33th 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



1.1 - Aircraft Design and Integrated System (Basics and Theory)

ICAS2022-P1.1.1 - ICAS2022_0189: P.B. Barros Soares, Embraer S.A., Brazil
INVENTIVE PROBLEM-SOLVING PRINCIPLES APPLIED TO DECISION-MAKING PROCESS OF PRODUCTS PLATFORM

1.2 - Aircraft Design and Integrated System (Applications)

ICAS2022-P1.2.1 - ICAS2022_0541: J. Gauvrit-Ledogar¹, N. Berend¹, J. Hermetz¹; ¹ONERA, France
FLIGHT EXPERIMENTS FOR THE ALTAIR SEMI-REUSABLE AIR-LAUNCH SYSTEM WITH THE DEMONSTRATOR EOLE
ICAS2022-P1.2.2 - ICAS2022_0778: J. J. Lee, Korea Aerospace Research Institute, South Korea
DESIGN STUDY OF BRAKE MECHANICAL CONTROL SYSTEM OF UAV

2 - Systems Engineering and Integration

ICAS2022-P2.1 - ICAS2022_0079: Stephen J Wright, Tampere University, Finland
FUEL CELLS AND NOVEL THERMAL MANAGEMENT ADVANCEMENTS REQUIRED FOR AVIATION
ICAS2022-P2.2 - ICAS2022_0472: T.I. Inal, Turkish Aerospace, Turkey
A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS
ICAS2022-P2.3 - ICAS2022_0477: A.D Oprea, Saab AB, Sweden
MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGN
ICAS2022-P2.4 - ICAS2022_0493: B.-W Bi, Northwestern Polytechnical University, China
HUMAN-MACHINE FUNCTION ALLOCATION METHOD FOR SINGLE PILOT OPERATION USING HESITANT FUZZY 2-TUPLE LINGUISTIC INFORMATION
ICAS2022-P2.5 - ICAS2022_0526: C. Jochims Lau, AEL Sistemas, Brazil
EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS
ICAS2022-P2.6 - ICAS2022_0655: Eric Razafimahazo¹, Pierre de Saqui-Sannes¹, Rob Vingerhoeds¹, Julien Soula², Romain Mège², Claude Baron, LAAS-CNRS, France; ¹ISAE-SUPAERO, France; ²CSTB, France
TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES
ICAS2022-P2.7 - ICAS2022_0661: Petter Andersson, GKN AErospace, Sweden
DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINE
ICAS2022-P2.8 - ICAS2022_0724: E. Allegaert, Siemens Digital Industries Software, Belgium
TEMPLATE-BASED SYNTHESIS OF 3D SYSTEMS FOR MBSE

3.1 - Aerodynamics – CFD Methods and Validation

ICAS2022-P3.1.1 - ICAS2022_0124: D. Standingford¹, C. Sequeira², M. Allan¹, G. Furse², J. Sharpe¹; ¹Zenotech, United Kingdom; ²Flare Bright, United Kingdom
VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA
ICAS2022-P3.1.2 - ICAS2022_0260: L.-V. Velandia, Brazil
VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOW
ICAS2022-P3.1.3 - ICAS2022_0353: GM Muchla, Warsaw University of Technology, Poland
COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS OBTAINED BY ANALYTICAL, PANEL AND CFD METHODS.
ICAS2022-P3.1.4 - ICAS2022_0414: B.G. Kierulf, United States
CRITICAL REVIEW OF SOUNDING ROCKET FLIGHT DATA AND COMPUTATIONAL FLUID DYNAMICS EFFORTS
ICAS2022-P3.1.5 - ICAS2022_0422: H.-Y. Li, Northwestern Polytechnical University, China
A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLES
ICAS2022-P3.1.6 - ICAS2022_0487: Z.-P Li, AECC Shenyang Engine Research Institute, China
REDESIGNING AND SIMULATION EVALUATION ON LARGE-FLOW HIGH-TEMPERATURE HIGH-PRESSURE BYPASS SURGE-OUT SYSTEM
ICAS2022-P3.1.7 - ICAS2022_0515: H.-Y. Li, Northwestern Polytechnical University, China
AERO PROPELLER NOISE SIMULATION BY CFD METHOD

3.2 - Experimental Aerodynamics

ICAS2022-P3.2.1 - ICAS2022_0078: YJ Shen, China
EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING
ICAS2022-P3.2.2 - ICAS2022_0256: X.W. Jiang, China
EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE
ICAS2022-P3.2.3 - ICAS2022_0417: R. Yao, Northwestern Polytechnical University, China
INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX
ICAS2022-P3.2.4 - ICAS2022_0589: B.-B. Jia, AECC Shenyang Engine Institute, China
SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR
ICAS2022-P3.2.5 - ICAS2022_0855: F. Petrosino, CIRA, Italy
COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE MODELLING

3.3 - Basic Fluid Dynamics and Flow Control

ICAS2022-P3.3.1 - ICAS2022_0388: HM Marbona, Universidad Politécnica de Madrid, Spain
INSTABILITY AND TRANSITION OF SEPARATED FLOW UNDER UNSTEADY INLET CONDITIONS AND EXTERNAL ACTUATION

3.4 - Applied Aerodynamics

ICAS2022-P3.4.1 - ICAS2022_0165: Wang-Yi Zhou¹, Guo-Qiang Yang¹, Xiang Gao¹, Xue-Yao Zhu¹, Bo-Xiao Zhou¹; ¹AVIC Xi’an Flight Automatic Control Research Institute, China
NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR
ICAS2022-P3.4.2 - ICAS2022_0319: W.-Z. Zhou, AVIC Chengdu Aircraft Industrial (Group) Co., Ltd. , China
RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY
ICAS2022-P3.4.3 - ICAS2022_0329: C. Ge, China
NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS
ICAS2022-P3.4.4 - ICAS2022_0860: D. Perdolt, German Aerospace Center, Institute of System Dynamics and Contro, Germany
EFFICIENT AERODYNAMIC MODELING PROCESS FOR A TILT-WING EVTOL USING A MID-FIDELITY COMPUTATIONAL TOOL

4.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance

ICAS2022-P4.1.1 - ICAS2022_0278: W.D. Wang, Northwestern Polytechnical University, China
STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE
ICAS2022-P4.1.2 - ICAS2022_0460: M.Z Polat, Ankara Yildirim Beyazit University, Turkey
DESIGN OF SANDWICH STRUCTURES FOR HIGH VIBRATION AND NOISE CONDITIONS
ICAS2022-P4.1.3 - ICAS2022_0894: M A Atif, NWPU, China
HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS

4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity

ICAS2022-P4.2.1 - ICAS2022_0311: K Lu, Northwestern Polytechnical University, China
A STUDY ON THE AEROELASTICITY OF AIR-TO-AIR MISSLE IN OVER-THE-SHOULDER LAUNCH
ICAS2022-P4.2.2 - ICAS2022_0770: B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia
BENDING-TORSION FLUTTER OF TAPERED COMPOSITE FINS: ANALYSIS AND EXPERIMENT
ICAS2022-P4.2.3 - ICAS2022_0867: Zia Ur Rehman Rehman, Pakistan
DEVELOPMENT OF NOVEL ANALYTICAL METHOD FOR TIME DOMAIN AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO WING USING UNSTEADY IND

5 - Propulsion

ICAS2022-P5.1 - ICAS2022_0019: S.B Bhurat, RVCE, India
NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAV FOR EXTRA-TERRESTRIAL APPLICATIONS
ICAS2022-P5.2 - ICAS2022_0094: J. Juracka¹, M. Cervenka¹, M. Horak¹, M. Splichal¹; ¹Brno University of Technology, Czech Republic
TREND MONITORING OF TURBOPROP ENGINES
ICAS2022-P5.3 - ICAS2022_0203: Zhang Chunlei¹, Chen Hao¹, Li Yi¹; ¹AECC, China
NUMERICAL INVESTIGATION ON TURBINE SHROUD FILM COOLING HEAT TRANSFER PERFORMANCE OF TURBINE BLADE WITH GROOVE TIP
ICAS2022-P5.4 - ICAS2022_0223: R. W. Wang, School of power and energy/Northwest Polytechnical University, China
NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS
ICAS2022-P5.5 - ICAS2022_0234: M. Bruno¹, R. Cambertoni¹, A. Pellegrino¹, P. Petrachi¹, C. Spampinato¹; ¹Polytechnic of Turin, Italy
ANALYSIS AND SIZING OF A GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT
ICAS2022-P5.6 - ICAS2022_0244: Z. Zhang, China
AEROACOUSTICS SIMULATION OF 3X3 CONTRA-ROTATING PROPELLER
ICAS2022-P5.7 - ICAS2022_0473: - Max, Germany
UNSTEADY FLOW PHENOMENA IN A HIGHLY BEND ENGINE INTAKE WITH PASSIVE AND ACTIVE FLOW CONTROL
ICAS2022-P5.8 - ICAS2022_0603: G.-F Gao, AECC, China
ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATE
ICAS2022-P5.9 - ICAS2022_0631: S.S. Sahoo, Mälardalen University, Sweden
THERMAL MANAGEMENT SYSTEM FOR A HYBRID ELECTRIC PROPULSION SYSTEM BASED AIRCRAFT DESIGN
ICAS2022-P5.10 - ICAS2022_0657: J. Schröder, TU Berlin, Germany
TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS
ICAS2022-P5.11 - ICAS2022_0756: M.H. Harada, Kanazawa institute of technology , Japan
EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT -
ICAS2022-P5.12 - ICAS2022_0813: Nhu Van Nguyen, Viettel Aerospace Institute, Viettel Group, Vietnam
MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES

6.1 - Flight Dynamics and Control (Control & Modelling)

ICAS2022-P6.1.1 - ICAS2022_0135: Y. Ochi, National Defense Academy, Japan
FLIGHT TESTS AND SIMULATION OF A HANG GLIDER
ICAS2022-P6.1.2 - ICAS2022_0490: T. J. Ludena Cervantes, Gyeongsang National University, South Korea
NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROL
ICAS2022-P6.1.3 - ICAS2022_0538: H. Lee, Korea Aerospace University, South Korea
GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWING
ICAS2022-P6.1.4 - ICAS2022_0873: Clecio Fischer, Aeronautics Institute of Technology, Brazil
IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING

7 - Systems, Subsystems and Equipment

ICAS2022-P7.1 - ICAS2022_0072: P.-X. Pang, AECC Shenyang Engine Research Institute, China
STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER
ICAS2022-P7.2 - ICAS2022_0100: Melody Liu, Science and Technology on Electro-optic Control Laboratory, China
HIGH-PRECISION MULTI-DISCIPLINARY OPTIMIZATION: CONFIGURATIONS, METHODS AND STRATEGIES
ICAS2022-P7.3 - ICAS2022_0297: W.-L Wang, China
DYNAMIC MODEL AND EXPERIMENT INVESTIGATION OF PIEZOELECTRIC-POWERED DRAGONFLY-SCALE WING FLAPPING
ICAS2022-P7.4 - ICAS2022_0537: - Guo, Shanghai Jiaotong University, China
EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF CFRP COMPOSITE ON ELECTROTHERMAL ANTI-ICING SYSTEM
ICAS2022-P7.5 - ICAS2022_0742: K. K. Borodacz, ?ukasiewicz Research Network – Institute of Aviation, Poland
IMPACT OF MOTION-DEPENDENT ERRORS ON THE ACCURACY OF AN UNAIDED STRAPDOWN INERTIAL NAVIGATION SYSTEM

9 - Air Transport System Efficiency

ICAS2022-P9.1 - ICAS2022_0574: M. Mendiguchia Meuser, University of Technology Hamburg, Germany
MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMISED TRAJECTORIES IN THE EUROPEAN AIRSPACE
ICAS2022-P9.2 - ICAS2022_0798: A Errico, CIRA - Italian Aerospace Research Center, Italy
A METHOD FOR EVALUATING AIRCRAFT DEPENDENCIES USING THE CLOSEST POINT OF APPROACH METHODOLOGY TO SUPPORT ATM OPERATIONS
ICAS2022-P9.3 - ICAS2022_0844: A. Lau, German Aerospace Center (DLR), Germany
CONSIDERATIONS FOR MULTI-CRITERIAL TRAJECTORY DESIGN ON DIFFERENT ATMOSPHERIC SCALES
ICAS2022-P9.4 - ICAS2022_0896: K. K. Silander, Kookiejar of Sweden AB, Sweden
VERTIPORT OPERATIONS IN AN AIRPORT ENVIRONMENT

10 - Safety and Security

ICAS2022-P10.1 - ICAS2022_0177: - Cheng, Chengdu Aircraft Design and research Institute, China
RESEARCH ON LASER COUNTERMEASURE TRACKING AND AIMING TECHNOLOGY BASED ON AIRCRAFT PLATFORM
ICAS2022-P10.2 - ICAS2022_0503: D.Jiewen Deng, Chengdu Aircraft Industry (Group) Co., Ltd, China
RESEARCH ON COUPLING INTERFERENCE CHARACTERISTICS OF AIRCRAFT ELECTRICAL CABLE
ICAS2022-P10.3 - ICAS2022_0669: T de Souza, Brazil
UNDERSTANDING AND IMPROVING SAFETY IN AERONAUTICAL MAINTENANCE: A SAFETY-II APPROACH IN MRO ORGANIZATION

11 - Operations and Sustainment

ICAS2022-P11.1 - ICAS2022_0021: A Sanks, United States Air Force Academy, United States
THE DIONYSUS PROGRAM: 99942 APOPHIS, TRANS-MARS INJECTION AND SPACE LIFT CONSTRUCTION (99942 AT-MIASLC)
ICAS2022-P11.2 - ICAS2022_0817: N/A Rameshbabu, Georgia Institute of Technology, United States
ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH
ICAS2022-P11.3 - ICAS2022_0865: X. Zhao, Nanjing University of Aeronautics and Astronautics, China
ECONOMIC PERFORMANCE EVALUATION OF AIRCRAFT MAINTENANCE USING DATA-DRIVEN APPROACH

14 - Education and Training

ICAS2022-P14.1 - ICAS2022_0209: Wen Zhao, Civil Aviation University of China, China
THE CORPUS-BASED STUDY ON AVIATION ENGLISH FROM SYSTEMATIC FUNCTIONAL LINGUISTICS PERSPECTIVE
ICAS2022-P14.2 - ICAS2022_0315: E.C. Cestino, Politecnico di Torino, Italy
A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCE
ICAS2022-P14.3 - ICAS2022_0675: G Kontos, Abu Dhabi University, United Arab Emirates
PILOT TRAINING CHALLENGES FOR ADVANCED AIR MOBILITY