Preliminary Programme - Interactive Presentations
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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.
ACCEPTED PAPERS - CATEGORY C - INTERACTIVE PRESENTATIONSThese papers will be presented in the Interactive Presentations area |
1.2 - Aircraft Design and Integrated System (Applications) |
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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 |
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ICAS2022-P1.2.2 - ICAS2022_0778: J.-J. Lee¹, J.-H. Lee¹; ¹Korea Aerospace Research Institute, South Korea DESIGN STUDY OF BRAKE MECHANICAL CONTROL SYSTEM OF UAV |
2 - Systems Engineering and Integration |
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ICAS2022-P2.1 - ICAS2022_0079: S.J. Wright¹, J. Aaltonen¹; ¹Tampere University, Finland FUEL CELLS AND NOVEL THERMAL MANAGEMENT ADVANCEMENTS REQUIRED FOR AVIATION |
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ICAS2022-P2.2 - ICAS2022_0472: M.E.A. Enes¹, E. Tugrul¹, M. Yuce¹, N. Sever¹, E. Yigit¹, T. Inal¹; ¹Turkish Aerospace, Turkey A FAULT INTEGRATOR BASED VOTE&MONITOR DESIGN FOR GRACEFULL DEGRADATION IN MULTIPLE REDUNDANT SAFETY CRITICAL SYSTEMS |
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ICAS2022-P2.3 - ICAS2022_0477: A. Oprea¹, R. Hällqvist¹, I. Staack, Linköping University, Sweden; M. Eek, Swedish National Road and Transport Research Institute, Sweden; H. Gavel¹; ¹Saab Aeronautics, Sweden MODEL FIDELITY AND ITS INFLUENCE ON AIRCRAFT CONCEPTUAL DESIGN |
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ICAS2022-P2.4 - ICAS2022_0493: B. Wenhao¹, L. Yuhui¹, W. Weixiang¹, Z. An¹; ¹Northwestern Polytechnical University, China HUMAN-MACHINE FUNCTION ALLOCATION METHOD FOR SINGLE PILOT OPERATION USING HESITANT FUZZY 2-TUPLE LINGUISTIC INFORMATION |
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ICAS2022-P2.5 - ICAS2022_0526: A.G. Slongo¹, C. Jochims Lau¹, T.B. Volkmann¹, G. de Oliveirra¹, G. Heberle¹, B.M. Ramos¹; ¹AEL Sistemas, Brazil EXTRACTING MODEL-BASED SYSTEMS ENGINEERING VALUE THROUGH A MINIMUM VIABLE PRODUCT CASE STUDY AT AEL SISTEMAS |
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ICAS2022-P2.6 - ICAS2022_0655: E. Razafimahazo¹, P. de Saqui-Sannes¹, R.A. Vingerhoeds¹, J. Soula², R. Mège², C. Baron, LAAS-CNRS, France; ¹ISAE-SUPAERO, France; ²CSTB, France TOWARDS A CUSTOMIZABLE ARCHITECTURE FOR INDOOR MULTI-USAGES DRONES |
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ICAS2022-P2.7 - ICAS2022_0661: P. Andersson¹, M. Lejon¹, A. Pradas¹, M. Jacobson¹; ¹GKN Aerospace Sweden, Sweden DEMONSTRATING AN APPROACH FOR MULTIDISCIPLINARY SET BASED DESIGN WITHIN AN AEROSPACE RESEARCH PROJECT - DEFAINE |
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ICAS2022-P2.8 - ICAS2022_0724: E. Allegaert¹, Y. Lemmens¹, E. Ongut¹; ¹Siemens Digital Industries Software, Belgium TEMPLATE-BASED SYNTHESIS OF 3D SYSTEMS FOR MBSE |
3.1 - Aerodynamics – CFD Methods and Validation |
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ICAS2022-P3.1.1 - ICAS2022_0124: D. Standingford¹, C. Sequeira², M. Allan¹, C. Rider², G. Furse², J. Sharpe¹; ¹Zenotech, United Kingdom; ²Flare Bright, United Kingdom VALIDATING AIRSPACE CFD MODELS FOR DRONE OPERATION WITH FLIGHT TEST DATA |
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ICAS2022-P3.1.2 - ICAS2022_0260: L.P. Velandia Luis¹, P. Celso Greco Junior¹; ¹University of Sao Paulo, Brazil VISCOUS CORRECTION FOR HIGH ORDER IMMERSED INTERFACE METHOD FOR COMPRESSIBLE TRANSONIC FLOWS |
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ICAS2022-P3.1.3 - ICAS2022_0414: B. Kierulf, Northeastern University, United States CRITICAL REVIEW OF SOUNDING ROCKET FLIGHT DATA AND COMPUTATIONAL FLUID DYNAMICS EFFORTS |
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ICAS2022-P3.1.4 - ICAS2022_0422: H.-Y. Li¹, X. Zhao¹, Z.-X. Xia¹; ¹School of Aeronautics, Northwestern Polytechnical University, China A FAST PREDICTION METHOD FOR DROPPING WATER OF FIRE FIGHTING AIRCRAFT BASED ON EXTERNAL BALLISTICS OF PARTICLES |
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ICAS2022-P3.1.5 - 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 |
3.2 - Experimental Aerodynamics |
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ICAS2022-P3.2.1 - ICAS2022_0078: Y. Shen¹, S. Feng¹, Y. Wang¹, C. Bu¹, H. Tan¹, W. Mu¹, H. Chen¹; ¹AVIC Aerodynamics Research Institute, China EXPERIMENTAL STUDY ON NON-COMMAND MOTION CHARACTERISTICS OF SMALL ASPECT RATIO FLYING WING |
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ICAS2022-P3.2.2 - ICAS2022_0256: X. Jiang¹, G. Liu¹, J. Zhou¹, Q. Jia¹; ¹AECC Shenyang Engine Research Institute, China EXPERIMENTAL INVESTIGATION ON JET IMPINGEMENT HEAT TRANSFER WITH CROSS FLOW FOR AERO-ENGINE INLET CONE |
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ICAS2022-P3.2.3 - ICAS2022_0417: M.-H. Kang¹, X. Zhao¹, R. Yao¹, H.-Y. Li¹; ¹Norhwestern Polytechnical University, China INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX |
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ICAS2022-P3.2.4 - ICAS2022_0589: B.-B. Jia¹, Z.-B. Zhang¹, H.-X. Li, AECC, China; ¹AECC Shenyang Engine Institute, China SURGE CHARACTERISTICS IN FRONT OF EACH STAGE FOR A HIGH PRESSURE FIVE STAGE COMPRESSOR |
3.4 - Applied Aerodynamics |
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ICAS2022-P3.4.1 - ICAS2022_0165: W.-Y. Zhou¹, G.-Q. Yang¹, X. Gao¹, X.-Y. Zhu¹, B.-X. Zhou¹; ¹AVIC Xi’an Flight Automatic Control Research Institute, China NUMERICAL SIMULATION OF MISSILE AIR-LAUNCHED DYNAMIC PROCESS UNDER DOWNWASH FLOW OF HELICOPTER ROTOR |
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ICAS2022-P3.4.2 - ICAS2022_0319: Z. Wei, China RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY |
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ICAS2022-P3.4.3 - ICAS2022_0329: C.H. Ge¹, P.Q. Liu¹, Q.L. Qu¹; ¹Beihang University, China NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS |
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ICAS2022-P3.4.4 - ICAS2022_0860: D. Perdolt¹, D. Milz¹, M. May¹, M. Thiele, Technical University of Munich, Germany; ¹German Aerospace Center, Germany EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS |
4.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance |
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ICAS2022-P4.1.1 - ICAS2022_0278: D. Wang, School of Aeronautics, Northwestern Polytechnical University, Xi, China; G.W. Li, School of civil aviation, Northwestern Polytechnical University, China; H.Y. Huang, School of Aeronautics, Northwestern Polytechnical University, China STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE |
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ICAS2022-P4.1.2 - ICAS2022_0894: M. Atif¹, X.Z. Shi¹, M.A. Raza¹, M.Z. Sheikh¹, J. Shen, Joint International Research Center of Impact Dynamics and Its E, China; Y. Li, School of Civil Aviation, Northwestern Polytechnical University, China; ¹Northwestern Polytechnical University, China HIGH IMPACT AND DAMAGE TOLERANT MULTICOMPONENT ALLOY FOR HIGH STRAIN RATE APPLICATIONS |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
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ICAS2022-P4.2.1 - ICAS2022_0311: K. Lu¹, W.-P. Song¹, K. Ye¹, C.-H. Gao¹, S.-Q. Han, Sichuan University, China; ¹Northwestern Polytechnical University, China A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES IN OVER-THE-SHOULDER LAUNCH |
5 - Propulsion |
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ICAS2022-P5.1 - ICAS2022_0019: S. Bhurat¹, S. Das¹, N.K. Shetty¹; ¹RV College of Engineering, India NUCLEAR POWERED AIR-BREATHING ELECTRIC THRUSTERS USED IN UAVS FOR EXTRA-TERRESTRIAL APPLICATIONS |
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ICAS2022-P5.2 - ICAS2022_0094: J. Juracka¹, M. Cervenka¹, M. Horak¹, M. Splichal¹; ¹Brno University of Technology, Czech Republic TREND MONITORING OF TURBOPROP ENGINES |
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ICAS2022-P5.3 - ICAS2022_0203: Z. Chunlei¹, C. Hao¹, L. Yi¹; ¹AECC, China NUMERICAL INVESTIGATION ON TURBINE SHROUD FILM COOLING HEAT TRANSFER PERFORMANCE OF TURBINE BLADE WITH GROOVE TIP |
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ICAS2022-P5.4 - ICAS2022_0223: R. Wang¹, Q. Yang¹, S. Zhang¹, K. Du, Guiyang Aero-engine Research Institute, China; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION ANALYSIS OF INFRARED RADIATION AND ELECTROMAGNETIC SCATTERING CHARACTERISTICS OF DIFFERENT MIXERS |
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ICAS2022-P5.5 - ICAS2022_0234: M. Bruno¹, R. Cambertoni¹, A. Pellegrino¹, P. Petrachi¹, C. Spampinato¹; ¹Polytechnic of Turin, Italy ANALYSIS AND SIZING OF GREEN PROPULSION SYSTEM FOR A SUBORBITAL AIRCRAFT |
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ICAS2022-P5.6 - ICAS2022_0603: F. Gao, Northwestern Polytechnical University, China; Z. Zhang¹, J. Li¹; ¹AECC Shenyang Engine Research Institute, China ANALYSIS OF THE AERODYNAMIC CHARACTERISTICS AND ITS INFLUENCE OF TURBOMACHINERY IN TRANSITION STATE |
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ICAS2022-P5.7 - ICAS2022_0657: B.-O. Schröder¹, P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany TESTING AND MODELLING OF A DUCTED FAN MOTOR FOR UAV APPLICATIONS |
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ICAS2022-P5.8 - ICAS2022_0756: M. Harada¹, N. Osawa¹, H. Moriai¹; ¹Kanazawa Institute of Technology, Japan EXPERIMENTAL STUDY ON THE LASER PLASMA JET PROPULSION - PLASMA JET GENERATION AND THRUST MEASUREMENT |
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ICAS2022-P5.9 - ICAS2022_0855: F. Petrosino¹, M. Barbarino¹; ¹CIRA, Italy COMPARISON OF ANALYTICAL SEMI-EMPIRICAL MODEL FOR JET NOISE PREDICTION |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2022-P6.1.1 - ICAS2022_0135: T. Takamatsu¹, Y. Ochi¹; ¹National Defense Academy, Japan FLIGHT TESTS AND SIMULATION OF A HANG GLIDER |
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ICAS2022-P6.1.2 - ICAS2022_0490: T.J. Ludena Cervantes, Peru; Y. Kim, South Korea; B.S. Kim, South Korea NEURAL-NETWORK ADAPTIVE DECENTRALIZED FORMATION CONTROL |
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ICAS2022-P6.1.3 - ICAS2022_0538: H.J. Lee¹, S.H. Hahn¹, S.C. Lee¹; ¹Korea Aerospace University, South Korea GENERATION OF TERRAIN PROFILE FOR TERRAIN FOLLOWING |
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ICAS2022-P6.1.4 - ICAS2022_0873: C. Fischer, ITA and IFSP, Brazil; L.M. Nepomuceno¹, E.A. Moura¹, R.G.A. da Silva¹, L.C.S. Góes¹; ¹ITA, Brazil IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING |
7 - Systems, Subsystems and Equipment |
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ICAS2022-P7.1 - ICAS2022_0072: X. Pang¹, H. Sui¹, X. Jiang¹, G. Liu¹; ¹AECC, China STUDY ON OIL-GAS TWO-PHASE FLOW CHARACTERISTICS IN AIR-OIL HEAT EXCHANGER |
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ICAS2022-P7.2 - ICAS2022_0537: X. Guo¹, Q. Yang¹, H. Zheng¹, W. Dong¹; ¹Shanghai Jiaotong University, China EFFECTS OF ANISOTROPIC THERMAL CONDUCTIVITY OF COMPOSITE SHIELD ON THE ELECTROTHERMAL ANTI-ICING SYSTEMS |
9 - Air Transport System Efficiency |
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ICAS2022-P9.1 - ICAS2022_0574: M. Mendiguchia Meuser¹, B. Luehrs², V. Gollnick¹, F. Linke², S. Matthes³, S. Dietmüller³, S. Baumann³, M. Soler*, A. Simorgh*, F. Yinº, F. Castinoº; ¹University of Technology Hamburg, Institute of Air Transportatio, Germany; ²German Aerospace Center, Air Transportation Systems, Germany; ³German Aerospace Center, Institute of Atmospheric Physics, Germany; *Universidad Carlos III de Madrid, 4Department of Aerospace Engin, Spain; ºDelft University of Technology, Aircraft Noise and Climate Effe , Netherlands MITIGATION OF AVIATION’S CLIMATE IMPACT THROUGH ROBUST CLIMATE OPTIMIZED TRAJECTORIES IN INTRA-EUROPEAN AIRSPACE |
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ICAS2022-P9.2 - ICAS2022_0798: A. Errico¹, V. Di Vito¹; ¹CIRA - Italian Aerospace Research Center, Italy A METHOD FOR EVALUATING AIRCRAFT DEPENDENCIES USING THE CLOSEST POINT OF APPROACH METHODOLOGY TO SUPPORT ATM OPERATIONS |
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ICAS2022-P9.3 - ICAS2022_0844: A. Lau¹, T. Ehlers¹, M. Derra¹, B. Lührs¹; ¹German Aerospace Center (DLR), Germany CONSIDERATIONS FOR MULTI-CRITERIA ROUTE DESIGN ON DIFFERENT ATMOSPHERIC SCALES |
10 - Safety and Security |
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ICAS2022-P10.1 - ICAS2022_0503: J. Deng, China; L. Zhang, China; K. Zhang, China; Z. Wang, China RESEARCH ON CROSSTALK CHARACTERISTICS OF AIRCRAFT ELECTRICAL CABLE |
11 - Operations and Sustainment |
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ICAS2022-P11.1 - ICAS2022_0817: R. Rameshbabu¹, D. Rajaram¹, O.J.P. Fischer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH |
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ICAS2022-P11.2 - ICAS2022_0922: M.P.P. Osund-Ireland¹, A.J. Powell¹, C.J. Ireland¹; ¹susteer AB, Sweden A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS |
14 - Education and Training |
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ICAS2022-P14.1 - ICAS2022_0209: W. Zhao, Civil Aviation University of China, China THE CONVERSATION ANALYSIS OF AVIATION ENGLISH FROM SYSTEMIC FUNCTIONAL LINGUISTICS PERSPECTIV |
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ICAS2022-P14.2 - ICAS2022_0315: E. Cestino, Politecnico di Torino, Italy; V. Sapienza, Aerospace Consultant, Italy; S. Sapienza, Istituto Italiano Psicoanalisi di Gruppo, Italy; F. Carena, Trainer and HR Senior Consultant, Italy A STUDENT TEAM BASED TEACHING APPROACH: THE TEAM S55 EXPERIENCE |
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ICAS2022-P14.3 - ICAS2022_0675: G. Kontos¹, O. Lehmann¹; ¹Abu Dhabi University, United Arab Emirates PILOT TRAINING CHALLENGES FOR ADVANCED AIR MOBILITY |