ACCEPTED PAPERS - CATEGORY C - POSTERS

These papers were presented in the Poster area



1 - Aircraft Design and Integrated Systems

ICAS2018_0222: H. Zhang╣, B.F. Song╣, H. Ma╣, W. Fang╣; ╣ School of Aeronautics, Northwestern Polytechnical University, China
ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE
ICAS2018_0522: M. Gehlen╣, P. Tadeu de Mello Lourencao╣, L. Gonzaga Trabasso, ITA, Brazil; ╣EMBRAER 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. Hong╣, D. Han╣, K. Yee╣; ╣Seoul National University, South Korea
DESIGN PARAMETER STUDY OF DRONE BLADE CONSIDERING AEROACOUSTICS
ICAS2018_0598: J.M. Souza╣, F.M. Catalano╣; ╣University of SŃo Paulo, Brazil
MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLET
ICAS2018_0385: S.-M. Hong╣, M.-J. Tahk╣; ╣KAIST, 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-Mosquera╣, A.M. Abdalla╣, H.D. Cerˇn-Mu˝oz╣, F.M. Catalano ╣; ╣EESC-USP, Brazil
DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION
ICAS2018_0627: C. Lˇpez Sßnchez, Spain; D. Sßnchez 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. Wu╣, X. Qiu╣, F. Fang╣, Z. Yao╣; ╣COMAC Shanghai Aircraft Design and Research Institute, China
CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH
ICAS2018_0553: L.J. Ribeiro╣, M.S. de Sousa╣; ╣Federal University of Itajubß, Brazil
STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENT
ICAS2018_0610: Z. Yao╣, B. Guo, China-Russia Commercial Aircraft International Co., China; D. Xie╣, Z. Li╣; ╣Shanghai 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. Qian╣, D. Wu╣, C. Ma╣; ╣COMAC, China
NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFT
ICAS2018_0525: D. Han╣, J.Y. Huh╣, S. Noh╣, K.H. Kim╣; ╣Seoul National University, South Korea
ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHOD
ICAS2018_0001: G. Qian╣, J. Si╣, K. Liu╣; ╣COMAC, China
NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON SUPERCRITICAL WING AERODYNAMIC LOADS

3.2 - Experimental Aerodynamics

ICAS2018_0116: Y. Sun╣, C. Breard╣, X. Li╣, Y. Chen╣; ╣Shanghai 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. Vukovic╣, V. Lapcevic╣, D. Marinkovski╣, M. Samardzic╣, L. Petrovic╣; ╣Military technical institute (VTI), Serbia
DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES

3.4 - Applied Aerodynamics

ICAS2018_0846: T. Melin, Svenska Flygtekniska Institutet, Sweden; A.A. Gastaldi╣, M. Zhang╣; ╣Airinnova, 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. Campos╣, J.T. Tomita╣, F.P. Costa╣, C. Bringhenti╣, O. Petit▓, T. Gr÷nstedt▓, A.C. Patrao▓, G. Trapp│, C.R.I. Silva│, A. Lundbladh, GKN, Sweden; ╣Instituto Tecnolˇgico de Aeronßutica, Brazil; ▓Chalmers, Sweden; │Embraer, Brazil
PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS
ICAS2018_0151: Y.L. Zheng╣, Q.L. Qu╣, P.Q. Liu╣; ╣Beihang University, China
HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHT
ICAS2018_0258: R. Kulhßnek╣, Z. Pßtek╣, P. Vrchota╣, N. Äi×kovskř╣, J. Cecrdle╣; ╣VZL┌, a.s., Czech Republic
EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS
ICAS2018_0670: A.A.F. Barbosa╣, F.M. Catalano╣; ╣University 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. Nolli╣, A.T.A. Melo╣, C.A. Cimini Jr.╣; ╣UFMG, Brazil
CRACK PROPAGATION STARTING AT HOLEĺS EDGE GROWING TO PLATEĺS 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 Catˇlica 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. Melo╣, B.L. Nolli╣, C.A. Cimini Jr.╣; ╣Universidade 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. Andrade╣, W. Corbelli╣, R. Martins╣, R. Queiroz╣; ╣Universidade Federal de Minas Gerais, Brazil
STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS
ICAS2018_0659: R.S. Martins╣, M.T. Santos, Embraer, Brazil; E.S. Palma╣; ╣UFMG, Brazil
FASTENING ANALYSIS USING LOW FIDELITY FINITE ELEMENT MODELS
ICAS2018_0173: L.A. Magerramova╣, M.E. Volkov╣, A.I. Afonin╣, M.S. Svinareva╣, D.V. Kalinin╣; ╣CIAM, Russia
APPLICATION OF LIGHT LATTICE STRUCTURES FOR GAS TURBINE ENGINE FAN BLADES
ICAS2018_0356: M. Wojtas╣, T. Szczepanik╣, L. Czajkowski╣; ╣Institute of Aviation, Poland
NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTS
ICAS2018_0329: V. Paiva╣, P. Kurka╣, J. Izuka, UNICAMP - FCA, Brazil; ╣UNICAMP - 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. Aleksandrov╣, M.V. Ananyan, MIPT, Russia; K.Y. Arefyev╣, O.D. Dikova▓, A.N. Prokhorov╣, K.V. Fedotova▓, L.S. Yanovskiy╣; ╣CIAM, Russia; ▓BMSTU, Russia
INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONS IN PERMANENT SECTION CHANNELS
ICAS2018_0119: Y. Sun╣, C. Breard╣, X.P. Li╣, Y. Mei▓, P. Liu▓, M.B. Pang▓; ╣Shanghai Aircraft Design and Research Institute of COMAC, China; ▓COMAC 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. Rogalski╣, A. Tomczyk╣; ╣Rzeszˇw 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. Theron╣, L. Dala, Northumbria University Newcastle, United Kingdom; D.N. Wilke╣, P. Barrier, UAS consultant, South Africa; ╣University of Pretoria, South Africa
PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV
ICAS2018_0260: J.-W. Lee╣, A.T. Nguyen, Le Quy Don Technical University , Vietnam; J.-H. Han╣; ╣KAIST, 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. Schminder╣, R. Hńllqvist▓, M. Eek▓, R. Gňrdhagen╣; ╣Link÷ping University, Sweden; ▓Saab Aeronautics, Sweden
PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL
ICAS2018_0569: A.C. Sanches╣, F.J. Silvestre╣, M.A.V. Morales╣, H. Hesse, University of Glasgow, Singapore; ╣Aeronautics Institute of Technology, Brazil
DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION
ICAS2018_0684: H. Pham╣, Y. Lim╣, A. Gardi╣, R. Sabatini╣, E. Pang╣; ╣RMIT University, Australia
A NOVEL BISTATIC LIDAR SYSTEM FOR EARLY-DETECTION OF PLANT DISEASES FROM UNMANNED AIRCRAFT
ICAS2018_0214: J.P. Kang╣, G.J. Shim╣, K.J. Yee╣; ╣Seoul national university, South Korea
COST-EFFECTIVE TELEMETRY, TRACKING AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOON
ICAS2018_0402: D.H. Arjoni╣, E. Villani╣, M. RodrÝguez╣, A. Matheus╣, A. Almeida╣, G. Rocha╣, L.G. Trabasso╣, D. Hidalgo, UPB, Colombia; ╣ITA, Brazil
EXPERIMENTAL ANALYSIS OF FLIGHT PERFORMANCE UNDER WORKLOAD VARIATIONS

8 - Manufacturing and Supply Chain Management

ICAS2018_0319: P. Xu╣, X. Wang╣, S. Bi╣, H. Cui╣; ╣Shenyang 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. Cui╣, L. Meilong╣, R. Curran, Delft University of Technology, Netherlands; ╣Nanjing University of Aeronautics and Astronautics, China
CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORK
ICAS2018_0282: J. Ren╣, L. Wang╣; ╣Civil Aviation University of China, China
VISUAL FLIGHT PROCEDURE DESIGN IN CHINA
ICAS2018_0211: Y. Eun╣, D. Jeon╣; ╣Korea Aerospace Research Institute, South Korea
AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONS
ICAS2018_0810: S.L. MourŃo╣, K.A. Oliveira╣; ╣University Center UNA, Brazil
THE PRIVATE MANAGEMENT OF BRAZILIAN AIRPORTS - A SHORT ANALYSIS

10 - Safety and Security

ICAS2018_0043: L. H÷hndorf╣, C. Wang╣, P. Koppitz╣, S. Wei▀╣, S. Olmos, Evelop Airlines, Spain; C. Czado, Technical University of Munich, Mathematical Statistics, Germany; F. Holzapfel╣; ╣Technical University of Munich, Flight System Dynamics, Germany
INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS
ICAS2018_0232: C. Wang╣, F. Holzapfel╣; ╣Technical 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. Trabasso╣, A.N. Almeida╣, A.C. Matheus╣, D.H. Arjoni╣, M.A.R. Diaz╣; ╣ITA, 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. Lu╣, T.X. Wu╣; ╣Chengdu Aircraft Design & Institute, China
THE TECHNIQUE AND MODELLING FOR EQUIPMENT MAINTAINABILITY QUANTIFICATION IN 3D DIGITAL AIRCRAFT DESIGN CONDITION
ICAS2018_0307: R.B. Parra╣, J. Laguardia╣; ╣FUMEC University, Brazil
ERRORS FROM ENGINEERING IN FLIGHT SAFETY

12 - Host nation

ICAS2018_0301: R.B. Parra, FUMEC University, Brazil
LEONARDO DA VINCI INTERDISCIPLINARITY