ACCEPTED PAPERS - CATEGORY C - POSTERSThese papers will be presented in the Poster area |
1 - Aircraft and Systems Integration |
ICAS2016_0058: C. Ma¹, S.P. Yang¹; ¹COMAC, China SYNTHESIZED ANALYSIS FROM DESIGN RANGE TO THE CONCETUAL DESIGN OF WIDEBODY AIRLINER |
ICAS2016_0268: W. Gu¹, Z. Chen¹, B. Zhang¹; ¹Northwestern Polytechnical University, China PHYSICALLY-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION FRAMEWORK COUPLING AIRFRAME AND PROPULSION |
ICAS2016_0020: C. Song, China; X.-D. Yang, China; W.-P. Song, China EFFICIENT AERODYNAMIC OPTIMIZATION USING HIERARCHICAL KRIGING COMBINED WITH GRADIENT |
ICAS2016_0253: C. Ma¹, Z.G. Tan¹; ¹COMAC, China A CONCEPTUAL ANALYSIS OF AN AIRCRAFT WITH REAR-MOUNTED OPEN ROTOR ENGINES |
ICAS2016_0280: C.-J. Kim, Korea Aerospace Industries, Ltd, South Korea FLIGHT TEST FOR TYPE CERTIFICATION ACQUISITION OF SMALL CIVIL AIRPLANE KC-100 |
2.1 - Aerodynamics - CFD Methods and Validation |
ICAS2016_0600: K.-J. Lee, KAI, South Korea FIGHTER AIRCRAFT HIGH AOA DIRECTIONAL STABILITY IMPROVEMENT DESIGN |
ICAS2016_0140: F.-W. Wang¹, L.-C. Chen¹, H. Qin¹, J. Yu¹; ¹CAAA, China DETACHED EDDY SIMULATION OF AIRCRAFT MASSIVELY SEPARATED FLOWS |
ICAS2016_0502: J.S. Rhee¹, J.Y. Huh¹, D. Han¹, K.H. Kim¹, S.Y. Jung, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea A DEVELOPMENT OF MESHLESS POINT GENERATION TECHNIQUE FOR ANALYSIS OF THE UNSTEADY FLOW AROUND THE MULTI-BODY |
ICAS2016_0154: G.P. Qian¹, J.T. Si¹, X.H. Qin¹, Y. Zhong¹; ¹Shanghai Aircraft Design and Research Institute, China NUMERICAL STUDY OF FIXED TRANSITION LOCATION EFFECT ON SUPERCRITICAL WING AERODYNAMIC CHARACTERISTICS |
ICAS2016_0417: R. Szczepaniak¹, R. Babel¹, W. Stryczniewicz, Institute of Aviation , Poland; ¹Air Force Academy, Poland COMPARATIVE ANALYSIS OF AIR FLOW IN THE COMPRESSOR OF THE GTD-350 ENGINE |
ICAS2016_0589: F. Yang¹, S. Yi-Feng¹, Y. Shi-Pu¹; ¹Shanghai Aircraft Design and Reserach Institute, China AERODYNAMIC ANALYSIS OF FLUSH-MOUNTED STATIC PORTS PLACEMENT ON THE COMMERCIAL TRANSPORT AIRCRAFT |
ICAS2016_0125: R.R. Xue¹, Z.Y. Ye¹, G. Wang¹; ¹Northwestern Polytechnical Univ, China AERODYNAMIC CHARACTERISTIC COMPARISON OF THE FORWARD AND BACKWARD-SWEPT WINGS |
2.2 - Experimental Aerodynamics |
ICAS2016_0329: D. Vukovic¹, D. Damljanovic¹; ¹Military Technical Institute (VTI), Serbia A GENERALISATION OF THE MATHEMATICAL MODEL OF INTERNAL WIND TUNNEL BALANCES |
ICAS2016_0671: K.-A. Surmacz, Institute of Aviation, Poland; J. -P. Bons, Ohio State University, United States AN AERODYNAMIC ANALYSIS OF THE 3D FLOW AROUND THE SSC-A09 AIRFOIL |
ICAS2016_0112: S. Yuan¹, Q. Sun¹, L. Wang¹, G. Liu¹; ¹AVIC Shenyang Engine Design & Research Institute, China TOTAL TEMPERATURE RECOVERY CHARACTERISTICS TEST TECHNIQUE BASED ON TOTAL PRESSURE CALIBRATION WIND TUNNEL |
ICAS2016_0593: J. Cervinka¹, R. Kulhánek¹, Z. Pátek¹, V. Kumar, C-CADD, CSIR-NAL, India; ¹VZLÚ - Aerospace Research and Test Establishment, Czech Republic SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL |
ICAS2016_0262: H.D. Cerón-Muñoz¹, D.O. Diaz-Izquierdo¹, P.D. Bravo-Mosquera ¹, F.M. Catalanode¹, L.D. Santana, University of Twente, Netherlands; ¹São Carlos Engineering School-University of São Paulo, Brazil EXPERIMENTAL ANALYSES OF DROOP, WINGTIPS AND FENCES ON A BWB MODEL |
ICAS2016_0587: Z.B. Yan¹, W. Qian¹, R. Yang¹, X.J. Sheng¹; ¹Dalian University of Technology, China THE MANUFACTURE AND APPLICATION FOR COMPOSITES AEROELASTIC MODEL OF CIVIL AIRLINER WING IN FL-26 TRANSONIC WIND-TUNNEL |
ICAS2016_0300: W. Stryczniewicz¹, R. Placek¹, P. Ruchala¹; ¹Institute of Aviation, Poland INVESTIGATION OF UNSTEADY TRANSONIC FLOW FIELD ABOVE LAMINAR AIRFOIL BY PIV METHOD |
ICAS2016_0122: Z. Pátek¹, P. Vrchota¹, J. Cervinka¹; ¹VZLU Aerospace Research and Test Establishment, Czech Republic EXPERIMENATAL AND COMPUTATIONAL STUDY OF GROUND EFFECT ON AIRFOIL SECTION |
ICAS2016_0216: D. Damljanovic¹, D. Vukovic¹, G. Ocokoljic¹, J. Isakovic, College of Applied Engineering Studies, Serbia; B. Rasuo, University of Belgrade, Serbia; ¹Military Technical Institute (VTI), Serbia A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS |
2.3 - Basic Fluid Dynamics and Flow Control |
ICAS2016_0521: T. Kwiatkowski, Institute of Aviation, Poland; P. Flaszynski, The Szewalski Institute of Fluid-Flow Machinery, Poland SOURCE TERM MODEL FOR STREAMWISE JET VORTEX GENERATOR MODELLING |
ICAS2016_0409: J. Li¹, W.-W. Zhang¹, X.-T. Li¹; ¹Northwestern Polytechnical University, China RESEARCH ON THE IMPACT OF SHOCK WAVE TO EXTENSIONALITY OF POD METHOD |
2.4 - Applied Aerodynamics |
ICAS2016_0421: Y. Zhong¹, Z.-Y. Zhang¹; ¹Shanghai Aircraft Design and Research Institute, China INVESTIGATION ON FLOW SEPARATION EFFECTS ON AIRCRAFT LONGITUDINAL MOMENT CHARACTERISTIC FOR FUSELAGE-MOUNTED AIRCRAFT |
3.1 - Materials issues, Fatigue and Damage Tolerance |
ICAS2016_0706: W.R. Kang¹, D.J. Lee¹; ¹KAIST, South Korea PERIODICALLY OSCILLATING TWO TRAILING EDGE FLAPS ACTUATED BY SMA WIRES |
3.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity |
ICAS2016_0622: I. Mareskin, DAFE MIPT, Russia MULTIDISCIPLINARY OPTIMIZATION OF PRO-COMPOSITE STRUCTURAL LAYOUTS OF HIGH LOADED AIRCRAFT CONSTRUCTIONS |
ICAS2016_0615: L.M.F. Barbosa¹, R.L.U. de Freitas Pinto¹, B.O. Hargreaves¹, L. Gori¹; ¹Universidade Federal de Minas Gerais, Brazil STUDY OF THE COMPROMISE OF AERODYNAMIC AND STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO WING DESIGN |
ICAS2016_0507: P.G. Karkle¹, G.V. Liseykin¹, M.A. Pronin¹; ¹TsAGI, Russia EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS FOR DETERMINING MODAL CHARACTERISTICS OF AIRCRAFT STRUCTURES |
ICAS2016_0266: Y.-Y. Hou¹, Z.-Q. Liu¹, C. Ji¹; ¹China Academy o f Aerospace Aerodynamics , China SOLAR UAV GUST LOAD AMENDMENT |
ICAS2016_0609: Z.H. Wu¹, R. Müller², J. Bayandor², J.P. Qian¹; ¹Nanjing University of Science and Technology, China; ²Virginia Tech, United States A FOLDABLE FLAPPING WING DESIGN INSPIRED BY THE ELBOW-WRIST ANATOMY OF BATS |
ICAS2016_0505: J.-M. Yun¹, J.-H. Han¹; ¹KAIST, South Korea SELECTION OF PARAMETERS IN SPR CAMERA SYSTEM FOR STRUCTURAL HEALTH MONITORING OF UAV MAIN WING |
ICAS2016_0279: G.C. Fonseca, Embraer, Brazil; S.F.M. Almeida, ITA - Instituto Tecnológico de Aeronáutica, Brazil NUMERICAL SIMULATION IN FINITE ELEMENT METHOD AND MANUFACTURING OF LUG MATERIAL COMPOSITE BY RTM PROCESS |
ICAS2016_0271: M. Dinulovic¹, B. Rasuo¹, B. Krstic, University of Defense, Serbia; ¹University of Belgrade, Serbia THE ANALYSIS OF LAMINATE LAY-UP EFFECT ON THE FLUTTER SPEED OF COMPOSITE STABILIZERS |
ICAS2016_0633: E.S. Dias, Brazil; C.A. Cimini Jr., Brazil BEARING STRENGTH ASSESSMENT OF COMPOSITE MATERIAL THROUGH NUMERICAL MODELS |
4 - Propulsion |
ICAS2016_0566: V. Baklanov, Russia DYNAMICS AND VIBRATION OF NEW GENERATION AVIATION ENGINES |
ICAS2016_0702: N. Liu¹, P. Wang¹, Y. Zhu¹; ¹Shanghai Aircraft Design and Research Institute, China LINEAR MODELING BASED ON INSTRUMENTAL MODEL ESTIMATION AND PID PARAMETERS TUNING IN FREQUENCY-DOMAIN OF AIRCRAFT ENGINE |
ICAS2016_0270: L. Yanovskiy¹, V. Ezhov¹, A. Molokanov¹; ¹Central Institute of Aviation Motors , Russia THE FOAMING PROPERTIES OF LUBRICATING OILS FOR AIRCRAFT GAS TURBINE ENGINES |
ICAS2016_0212: W. Ma¹, H. Huang¹, G. Feng¹; ¹Shenyang Aeroengine Research Institute, Shenyang, China, China LABYRINTH SEALS DYNAMIC COEFFICIENTS AND CRITICAL SPEED RESEARCH BASE OF CHILDS´ MODEL |
ICAS2016_0296: X.-W. Liu, China; A.-L. Gong, China; M. Yan, China; W.-J. Zhou, China NUMERICAL INVESTIGATION OF INLET STARTING CHARACTERISTICS |
ICAS2016_0008: D.A. Akhmedzyanov¹, A.E. Kishalov¹, K.V. Markina¹, V.D. Lipatov¹; ¹USATU, Russia KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES |
ICAS2016_0433: V.G. Nesterenko¹, A. Revanth Reddy¹; ¹Moscow Aviation Institute, Russia IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING TUBULER AIR-TO-AIR HEAT EXHANGERS COOLING SYSTEMS OF GAS TURBINES |
ICAS2016_0077: J. Cui¹, S. Shang¹, Q. Yang¹, L. Chen¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION OF RCS FOR A SPHERICAL CONVERGENT FLAP NOZZLE WITH A NON-RECTANGULAR DIVERGENT DUCT |
5.1 - Flight Dynamics and Control (Control & Modelling) |
ICAS2016_0498: J.G. Park¹, J.H. Moon¹, J.E. Jang¹, M.S. Park¹; ¹Koreanair, South Korea MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER |
ICAS2016_0387: D. Lee¹, J.-H. Kim, Agency for Defense Development, South Korea; H.-L. Choi¹; ¹KAIST, South Korea CLOSED-FORM COOPERATIVE GUIDANCE LAW FOR TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINTS |
ICAS2016_0183: O.D. Kreerenko, Beriev Aircraft Company, Russia; E.S. Kreerenko, Southern Federal University , Russia SYNTHESIS OF CONTROL LAWS OF AEROSPACE SYSTEM BASED ON A SYNERGISTIC APPROACH |
ICAS2016_0316: W. Yi¹, C. Xiaoqian¹, Z. Yong¹, B. Yuzhu¹; ¹College of Aerospace Science and Engineering, China THE EFFECT OF SATELLITE FORMATION FLYING ON AUTONOMOUS NAVOGATION |
ICAS2016_0227: P. Stojakovic, Military Technical Institute, Serbia; B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia GENERAL APPROACH TO THE ANALYSIS OF THE ASYMMETRICALLY LOADED AIRPLANE FLIGHT LIMITATIONS |
ICAS2016_0143: J. Liu¹, J. Xiang, School of Aeronautica Science and Enginering, Beijing University, China; G. Hu¹, Y. Zhang¹; ¹PLA Naval Aeronautical and Astronautical University, China HANDLING QUALITIES PREDICTION BASED ON ADAPTIVE OPTIMAL CONTROL PILOT MODEL |
5.2 - Flight Dynamics and Control (UAV related) |
ICAS2016_0388: S.V. Serokhvostov, MIPT, Russia; T.E. Churkina, MAI, Russia OPTIMIZATION OF THE TRAJECTORY AND ACCUMULATOR MASS FOR THE SOLAR-POWERED AIRPLANE |
ICAS2016_0326: M. Ariola¹, M. Mattei², E. D\\\'Amato², I. Notaro², G. Tartaglione¹; ¹University of Naples ‘’Parthenope’’, Italy; ²Second University of Naples, Italy MODEL PREDICTIVE CONTROL FOR A SWARM OF FIXED WING UAVS |
ICAS2016_0076: F. Schettini¹, G. Di Rito¹, E. Denti¹, R. Galatolo¹; ¹Università di Pisa, Dip. di Ingegneria Civile e Industriale, Italy NONLINEAR MODEL IDENTIFICATION OF A SMALL-SCALE UNMANNED ROTORCRAFT |
6 - Systems, Subsystems and Equipment |
ICAS2016_0159: H.W. Zhao¹, S.H. Duan¹, J.M. Feng¹; ¹Aircraft Strength Research Institute of China, China PID TUNING FOR MULTI-CHANNEL STRUCTURAL FATIGUE TESTING SYSTEM |
ICAS2016_0137: J. Zang ¹, X. Wang¹, H. Zhang¹; ¹Aviation Industry Development Research Center of China, China COMBAT EFFECTIVENESS EVALUATION-ORIENTED AVIONICS SYSTEM MODELING |
ICAS2016_0167: C.Y. Cheng¹, C.W.W. Chen¹; ¹AVIC Chengdu Aircraft Design and Research Institute, China A TEST METHOD BASED ON AIRCRAFT PLATFORM FOR ATMOSPHERIC LASER VISIBILITY |
8 - Air Transport System Efficiency |
ICAS2016_0490: A. Kan¹, V. Kanadin¹; ¹GosNIIAS, Russia INTEGRATED RESEARCH SIMULATION STAND ADVANCED AIR TRAFFIC CONTROL SYSTEMS |
ICAS2016_0719: S. Bagassi¹, F. De Crescenzio¹, F. Lucchi¹, N. Masotti¹; ¹University of Bologna, Italy AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER |
ICAS2016_0385: D. Steiner¹, F. Burgstaller¹, E. Gringinger, Frequentis AG, Austria; M. Schrefl¹, I. Kovacic¹; ¹Johannes Kepler University Linz, Austria IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION |
9 - Safety and Security |
ICAS2016_0400: H. Yuan¹, C. Lu¹, Z.-Y. Wang¹, F.-M. Li, Chinese Flight Test Establishment, China; ¹Beihang University, China MAKING HEALTH MANAGEMENT MORE CONCISE AND EFFICIENT: AIRCRAFT CONDITION MONITORING BASED ON COMPRESSED SENSING |
10 - Challenge of the Environment |
ICAS2016_0667: A. Jankowski¹, M. Kowalski¹, Z. Slawinski, Lublin Uniwersity of Technology, Poland; ¹Air Force Institute of Technology, Poland RESEARCH OF ALTERNATIVE FUEL WATER-FUEL MICRO EMULSION FROM POINT OF VIEW REDUCTION OF EMISSIONS |
11 - Operations and Sustainment |
ICAS2016_0273: D.Y. Kiselev¹, Y.V. Kiselev¹, R.V. Birukov¹; ¹Samara State Aerospace Univers, Russia CONTROL OF CONDITION OF GAS TURBINE ENGINE ROTOR BEARINGS IN DIAGNOSTIC PARAMETERS IN A DIFFERENT PHYSICAL NATURE |