ACCEPTED PAPERS - CATEGORY C - POSTERS

These papers will be presented in the Poster area



1 - Aircraft and Systems Integration

ICAS2014_1009: S. Bagassi¹, F. Lucchi¹, F. Persiani¹; ¹University of Bologna, Italy
AIRCRAFT PRELIMINARY DESIGN: GENETIC ALGORITHM BASED OPTIMIZATION METHOD
ICAS2014_0506: Z. Xu, Beihang University, China; D. Cui, AVIC, China; H. Du, Chinese Aeronautical Establishment, China
A RESEARCH ON ACCELERATED SEARCH GENETIC ALGORITHM OPTIMIZATION PLATFORM ORIENTED TO AIRCRAFT AERODYNAMIC DESIGN
ICAS2014_1021: C. Döll¹, B. Paluch¹, A. Guigon¹, D. Fraboulet, CEA Tech, France; ¹ONERA - The French Aerospace Lab, France
CONCEPTUAL FEASIBILITY STUDY FOR A FULLY ELECTRICALLY POWERED REGIONAL TRANSPORT AIRCRAFT
ICAS2014_0451: G.A. Popov , Research Institute of Applied Mechanics and Electrodynamics , Russia; V.M. Kulkov¹, V.G. Petukhov¹; ¹Research Institute of Applied Mechanics and Electrodynamics, Russia
ANALYSIS FOR POSSIBILITY TO USE SPACE PLATFORM WITH ELECTRIC PROPULSION SYSTEM IN COMBINATION WITH THE LAUNCH VEHICLE FOR AIR LAUNCH
ICAS2014_0314: P.V. Zhuravlev, MAI, Russia
APPLICATION OF FLEET CREATION PROBLEMS IN AIRCRAFT PRE-DESIGN
ICAS2014_0930: D. Duritsyn¹, A. Ternovoy¹, D. Krivonosova¹, V. Sokolyansky, Central Aerohydrodynamic Institute, TsAGI, Russia; ¹Beriev Aircraft Company, Russia
THE BE-200ES FIREFIGHTING AMPHIBIOUS AIRCRAFT EFFECTIVENESS DURING THE FIRE SEASONS 2004÷2011 YEARS IN THE EUROPEAN UNION COUNTRIES
ICAS2014_0484: R. Zhang¹, H. Du¹, D.-G. Cui, AVIC, China; ¹Chinese Aeronautical Establishment, China
OPTIMIZATION DESIGN OF COMPOSITE WING WITH MULTIPLE LOAD CASES AND LARGE SCALE DESIGN VARIABLES
ICAS2014_0301: J. Hanjie¹, D. Zhuoyi¹, P. Hongbin¹; ¹The First Aircraft Institute, Aviation Industry Corporation of C, China
RESEARCH ON FLYING-PYLON TECHNOLOGY

2.1 - Aerodynamics - CFD Methods and Validation

ICAS2014_0402: R.V. Bulbovich¹, V.V. Pavlogradskiy¹, V.V. Palchikovskiy¹; ¹Perm National Research Polytechnic University, Russia
THE PROCEDURE OF LINER IMPEDANCE EDUCTION BY FINITE ELEMENT METHOD
ICAS2014_0788: H. Takano¹, K. Fukuda¹; ¹Tokai University, Japan
NUMERICAL INVESTIGATION OF FLOW AROUND AN AIRFOIL WITH UNSTEADY MOVING
ICAS2014_0619: V.V. Gorsky¹, V.G. Resh¹; ¹MIC NPO MASHINOSTROYENIA, Russia
THE STUDY OF CARBON MATERIAL’S AEROTHERMOCHEMICAL DESTRUCTION IN COMBUSTION PRODUCTS OF LIQUID-PROPELLANT ROCKET ENGINES
ICAS2014_0918: T. Sulaiman¹, S. Sekimoto¹, T. Nonomura², M. Anyoji², K. Fujii²; ¹University of Tokyo, Japan; ²ISAS / JAXA, Japan
DBD PLASMA ACTUATOR MULTI-OBJECTIVE DESIGN OPTIMIZATION AT REYNOLDS NUMBER 63,000 : STROUHAL NUMBER EFFECT
ICAS2014_0964: C.W. Skaleski, Instituto Tecnológico de Aeronáutica, Brazil; F.I.K. Odaguil¹, J.H.A. Azevedo¹, L.S.M. Lima¹, R.A.S. Cardoso¹, P.H. Iscold, Universidade Federal de Minas Gerais, Brazil; ¹Embraer, Brazil
CFD – BASED STUDY ON GOLDSCHMIED PROPULSION CONCEPT APPLICATION FOR DRAG REDUCTION
ICAS2014_0687: M.M. Dubinina¹, M.Y. Sorokin¹; ¹PJSC “Ulyanovsk instrument manufacturing design bureau”, Russia
INFLUENCE NUMERICAL SCHEMES TO ESTIMATE ERROR OF AIR PRESSURE PROBE
ICAS2014_0839: J.H. Lee, Chungnam National University, Russia; L. Kartovitskiy¹, A. Tsipenko¹; ¹Moscow Aviation Institute (National Research University), Russia
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF NON-STATIONARY PROCESSES IN SUPERSONIC GAS EJECTOR
ICAS2014_0642: A.A. Aksenov, TESIS, Russia; A.A. Dyadkin ¹, S.P. Rybak ¹, T.V. Simakova ¹; ¹RSC Energia, Russia
NUMERICAL SOLVING PROBLEMS OF SPACECRAFT DESIGN
ICAS2014_0472: Y.I. Khlopkov, Central Aerohydrodynamic Institute, Russia; A.Y. Khlopkov¹, Z.Y. Myo Myint¹, T.V. Vyong¹; ¹Moscow Institute of Physics and Technology, Russia
MONTE CARLO METHODS IN APPLIED MATHEMATICS AND COMPUTATIONAL AERODYNAMICS
ICAS2014_0101: Y.M. Ignatkin¹, P.V. Makeev¹, A.I. Shomov¹; ¹Moscow aviation institute, Russia
COMPUTATIONAL MODELING OF HELICOPTER'S MAIN AND TAIL ROTOR INTERFERENCE ON THE BASE OF NON-LINEAR BLADE VORTICAL MODEL
ICAS2014_0062: I.A. Gubanova¹, M.A. Gubanova¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
INVERSE METHODS FOR AERODYNAMIC DESIGN USING THE NAVIER-STOKES EQUATIONS
ICAS2014_0634: E.V. Larina¹, I.A. Kryukov¹, I.E. Ivanov¹; ¹Moscow Aviation Institute (National Research University), Russia
NUMERICAL SIMULATION OF HIGH-SPEED SEPARATION FLOW IN THE AEROSPACE PROPULSION SYSTEMS
ICAS2014_0310: O. Tretiyakova, MAI, Russia
NUMERICAL SIMULATION OF MULTIPLE TURBULENT SUPERSONIC UNDEREXPANDED JETS
ICAS2014_0774: L.I. Garipova¹, A.N. Kusyumov¹, G.N. Barakos, The University of Liverpool, United Kingdom; ¹KNRTU-KAI, Russia
CFD MODELING OF 2D AEROFOIL DYNAMIC STALL
ICAS2014_0738: M. Sueki¹, T. Mizukaki¹; ¹Tokai University, Japan
NUMERICAL ANALYSIS OF SHOCK WAVES BEHAVIOR AROUND AERODYNAMIC DECELERATOR FOR MARS PLANETARY PROBE
ICAS2014_0566: A. Rumyantsev¹, V. Silantyev¹; ¹FSUE “SibNIA named after S.A. Chaplygin”, Russia
NUMERICAL AND EXPERIMENTAL STUDY OF A FLOW OVER STRAIGHT AND SWEPT HIGH-LIFT WINGS
ICAS2014_0094: M.A. Gubanova¹, N.N. Bragin¹, E.S. Perchenkov¹, A.Y. Slitinskaya¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
HIGH-LIFT SYSTEM DESIGN BY NUMERICAL METHODS AND WIND TUNNEL VERIFICATION
ICAS2014_0622: A.S. Batrakov¹, A.N. Kusyumov¹, G. Barakos, The University of Liverpool, United Kingdom; ¹KNRTU-KAI, Russia
SIMULATION OF FLOW AROUND FUSELAGE OF HELICOPTER USING ACTUATOR DISC THEORY

2.2 - Experimental Aerodynamics

ICAS2014_0601: B. Li¹, B. Song¹, L. Wang¹; ¹Northwestern Polytechnical University , China
A THREE-DIMENSIONAL FLAPPING WING MECHANISM FOR WIND TUNNEL EXPERIMENTS
ICAS2014_0138: D. Vukovic¹, D. Curcic¹, D. Marinkovski¹, D. Damljanovic¹, M. Samardžic¹, A. Vitic¹; ¹Vojnotehnicki institut, Serbia
LIVING WITH SUPERSONIC STARTING LOADS IN THE T-38 TRISONIC WIND TUNNEL OF VTI
ICAS2014_0124: V.I. Birukov¹, N.N. Bragin¹, M.F. Garifulin¹, S.I. Skomorokhov¹, V.V. Yanin¹; ¹TsAGI, Russia
INVESTIGATION OF UNSTEADY FLOW ON A HIGH ASPECT RATIO WING
ICAS2014_0354: V.V. Petronevich¹, Y.V. Kartashev¹, A.R. Gorbushin¹, K.D. Bukharov¹; ¹FSUE, Russia
REALIZATION OF A CONTINUOUS BALANCE TESTING PROCEDURE IN A COMPRESSOR-DRIVEN TRANSONIC WIND TUNNEL
ICAS2014_0190: S.A. Glazkov¹, A.R. Gorbushin¹, I.A. Kursakov¹; ¹Central Aerohydrodynamic Institute, Russia
FIN AND REAR STINGS SUPPORT EFFECTS ON THE FLOW AROUND THE AIRCRAFT MODEL
ICAS2014_0162: D. Damljanovic¹, B. Rasuo, Faculty of Mechanical Engineering University of Belgrade, Serbia; S. Mandic¹, D. Vukovic¹, J. Isakovic, College of Applied Engineering Studies, Serbia; ¹Military Technical Institute (VTI), Serbia
USABILITY OF COMPARATIVE EXPERIMENTAL - NUMERICAL SUPERSONIC TEST CASES WITH THE HB REFERENCE MODEL

2.3 - Basic Fluid Dynamics and Flow Control

ICAS2014_0184: T. Atobe, Japan Aerospace Exploration Agency, Japan
OBLIQUE MODE ENHANCEMENT BY LONGITUDINAL WALL OSCILLATION IN 2D CHANNEL FLOW
ICAS2014_0479: N. Morimoto¹, S. Aso¹, Y. Tani¹; ¹Kyushu University, Japan
REDUCTION OF AERODYNAMIC HEATING AND DRAG WITH OPPOSING JET THROUGH EXTENDED NOZZLE IN HIGH ENTHALPY FLOW
ICAS2014_0769: I.I. Lipatov¹, A.A. Prihodko, Dnepropetrovsk State University, Ukraine; R.Y. Tugazakov¹, T.W. Fam, MIPT, Russia; ¹TsAGI, Russia
NUMERICAL MODELING OF THE BUFFET ONSET IN 2-D AND 3-D FLOWS

2.4 - Applied Aerodynamics

ICAS2014_0387: A.L. Bolsunovsky¹, N.P. Buzoverya¹, I.L. Chernyshev¹, V.G. Sudokov¹, A.V. Voyevodin¹; ¹TsAGI, Russia
NOVEL CONFIGURATION OF A BUSINESS JET WITH A DROP-SHAPED FUSELAGE
ICAS2014_0700: B. Goliszek, Warsaw University of Technology, Poland
DESIGN AND OPTIMAZATION OF THE WING WITH VERY HIGH LIFT POSSIBILITIES.
ICAS2014_0030: V.V. Riabov, Rivier University, United States
INTERFERENCE BETWEEN BODIES IN HYPERSONIC RAREFIED-GAS FLOWS
ICAS2014_0751: M. Figat, Warsaw University of Technology, Poland
AERODYNAMIC DESIGN OF FLYING WING WITH EMPHASIS ON HIGH WING LOADING
ICAS2014_0228: N. Tokugawa, Japan Aerospace Exploration Agency, Japan; T. Osada, Gakushuin University, Japan; Y. Ueda, Tokyo Business Service Co. Ltd., Japan; H. Ishikawa, TOUA Co. Ltd., Japan
NATURAL LAMINAR FLOW DESIGN OF FUSELAGE NOSE FOR SMALL SUPERSONIC CIVIL TRANSPORT
ICAS2014_0214: S.Y. Soloviev, KSRC, Russia
INTERACTION OF KARMAN VORTICES WITH LONGITUDINAL VORTEX SYSTEMS IN FLOWS AROUND BODIES
ICAS2014_0249: M. Principi, City University London, United Kingdom; S. Prince, Cranfield University, United Kingdom
FEASIBILITY ASSESSMENT OF SPINNING CYLINDER LIFT FOR REMOTE FLIGHT IN MARS AND TITAN ATMOSPHERES
ICAS2014_0390: A.L. Bolsunovsky¹, N.P. Buzoverya¹, S.I. Skomorohov¹; ¹TsAGI, Russia
INVESTIGATION OF ADAPTIVE WING BENEFITS FOR TRANSPORT AIRCRAFT
ICAS2014_0663: K. Bogdanski¹, W. Krusz¹, M. Rodzewicz¹, M. Rutkowski¹; ¹Warsaw University of Technology, Poland
DESIGN AND OPTIMIZATION OF LOW SPEED DUCTED FAN FOR A NEW GENERATION OF JOINED WING AIRCRAFT
ICAS2014_0483: M.H. Ryu, Hanyang Univ./Department of Mechanical Engineering, South Korea; L.S. Cho, Hansung Univ./Department of Mechanical Systems Engineering, South Korea; J.S. Cho, Hanyang Univ./School of Mechanical Engineering, South Korea
INVESTIGATION OF THE TIP CLEARANCE EFFECT IN A COUNTER-ROTATING DUCTED FAN FOR VTOL UAV

3.1 - Materials issues, Fatigue and Damage Tolerance

ICAS2014_0392: V.S. Pisarev¹, S.I. Eleonsky¹, A.V. Chernov¹; ¹TsAGI, Russia
RESIDUAL STRESS CHARACTERIZATION IN ORTHOTROPIC PLATE BY COMBINING HOLE-DRILLING METHOD AND SPECKLE INTERFEROMETRY
ICAS2014_0262: F. Zhang, Beijing Aeronautical Technology Research Center, China
HEAVY SPECTRA UNDER OPERATIONAL LOADS CAN REDUCE LIFE BUT NOT FATIGUE SCATTER FACTOR
ICAS2014_0931: V.I. Korolkov, Voronezh State Technical University, Russia
METHOD DISTURBANCES IN THE LIMIT DEFORMATIONS IN THE CROSS-SECTION WING IS
ICAS2014_0386: J. Lu¹, N. Kashaev¹, N. Huber¹; ¹Helmholtz-Zentrum Geesthacht, Germany
DAMAGE TOLERANCE IMPROVEMENT OF LASER BEAM WELDED FUSELAGE STRUCTURES VIA CRENELLATIONS
ICAS2014_0569: L.B. Getsov, NPO CKTI, Russia; A.S. Semenov¹, S.G. Semenov¹, E.A. Tikhomirova, JSK Klimov, Russia; ¹Saint-Petersburg State Polytechnical University, Russia
EXPERIMENTS AND FAILURE CRITERIA FOR SINGLE CRYSTAL ALLOYS OF GAS TURBINE ENGINE UNDER STATIC AND THERMOCYCLIC LOADING
ICAS2014_0512: C. Liu¹, B. Zang¹, X. Chen¹, C. Tao¹, D. Liu¹; ¹Beijing Institute of Aeronautical Materials, China
FAILURE ANALYSIS ON REAR GEARBOX OUTPUT GEAR OF HELICOPTER
ICAS2014_0631: G. Komarov¹, S. Bukharov¹, A. Lebedev¹; ¹MATI, Russia
THERMOPLASTIC COMPOSITE AIRCRAFT STRUCTURE REPAIR METHODOLOGY
ICAS2014_0907: T.V. Larionova, St.Petersburg State Polytechnical University, Russia; B.-S. You, Korea Insitute of Materials Science, South Korea
RAPID SOLIDIFIED MG-CA-ZN ALLOYS WITH MICROALLOYING OF LA, ND, Y, ZR
ICAS2014_0510: B. Zhang, Beijing Institute of Aeronautical Materials, China
EFFECT OF SURFACE COATING ON RECRYSTALLIZATION OF SINGLE CRYSTAL SUPERALLOY

3.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity

ICAS2014_0849: L. Chen¹, Z.Q. Dou¹; ¹Shang Aircraft Design and Research Institute, China
THE FLUTTER MODEL CHARACTERISTIC STUDY AND WIND-TUNNEL TEST FOR WING-MOUNTED CIVIL AIRCRAFT
ICAS2014_0701: V. Soloshenko, Moscow Aviation Institute (National Research University), Russia
CONCEPTUAL DESIGN OF CIVIL AIRPLANE COMPOSITE WINGBOX STRUCTURES
ICAS2014_0151: G.A. Amiryants¹, V.P. Kulesh¹, V.A. Malyutin¹, A.V. Chedrik¹; ¹Central aerohydrodynamic institute - TsAGI, Russia
AEROELASTIC ANALYSIS OF THE ADAPTIVE WING WIND TUNNEL DEMONSTRATOR OF THE SADE PROJECT
ICAS2014_0141: Q. Xiong, CASIC, China; D.-G. Cui, AVIC, China
AEROELASTIC OPTIMIZATION OF COMPOSITE WING BASED ON IMPROVED ADAPTIVE GENETIC ALGORITHM
ICAS2014_0755: Z.W. Liu ¹, Z.X. Hou¹, J.T. Zhang¹, X.Z. Gao¹; ¹National University of Defense Technology, China
THE VERY FLEXIBLE AIRCRAFTS AND ALBATROSS FLIGHT
ICAS2014_0711: T.H.L. Pinto, UFVJM - ICT, Brazil; R.G.A. da Silva, ITA, Brazil; G.R. Begnini, Embraer, Brazil
COMPARATIVE STUDY OF SYSTEM IDENTIFICATION METHODS APPLIED TO AEROELASTIC MODELS TESTED IN WIND TUNNEL
ICAS2014_0497: D. XUE¹, B.-F. SONG¹, W.-Q. YANG¹; ¹Northwestern Polytechnical University, China
RESEARCH ON LONG PERIODICAL STRUCTURAL DEFORMATION OF FLEXIBLE FLAPPING WING IN FLIGHT
ICAS2014_0861: M.A. Arbelo, PFH - Private University of Applied Sciences, Germany
BUCKLING OF IMPERFECTION SENSITIVE SHELL STRUCTURES: NUMERICAL MODELS TO PREDICT LESS CONSERVATIVE KNOCK-DOWN FACTORS
ICAS2014_0702: M. Rodzewicz¹, D. Glowacki¹; ¹Warsaw University of Technology, Poland
INVESTIGATIONS INTO LOAD SPECTRA OF LIGHT-WEIGHT UAV’S

4 - Propulsion

ICAS2014_0093: A.L. Kartashev¹, M.A. Kartasheva¹; ¹South Ural State University, Russia
PROFILING OF OPTIMAL ANNULAR NOZZLES WITH POLYPHASE WORKING MEDIUM
ICAS2014_0219: L.S. Yanovskiy¹, A.V. Baykov¹, I.S. Averkov¹; ¹Central Institute of Aviation Motors named after P.I. Baranov, Russia
FUNDAMENTALS OF THE THEORY OF AVIATION \\\"ELECTROCHEMICAL\\\" GAS TURBINE ENGINES WITH SOLID OXIDE FUEL CELLS
ICAS2014_0296: K. Yang¹, Q.Y. Tu¹, Y.H. Cai¹; ¹Northwestern Polytechnical University, China
PERFORMANCE ANALYSIS OF BALL BEARING CONTROLS FOR ENGINE OPERATING SYSTEM
ICAS2014_0119: Y.A. Ravikovich¹, Y.I. Ermilov¹, A.O. Pugachev¹, A.A. Matushkin¹, D.P. Kholobtsev¹; ¹MAI, Russia
PREDICTION OF OPERATIONAL CHARACTERISTICS OF FLUID-FILM AND GAS BEARINGS FOR HIGH-SPEED TURBOMACHINERY USING COMPUTATIONAL FLUID DYNAMICS
ICAS2014_0397: A.I. Lanshin¹, Y.V. Fokin¹, I.V. Osipov¹, V.V. Gavrilov¹; ¹CIAM, Russia
PERSPECTIVE OF SMALL GAS TURBINE ENGINES DEVELOPMENT
ICAS2014_0218: O. Gurevich¹, A. Gulienko¹, U. Schurovskiy¹; ¹CIAM, Russia
DEMONSTRATION SYSTEMS OF THE “ELECTRIC” GAS TURBINE ENGINE
ICAS2014_0294: B.-W. Wang, NUDT, China
AERODYNAMIC CHARACTERISTICS OF ANNULAR WING AND THE IMPACT ON THE PERFORMANCE OF DUCTED FAN
ICAS2014_0902: I.V. Eremkin¹, I.N. Shirokov¹; ¹Moscow Aviation Institute (National Research University), Russia
THE STUDIES OF CONSTRUCTION ELEMENTS OF SCRAMJET ENGINE CONDUCTED BY ON UNIVERSAL MODEL AERODYNAMIC FACILITY
ICAS2014_0396: A.I. Lanshin¹, A.S. Polev¹; ¹CIAM, Russia
ANALYSIS OF TRENDS AND FORECAST OF GTE DEVELOPMENT FOR SUBSONIC CIVIL AIRCRAFT
ICAS2014_0373: L.A. Benderskiy¹, D.A. Lyubimov¹; ¹CIAM, Russia
INVESTIGATION OF FLOW PARAMETERS AND NOISE OF SUBSONIC AND SUPERSONIC JETS USING RANS/ILES HIGH RESOLUTION METHOD
ICAS2014_0217: L.S. Yanovskiy¹, V.V. Raznoschikov¹, A.V. Baykov¹, I.S. Averkov¹; ¹Central Institute of Aviation Motors named after P.I. Baranova, Russia
TRANSPORT AIRCRAFT WITH HIGH FUEL EFFICIENCY WITH \"ELECTROCHEMICAL\" GAS TURBINE ENGINE BASED ON SOFC
ICAS2014_1007: T. Popova¹, M. Drobysh¹, A. Lanshin¹, V. Lomazov¹; ¹CENTRAL INSTITUTE of AVIATION MOTORS, Russia
DEVELOPMENT OF KEY TECHNOLOGIES FOR MICRO REGENERATIVE GAS TURBINES
ICAS2014_0746: A. Zubko¹, I. Zubko¹, V. Kritsky¹; ¹Lyulka Design Bureau, Russia
IMPLEMENTATION OF HIGH STRENGTH COMPOSITE CERAMIC MATERIALS FOR PRODUCING TRIBOTECHNICAL PARTS OF GAS TURBINE ENGINES AS CONSTRUCTIONAL NANO-STRUCTURED MATERIALS
ICAS2014_0227: N.A. Zlenko¹, S.V. Mikhaylov¹, A.V. Shenkin¹; ¹TsAGI, Russia
CONSTRUCTION AND USE OF IMITATING MODEL IN THE PROCESS OF MULTI-CRITERIA OPTIMIZATION OF THE SEPARATE-FLOW NOZZLE
ICAS2014_0856: Y.M. Tsirkunov¹, D.A. Romanyuk¹, S.V. Panfilov¹; ¹Baltic State Technical University, Russia
COMPUTATIONAL SIMULATION OF TWO-PHASE GAS-PARTICLE FLOW IN AN INLET “ROTOR-STATOR” STAGE OF A TURBOJET ENGINE COMPRESSOR
ICAS2014_0035: W. Dong¹, J.J. Zhu¹, M. Zheng¹, R. Wang¹; ¹Shanghai Jiao Tong University, China
NUMERICAL STUDY OF ICE ACCRETION ON ROTATING AERO-ENGINE CONE
ICAS2014_0791: N. Kapyrin, MAI (Moscow Aviation Institute), Russia
DESIGNING GAS TURBINE CONTROL SYSTEMS AT DIFFERENT LEVELS OF ABSTRACTION
ICAS2014_0461: M.J. Ivanov¹, V.K. Mamaev¹, G.B. Zhestkov¹; ¹Central Institute of Aviation Motors, Russia
THERMODYNAMICALLY COMPATIBLE THEORY OF HIGH TEMPERATURE TURBOJET ENGINES

5.1 - Flight Dynamics and Control (Control & Modelling)

ICAS2014_0270: T. Goetzendorf-Grabowski, Warsaw University of Technology, Poland
STABILITY PROBLEMS OF THREE SURFACE CONFIGURATION
ICAS2014_0121: A.A. Dementyev¹, Y.I. Didenko¹, N.B. Lysenkova¹; ¹TsAGI, Russia
PRINCIPLES OF THE AUTOMATED CONTROL FOR THE CIVIL AIRCRAFT, WHICH PROVIDE FLIGHT SAFETY
ICAS2014_0893: A. Kwiek, Warsaw University of Technology, Poland
STUDY ON CONTROL AND STABILITY OF THE ROCKET PLANE TO SPACE TOURISM
ICAS2014_0447: A.M. Shmatkov¹, A.E. Utemov¹, Y.N. Zhelnin, TsAGI, Russia; F.L. Chernousko¹; ¹IPMech RAS, Russia
NUMERICAL CALCULATION OF OPTIMAL 3D-TRAJECTORIES FOR THE MANEUVERABLE AIRCRAFT
ICAS2014_0777: V. Ovcharenko , Moscow Aviation Institute (State Technical University), Russia; E. Egorova, Russian Aircraft Corporation \, Russia
IDENTIFICATION OF THE AERODYNAMIC COEFFICIENTS OF THE MULTIROLE MANEUVERABLE AIRCRAFT BASED ON UNSTEADY FLIGHT
ICAS2014_0438: A. Andreeva-Mori¹, K. Kobayashi¹, M. Shindo¹; ¹Japan Aerospace Exploration Agency, Japan
EVALUATION OF SATELLITE IMAGERY INTEGRATION IN OPTIMAL AIRCRAFT OPERATION PLANNING FOR DISASTER RELIEF
ICAS2014_0671: S. Kannokkada¹, N.K. Sinha¹; ¹Indian Institute of Technology Madras, India
EFFECT OF AERODYNAMIC UNCERTAINTIES ON HIGH-ALPHA SPIN
ICAS2014_0166: T.A. Tikhomirova¹, G.T. Fedorenko¹; ¹FGUP GosNIIAS, Russia
FAST ANALYSIS OF THE NATURAL EDGE LANDMARKS FOR AUTONOMOUS NAVIGATION
ICAS2014_0464: M. Zhang¹, M. Cristofaro², Y. Wang, China Academy of Aerospace Aerodynamics, China; A. Da Ronch², A. Rizzi¹; ¹Royal Institute of Technology, Sweden; ²University of Southampton, United Kingdom
INVESTIGATING THE PIAGGIO AVANTI DESIGN USING CEASIOM
ICAS2014_0421: Y. Liu¹, Z. Gao¹; ¹Northwestern Polytechnical University, China
AN EVALUATING MODEL FOR CONTROL EFFECTOR SUPERIORITY BASED ON PERFORMANCE REQUIREMENTS
ICAS2014_0122: A.A. Bondarenko¹, V.I. Zhelonkin¹, M.V. Zhelonkin¹, O.I. Tkachenko¹; ¹TSAGI, Russia
TRAINING TECHNIQUE TO EXERCISE AT SIMULATOR THE DIFFICULT FLIGHT STAGES

5.2 - Flight Dynamics and Control (UAV related)

ICAS2014_0587: S. Chiesa¹, S.C. Aleina¹, G.A. Di Meo¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy
AUTONOMOUS TAKE-OFF AND LANDING FOR UNMANNED AIRCRAFT SYSTEM: RISK AND SAFETY ANALYSIS
ICAS2014_0527: Y.Q. Dong¹, X.Z. YANG¹, J.L. AI¹; ¹Fudan University, China
RESEARCH ON ENEMY AIRCRAFT BANK ANGLE ESTIMATION FOR AUTONOMOUS AIR COMBAT
ICAS2014_0259: W. Shi¹, Z. Yuan¹, L. Zhang¹; ¹AVIC Chengdu Aircraft Design & Research Institute, China
AUTOMATED CONTROL STRATEGY FOR HALE UAV FLAMEOUT LANDING AND ITS FLIGHT SIMULATION STUDY
ICAS2014_0285: G. Di Francesco¹, G. Scapaticci¹, M. Mattei¹; ¹Seconda Università di Napoli, Italy
TRANSITION CONTROL AND REDUNDANCY MANAGEMENT FOR A TILT ROTOR UAV USING GENETIC ALGORITHMS
ICAS2014_0765: G.H. Moon¹, D.W. Yoo¹, B.Y. Lee¹, H.I. Lee¹, M.J. Tahk¹; ¹KAIST, South Korea
MULITLE TASK ASSIGNMENT FOR COOPERATIVE TRANSPORT SYSTEM WITH GROUP BUYING APPROACH

6 - Systems, Subsystems and Equipment

ICAS2014_0709: K. Shiomi, ENRI, Japan; S. Aoyama, IRT Corp., Japan
DEVELOPMENT OF PASSIVE SURVEILLANCE RADAR
ICAS2014_0676: S.V. Semenov¹, M.S. Nikhamkin¹, O.V. Korepanova², Y.A. Berendorf²; ¹Perm National Research Polytechnic University, Russia; ²OJSC “Aviadvigatel”, Russia
EXPERIMENTAL INVESTIGATION OF ROTOR DYNAMICS IN AIRCRAFT ENGINE WITH TWO-AXIS STIFFNESS ANISOTROPY OF SUPPORTS

7 - Systems Engineering and Supply Chain

ICAS2014_0646: I. Svadkovskiy¹, L. Zhemuranova¹; ¹CIAM, Russia
USING THE VIRTUAL REALITY SYSTEM IN THE DEVELOPMENT OF AIRCRAFT ENGINE
ICAS2014_0910: V. Zdanevich¹, A. Mazin¹; ¹Southern Federal University, Russia
DEVELOPMENT TRENDS OF AMPHIBIAN'S SHAPE.
ICAS2014_0309: N.N. Shabrov¹, A.K. Kuzin¹, S.G. Orlov¹, B.N. Chetverushkin², M.V. Iakobovski²; ¹St. Petersburg State Polytechnical University, Russia; ²Institute for Mathematical Modeling of RAS, Russia
VIRTUAL PROTOTYPING MODELING IN THE CAVE 3D ENVIRONMENT

8 - Air Transport System Efficiency

ICAS2014_0952: Pan Weijun¹, Qiu Wenbin¹, Kang Rui¹; ¹Civil Aviation Flight University of China, China
BALANCED ALLOCATION ON ARRIVAL AIR TRAFFIC FLOW

9 - Safety and Security

ICAS2014_0999: A.G. Kuznetsov¹, L.N. Aleksandrovskaya¹, V.N. Masur¹; ¹JSC Moscow Institute of Electromechanics & Automatics, Russia
METHOD OF REQUIREMENTS CONFIRMATION TO AIRCRAFT AUTOMATIC LANDING SAFETY AT MATHEMATICS SIMULATION STAGE
ICAS2014_0723: H. Tsuda¹, K. Funabiki¹, H. Shirouzu¹, K. Tawada, Shimadzu co., Japan; T. Toshida, NEC co., Japan; ¹JAXA, Japan
FLIGHT TESTS OF SYNTHETIC TERRAIN AND FLIR IMAGES ON HELMET-MOUNTED DISPLAY
ICAS2014_0235: G. Lu, Chengdu Aircraft Design & Research Institute, China
THE TRANSFORM PRINCIPLE AND MODEL FOR AIRCRAFT MTTR IN THREE-DIMENSIONAL DIGITAL DESIGN CONDITION
ICAS2014_0882: T. Levora¹, O. Bruna¹, P. Paces¹; ¹Czech Technical University in Prague, Czech Republic
PATH PLANNING FOR ULTRALIGHTS UNDER EMERGENCY CONDITIONS
ICAS2014_0318: D.A. Aggromito¹, R. Thomson, CRC-ACS, Australia; J. Wang, DSTO, Australia; B. Chen¹, W. Yan¹; ¹Monash University, Australia
USING A BIODYNAMIC MODEL TO INVESTIGATE THE EFFECTS OF BODY-BORNE EQUIPMENT ON FORCES EXPERIENCED IN A SIMULATED HELICOPTER CRASH
ICAS2014_0012: P.M. Politano, The Citadel, United States; R.O. Walton, Embry-Riddle Aeronautical University - Worldwide, Germany
GENDER RELATED PERCEPTIONS, STRESS, ANXIETY, DEPRESSION, AND PERSONALITY CHARACTERISTICS: FEMALES ON THE FLIGHT DECK
ICAS2014_0305: D.-Y. Wang¹, Y.-L. Fu¹, X.-Y. Qi¹; ¹Beihang University, China
RESEARCH ON A PROGNOSTIC AND HEALTH MONITORING APPROACH FOR EMAS IN THE FLIGHT CONTROL SYSTEM

10 - Challenge of the Environment

ICAS2014_0581: Z. Ilic¹, B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia; M. Jovanovic¹, S. Jovicic¹; ¹Technical Test Center , Serbia
IMPACT OF IRREGULARITIES IN THE PISTON ENGINE OPERATION ON THE INFLIGHT VIBRATION LEVEL

11 - Operations and Sustainment

ICAS2014_0543: B. Rasuo¹, G. Djuknic¹; ¹University of Belgrade, Serbia
IMPROVEMENT OF THE AIRCRAFT GENERAL OVERHAUL PROCEDURE
ICAS2014_0240: A.A. Fedotov, Moscow Aviation Institute (National Research University), Russia
MODELING AND OPTIMIZING OF BONDED PATCH REPAIRS FOR POLYMER COMPOSITE STRUCTURES
ICAS2014_0071: C. Bil¹, R. Hadgraft¹, P. Ruamtham¹; ¹RMIT University, Australia
AEROSPACE ENGINEERING: INVESTIGATING STUDENT PERCEPTIONS AND INDUSTRY REALITIES
ICAS2014_0179: A.Z. Bagerman¹, I.P. Leonova¹, A.V. Konopatova¹; ¹Krylov State Research Centre, Russia
PLANNING OF AN EXPENDITURE OF THE RESOURSE OF GAS TURBINE ENGINE IN OPERATION

12 - Host nation

ICAS2014_1043: M. Kanevsky, Russia
WAKE VORTEX FLIGHT SAFETY SYSTEM: CURRENT STATUS AN PERSPECTIVES