 20 15:00 15:30 4.2.3 A BENCHMARK METHOD FOR PREDICTING OBLIQUE SHOCK STRUCTURE
A. Shi, Northwestern Polytechnical University, China
Reserve Paper 4.2.R ACCURATE SIMULATIONS OF AIRCRAFT WAKE VORTICES WITH HIGH-ORDER NUMERICAL METHOD
S. Bosnyakov, TsAGI, Russia
5.2Rotating Wings
Chair(s): Gowree, E., Rasuo, B.
Track 5
03.2 - Experimental Aerodynamics
16. Sep 20 14:00 14:30 5.2.1 COMPARISON OF ISOLATED AND DUCTED FIXED-PITCH PROPELLERS UNDER NON-AXIAL INFLOW CONDITIONS
M. Cerny, Germany
16. Sep 20 14:30 15:00 5.2.2 INVESTIGATION OF THE CHARACTERISTICS OF THE HELICOPTER MAIN ROTOR WITH ELASTIC MOUNTING BLADES
O.-E. Kirillov, Central Aerohydrodynamic Institute (TsAGI), Russia
16. Sep 20 15:00 15:30 5.2.3 EXPERIMENTAL MEASUREMENTS ON BIOMIMETIC WIND TURBINE BLADES BY P. TOMENTOSA SEED
L.-P Paiva, UFU, Brazil
Reserve Paper 5.2.R EXPERIMENTAL INVESTIGATION OF PULSATION OF THE ROTOR SLIPSTREAM ACTING ON AN ELEVATED HELIPORT
P. Ruchala, Institute of Aviation, Poland
6.2Flow Control Applications 2
Chair(s): Goraj, Z., Prince, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
16. Sep 20 14:00 14:30 6.2.1 IMPROVEMENT OF HELICOPTER PERFORMANCE THROUGH PULSE AIR-JETS BLOWN FROM THE TRAILING EDGE OF MAIN ROTOR BLADES
W.S. STALEWSKI, LUKASIEWICZ RESEARCH NETWORK - INSTITUTE OF AVIATION, Poland
16. Sep 20 14:30 15:00 6.2.2 ENHANED STRAIGHT BLADED VAWT BY RETRACTABLE GURNEY FLAPS
K. Song, Northwestern Polytechnical University, China
16. Sep 20 15:00 15:30 6.2.3 STUDY ON THE EFFECTS OF PROPLET GEOMETRIC PARAMETERS ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLER
B.W Wang, China
Reserve Paper 6.2.R APPLICATION OF A LEADING-EDGE TIP EXTENSION ON DELTA WING WITH WINGLET FOR HIGH LIFT
X.Y. Feng, Northwestern Polytechnical University, China
7.2Optimization 2
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
16. Sep 20 14:00 14:30 7.2.1 AERODYNAMIC OPTIMIZATION DESIGN OF DOUBLE BLUNT ROTOR AIRFOIL WITH LARGE THICKNESS IN FORWARD AND REVERSE FLOW
Y.-M. YAO, China
16. Sep 20 14:30 15:00 7.2.2 PARETO FRONT EXPLORATION USING MANIFOLD LEARNING APPROACH FOR ROTORCRAFT AIRFOILS DESIGN
C.-S. Song, Computational Aerodynamics Institute, China Aerodynamics Researc, China
16. Sep 20 15:00 15:30 7.2.3 MULTI-OBJECTIVE AERODYNAMIC SHAPE OPTIMIZATION OF WIDE-MACH-NUMBER-RANGE WING CONSIDERING LIFT MATCHING
Y Zhang, NORTHWESTERN POLYTECHNICAL UNIVERSITY, China
Reserve Paper 7.2.R DESIGN OPTIMIZATION OF AIRFOILS AT ULTRA-LOW REYNOLDS NUMBERS
J.-H. Xu, Northwestern Polytechnical University, China
8.2Morphing Structures
Chair(s): Franke, F., Abramovich, H.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
16. Sep 20 14:00 14:30 8.2.1 RESEARCH PROGRESS OF DISTRIBUTED OPTICAL FIBER SENSING DEFORMATION MEASUREMENT FOR MORPHING WING
X-Jf Xue, Chinese Aeronautical Establishment, China
16. Sep 20 14:30 15:00 8.2.2 ACTUATION MECHANISM USING SHAPE MEMORY ALLOY WIRES IN SPIRAL ARRANGEMENT
R Tsukamoto, Meijo University, Japan
16. Sep 20 15:00 15:30 8.2.3 MORPHING AIRCRAFT BASED ON SMART MATERIALS AND STRUCTURES
J. Sun, Harbin Institute of Technology, China
9.2Additive Manufacturing
Chair(s): Zhang, J.
Track 9
08 - Manufacturing and Supply Chain Management
16. Sep 20 14:00 14:30 9.2.1 EFFECTS OF COOLANT BUILD DIRECTION ON ADDITIVELY MANUFACTURED FAN-SHAPED COOLING HOLES
Z.-Q QI, AECC HUNAN AVIATION POWERPLANT RESEARCH INSTITUTE, China
16. Sep 20 14:30 15:00 9.2.2 APPLICATION OF ADDITIVE MANUFACTURING TO THE PRODUCTION OF RPAV COMPONENTS
E. Cestino, Politecnico di Torino, Italy
16. Sep 20 15:00 15:30 9.2.3 DESIGNING AERONAUTICAL PARTS FOR ADDITIVE MANUFACTURING – SUPPORTED BY A VIRTUAL DESIGN ADVISOR
J. Abulawi, HAW Hamburg, Germany
Reserve Paper 9.2.R AN EFFICIENT FINITE ELEMENT SIMULATION METHOD FOR ADDITIVE MANUFACTURING PROCESSES
Q.-Y. Liu, Beihang University, China
10.2Flying Quality
Chair(s): Yokoyama, N.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 20 14:00 14:30 10.2.1 GUARANTEED FLYING QUALITIES UNDER REAL AND COMPLEX UNCERTAINTIES
D. Seiferth, Technical University of Munich, Germany
16. Sep 20 14:30 15:00 10.2.2 CONTROL ALLOCATION FOR ONERA\'S SMALL BUSINESS CONCEPT PLANE AMPERE WITH DISTRIBUTED ELECTRIC PROPULSION
C. DÖLL, ONERA, France
16. Sep 20 15:00 15:30 10.2.3 ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A BWB CONFIGURATION
L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal
Reserve Paper 10.2.R AN ACTIVE SIDESTICK CONTROLLER FOR AIRCRAFT GROUND OPERATIONS
J Gauci, University of Malta, Malta
Reserve Paper 10.2.R THE APPLICATION OF THE PILOT-AIRCRAFT SYSTEM APPROACH FOR OPTIMIZING 3D DISPLAY PARAMETERS
A. V. Efremov¹, M. S. Tiaglik¹, I. Kh. Irgaleev¹; ¹Moscow Aviation Institute, Russia
11.2System Health Monitoring
Chair(s): Mare, J., Stumpf, E.
Track 11
07 - Systems, Subsystems and Equipment
16. Sep 20 14:00 14:30 11.2.1 DAMAGE DETECTION OF AERONAUTICAL PANELS BY USING CROSS-CORRELATION OF SPATIALLY SHIFTED DISTRIBUTED STRAIN SENSORS
M. Ciminello, C.I.R.A. Italian Aerospace Research Center, Italy
16. Sep 20 14:30 15:00 11.2.2 THEORETICAL AND EXPERIMENTAL STUDY FOR THE DEVELOPMENT OF SELF-POWERED MONITORING SYSTEMS WITH MFC PIEZOELECTRIC PATCHES
G. Di Rito¹, M.-R. Chiarelli¹, V. Franchi¹, L. Bancallari, MBDA Italia S.p.A., Italy; B. Luciano, AESIS s.r.l., Italy; ¹Università di Pisa - Dipartimento di Ing. Civile ed Industriale, Italy
16. Sep 20 15:00 15:30 11.2.3 STUDY ON CLOSED-LOOP CROSS COMPENSATION CONTROL TECHNOLOGY IN ACCELERATED FATIGUE TEST
HONGWEI ZHAO¹, TAO HAN¹, ZHENZHONG GU, Chongqing Hongyu Precision Industrial Co., Ltd., China; GUANGSHENG SHI, Shenyang Aircraft Design & Research Institute of China, China; SHIHUI DUAN¹, JIANMIN FENG¹; ¹Aircraft Strength Research Institute of China, China
Reserve Paper 11.2.R DESIGN OF DATA SERVICE ARCHITECTURE FOR AVIATION PHM SYSTEM BASED ON MULTI-LAYER PROTOCOL
P.J. Wang, Tsinghua University, China
Reserve Paper 11.2.R RELIABILITY ANALYSIS AND EVALUATION METHOD FOR DESIGN APPRAISAL OF AIRBORNE EQUIPMENTS
Z-J-L Zhang, AVIC XI’AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD., China
12.2Airspace Management
Chair(s): Andreeva Mori, A.
Track 12
09 - Air Transport System Efficiency
16. Sep 20 14:00 14:30 12.2.1 ANGULAR 3D INSTRUMENT APPROACHES FOR GLS EQUIPPED AIRCRAFT USING A LIGHT AND MOBILE SBAS TO GBAS CONVERTER
T. Dautermann, DLR , Germany
16. Sep 20 14:30 15:00 12.2.2 ON THE MINIMUM SEPARATION BETWEEN ANY PAIR OF FLIGHT PATHS
L.M.B.C. Campos, IDMEC/CCTAE/IST, Portugal
16. Sep 20 15:00 15:30 12.2.3 AIRSPACE CAPACITY MANAGEMENT OPTIMISATION FOR TRAJECTORY BASED OPERATIONS
D. Zheng Zhang¹, E. Puntero Parla¹, M. Sánchez Cidoncha¹, F. Gómez Comendador², R. Arnaldo Valdés²; ¹CRIDA A.I.E., Spain ;²Technical University of Madrid, Spain
Reserve Paper 12.2.R DESIGNING AIRCRAFT TRAFFIC FLOWS USING DATA-DRIVEN QUEUING MODELS
E. Itoh, ENRI, Japan
13.2Structural Integrity and Fatigue
Chair(s): Liao, M., Blom, A.
Track 13
04.1 - Material Issues, Fatigue and Damage Tolerance
16. Sep 20 14:00 14:30 13.2.1 DEVELOPMENT OF AIRFRAME DIGITAL TWIN TECHNOLOGY FOR AIRCRAFT STRUCTURAL INTEGRITY MANAGEMENT PROGRAM
Min Liao, National Research Council Canada, Canada
16. Sep 20 14:30 15:00 13.2.2 A DIGITAL EQUIVALENT DEVELOPMENT FOR FATIGUE AND DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES
L. ZAPLANA MANZANO, AIRBUS , Spain
16. Sep 20 15:00 15:30 13.2.3 EXPERIMENTAL STUDY OF THE EFFECT OF BIAXIAL STRESS STATE ON THE GROWTH RATE OF FATIGUE CRACKS
A.V. Kulemin, Central Aerohydrodynamic Institute n. a. N.E. Zhukovsky (TsAGI), Russia
Reserve Paper 13.2.R INVESTIGATION OF THE INFLUENCE OF LOW AMPLITUDE LOADS ON THE FATIGUE LIFE OF CFRP SAMPLES WITH IMPACT DAMAGE UNDER IRRE
V.G. Lukyanchuk, Central Aerohydrodynamic Institute, TsAGI, Russia, Russia

15:30 - 16:00Break

1.3Hybrid/Electric & Unconventional Aircraft 3
Chair(s): Prakasha, P.
Track 1
01 - Aircraft Design and Integrated Systems
16. Sep 20 16:00 16:30 1.3.1 DESIGN, OPERATIONAL AND ENVIRONMENTAL ASSESSMENT OF A HYBRID-ELECTRIC AIRCRAFT
A. E. Scholz, Technical University of Munich, Germany
16. Sep 20 16:30 17:00 1.3.2 DESIGN FOR DIRECTIONAL CONTROL AND STABILITY OF AIRCRAFT WITH DISTRIBUTED PROPULSION
J.S.E. Soikkeli¹, M.F.M. Hoogreef¹; ¹Delft University of Technology, Netherlands
16. Sep 20 17:00 17:30 1.3.3 VALIDATION OF AN AERODYNAMIC MODEL FOR THE DESIGN OF SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRICAL PROPULSION
O. Luderer, Hamburg University of Technology, Germany
16. Sep 20 17:30 18:00 1.3.4 CONCEPTUAL DESIGN OF SILENT ELECTRIC COMMUTER AIRCRAFT
G. Atanasov, Germany
Reserve Paper 1.3.R REQUIREMENTS AND LIMITATIONS FOR GENERAL AVIATION ELECTRIC AIRPLANES
Z. Lei, Suwa University of Science, Japan
2.3UAS 2
Chair(s): Gerhards, R.
Track 2
01 - Aircraft Design and Integrated Systems
16. Sep 20 16:00 16:30 2.3.1 HYBRID POWER SYSTEM FOR NEW GENERATION OF VTOL UNMANNED AERIAL VEHICLES WITH A TAKE-OFF WEIGHT OF UP TO 300 KG
L. Czajkowski, ?ukasiewicz Research Network - Institute of Aviation, Poland
16. Sep 20 16:30 17:00 2.3.2 DEVELOPMENT OF A TURN-KEY, INTEGRATED RAPID DESIGN AND MANUFACTURING ENVIRONMENT FOR SUAS
D. Verstraete, The University of Sydney, Australia
16. Sep 20 17:00 17:30 2.3.3 DATABASE BASED MULTI-MISSION DESIGN FOR E-VTOL UAVS
T. Seren, Institute of Aircraft Design - Technical University of Munich, Germany
16. Sep 20 17:30 18:00 2.3.4 METHODOLOGY FOR OBTAINING AN OPTIMIZED BAFFLED AIRFOIL FOR AN INFLATABLE WING
S.R.M. Mistri, Indian Institute of Technology- Bombay, India
3.3AFLoNext
Chair(s): ,
Track 3
15 - Guest lectures
16. Sep 20 16:00 16:30 3.3.1 FLIGHT TEST OF AN ADVANCED HYBRID-LAMINAR-FLOW-CONTROL (HLFC) SYSTEM ON AN A320 VERTICAL TAIL PLANE
H. von Geyr, German Aerospace >Centre, DLR, Germany
16. Sep 20 16:30 17:00 3.3.2 ACTIVE FLOW CONTROL (AFC) AT PYLON / WING JUNCTION OF CIVIL AIRCRAFT – A FULL-SCALE DEMONSTRATION
T. M. Gibson, Airbus Operations Limited, United Kingdom
16. Sep 20 17:00 17:30 3.3.3 NOISE REDUCTION AT FLAP SIDE EDGE AND UNDERCARRIAGE
S Pott-Pollenske, DLR, Germany
16. Sep 20 17:30 18:00 3.3.4 MAIN LANDING GEAR DOORS VIBRATION REDUCTION BASED ON FLIGHT TEST
R Abarca Lopez, Airbus, Spain
4.3Applied CFD 2
Chair(s): Wan, T., Liu, P.
Track 4
03.1 - Aerodynamics - CFD Methods and Validation
16. Sep 20 16:00 16:30 4.3.1 STALL PREDICTION OF AIRCRAFT WITH ADAPTIVE HYBRID MESH
J. Tang¹, J. Zhang¹, N.-C. Zhou¹, B. Li¹, P.-C. Cui¹; ¹China Aerodynamics Research and Development Center, China
16. Sep 20 16:30 17:00 4.3.2 LATTICE BOLTZMANN SIMULATIONS OF STORE SEPARATION TRAJECTORIES
G. Trapani, Dassault Systemes Spain, Spain
16. Sep 20 17:00 17:30 4.3.3 TRAJECTORY PREDICTIONS FOR THE MK-82 STORE FROM A GENERIC CAVITY
Alex CENKO, AIWS, United States
16. Sep 20 17:30 18:00 4.3.4 COMPUTATIONAL STUDY ON COAND? BLANKET CURVATURE EFFECTS ON HALF-SPHERICAL COAND? DEVICE PERFORMANCE
HD Djojodihardjo, Retired Professor, Indonesia
Reserve Paper 4.3.R NUMERICAL SIMULATION AND ANALYSIS OF SECOND THROAT IN LARGE WIND TUNNELS
B.-B.-X. Xu, CARDC, China
Reserve Paper 4.3.R A VALIDATION STUDY FOR EFFECT OF CAMBER IN A MULTI ELEMENT AIRFOIL IN SUBSONIC FLOW CONDITIONS
E. GULRAIZ, RCMS, NUST, Pakistan
5.3Configurations
Chair(s): ,
Track 5
03.4 - Applied Aerodynamics
16. Sep 20 16:00 16:30 5.3.1 INTAKE BOUNDARY LAYER PROFILE ESTIMATION FOR BLI PERFORMANCE PREDICTION ON A BLENDED WING BODY
K. Ma¹, S. Prince¹; ¹Cranfield University, United Kingdom
16. Sep 20 16:30 17:00 5.3.2 NUMERICAL STUDY OF HEAT TRANSFER ENHANCEMENT OF CONFINED JET IN AIRCRAFT ANTI-ICING CHAMBER
J.-J Niu, Northwestern Polytechnical University, China
16. Sep 20 17:00 17:30 5.3.3 NUMERICAL INVESTIGATION ON FLOW INTERFERENCE BETWEEN BLENDED-WING-BODY AIRCRAFT AND OVERHANGING NACELLE
A.X.Q Qiu, China
16. Sep 20 17:30 18:00 5.3.4 PRELIMINARY AERODYNAMIC DESIGN AND ANALYSIS OF TRUSS-BRACED WING REGIONAL AIRCRAFT USING HIGH-FIDELITY METHODS
S. Hosseini, Amirkabir University of Technology, Iran
Reserve Paper 5.3.R AN INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS FOR SAAB J-29 AIRCRAFT DESIGN USING HIGH FIDELITY CFD
M. Zhang, Airinnova AB, Sweden
6.3Transition Physics 2
Chair(s): Atkin, C., Mugal, S.
Track 6
03.3 - Basic Fluid Dynamics and Flow Control
16. Sep 20 16:00 16:30 6.3.1 STABILIZATION OF SUPERSONIC BOUNDARY LAYERS IN THE PRESENCE OF FAVORABLE PRESSURE GRADIENT
P.V. Chuvakhov¹, A.V. Fedorov, Moscow Institute of Physics and Technology (MIPT), Russia; A.O. Obraz¹; ¹Central Aerohydrodynamic Institue (TsAGI), Russia
16. Sep 20 16:30 17:00 6.3.2 NUMERICAL SIMULATION OF THREE-DIMENSIONAL DISTURBANCES EVOLUTION IN SUPERSONIC FLOW OVER A WAVY SURFACE
A.V. Novikov, Central Aerohydrodynamic Institute, Russia
16. Sep 20 17:00 17:30 6.3.3 MECHANISMS OF NATURAL LAMINAR-TURBULENT TRANSITION ON AN UNSWEPT WING IN SUPERSONIC FLIGHT
P.V. Chuvakhov¹, A.V. Fedorov², A.O. Obraz¹, I.O. Pogorelov²; ¹Central Aerohydrodynamic Institue (TsAGI), Russia ;²Moscow Institute of Physics and Technology (MIPT), Russia
16. Sep 20 17:30 18:00 6.3.4 TRIGGERING SUPERSONIC BOUNDARY-LAYER INSTABILITY BY SMALL-SCALE VORTEX SHEDDING
G. Tu, State Key Laboratory of Aerodynamics, China
7.3Performance
Chair(s): ,
Track 7
03.4 - Applied Aerodynamics
16. Sep 20 16:00 16:30 7.3.1 GRADIENT-BASED ROBUST DESIGN OF A WING WITH 3D SHOCK CONTROL BUMPS
C. Sabater, German Aerospace Center (DLR), Germany
16. Sep 20 16:30 17:00 7.3.2 AERODYNAMIC PERFORMANCE ANALYSIS USING AN EXERGY BALANCE METHOD
I. Petropoulos, ONERA, France
16. Sep 20 17:00 17:30 7.3.3 DRAG REDUCTION ANALYSIS IN CLOSE-FORMATION FLIGHT
X.X. Meng, Northwestern Polytechnical University, China
16. Sep 20 17:30 18:00 7.3.4 INCREASING THE EFFECTIVENESS OF AN AERODYNAMICALLY BALANCED CONTROL SURFACE ON A MODIFIED AIRFOIL WITH REDUCED DRAG
V.V. Bogatyrev, TsAGI, Russia
Reserve Paper 7.3.R DESIGN OF WINGTIP SAILS FOR A LARGE-ASPECT-RATIO WING
Y. Liu¹, R. Zeng¹, L. Ping¹; ¹CETC Wuhu Diamond Aircraft Manufacture co., LTD, China
Reserve Paper 7.3.R AERODYNAMIC DESIGN AND ANALYSIS ON A NEW STEPPED WINGLET BASED ON THE DYNAMIC CHARACTERISTICS OF THE WINGTIP VORTEX
J.Jin Jin, Shanghai Aircraft Design and Research Institute,COMAC, China
8.3Testing and Measurement
Chair(s): Bisagni, C., Li, K.
Track 8
04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
16. Sep 20 16:00 16:30 8.3.1 RESEARCH ON ATTITUDE CONTROL AND CONSTRAINT SYSTEM DESIGN OF FULL-SCALE AIRCRAFT STATIC TEST BASED ON BARYCENTRE
JJ ZHENG, AVICASRI, China
16. Sep 20 16:30 17:00 8.3.2 NON-CONTACT MEASUREMENT OF SURFACE DEFORMATION FIELDS BY VIDEOGRAMMETRY METHOD
K.A. Kuruliuk, Central Aerohydrodynamic Institute n. a. prof. N.E. Zhukovsky, Russia
16. Sep 20 17:00 17:30 8.3.3 OPTIMIZATION FOR PROCESS AND MANAGEMENT IN MASSIVE STRAIN MEASUREMENT IN THE FULL SCALE AIRCRAFT STRUCTURE STRENGTH TEST
J. Zuo, Aircraft Strength Research Institute of China, China
16. Sep 20 17:30 18:00 8.3.4 DESIGN OF A VERTICAL DITCHING TEST
E. Cestino, Politecnico di Torino, Italy
Reserve Paper 8.3.R A SUBJECTIVE EVALUATION METHOD OF AIRCRAFT VIBRATION IN FLIGHT TEST
H.G WANG, COMAC, China
9.3Advanced Manufacturing Management
Chair(s): Wang, S.
Track 9
08 - Manufacturing and Supply Chain Management
16. Sep 20 16:00 16:30 9.3.1 ASSESSING THE IMPACT OF PRODUCTION MODELING IN CONCEPTUAL AIRCRAFT DESIGN
J. Page Risueno, German Aerospace Center (DLR), Germany
16. Sep 20 16:30 17:00 9.3.2 A STRUCTURED AND SCALABLE APPROACH FOR THE DEFINITION OF DEEP LEARNING ARCHITECTURES FOR BEARING ANOMALY DETECTION
O Pinon Fischer, Georgia Institute of Technology, United States
16. Sep 20 17:00 17:30 9.3.3 INCORPORTING KNOWLEDGE COVERAGE MEASUREMENT INTO KNOWLEDGE TRANSFORMATION FROM DATA FOR KNOWLEDGE ACCUMULATION
Y.-B. Fan, NanChang HangKong University, China
16. Sep 20 17:30 18:00 9.3.4 DESIGN AND BEST PRACTICES OF SUPPLIER PERFORMANCE EVALUATION IN SUPPLY CHAIN
HZ-L Li, AECC SHANGHAI COMMERCIAL AIRCRAFT ENGINE MANUFACTURING CO.,LTD., China
10.3Fault Detection
Chair(s): Wang, Y.
Track 10
06.1 - Flight Dynamics and Control (Control & Modelling)
16. Sep 20 16:00 16:30 10.3.1 AIRCRAFT BRAKING DYNAMICS AND BRAKE SYSTEM MODELING FOR FAULT DETECTION AND ISOLATION
L.C.N. Cardoso Navarro, ITA, Brazil
16. Sep 20 16:30 17:00 10.3.2 FLIGHT SIMULATOR EVALUATION OF SIMPLE ADAPTIVE CONTROL FOR LOSS-OF-CONTROL RECOVERY
R. T. Takase, The University of Tokyo, Japan
16. Sep 20 17:00 17:30 10.3.3 TWO-LAYER ADAPTIVE AUGMENTATION FOR INCREMENTAL BACKSTEPPING FLIGHT CONTROL OF AIRCRAFT IN FAILURE CONDITIONS
D. Ignatyev, Cranfield University, United Kingdom
16. Sep 20 17:30 18:00 10.3.4 FEEDBACK ERROR LEARNING WITH ENHANCED SAMPLING: NEURAL FAULT TOLERANT CONTROL OF AIRCRAFT
N. Yoshikawa, University of Tokyo, Japan
11.3Aspects of Landing Gear Design
Chair(s): Krus, P., Shang, Y.
Track 11
07 - Systems, Subsystems and Equipment
16. Sep 20 16:00 16:30 11.3.1 IMPROVED DESIGN OF AIRCRAFT NOSEWHEEL STEERING SYSTEM
L.-X. Xin, FAI AVIC, China
16. Sep 20 16:30 17:00 11.3.2 NEW SOLUTION OF A DAMPER WITH A MAGNETORHEOLOGICAL ELASTOMER
P. Skalski, Institute of Aviation, Poland
16. Sep 20 17:00 17:30 11.3.3 INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL
Z. Skorupka, ?ukasiewicz Research Network - Institute of Aviation, Poland
16. Sep 20 17:30 18:00 11.3.4 A STOCHASTIC ROBUSTNESS VERIFICATION OF NLG SIMPLE ADAPTIVE SHIMMY SUPPRESSION SYSTEM
C. Orlando, Italy
Reserve Paper 11.3.R STUDY ON THE DYNAMIC COUPLING CHARACTERISTICS OF AIRCRAFT LOW SPEED BRAKE
ZHAO HAO, Shanghai Aircraft Design And Research Institute , China
Reserve Paper 11.3.R RESEARCH ON DESIGN OF HYDRAULIC ACCUMULATOR FOR A CIVIL AIRCRAFT BRAKE SYSTEM
G.-C Zhang, Shanghai Aircraft Design and Research Institute, China
Reserve Paper 11.3.R A NOVEL OF CONTROL METHOD BASED ON PWM FOR HIGH_SPEED ON/OFF VALVES ARRAY OF AIRCRAFT BRAKE SYSTEMS
Renjie Li Li, Beihang unversity, China
12.3Airport/Aircraft Operation
Chair(s): Itoh, E.
Track 12
09 - Air Transport System Efficiency
16. Sep 20 16:00 16:30 12.3.1 INTEGRATION AND EVALUATION OF AN AIRCRAFT TAXIING SOLUTION USING AUTONOMOUS TOW TRUCKS
J Gauci, University of Malta, Malta
16. Sep 20 16:30 17:00 12.3.2 ERAS - EVALUATION OF REALISTIC APPROACH SCENARIOS FOR MINIMAL NOISE - PRELIMINARY FINDINGS
B Moberg, Vernamack AB, Sweden
16. Sep 20 17:00 17:30 12.3.3 DESIGN AND TRIALING OF A CONCEPT OF OPERATIONS (CONOPS) FOR OPTIMAL CLIMBS AND DESCENTS INTO MEDIUM DENSITY AIRFIELDS
D. Zammit-Mangion, University of Malta, Malta
16. Sep 20 17:30 18:00 12.3.4 A NOVEL APPROACH FOR TURNAROUND TIME ALLOCATION BASED ON REINFORCEMENT LEARNING
A. Rodriguez-Sanz, Universidad Politecnica de Madrid (UPM), Spain
Reserve Paper 12.3.R OPERATION PLANNING AIDED METHOD OF GENERAL AIRCRAFT BASED ON MULTI-CBR AND COMBINATION EVALUATION METHOD
R.-X. Xie, Beihang University, China
13.3Failure And Fracture Mechanics
Chair(s): Liao, M., Kanerva, M.
Track 13
04.1 - Material Issues, Fatigue and Damage Tolerance
16. Sep 20 16:00 16:30 13.3.1 FAILURE PROCESS IDENTIFICATION OF C-SIC WITH DIFFERENT TENSILE PERFORMANCE
Y.Z. Zhang, Northwestern Polytechnical University, China
16. Sep 20 16:30 17:00 13.3.2 INVESTIGATION OF STOPPER STRAPS EFFECTS ON LONGITUDINAL CRACK GROWTH RATES IN A SKIN OF PRESSURIZED AIRCRAFT FUSELAGE
A.S. Kim, TsAGI, Russia
16. Sep 20 17:00 17:30 13.3.3 INFLUENCE OF NOTCH EFFECTS ON STATIC CHARACTERISTICS OF STEEL BASED ON THERMOGRAPHIC METHOD
Junling Fan¹, Pengfei Yang¹, Shaozheng Zhan¹; ¹Aircraft Strength Research Institute, China
16. Sep 20 17:30 18:00 13.3.4 EXPERIMENTAL INVESTIGATION AND NUMERICAL SIMULATION OF SINGLE LAP JOINTS OF ALLOY-ARAMID FIBER COMPOSITE BASED ON COHESI
ZTC Zou, Civil Aviation University of China, China
Reserve Paper 13.3.R A MICROPHONE POSITION CALIBRATION METHOD FOR A RANDOM ARRAY
Q He, China
Reserve Paper 13.3.R EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY
SHI Y. SHI, Beihang University, China