30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Interactive Presentations

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ACCEPTED PAPERS - CATEGORY C - INTERACTIVE PRESENTATIONS

These papers will be presented in the Interactive Presentations area
Most papers will also appear in the Congress CD Proceedings



1 - Aircraft Design and Integrated Systems

ICAS2020-P1.1: Hailong H.-L. Liu, Chengdu Aircraft Industrial (Group) Co., Ltd., China
RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES
ICAS2020-P1.2: X. GU, China Academy of Launch Vehicle Technology, China
A RAPID SHAPE DESIGN METHOD OF LIFTING HIGH SPEED VEHICLE FOR ENGINEERING APPLICATIONS
ICAS2020-P1.3: J.-G. Guo, Northwestern Polytechnical University, China
AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGY
ICAS2020-P1.4: Wei Wang, School of Aeronautics, Northwestern Polytechnical University, China; Wenqing Yang¹, Bifeng Song¹; ¹Research & Development Institute of NWPU, China
NUMERICAL SIMULATION ON AERODYNAMIC CHARACTERISTICS OF BIONIC CORRUGATED FLAPPING WING
ICAS2020-P1.5: D Chen, Northwestern Polytechnical University, China
CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERING
ICAS2020-P1.6: Y.B.-L Li, China
MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WING
ICAS2020-P1.7: Cyf Chen, China
GEOMETRIC PARAMETERIZATION OF CYLINDRICAL BODIES AND ITS APPLICATION IN AERODYNAMIC OPTIMIZATION DESIGN
ICAS2020-P1.8: S.-Q. Li, Xi'an Jiaotong University, China
LOW-ALTITUDE LONG-ENDURANCE UAV WING OPTIMIZATION
ICAS2020-P1.9: A Nagy, University of Dunaujvaros, Hungary
DEVELOPMENT OF ADVANCED UAV FOR WIND TURBINE MEASUREMENT

2 - Systems Engineering and Integration

ICAS2020-P2.1: C Yanxin, AECC, China
APPLICATION OF MBSE IN AEROENGINE STRUCTURAL PARAMETER CALCULATING SYSTEM
ICAS2020-P2.2: JY-L Li, Global Crown Technology Co.,Limited., China
FAULT INJECTION TECHNOLOGY OF AERONAUTICAL VEHICLE BASED ON GCAIR
ICAS2020-P2.3: Wenyuan CHENG¹, Chenguang XING¹, Jia XU¹, Gang SONG¹; ¹Aviation Industry Development Research Center of China , China
RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENT
ICAS2020-P2.4: Xinyu Zhang, Commercial Aircraft Corporation of China Ltd, China
A FUNCTIONAL REQUIREMENTS CAPTURE AND VALIDATION APPROACH BASED ON PLM PLATFORM APPLIED IN THE CIVIL AIRCRAFT
ICAS2020-P2.5: Bw.L. Liu, China Aeronautical Radio Electronics Research Institute, China
MODEL DESIGN AND APPLICATION OF UAV'S MISSION SYSTEM BASED ON HARMONY-SE
ICAS2020-P2.6: WANG YI, COMAC, China
REQUIREMENTS MANAGEMENT APPLIED IN AIRWORTHINESS CERTIFICATION IN THE CIVIL AIRCRFAT
ICAS2020-P2.7: Bing Xue¹, Zhijuan Zhan¹, Yunhui Wang¹; ¹Laboratory of Avionics System Integration, China
A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOS
ICAS2020-P2.8: V Kan, NRC Zhukovsky, Russia
CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTS
ICAS2020-P2.9: JS Jieshi, Chinese Aeronautical Radio and Electronics Research Institute, China
CO-SIMULATION OF SYSML AND SIMULINK OR MODELICA USING FMI
ICAS2020-P2.10: Wenyuan CHENG¹, Chenguang XING¹, Gang SONG¹; ¹Aviation Industry Development Research Center of China , China
A CONTRASTIVE STUDY OF STANDARD SPECIFICATION FOR TECHNOLOGY READINESS ASSESSMENT
ICAS2020-P2.11: Shuo Lu Lu, Aero Engine Academy of China, China
THE STUDY ON PROGRAM MANAGEMENT METHOD BASED ON SYSTEM ENGINEERIING
ICAS2020-P2.12: Y Peng, Shanghai Aircraft Design and Research Institute, China
TRADE-OFF RESEARCH FOR LARGE PASSENGER AIRCRAFT SUPPLEMENTAL COOLING SYSTEM INTEGRATION DESIGN
ICAS2020-P2.13: WB Bin, COMAC Shanghai Aircraft Design And Research Institute, China
BASED ON ARP4754A THE CIVIL AIRCRAFT PROJECT DEVELOPMENT PLAN DEVELOPMENT RESEARCH
ICAS2020-P2.14: L LIU, State Key Laboratory of Aerodynamics, China
AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES
ICAS2020-P2.15: L-Q Li, AVIC XI’AN AIRCRAFT INDUSTRY (GROUP) COMPANY LTD., China
RESEARCH ON FUNCTIONAL RISK ASSESSMENT TECHNOLOGY OF MILITARY AIRCRAFT
ICAS2020-P2.16: HYB Huang, Beijing Aeronautical Science & Technology Research Institute, Co, China
ANALYSIS OF RELIABILITY SCREENING SCHEME BY SIRS EPIDEMIC MODEL
ICAS2020-P2.17: he chengjun, AVIC Xian Aircraft Design Institute, China
COMPREHENSIVE REDUNDANCY MANAGEMENT AND VERIFICATION STRATEGY FOR TASK-BASED AIR MANAGEMENT SYSTEM
ICAS2020-P2.18: Luo Run¹, Chong Yu¹; ¹XI’AN AIRCRAFT INDUSTRY (GROUP) COMPANY.LTD, China
A PRODUCT DESIGN METHOD BASED ON THE QFD-TRIZ-DOE AND ITS ENGINEERING APPLICATION
ICAS2020-P2.19: J. -Y Ye, BIT, China
MODEL-BASED VIRTUAL SIMULATION OF AIRCRAFT OPERATION SCENARIOS
ICAS2020-P2.20: Y. Guo, Northwestern Polytechnical University, China
RESEARCH ON SELECTION METHODS FOR AIRCRAFT LANDING GEAR SYSTEM HEALTH FEATURE PARAMETERS
ICAS2020-P2.21: SXB Shi, Civil Aviation Flight University of China, China
OVERVIEW OF THE DEVELOPMENT OF INTEGRATED NAVIGATION TECHNOLOGY BASED ON STAR SENSOR
ICAS2020-P2.22: S. Chang, COMAC, China
SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST
ICAS2020-P2.23: W.-L. Liu, Beihang University, China
CONSTRUCTION AND SUPPORT TECHNOLOGY OF MULTIDISCIPLINARY COLLABORATIVE DESIGN MODEL FOR CIVIL AIRCRAFT BASED ON MBSE

3.1 - Aerodynamics - CFD Methods and Validation

ICAS2020-P3.1.1: H.-C. Chen, Beijing Institute of Space Long March Vehicle, China
INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE
ICAS2020-P3.1.2: Jinyou SU, China; JINHU TIAN, China; Zhili TANG, China; Biao PAN, Germany
CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL
ICAS2020-P3.1.3: S.H. Zhang, China
AERODYNAMIC SHAPE OPTIMIZATION DESIGN OF WING-PROPELLER CONFIGURATION BASED ON A CST-DGM APPROACH
ICAS2020-P3.1.4: J.Y. Shen, AECC Commercial Aircraft Engine Co., Ltd, China
PERFORMANCE ANALYSIS OF AN OIL SCOOP LUBRICATION SYSTEM FOR DUAL-BEARING FULCRUM IN A GAS TURBINE ENGINE
ICAS2020-P3.1.5: H. A. H. Sehole, National University of Science and Technology, Pakistan
COMPUTATIONAL MODELING & ANALYSIS OF REACTING FLOW INSIDE A GENERIC GAS TURBINE COMBUSTOR
ICAS2020-P3.1.6: G.-Y. LI, AVIC Xi’an Aircraft Industry(Group) Company LTD, China
AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESS
ICAS2020-P3.1.7: D Lu, Shanghai Jiao Tong University, China
A VARIABLE TURBULENT PRANDTL AND SCHMIDT NUMBER MODEL FOR SUPERSONIC REACTIVE FLOW
ICAS2020-P3.1.8: H. C. Chen, China
SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID
ICAS2020-P3.1.9: R.B B?bel, Polish Air Force Academy, Poland
COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF AN INFLUENCE OF ICING ON AIRFOIL AERODYNAMIC CHARACTERISTICS
ICAS2020-P3.1.10: S.P. Patial, University of Petroleum and Energy Studies, India
THE STUDY OF THE EFFECT OF CAVITY ON THE FLOW OVER NACA 0012 AND SELIG 7003 AEROFOIL AT LOW REYNOLDS NUMBER
ICAS2020-P3.1.11: Dan Liu, School of Aeronautics,Northwestern Polytechnical University, China; Wenqing Yang¹, Bifeng Song¹; ¹Research & Development Institute of NWPU in Shenzhen, China
NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING WITH SLOTTED-TIP

3.2 - Experimental Aerodynamics

ICAS2020-P3.2.1: XU xiwang, National University of Defense Technology, China
EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACK
ICAS2020-P3.2.2: C.-X. Xiao, China Aerodynamics Research and Development center, China
PRELIMINARY STUDY ON ICE RIDGE FORMATION DURING ELECTROTHERMAL DE-ICING PROCESS
ICAS2020-P3.2.3: Z.-Z. Zhang, AECC Shenyang Engine Research Institute, China
EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIV
ICAS2020-P3.2.4: Q. Liu, National University of Defence Tecchnology, China
EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTS
ICAS2020-P3.2.5: Z.-S. Sun, China
SUPPRESSION OF ACOUSTIC RESONANCE IN CAVITY FLOW USING CROSS CYLINDER COATED WITH POROUS METAL
ICAS2020-P3.2.6: L-XF Xuefei, AVIC Aerodynamics Research Institute, China
A STUDY OF SONIC BOOM TEST WITH NOZZLE PLUME INTERACTIONS
ICAS2020-P3.2.7: D.-M.C.C.A de Camargo Araujo Daher, ITA - Instituto Tecnológico da Aeronáutica, Brazil
STUDY OF SHOCK WAVES ON THE VEHICLE SONDA III IN HIGH-SPEED REGIMES
ICAS2020-P3.2.8: x Honghui, AECC Sichuan Gas Turbine Establishment, China
EXPERIMENTAL DISCOVERY OF THE VIBRATION PHENOMENON OF COMPRESSOR ROTOR BLADE INDUCED BY INLET PROBE SUPPORT
ICAS2020-P3.2.9: Q. Wang, BASTRI, COMAC, China
STUDY ON THE STING INTERFERENCE IN TRANSONIC WIND TUNNEL TESTS OF A BLENDED WING BODY CONFIGURATION
ICAS2020-P3.2.10: H. Qin, China Academy of Aerospace Aerodynamics, China
ANALYSIS AND CORRECTION OF SUPPORT INTERFERENCE FOR A LARGE SLENDERNESS RATIO MODEL AT HIGH SPEED WIND TUNNEL
ICAS2020-P3.2.11: Y. Jiao, Northwestern Polytechnical University, China
CONTROL AND CORRECTION OF INERTIAL FORCES IN DIRECT FORCE MEASURING TEST OF AIRFOIL DYNAMIC AERODYNAM PERFORMANCE

3.3 - Basic Fluid Dynamics and Flow Control

ICAS2020-P3.3.1: Y.-C. Lei, Air Force Engineering University, China
NUMERICAL SIMULATION OF AERODYNAMIC CHARACTERISTICS OF SUPERCRITICAL AIRFOIL BASED ON DOUBLE JETS CIRCULATION CONTROL
ICAS2020-P3.3.2: H.-G. Guo, Beihang University, China
EFFECTS OF THE SELF-ADAPTIVE MODULATION OF BOUNDARY CONDITIONS ON THE SKIN FRICTION REDUCTION RATE OF WALL-BOUNDED TURBU
ICAS2020-P3.3.3: M.X Tang, China
SHOCK WAVE BOUNDARY LAYER INTERACTION CONTROL USING PULSED ARC-DISCHARGE PLASMA ACTUATOR ARRAY

4.1 - Material Issues, Fatigue and Damage Tolerance

ICAS2020-P4.1.1: W.Y.J Wang, Chengdu Aircraft design and Research Institute, China
STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUM
ICAS2020-P4.1.2: Y.L. SU, Aircraft Strength Research Institute of AVIC, China
DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISK
ICAS2020-P4.1.3: W.-D. Dong, Computational Aerodynamic Institute(CAI), CARDC, China
A NEW METHOD FOR ESTIMATING THE THERMOPHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS
ICAS2020-P4.1.4: S.-S SU, Aircraft Strength Research Institute, China
FRACTURE CRITERION AND CRACK GROWTH PROPERTY ANALYSIS OF MIXED MODE CRACK STRUCTURES
ICAS2020-P4.1.5: S Olsson, Quintus Technologies, Sweden
FORMABILITY OF TITANIUM TI-6AL-4V SHEETS AT MODERATE TEMPERATURE COMBINED WITH HIGH-PRESSURE
ICAS2020-P4.1.6: B Xiao, Carleton University, Canada
TRANSIENT OXIDE FORMATION AND OXIDE SPALLATION ON IN738 AT 1050ºC
ICAS2020-P4.1.7: S.-L. Li, Beihang University, China
A CONTINUUM DAMAGE MECHANICS BASED LIFETIME MODEL FOR CORROSION FATIGUE ANALYSIS OF A TURBINE BLADE MATERIAL
ICAS2020-P4.1.8: A.R. Lepeshkin, Russia
INVESTIGATIONS OF THE THERMAL CONDUCTIVITY OF TURBINE BLADE MATERIALS IN A FIELD OF CENTRIFUGAL ACCELERATIONS AND FORCES

4.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity

ICAS2020-P4.2.1: Y.-L. Liu, Chengdu Aircraft Industrial (Group) Co., Ltd, China
PROCESS RESEARCH AND OPTIMIZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTS
ICAS2020-P4.2.2: XB Huang, NanChangHangKongUniversity, China
EFFECT OF STRUCTURAL PARAMETERS OF W-SHAPED METAL SEALING RING OF AEROENGINE ON ITS SEALING PERFORMANCE
ICAS2020-P4.2.3: Z.Y LI, AVIC, China
A STRUCTURE DESIGN OF CFRP REAR PRESSURE BULKHEAD WITHOUT STIFFENERS
ICAS2020-P4.2.4: L.-F. Luo, AECC Hunan Aviation Powerplant Research Institute, China
OPTIMIZATION OF TURBINE DISK STRUCTURE OF AERO-ENGINE BASED ON KPCA
ICAS2020-P4.2.5: M J Qu, Xi’an Polytechnic University, China
RESEARCH ON MULTI-OBJECTIVE OPTIMIZATION DESIGN METHOD OF WHOLE AEROENGINE COUPLING VIBRATION
ICAS2020-P4.2.6: D. Gueraiche, Moscow Aviation Institute, Russia
PASSIVE FLEXIBLE WINGTIP AREA FOR IMPROVING AIRLINERS CRUISE EFFICIENCY AND GUST ALLEVIATIO
ICAS2020-P4.2.7: Y Li, China
THE APPLICATION OF POD BASED NON-INTRUSIVE REDUCED ORDER MODEL IN STATIC AEROELASTIC ANALYSIS
ICAS2020-P4.2.8: Z. Jia, China
BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIALS WITH ACTIVE CARBON AS ABSORBER
ICAS2020-P4.2.9: M.J Collins, Airbus Operations Ltd, United Kingdom
COMPETENCIES OF A 21ST CENTURY AEROSPACE STRUCTURES ENGINEER
ICAS2020-P4.2.10: Weijian NIE¹, Wangqun DENG¹, Yanong CHEN¹, Lei ZOU¹; ¹AECC Hunan Aviation Powerplant Research Institute , China
TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORT
ICAS2020-P4.2.11: M. Zhang Zhang, University Of Shanghai For Science And Technology, China
THE OPTIMAL DESIGN OF GYROID STRUCTURE
ICAS2020-P4.2.12: L.Z. Zhang, AECC Hunan Aviation Powerplant Research Institute, China
TOPOLOGY OPTIMIZATION OF AEROENGINE PARTS FOR 3D PRINTING
ICAS2020-P4.2.13: F.-C. CHEN, COMAC, China
RESEARCH OF DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSING
ICAS2020-P4.2.14: J.W Wang, AVIC XI’AN AIRCRAFT INDUSTRY(GROUP)COMPANY LTD., China
OPTIMIZED DESIGN OF SEALING RING ON AIRCRAFT PIPELINE SYSTEM BASED ON C++
ICAS2020-P4.2.15: L-J-P jianping, AVIC XI'AN AIRCRAFT INDUSTRY(GROUP) COMPANY LTD., China
DYNAMICS ANALYSIS OF THE FLUID-STRUCTURE INTERACTION SLOSHING SYSTEM IN AIRCRAFT FUEL TANK.
ICAS2020-P4.2.16: HAO CUI, Aviation Industry of China, China
THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATES
ICAS2020-P4.2.17: SY.Z Zhu, China
MINIMUM STIFFNESS OF SUPPORT FOR CONTROL OF FUNDAMENTAL NATURAL FREQUENCY OF THIN CIRCLE PLATE BY RAYLEIGH-RITZ METHOD
ICAS2020-P4.2.18: H.-C. Qiu, COMAC, China
IMPROVED STOCHASTIC PERTURBATION ALGORITHM FOR GENERALIZED REPEATED EIGENVALUES PROBLEM BASED ON SURROGATE MODEL
ICAS2020-P4.2.19: W.-L Weihan, AECC, China
STATIC STRUCTURAL ANALYSIS OF A HOLLOW DISK DESIGNED TO ACHIEVE WEIGHT REDUCTION OF A TURBINE DISK.
ICAS2020-P4.2.20: P.LI LI, AVIC,CHINA, China
TRANSFER PATH ANALYSIS OF RANDOM VIBRATION LOADS FOR AIRCRAFT COMFORT DESIGN
ICAS2020-P4.2.21: G.W.F Gao, China
STRESS-BASED TOPOLOGY OPTIMIZATION OF CONTINUUM STRUCTURES WITH LOAD POSITION UNCERTAINTY
ICAS2020-P4.2.22: S.B. Rayhan Rayhan, Northwestern Polytechnical University, China
STRUCTURAL PERFORMANCE ANALYSIS OF A COMPOSITE WIND TURBINE BLADE BASED ON TWO-WAY FLUID-STRUCTURE INTERACTION
ICAS2020-P4.2.23: Y.-K.H. Kaihua, Beijing Institute of Mechanical and Electrical Engineering, China
SUPERSONIC AEROELASITIC ANALYSIS OF AN ALL-MOVABLE WING WITH FREE PLAY
ICAS2020-P4.2.24: Ye Jia, Aviation Industry of China, China
ULTIMATE LOAD-CARRYING ANALYSIS OF FRICTION STIR WELDED STIFFENED PANEL UNDER COMPRESSION
ICAS2020-P4.2.25: Y-D Ding, Northwestern Polytechnical University, China
BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAV
ICAS2020-P4.2.26: P Pang, China
DESIGN AND PERFORMANCE RESEARCH OF ARTIFICIAL ELECTROMAGNETIC STRUCTURE WITH TRANSMISSION AND ABSORPTION CHARACTERISTICS
ICAS2020-P4.2.27: S. Hosseini, Amirkabir University of Technology, Iran
WING STRUCTURE WEIGHT ESTIMATION OF TRUSS-BRACED WING REGIONAL AIRCRAFT
ICAS2020-P4.2.28: L. A. Magerramova, Central Institute of Aviation Motors, Russia
THE APPLICATION OF POWDER TECHNOLOGIES TO CREATE WHEELS FOR ADVANCED GAS TURBINE ENGINES
ICAS2020-P4.2.29: Y xz Yue, University of Shanghai for Science and Technology, China
EFFECT OF STRUCTURE PARAMETER ON MECHANICAL PROPERTIES OF TWO-DINEBSIONAL IRREGULAR HONEYCOMB STRUCTURE
ICAS2020-P4.2.30: Cheng Chang, China
A STRUCTURE DESIGN METHOD OF ENERGY-ABSORBING COMPOSITE WAVED BEAMS BASED ON THE MACROSCOPIC FAILURE MODE

5 - Propulsion

ICAS2020-P5.1: Y.G. Goto, Hiroshima Institute of Technology, Japan
MEASUREMENT OF FLAME IN 2-STROKE GASOLINE ENGINE BY MULTIPLE-ION-PROBE METHOD
ICAS2020-P5.2: H. Li, Aero Engine Corporation of China, China
MODELING AND SIMULATION APPLICATION THROUGHOUT THE AEROENGINE LIFE CYCLE
ICAS2020-P5.3: L.-H. Li, Northwestern Polytechnical University, China
DESIGN AND OPTIMIZATION OF COMBUSTION CHAMBER OF HYDROGEN-FUELED SCRAMJET BASED ON "CONSTANT AREA + CONSTANT TEMPERATURE
ICAS2020-P5.4: Y F.-L Li, Shenyang Engine Design Research Institute, China
EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICS
ICAS2020-P5.5: P. Skalski, Institute of Aviation, Poland
IMPACT OF AVIATION NOISE ON A HUMAN BLOOD PRESSURE
ICAS2020-P5.6: S.H. Hiroi, Hiroshima Institute of Technology, Japan
EFFECT OF THE NUMBER AND THE DENSITY OF ION-PROBES ON FLAME MEASUREMENT CHARACTERISTICS BY MULTIPLE-ION-PROBE METHOD
ICAS2020-P5.7: L.-H. Li, Northwestern Polytechnical University, China
STUDY ON STEADY STATE CONTROL SCHEDULE AND CHARACTERISTIC CALCULATION OF HYDROGEN-FUELED SCRAMJET
ICAS2020-P5.8: A. Kartashev, South Ural State University, Russia
A DESIGN AND OPTIMIZATION OF TURBINE OF MICRO GAS TURBINE POWER PLANT
ICAS2020-P5.9: CY.-H Hu, AVIC The First Aircraft Institute, China
THE RESEARCH ON PROPELLER NOISE PREDICTION METHOD FOR TURBOPROP AIRCRAFT
ICAS2020-P5.10: D-L Liu, Avic, China
A SPACE VECTOR MODULATION SCHEME FOR A SIX-PHASE BEARINGLESS MOTOR
ICAS2020-P5.11: Y.-L. Liu, Beihang University, China
APPLICATION OF REINFORCEMENT LEARNING IN AERODYNAMIC DESIGN OF 1-D AXIAL COMPRESSOR
ICAS2020-P5.12: J.-J Jun, Institute of Engineering Thermophysics, Chinese Academy of Scien, China
AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLES
ICAS2020-P5.13: X.-S. Yang, Shanghai Jiao Tong University, China
A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINE
ICAS2020-P5.14: M. Zhang, AECC Commercial Aircraft Engine, China
NUMERICAL INVESTIGATION OF NACELLE INTAKE FLOW DISTORTION AT CROSSWIND CONDITIONS

6.1 - Flight Dynamics and Control (Control & Modelling)

ICAS2020-P6.1.1: Xin Hu¹, Hui Xie, China Special Vehicle Research Institute, China; Yiming Liu¹, Yaoming Zhou¹; ¹Beihang University, China
RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS
ICAS2020-P6.1.2: CHANG.-L.F CHANG, China National Aeronautical Radio Electronics Research Institute, China
A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGET
ICAS2020-P6.1.3: O.N. Korsun, Moscow Aviation Institute(National Research University), Russia
APPROACHES TO AIRCRAFT MANEUVERS DESIGN USING OPTIMAL CONTROL
ICAS2020-P6.1.4: Z-S-J Shaojiang, China
SAFETY ANALYSIS OF UAV BUILT-IN AERIAL LAUNCH
ICAS2020-P6.1.5: L.-M. Zheng, China
APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROL
ICAS2020-P6.1.6: Y Liu, Northwestern Polytechinical University, China
MODELING AND DYNAMIC STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFT
ICAS2020-P6.1.7: O. Kreerenko, Moscow Aviation Institute, Beriev Aircraft Company, Russia
SYNERGETIC CONTROLS OF THE SYSTEM “CARRIER AIRCRAFT - UPPER-STAGE ROCKET
ICAS2020-P6.1.8: S. Serokhvostov, MIPT, Russia
OPTIMAL TRAJECTORY DEPENDENCE ON THE ATMOSPHERE MODEL FOR THE SUN-POWERED AIRPLANE
ICAS2020-P6.1.9: C. Qi, China Aeronautical Radio Electronics Research Institute, China
L1 ADAPTIVE CONTROL AUGMENTATION FOR A FLEXIBLE AIR-BREATHING HYPERSONIC VEHICLE MODEL
ICAS2020-P6.1.10: X Du, China Aerodynamics Research and Development Center, China
A FINITE HORIZON SUBOPTIMAL CONTROLLER FOR WING ROCK SUPPRESSION
ICAS2020-P6.1.11: zhang Wensen Zhang, Beihang University, China
SIMULATION AND CONTROL OF DUAL-MOTOR DRIVE ELECTRO-MECHANICAL ACTUATOR
ICAS2020-P6.1.12: D-X Du, China
RESEARCH ON MULTI-CONSTRAINT CONTROL AND GUIDANCE LAW FOR MULTI- MISSILE COOPERATIVE COUNTERING LARGE MANEUVERING TARGET
ICAS2020-P6.1.13: TR Rogalski, Rzeszow University of Technology, Poland
AIRCRAFT FLIGHT CONTROL SYSTEM FOR AEROBATIC FLIGHT
ICAS2020-P6.1.14: D. Shi, Technical University of Munich, Germany
PROBABILISTIC PERFORMANCE GUARANTEED CONTROL OPTIMIZATION FOR FLIGHT CONTROL SYSTEMS WITH UNCERTAINTIES
ICAS2020-P6.1.15: D.-N. Liu, China Aerodynamics Research and Development Center , China
PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL

6.2 - Flight Dynamics and Control (UAV related)

ICAS2020-P6.2.1: A Satoh, Iwate University, Japan
ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODEL
ICAS2020-P6.2.2: E. R. De Pieri De Pieri, Federal University of Santa Catarina, Brazil
ROBUST CONTROL OF UNMANNED AERIAL VEHICLE WITH TILT ROTORS AND CAMERA
ICAS2020-P6.2.3: Z.Y. Wang, China
RESEARCH ON OBSTACLE AVOIDANCE METHOD OF UAV BASED ON 2D LIDAR
ICAS2020-P6.2.4: M. H. Sadraey, SNHU, United States
ROCKET HYBRID LAUNCH SYSTEM
ICAS2020-P6.2.5: P-H Haijun, Northwestern Polytechnical University, China
DYNAMICS MODELING AND SIMULATION OF UAVS WITH LIFT FAN
ICAS2020-P6.2.6: Y.-Q Qi, China
RESARCH OF COOPERATIVE TRACKING AND OBSTACLE AVOIDANCE FOR MULTIPLE UAVS
ICAS2020-P6.2.7: Y. A. Díaz-Méndez, Federal University of Itajubá, Brazil
SIMULATION AND CONTROL OF AN SMALL UNMANNED AERIAL VEHICLE DYNAMICS DURING AN AIRDROP MANUEVER
ICAS2020-P6.2.8: R. WANG, Nanjing University of Aeronautics and Astronautics, China
EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL
ICAS2020-P6.2.9: G. Yu Yu, AVIC Xi’an Aeronautics Computing Technique Research Institute, China
A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDING

7 - Systems, Subsystems and Equipment

ICAS2020-P7.1: Valentin: V Olenev, St. Petersburg State University of Aerospace Instrumentation, Russia
DESIGN AND SIMULATION OF ON-BOARD COMMUNICATION NETWORKS
ICAS2020-P7.2: Wang Yaping, AVIC XI'AN AIRCRAFT INDUSTRIAL(GROUP)CO.,LTD., China; Wang Jun, AVIC XI'AN AIRCRAFT INDUSTRIAL(GROUP)CO,.LTD., China
STUDY ON COMPRESSION MODE OF THE FRONT LANDING GEAR OF MODERN ARK SERIES AIRCRAFT ON THE TEST BENCH
ICAS2020-P7.3: Q.-XS Xianshuang, Nanjing Engineering Institute of Aircraft Systems,AVIC(NEIAS), China
PATENT ANALYSIS OF APPLICATION OF FUEL CELLS IN AIRCRAFT AS ELECTRICAL POWER SOURCE
ICAS2020-P7.4: Y.-Q. Jia, AVIC Nanjing Engineering Institute of Aircraft System, China
RESEARCH ON DESIGN AND EXPERIMENT OF INTERMEDIATE FREQUENCY LINE-START PMSM USED IN AVIATION
ICAS2020-P7.5: C.-C Chen, AVIC, China
PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORK
ICAS2020-P7.6: W.-J Mo, Chengdu Aircraft Industrial (Group) Co., Ltd, China
RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUE
ICAS2020-P7.7: W K KAI, AVIC XI’AN AIRCRAFT INDUSTRY(GROUP) COMPANY LTD, China
RESEARCH AND TEST ON ELECTROSTATIC MEASUREMENT TECHNOLOGY OF AIRCRAFT FUEL SYSTEM PIPELINE AND FUEL TANK
ICAS2020-P7.8: Bin Wu¹, Yifan Zhu¹, Feng Fang¹; ¹COMAC Shanghai Aircraft Design and Research Institute, China
BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCH
ICAS2020-P7.9: R.F. FAN, AVIC, China
RESEARCH AND APPLICATION OF THE BOOST ENERGY STORAGE SUBSYSTEM
ICAS2020-P7.10: H.C.L Chenglong, China National Aeronautical Radio Electronics Research Institute, China
FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION
ICAS2020-P7.11: Z Liu, Xi'an Flight Automatic Control Research Institute, China
MEMS-BASED DISTRIBUTED NAVIGATION SYSTEM

8 - Manufacturing and Supply Chain Management

ICAS2020-P8.1: Z.X.S Zhu, AVIC Chengdu Aircraft Industrial (Group)Co., Ltd, China
ASSEMBLY QUALITY OPTIMIZATION APPROACH FOR LARGE-SCALE ACTIVE COMPONENTS BASED ON REVERSE ENGINEERING
ICAS2020-P8.2: Aiming Xu Aiming, Chengdu Aircraft Industrial (Group) Co., Ltd., China
ENABLING THE SMART SHOP FLOOR THROUGH THE INTEGRATION OF IOT AND AUTONOMOUS INTELLIGENCE

9 - Air Transport System Efficiency

ICAS2020-P9.1: A. Jankowski, Air Force Institute of Technology, Warsaw Poland, Poland
THE DECISION MODEL OF MOVEMENT MANAGEMENT ON AN AIRPORT APRON IN THE ASPECT OF MINIMIZING EMISSION OF EXHAUST GASES
ICAS2020-P9.2: A. Jankowski, Air Force Institute of Technology, Warsaw Poland, Poland
THE ALGORITHM OF THE SELECTION OF VEHICLE ROUTES FOR SERVICING AIRCRAFTS ON THE APRON

10 - Safety and Security

ICAS2020-P10.1: P. V. Padrao, Federal University of Rio de Janeiro, Brazil
KINEMATIC MODEL-BASED SENSOR FAULT DETECTION AND DIAGNOSIS APPLIED TO AN AUTONOMOUS SOLAR-POWERED AIRCRAFT
ICAS2020-P10.2: T. Hajek, Brno University of Technology, Czech Republic
GRAVITY ACCELERATED FULL SCALE FREE FIGHT TEST FOR PARACHUTE RECOVERY SYSTEMS
ICAS2020-P10.3: S.-N. SONG, China
SIMULATION STUDY ON EMERGENCY EVACUATION OF TYPICAL CIVIL AIRCRAFT

11 - Operations and Sustainment

ICAS2020-P11.1: J SUN, AECC Shenyang Engine Research Institute, China
STUDY ON WEAR TREND PREDICTION OF THE AERO-ENGINE BASED ON GENERAL REGRESSION NEURAL NETWORK AND OIL ANALYSIS DATA
ICAS2020-P11.2: L.Yq Liu, AVIC, China
SYNCHRONOUS HYDRAULIC SYSTEM DESIGN OF AIRCRAFT JACK
ICAS2020-P11.3: LRp Liu, Nanchang Hangkong University, China
THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE
ICAS2020-P11.4: M. JACYNA, Warsaw University of Technology, Poland
DATABASE ARCHITECTURE FOR THE EVALUATION OF SERVICES CARRIED OUT BY AIR CARGO OPERATORS

15 - Guest lectures

ICAS2020-P15.1: M Peters, DGLR, Germany
TEST3