ACCEPTED PAPERS - CATEGORY C - POSTERSThese papers were presented in the Poster area |
1 - Aircraft Design and Integrated Systems |
ICAS2018_0222: H. Zhang¹, B.F. Song¹, H. Ma¹, W. Fang¹; ¹ School of Aeronautics, Northwestern Polytechnical University, China ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE |
ICAS2018_0522: M. Gehlen¹, P. Tadeu de Mello Lourencao¹, L. Gonzaga Trabasso, ITA, Brazil; ¹EMBRAER S.A., Brazil EDUCATING ENGINEERS FOR THE DEVELOPMENT OF PRODUCT SERVICE SYSTEMS (PSS) |
ICAS2018_0086: X. He, Aviation Industry Development Research Center of China, China STUDY ON RADRA CROSS SECTION FOR FLYING-WING UNMANNED AERIAL VEHICLE WITH CLOSE FORMATION FLIGHT |
ICAS2018_0216: Y. Hong¹, D. Han¹, K. Yee¹; ¹Seoul National University, South Korea DESIGN PARAMETER STUDY OF DRONE BLADE CONSIDERING AEROACOUSTICS |
ICAS2018_0598: J.M. Souza¹, F.M. Catalano¹; ¹University of São Paulo, Brazil MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLET |
ICAS2018_0385: S.-M. Hong¹, M.-J. Tahk¹; ¹KAIST, South Korea MULTISTAGE MISSILE TRAJECTORY AND STAGE OPTIMIZATION VIA DELTA-V APPROACH |
ICAS2018_0874: L. Pan, Shanghai Aircraft Design and Research Institute, China PRELIMINARY DESIGN FOR A LOW REYNOLDS NUMBER BWB UAV DEMONSTRATOR |
ICAS2018_0814: P.D. Bravo-Mosquera¹, A.M. Abdalla¹, H.D. Cerón-Muñoz¹, F.M. Catalano ¹; ¹EESC-USP, Brazil DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION |
ICAS2018_0627: C. López Sánchez, Spain; D. Sánchez Franco, Spain; R. Chaitanya Munjulurynjulury, Sweden HURRICANE-CS: CONTROL SURFACES AND HIGH LIFT DEVICES MODELING AND SIZING PROGRAM |
2 - Systems Engineering and Integration |
ICAS2018_0405: B. Wu¹, X. Qiu¹, F. Fang¹, Z. Yao¹; ¹COMAC Shanghai Aircraft Design and Research Institute, China CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH |
ICAS2018_0553: L.J. Ribeiro¹, M.S. de Sousa¹; ¹Federal University of Itajubá, Brazil STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENT |
ICAS2018_0610: Z. Yao¹, B. Guo, China-Russia Commercial Aircraft International Co., China; D. Xie¹, Z. Li¹; ¹Shanghai Aircraft Design and Research Institute, China RESEARCH ON DESKTOP VIRTUAL INTEGRATION AND VERIFICATION OF CIVIAL AIRCRAFT |
3.1 - Aerodynamics - CFD Methods and Validation |
ICAS2018_0326: Z. Tan, China; Y. Chen, China; J. Si, China; Y. Zhong, China NUMERICAL ANALYSIS OF BLEND-WING-BODY AIRFRAME AND ENGINE AERODYNAMIC INTERFERENCE |
ICAS2018_0231: G. Qian¹, D. Wu¹, C. Ma¹; ¹COMAC, China NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFT |
ICAS2018_0525: D. Han¹, J.Y. Huh¹, S. Noh¹, K.H. Kim¹; ¹Seoul National University, South Korea ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHOD |
ICAS2018_0001: G. Qian¹, J. Si¹, K. Liu¹; ¹COMAC, China NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADS |
3.2 - Experimental Aerodynamics |
ICAS2018_0116: Y. Sun¹, C. Breard¹, X. Li¹, Y. Chen¹; ¹Shanghai Aircraft Design and Research Institute of COMAC, China CHALLENGES OF AERO-ACOUSTIC MEASUREMENTS IN WIND TUNNEL: IDENTIFICATION AND ELIMINATION OF "PARASITE" NOISE |
ICAS2018_0364: D. Vukovic¹, V. Lapcevic¹, D. Marinkovski¹, M. Samardzic¹, L. Petrovic¹; ¹Military technical institute (VTI), Serbia DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES |
3.4 - Applied Aerodynamics |
ICAS2018_0846: T. Melin, Svenska Flygtekniska Institutet, Sweden; A.A. Gastaldi¹, M. Zhang¹; ¹Airinnova, Sweden IMPLEMENTATION OF A VORTEX LATTICE METHOD IN A HETEROGENEOUS PROGRAMMING LANGUAGE ENVIRONMENT |
ICAS2018_0685: T. Yoon, South Korea; K. Yee, South Korea DESIGN OPTIMIZATION OF AIRFOIL FOR WIND TURBINE WITH RESPECT TO ICE ACCRETION |
ICAS2018_0649: G.B. Campos¹, J.T. Tomita¹, F.P. Costa¹, C. Bringhenti¹, O. Petit², T. Grönstedt², A.C. Patrao², G. Trapp³, C.R.I. Silva³, A. Lundbladh, GKN, Sweden; ¹Instituto Tecnológico de Aeronáutica, Brazil; ²Chalmers, Sweden; ³Embraer, Brazil PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS |
ICAS2018_0151: Y.L. Zheng¹, Q.L. Qu¹, P.Q. Liu¹; ¹Beihang University, China HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHT |
ICAS2018_0258: R. Kulhánek¹, Z. Pátek¹, P. Vrchota¹, N. Žižkovský¹, J. Cecrdle¹; ¹VZLÚ, a.s., Czech Republic EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS |
ICAS2018_0670: A.A.F. Barbosa¹, F.M. Catalano¹; ¹University of Sao Paulo (EESC-USP), Brazil INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTS OF AN AIRPLANE |
4.1 - Material Issues, Fatigue and Damage Tolerance |
ICAS2018_0516: B.L. Nolli¹, A.T.A. Melo¹, C.A. Cimini Jr.¹; ¹UFMG, Brazil CRACK PROPAGATION STARTING AT HOLE’S EDGE GROWING TO PLATE’S MAJOR DIMENSION USING FEM |
ICAS2018_0293: Q. Wang, The Research Institute for Special Structures of Aeronautical Co, China; J. Tian, he Research Institute for Special Structures of Aeronautical Com, China EFFECT OF DIELECTRIC PROPERTIES DUE TO THE CHANGE OF DIELECTRIC AS A RESULT OF ELEVATORY TEMPERATURE |
ICAS2018_0017: R.M.V. Campos, Universidade Católica de Minas Gerais, Brazil COMPARATIVE STUDY AND VALIDATION OF MATERIAL WITH BETTER PERFORMANCE IN TERMS OF THERMAL ABSORPTION INSIDE AN AIRCRAFT |
ICAS2018_0512: A.T.A. Melo¹, B.L. Nolli¹, C.A. Cimini Jr.¹; ¹Universidade Federal de Minas Gerais, Brazil FINITE ELEMENT MODEL DEVELOPMENT FOR SIMULTANEOUS CRACK PROPAGATION IN TWO COOPERATIVE LUGS |
4.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity |
ICAS2018_0579: D. Andrade¹, W. Corbelli¹, R. Martins¹, R. Queiroz¹; ¹Universidade Federal de Minas Gerais, Brazil STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS |
ICAS2018_0659: R.S. Martins¹, M.T. Santos, Embraer, Brazil; E.S. Palma¹; ¹UFMG, Brazil FASTENING ANALYSIS USING LOW FIDELITY FINITE ELEMENT MODELS |
ICAS2018_0173: L.A. Magerramova¹, M.E. Volkov¹, A.I. Afonin¹, M.S. Svinareva¹, D.V. Kalinin¹; ¹CIAM, Russia APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADES |
ICAS2018_0356: M. Wojtas¹, T. Szczepanik¹, L. Czajkowski¹; ¹Institute of Aviation, Poland NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTS |
ICAS2018_0329: V. Paiva¹, P. Kurka¹, J. Izuka, UNICAMP - FCA, Brazil; ¹UNICAMP - FEM, Brazil KINEMATICS AND DYNAMICS OF A TENSEGRITY STRUCTURE IN EXPANSION |
5 - Propulsion |
ICAS2018_0027: N. Liu, Shanghai Aircraft Design & Research Institute, China A ROBUST STABLE PI CONTROLLER DESIGN IN TIME-FREQUENCY DUAL DOMAINS FOR AIRCRAFT ENGINE |
ICAS2018_0058: J.-F. Sui, COMAC, China THRUST REVERSER INADVERTENT DEPLOYMENT IMPACT STUDY ON AIRPLANE CONTROLLABILITY |
ICAS2018_0645: V.Y. Aleksandrov¹, M.V. Ananyan, MIPT, Russia; K.Y. Arefyev¹, O.D. Dikova², A.N. Prokhorov¹, K.V. Fedotova², L.S. Yanovskiy¹; ¹CIAM, Russia; ²BMSTU, Russia INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS |
ICAS2018_0119: Y. Sun¹, C. Breard¹, X.P. Li¹, Y. Mei², P. Liu², M.B. Pang²; ¹Shanghai Aircraft Design and Research Institute of COMAC, China; ²COMAC Flight Test Center, China IN-FLIGHT ACOUSTIC LOADS MEASUREMENTS ON AN ENGINE FLYING TEST BED |
ICAS2018_0243: X.D. Yang, China; Z.B. Liu, China; S.L. Zhang, China; C. Song, China AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDE |
6.1 - Flight Dynamics and Control (Control & Modelling) |
ICAS2018_0613: T. Rogalski¹, A. Tomczyk¹; ¹Rzeszów University of Technology, Poland APPLICATION OF THE DISTURBANCE VALUE MEASURED DURING THE REAL FLIGHT TO THE FLIGHT CONTROL SYSTEM SYNTHESIS |
6.2 - Flight Dynamics and Control (UAV related) |
ICAS2018_0233: J.-P. Theron¹, L. Dala, Northumbria University Newcastle, United Kingdom; D.N. Wilke¹, P. Barrier, UAS consultant, South Africa; ¹University of Pretoria, South Africa PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV |
ICAS2018_0260: J.-W. Lee¹, A.T. Nguyen, Le Quy Don Technical University , Vietnam; J.-H. Han¹; ¹KAIST, South Korea LONGITUDINAL FLIGHT CONTROL OF BIOINSPIRED FLAPPING-WING MICRO AIR VEHICLE WITH EXTENDED UNSTEADY VORTEX-LATTICE METHOD. |
7 - Systems, Subsystems and Equipment |
ICAS2018_0463: J. Schminder¹, R. Hällqvist², M. Eek², R. Gårdhagen¹; ¹Linköping University, Sweden; ²Saab Aeronautics, Sweden PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL |
ICAS2018_0569: A.C. Sanches¹, F.J. Silvestre¹, M.A.V. Morales¹, H. Hesse, University of Glasgow, Singapore; ¹Aeronautics Institute of Technology, Brazil DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION |
ICAS2018_0684: H. Pham¹, Y. Lim¹, A. Gardi¹, R. Sabatini¹, E. Pang¹; ¹RMIT University, Australia A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFT |
ICAS2018_0214: J.P. Kang¹, G.J. Shim¹, K.J. Yee¹; ¹Seoul national university, South Korea COST-EFFECTIVE TELEMETRY, TRACKING AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOON |
ICAS2018_0402: D.H. Arjoni¹, E. Villani¹, M. Rodríguez¹, A. Matheus¹, A. Almeida¹, G. Rocha¹, L.G. Trabasso¹, D. Hidalgo, UPB, Colombia; ¹ITA, Brazil EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS |
8 - Manufacturing and Supply Chain Management |
ICAS2018_0319: P. Xu¹, X. Wang¹, S. Bi¹, H. Cui¹; ¹Shenyang Aircraft Design and Resesarch Institute, China APPLICATION RESEARCH OF LARGE-SCALED COMPLICATED FRAME-BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURING |
9 - Air Transport System Efficiency |
ICAS2018_0268: B. Cui¹, L. Meilong¹, R. Curran, Delft University of Technology, Netherlands; ¹Nanjing University of Aeronautics and Astronautics, China CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORK |
ICAS2018_0282: J. Ren¹, L. Wang¹; ¹Civil Aviation University of China, China VISUAL FLIGHT PROCEDURE DESIGN IN CHINA |
ICAS2018_0211: Y. Eun¹, D. Jeon¹; ¹Korea Aerospace Research Institute, South Korea AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONS |
ICAS2018_0810: S.L. Mourão¹, K.A. Oliveira¹; ¹University Center UNA, Brazil THE PRIVATE MANAGEMENT OF BRAZILIAN AIRPORTS - A SHORT ANALYSIS |
10 - Safety and Security |
ICAS2018_0043: L. Höhndorf¹, C. Wang¹, P. Koppitz¹, S. Weiß¹, S. Olmos, Evelop Airlines, Spain; C. Czado, Technical University of Munich, Mathematical Statistics, Germany; F. Holzapfel¹; ¹Technical University of Munich, Flight System Dynamics, Germany INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS |
ICAS2018_0232: C. Wang¹, F. Holzapfel¹; ¹Technical University of Munich, Germany EVALUATION OF AIRCRAFT BRAKING PERFORMANCE BASED ON OPERATIONAL FLIGHT DATA |
ICAS2018_0309: G.C. Rocha, Konatus, Brazil; J. Alfredson, Saab, Sweden; L.G. Trabasso¹, A.N. Almeida¹, A.C. Matheus¹, D.H. Arjoni¹, M.A.R. Diaz¹; ¹ITA, Brazil A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS |
ICAS2018_0378: P.M. Razaboni, Embraer SA, Brazil UNIVERSAL DESIGN FOR AIRCRAFT SAFETY |
11 - Operations and Sustainment |
ICAS2018_0336: R.B. Parra, Fumec University , Brazil; J.C. Almeida Jr, Fumec University, Brazil PREDICTIVE & DETECTIVE MAINTENANCE: EFFECTIVE TOOLS IN THE MANAGEMENT OF AERONAUTICAL PRODUCTS |
ICAS2018_0055: G. Lu¹, T.X. Wu¹; ¹Chengdu Aircraft Design & Institute, China THE TECHNIQUE AND MODELLING FOR EQUIPMENT MAINTAINABILITY QUANTIFICATION IN 3D DIGITAL AIRCRAFT DESIGN CONDITION |
ICAS2018_0307: R.B. Parra¹, J. Laguardia¹; ¹FUMEC University, Brazil ERRORS FROM ENGINEERING IN FLIGHT SAFETY |
12 - Host nation |
ICAS2018_0301: R.B. Parra, FUMEC University, Brazil LEONARDO DA VINCI INTERDISCIPLINARITY |