ICAS 2016: TOPICS AND TITLES



1 - Aircraft and Systems Integration

ICAS2016_0002: I. Berlowitz, Israel Aerospace Industries, Israel
COMMERCIAL DERIVATIVE AIRCRAFT AND TURBINE ENGINE
ICAS2016_0015: J. Hanjie¹, D. Zhuoyi¹, P. Hongbin¹, S. Liying¹; ¹AVIC, China
CONCEPTUAL STUDY OF AN INNOVATIVE HIGH ALTITUDE SOLAR POWERED FLIGHT VEHICLE
ICAS2016_0020: C. Song, China; X.-D. Yang, China; W.-P. Song, China
EFFICIENT AERODYNAMIC OPTIMIZATION USING HIERARCHICAL KRIGING COMBINED WITH GRADIENT
ICAS2016_0052: N.R. El Haddad¹, L. Gonzalez¹; ¹EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States
DETAILED AERO-STRUCTURAL DESIGN OF WINGLET FOR BUSINESS JET
ICAS2016_0053: L. Gonzalez, EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States
SUPERSONIC BUSINESS JET TECHNOLOGY AND MISSION TRADE STUDIES
ICAS2016_0058: C. Ma¹, S.P. Yang¹; ¹COMAC, China
SYNTHESIZED ANALYSIS FROM DESIGN RANGE TO THE CONCETUAL DESIGN OF WIDEBODY AIRLINER
ICAS2016_0064: A. Joulia¹, T. Dubot¹, J. Bedouet¹; ¹ONERA - The French Aerospace Lab, France
TOWARDS A 4D TRAFFIC MANAGEMENT OF SMALL UAS OPERATING AT VERY LOW LEVEL
ICAS2016_0067: T. Goetzendorf-Grabowski¹, J. Mieloszyk¹; ¹Warsaw University of Technology, Poland
UNCONVENTIONAL CONFIGURATIONS - DESIGN AND OPTIMIZATION
ICAS2016_0086: K.-S. Zhang¹, H. Zhang¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China
STRUCTURAL CONSTRAINTS INVESTIGATION IN WING AERODYNAMIC/STRUCTURAL OPTIMIZATION
ICAS2016_0092: L. Wiart¹, O. Atinault¹, J.-C. Boniface¹, R. Barrier¹; ¹ONERA, France
AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS
ICAS2016_0145: T. Pfeiffer¹, E. Moerland¹, J. Gibbs¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
EXPLORING PROPAGATED UNCERTAINTIES IN A MULTI-DISCIPLINARY AIRCRAFT DESIGN FRAMEWORK
ICAS2016_0150: Z. Goraj¹, A. Sieradzki¹; ¹Institute of Aviation, Poland
INFLUENCE OF POWER UNIT CONFIGURATION LAYOUT OF A REGIONAL JET ON PERFORMANCE AND DIRECT OPERATING COST
ICAS2016_0174: S. Herbst¹, A. Staudenmaier¹; ¹Technical University of Munich / Institute of Aircraft Design, Germany
USING OPENVSP IN A CONCEPTUAL AIRCRAFT DESIGN ENVIRONMENT IN MATLAB
ICAS2016_0252: J. Kimura, The University of Tokyo, Japan
STUDENT DESIGN PROCESSES IN INTERDISCIPLINARY COLLABORATION ACTIVITIES IN AERONAUTICS ENGINEERING EDUCATION
ICAS2016_0253: C. Ma¹, Z.G. Tan¹; ¹COMAC, China
A CONCEPTUAL ANALYSIS OF AN AIRCRAFT WITH REAR-MOUNTED OPEN ROTOR ENGINES
ICAS2016_0268: W. Gu¹, Z. Chen¹, B. Zhang¹; ¹Northwestern Polytechnical University, China
PHYSICALLY-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION FRAMEWORK COUPLING AIRFRAME AND PROPULSION
ICAS2016_0280: C.-J. Kim, Korea Aerospace Industries, Ltd, South Korea
FLIGHT TEST FOR TYPE CERTIFICATION ACQUISITION OF SMALL CIVIL AIRPLANE KC-100
ICAS2016_0317: T. Chiba¹, K. Rinoie¹; ¹The University of Tokyo, Japan
INTEGRATED CONCEPTUAL DESIGN METHOD CONSIDERING ADVANCED AIRCRAFT SYSTEMS AND AIRCRAFT TRAJECTORY
ICAS2016_0328: E. Moerland¹, S. Deinert², F. Daoud², J. Dornwald², B. Nagel¹; ¹German Aerospace Centre (DLR), Germany; ²Airbus Defence & Space, Germany
COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS
ICAS2016_0359: K. Sibilski¹, K. Fakkowski, Military University of Technology Technology, Poland; R. Kaleta, Air Force Institute of Technology, Poland; E. Ladyzynska-Kozdras¹, A.-M. Sibilska-Mroziewicz¹, W. Wróblewski, Wroclaw University of Technology, Poland; ¹Warsaw University of Technology, Poland
DEVELOPMENT OF THE SMALL-SCALE MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT SAFETY TAKE-OFF AND LANDING
ICAS2016_0397: P.D. Bravo-Mosquera¹, A. Martins-Abdalla¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹Aerodynamic Laboratory, São Carlos Engineering School-University, Brazil
CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING
ICAS2016_0398: X. Wu, China; W. Zhang, China
STOCHASTIC TRANSONIC AERODYNAMICS ANALYSIS
ICAS2016_0438: Y. Fefermann¹, C. Maury¹, C. Level¹, K. Zarati¹, J.-P. Salanne¹, C. Pornet¹, B. Thoraval¹, A.T. Isikveren¹; ¹SAFRAN S.A., France
HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT APPLICATIONS
ICAS2016_0461: J. Hermetz¹, M. Ridel¹, C. Döll¹; ¹ONERA, The French Aerospace Lab, France
DISTRIBUTED ELECTRIC PROPULSION FOR SMALL BUSINESS AIRCRAFT A CONCEPT-PLANE FOR KEY-TECHNOLOGIES INVESTIGATIONS
ICAS2016_0479: A. Ariyarit¹, M. Sugiura², Y. Tanabe², M. Kanazaki¹; ¹Tokyo Metropolitan University, Japan; ²Japan Aerospace Exploration Agency, Japan
DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION
ICAS2016_0483: S. Kim¹, K. Lee¹; ¹Pusan National University, South Korea
REDUCED ORDER MODELING OF AVIATION ENVIRONMENTAL DESIGN TOOL WITH PROPER ORTHOGONAL DECOMPOSITION AND KRIGING
ICAS2016_0506: R. Fusaro¹, N. Viola¹, D. Ferretto¹, F. Santoro, Altec S.p.A, Italy; F. Fenoglio, Thales Alenia Space, Italy; ¹Politecnico di Torino, Italy
CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS
ICAS2016_0510: M. Zhang¹, Z. Chen¹, B. Zhang¹; ¹Northwestern Polytechnical University, China
A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS
ICAS2016_0525: A.S.J. van Heerden¹, M.D. Guenov¹, A. Molina-Cristobal¹, A. Riaz¹; ¹Cranfield University, United Kingdom
ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN
ICAS2016_0538: R.C. Munjulury¹, A.M. Abdalla, University of São Paulo, Brazil; I. Staack¹, P. Krus¹; ¹Linköping University, Sweden
KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION
ICAS2016_0563: P.D. Ciampa¹, B. Nagel¹; ¹German Aerospace Center, DLR, Germany
TOWARDS THE 3RD GENERATION MDO COLLABORATIVE ENVIRONMENT
ICAS2016_0602: A. Mirzoyan¹, A. Isyanov¹, A.T. Isikveren, Safran Tech, France; ¹CIAM, Russia
COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT "DISPURSAL"
ICAS2016_0607: C. Lee, Korea Aerospace Industries, LTD., South Korea
MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR FIGHTER AIRCRAFT CONFIGURATION
ICAS2016_0610: F. Hashim¹, C.P. Lawson¹, D.M. Judt¹; ¹Cranfield University, United Kingdom
ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE HEAVY HELICOPTER
ICAS2016_0626: A.A. Desai¹, P. Hollingsworth¹, P. Chinchapatnam, Rolls-Royce plc, United Kingdom; ¹University of Manchester, United Kingdom
IDENTIFYING THE BEST DESIGN FOR UNCERTAIN MARKETS
ICAS2016_0632: K.G. Schwartz¹, D. Mavris¹; ¹Georgia Institute of Technology, United States
LINKING TECHNOLOGY READINESS TO UNCERTAINTY REDUCTION
ICAS2016_0646: M. Babiak¹, A. Garstka¹, M. Mazur¹, I. Skawinski¹; ¹Warsaw University of Technology, Poland
IS TO BE THE MICRODRONE
ICAS2016_0650: P. Raj, Virginia Polytechnic Institute & State University, United States; J. Abulawi, Hochschule für Angewandte Wissenschaften, Germany
USING INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN PROJECTS TO ENHANCE UNDERGRADUATE DESIGN EDUCATION: LESSONS LEARNED
ICAS2016_0665: H.D. Schwartz¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
UNCERTAINTY QUANTIFICATION OF AIRFOIL DESIGN FOR ADVANCED PROPELLER MODELS
ICAS2016_0701: T. Prakash, Indian Institute of Technology Bombay, India
FEASIBILITY ANALYSIS OF SPAN EXTENSION OF MORPHING HALE UAV WING
ICAS2016_0703: M.I. Alam, Indian Institute of Technology Bombay, India
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF STRATOSPHERIC AIRSHIP
ICAS2016_0727: J. Bijewitz¹, A. Seitz¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION
ICAS2016_0731: E. Joubert¹, D. Chapuis¹, D. Esteyne¹, J.-C. Lambert¹, O. Siri¹, D. Müller-Wiesner¹; ¹Airbus, France
THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION
ICAS2016_0744: A.T. Isikveren¹, P.-A. Lambert¹, J. Stuhlberger, Airbus Group, Germany; M.K. Bradley, Boeing Commercial Airplanes, United States; J.H. Stromberger, General Electric, Germany; J. Whurr, Rolls Royce, United Kingdom; F. Anton, Siemens, Germany; ¹SAFRAN S.A., France
HYBRID-ELECTRIC TRANSPORT AIRCRAFT: OPPORTUNITIES AND PERSPECTIVES
ICAS2016_0747: A. Uranga, University of Southern California, United States
THE D8 AIRCRAFT CONCEPT AND ITS BOUNDARY LAYER INGESTION BENEFIT
ICAS2016_0748: P. Laskaridis, Cranfield University, United Kingdom
HYBRID TURBO-ELECTRIC DISTRIBUTED PROPULSION APPLIED TO SHORT RANGE AIRCRAFT
ICAS2016_0749: K. Rinoie, The University of Tokyo, Japan
AIRCRAFT DESIGN EDUCATION FOR UNDERGRADUATE AND GRADUATE STUDENTS AT THE UNIVERSITY OF TOKYO
ICAS2016_0750: E. Moerland, German Aerospace Center (DLR), Germany; B. Nagel, German Aerospace Centre (DLR), Germany
THE COLLABORATIVE ENGINEER: HOW EDUCATION SHOULD BRING FORTH THE NEW GENERATION OF ENGINEERS

2.1 - Aerodynamics - CFD Methods and Validation

ICAS2016_0005: Q. Zhang¹, Z. Ye¹, S. Wang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
COMPUTATIONAL INVESTIGATION FOR FREE-FLIGHT AERODYNAMICS AND FLIGHT DYNAMICS OF SUBSONIC AND SUPERSONIC PROJECTILES
ICAS2016_0050: R.G. da Silva¹, J.L.F. Azevedo¹; ¹Instituto de Aeronautica e Espaco, Brazil
NUMERICAL SIMULATIONS OF TURBULENT FLOWS OVER THE ONERA-M6 AND DLR-F6 CONFIGURATIONS
ICAS2016_0065: X. Li¹, W. Zheng¹; ¹AVIC, China
ENGINEERING APPLICATION OF GAO-YONG RATIONAL TURBULENCE MODEL TO AN INTER-COOLED DUCT
ICAS2016_0099: I. Bosnyakov¹, A.I. Troshin¹, V.V. Vlasenko¹, A.V. Wolkov¹; ¹TsAGI, Russia
COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS
ICAS2016_0119: R.H. Hua ¹, Z.Y. Ye¹, L. Yang¹; ¹Northwestern Polytechnical University, China
EFFECT OF ELASTIC DEFORMATION ON FLIGHT DYNAMICS OF PROJECTILES WITH LARGE SLENDERNESS RATIO
ICAS2016_0125: R.R. Xue¹, Z.Y. Ye¹, G. Wang¹; ¹Northwestern Polytechnical Univ, China
AERODYNAMIC CHARACTERISTIC COMPARISON OF THE FORWARD AND BACKWARD-SWEPT WINGS
ICAS2016_0140: F.-W. Wang¹, L.-C. Chen¹, H. Qin¹, J. Yu¹; ¹CAAA, China
DETACHED EDDY SIMULATION OF AIRCRAFT MASSIVELY SEPARATED FLOWS
ICAS2016_0152: B.-G. Mi¹, H. Zhan¹, M.-H. Yang¹; ¹Northwestern Polytechnical University, China
MODELLING NONLINEAR HIGH-PRECISION UNSTEADY AERODYNAMICS FOR ADVANCED AIRCRAFT AT HIGH ANGLE OF ATTACK
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_0156: M. Tutty, JAIME Enterprises Australia, Australia; G. Akroyd, Akroyd Aeronautics, Australia; A. Cenko¹, A. Piranian¹; ¹AIWS LLC, United States
STORE SEPARATION FROM WEAPON BAYS
ICAS2016_0223: L. Smith¹, K.J. Craig¹, J.P. Meyer¹, G.R. Spedding, University of Southern California, United States; ¹University of Pretoria, South Africa
OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE
ICAS2016_0246: S. Park¹, K. Chang¹, d.-J. Sheen¹; ¹Hanseo University, South Korea
CFD OF BLENDED WING BODY UCAV WITH VORTEX GENERATOR
ICAS2016_0260: B. Koenig¹, A.F.P. Ribeiro¹, E. Fares¹, R. Zhang², P. Gopalakrishnan², Y. Li²; ¹Exa GmbH, Germany; ²Exa Corp., United States
EXTENDED VALIDATION OF A TRANSONIC LATTICEBOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL
ICAS2016_0330: G.L.O. Halila¹, A.P. Antunes¹, R.G. da Silva², J.L.F. Azevedo²; ¹Embraer S.A., Brazil; ²Instituto de Aeronautica e Espaco, Brazil
EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS
ICAS2016_0375: R.C. Munjulury¹, R. Gårdhagen¹, P. Berry¹, P. Krus¹; ¹Linköping University, Sweden
KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD OPTIMIZATION
ICAS2016_0381: I. Egorov¹, N. Palchekovskaya¹; ¹TsAGI, Russia
NUMERICAL SIMULATION OF AEROTHERMODYNAMIC CHARACTERISTICS OF FLOW OVER SPACE VEHICLE MODEL
ICAS2016_0386: I.V. Egorov¹, N.V. Palchekovskaya¹, M.A. Pugach¹; ¹TsAGI, Russia
AEROTHERMODYNAMICS CHARACTERISTICS OF A SPACE PROBE IN THE MARTIAN ATMOSPHERE
ICAS2016_0405: M. Zhong¹, G.L. Wang¹, J. Hua¹; ¹Chinese Aeronautical Establishment, China
STUDY OF MODEL DEFORMATION AND STING INTERFERENCE TO THE AERODYNAMIC ESTIMATIONS OF THE CAE-AVM MODEL
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_0427: S. Chae¹, H. Kang, Dongyang Mirae University, South Korea; S. Oh, Pusan National University, South Korea; K. Yee¹; ¹Seoul National University, South Korea
EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION
ICAS2016_0499: J.Y. Huh¹, J.S. Rhee¹, K.H. Kim¹, S.Y. Jung, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea
A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS 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_0549: J.W. Kim¹, O.J. Kwon¹; ¹Korea Advanced Institute of Science and Technology, South Korea
NUMERICAL SIMULATION OF MIXING IN AN INLET-FUELED HYPERSONIC AIR-BREATHING PROPULSION
ICAS2016_0550: A.A. Aksenov, TESIS; JIHT RAS, Russia; A.A. Dyadkin ¹, M.K. Mikhailova ², A.E. Schelyaev ², T.V. Simakova ¹, V.V. Zharckova ²; ¹JSV «RSC Energia» , Russia; ²TESIS, Russia
NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN
ICAS2016_0556: Y.-J. Choi¹, O.-J. Kwon¹; ¹Korea Advanced Institute of Science and Technology, South Korea
NUMERICAL INVESTIGATION OF SUBSONIC RAREFIED FLOWS USING DSMC-IP METHODS
ICAS2016_0564: Y.-G. Bai¹, W. Qian¹; ¹Dalian University of Technology, China
INFLUENCE OF THE RHOMBOID ZONE ON AEROELASTIC EXPERIMENTS OF SUPERSONIC AIRCRAFT
ICAS2016_0570: A. Viviani¹, G. Pezzella, Centro Italiano Ricerche Aerospaziali, Italy; E. D'Amato¹; ¹Seconda Università di Napoli, Italy
AERODYNAMIC ANALYSIS WITH SEPARATION DYNAMICS OF A LAUNCHER AT STAGING CONDITIONS
ICAS2016_0572: G.M. Carossa, LEONARDO S.p A., Italy; K. Anisimov¹, A. Chevagin¹, R. Efimov¹, I. Kursakov¹, A. Lysenkov¹, V. Malenko¹, A. Saprykin¹; ¹TsAGI, Russia
EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL
ICAS2016_0576: J.H. Cho¹, S.K. Jeong, Kyung Hee University, South Korea; K.J. Yee¹; ¹Seoul National University, South Korea
APPLICATION OF PROPER ORTHOGONAL DECOMPOSITION FOR AVIATION SAFETY
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_0600: K.-J. Lee, KAI, South Korea
FIGHTER AIRCRAFT HIGH AOA DIRECTIONAL STABILITY IMPROVEMENT DESIGN
ICAS2016_0657: J. Feaster¹, F. Battaglia¹, J. Bayandor¹; ¹Virginia Tech, United States
A COMPUTATIONAL STUDY ON AVIAN FLAPPING FLIGHT AND THE INFLUENCE OF FEATHER SEPARATION
ICAS2016_0658: B. Gater, Virginia Tech , United States; J. Bayandor, Virginia Tech, United States
DYNAMICS MODELLING FOR CONTROL OF AN UNSTEADY HYDRODYNAMIC STINGRAY ROBOT
ICAS2016_0666: Y.M. Tsirkunov¹, M.A. Lobanova¹, A.I. Tsvetkov², B.A. Schepanyuk²; ¹Baltic State Technical University, Russia; ²Saint Petersburg State University, Russia
LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING
ICAS2016_0705: M.H. Ahn¹, D.J. Lee¹; ¹Korea Advanced Institute of Science and Technolgy, South Korea
DEVELOPMENT OF HIGH-ORDER AND HIGH-RESOLUTION SCHEMES FOR EFFICIENT SHOCK CAPTURING IN HIGH-SPEED FLOWS
ICAS2016_0713: E.D.V. Bigarella¹, P.A.G. Ciloni¹, L.C. Scalabrin¹; ¹Embraer S.A., Brazil
EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS
ICAS2016_0715: A. Jahangirian¹, S. Sattarzadeh¹; ¹Amirkabir University of Technology, Iran
A MESH-LESS METHOD FOR COMPRESSIBLE FLOW CALCULATIONS AT ALL SPEED CONDITIONS

2.2 - Experimental Aerodynamics

ICAS2016_0034: D. Lei¹, H. Zenghong¹, G. Yongwei¹; ¹Northwestern Polytechnical university, China
DEVELOPMENT OF HALF-MODEL TEST CAPABILITY AT THE NF-3 WIND TUNNEL
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_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_0162: K.A. Kasim¹, S. Mat¹, I.S. Ishak¹, M. Said¹; ¹Universiti Teknologi Malaysia, Malaysia
EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL
ICAS2016_0196: S. Subagyo, BBTA3-BPPT, Indonesia
INLET DUCT ENGINE TEST FACILITIES IN INDONESIA LOW SPEED TUNNEL (ILST)
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
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_0300: W. Stryczniewicz¹, R. Placek¹, P. Ruchala¹; ¹Institute of Aviation, Poland
INVESTIGATION OF UNSTEADY TRANSONIC FLOW FIELD ABOVE LAMINAR AIRFOIL BY PIV METHOD
ICAS2016_0319: H. Jin¹, D. Lee¹, J. Lee¹, J. Ahn¹; ¹Department of Aerospace Engineering, KAIST, South Korea
HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING
ICAS2016_0329: D. Vukovic¹, D. Damljanovic¹; ¹Military Technical Institute (VTI), Serbia
A GENERALISATION OF THE MATHEMATICAL MODEL OF INTERNAL WIND TUNNEL BALANCES
ICAS2016_0339: X. Zhao¹, X. Xiang¹, L. Wei¹, Q. Shen¹; ¹China Academy of Aerospace Aerodynamics, China
AN EXPERIMENT INVESTIGATION ON SHOCKINDUCED TURBULENT BOUNDARY LAYER SEPARATION FLOW-FIELD
ICAS2016_0390: D. Lundström¹, A. Sobron¹, P. Krus¹, C. Jouannet, SAAB AB, Sweden; R.G.A. da Silva, Instituto Tecnológico de Aeronáutica, Brazil; ¹Linköping University, Sweden
SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT
ICAS2016_0403: X. Qu¹, Y. Yu¹, D. Liao¹, G. Yang¹, Q. Chen¹, G. Tang¹; ¹CARDC, China
DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN FOR 5.5- BY 4-M ACOUSTIC WIND TUNNEL
ICAS2016_0496: A.C. de Bruin, NLR, Netherlands; G. Fatigati, CIRA, Italy; H.B. Shin, KAI, South Korea
KAI SURION HELICOPTER FULL-SCALE AIR INTAKE TESTING AT CIRA ICING WIND TUNNEL
ICAS2016_0508: F. Knoth¹, C. Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TU Munich, Germany
AERODYNAMIC TESTING OF HELICOPTER NOVEL AIR INTAKES
ICAS2016_0553: Y. Sugioka¹, K. Nakakita, JAXA, Japan; K. Asai¹; ¹Tohoku Univ., Japan
NON-INTRUSIVE UNSTEADY PSP TECHNIQUE FOR INVESTIGATION OF TRANSONIC BUFFETING
ICAS2016_0561: R. Placek¹, M. Miller¹, P. Ruchala¹; ¹Institute of Aviation, Poland
THE ROUGHNESS POSITION INFLUENCE ON LAMINAR AEROFOIL AERODYNAMIC CHARACTERISTIC IN TRANSONIC FLOW REGIME
ICAS2016_0582: I. Fumarola, City University London, United Kingdom
AN EXPERIMENTAL INVESTIGATION ON THE FREESTREAM TURBULENCE UPSTREAM OF A SWEPT WING
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_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_0594: K. Matsushima¹, R. Namba¹, H. Kato, JAXA, Japan; ¹Univ. of Toyama, Japan
PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES
ICAS2016_0608: M. Said¹, S. Mat¹; ¹AeroLab, Universiti Teknologi Malaysia, Malaysia
EFFECTS OF REYNOLDS NUMBER ON THE ONSET OF LEADING EDGE VORTEX SEPARATION ABOVE BLUNT-EDGE DELTA WING VFE-2 CONFIGURATIONS
ICAS2016_0651: A. Matta¹, J. Bayandor¹; ¹Virginia Tech, United States
LOW ORDER MODELING OF THE UNSTEADY AND 3D EFFECTS OF CONTINUOUS WAKE FLAPPING FLIGHT
ICAS2016_0656: I.A. Amelyushkin, TsAGI, Russia
MATHEMATICAL MODELS AND OPTICAL INVESTIGATION OF TWO PHASE FLOWS IN WIND TUNNELS
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_0681: K. Nakakita, Japan Aerospace Exploration Agency, Japan
UNSTEADY AERODYNAMIC INFORMATION EXTRACTION USING FFT-BASED UNSTEADY PRESSURE-SENSITIVE PAINT MEASUREMENT
ICAS2016_0683: J.G. Medeiros, Instituto Tecnológico de Aeronáutica, Brazil; A.C. Avelar, Instituto de Aeronautica e Espaço, Brazil; J.B.P. Falcão Filho, Instituto de Aeronáutica e Espaço, Brazil
EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECT ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE
ICAS2016_0710: H.W. Wang¹, Z. Huang¹, L. Li¹, L.F. Wei¹, H.L. Xiong¹; ¹China Academy of Aerospace Aerodynamics, China
THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELDMEASUREMENT BASED ON FLUORESCENT OIL FILM

2.3 - Basic Fluid Dynamics and Flow Control

ICAS2016_0083: D. Veerasamy, United Kingdom
EXPERIMENTAL STUDY OF AEROFOIL-WAKE INDUCED TRANSITION IN BOUNDARY LAYERS
ICAS2016_0124: F. Liu¹, H. Yan¹, J. Xu¹; ¹Northwestern Polytechnical University, China
INVESTIGATION ON OBLIQUE SHOCK WAVE CONTROL BY SURFACE ARC DISCHARGE PLASMA
ICAS2016_0127: M.A. Brutyan¹, A.V. Petrov¹, A.V. Potapchik¹; ¹TsAGI, Russia
NEW METHOD OF TRANSONIC BUFFET DECREASING ON SUPERCRITICAL AIRFOIL
ICAS2016_0138: M.A. Brutyan¹, V.P. Budaev, NRCKI, Russia; A.V. Wolkov¹; ¹TsAGI, Russia
INFLUENCE OF SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER
ICAS2016_0170: A. Russell¹, H. Zare-Behtash¹, K. Kontis¹; ¹University of Glasgow, United Kingdom
CHARACTERISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL
ICAS2016_0173: A.V. Petrov¹, A.V. Potapchik¹, V.G. Soudakov¹; ¹TsAGI, Russia
INVESTIGATION OF FLOW CONTROL OVER THE SUPERCRITICAL AIRFOIL BY TANGENTIAL JET BLOWING AT TRANSONIC SPEEDS
ICAS2016_0225: M.-C. Meijer, University of Pretoria, South Africa; L. Dala, Council for Scientific and Industrial Research, South Africa; P.G. Karkle, Central Aerohydrodynamic Institute, Russia
ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS
ICAS2016_0244: A. Roussel¹, S. Prince¹, M. Viguer¹, A. Kshitij¹, J. Stollery¹, K. Garry¹; ¹Cranfield University, United Kingdom
THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW
ICAS2016_0249: A. Yadav¹, S. Prince¹, J. Holt¹; ¹Cranfield University, United Kingdom
AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS AN OSCILLATORY PITCHING NACA0012 AEROFOIL
ICAS2016_0250: S. Prince¹, J. Holt¹, P. Episkopou¹; ¹Cranfield University, United Kingdom
GEOMETRIC ROUGHNESS EFFECTS ON THE AERODYNAMIC CHARACTERISTICS OF A SPINNING CYLINDER IN CROSSFLOW
ICAS2016_0257: A. Buzica¹, J. Bartasevicius¹, C. Breitsamter¹; ¹Chair of Aerodynamics and Fluid Mechanics, TUM, Germany
ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING
ICAS2016_0333: M. Dong¹, X. Wu¹; ¹Imperial College London, United Kingdom
EXTENDED LOCAL SCATTERING THEORY AND THE ROLE OF A SCATTER ON BOUNDARY-LAYER INSTABILITY AND ACOUSTIC RADIATION
ICAS2016_0346: C.Q. Gao¹, W.W. Zhang¹, Z.Y. Ye¹; ¹Northwestern Polytechnical University , China
NUMERICAL STUDY ON TRANSONIC BUFFET ACTIVE CONTROL BY OPEN AND CLOSED-LOOP STRATEGIES
ICAS2016_0358: D.S. Sboev, TsAGI, Russia
DISTURBANCES IN AN ACCELERATED BOUNDARY LAYER UNDER INFLUENCE OF MODERATE FREE-STREAM TURBULENCE
ICAS2016_0362: J.-L. Bo¹, Y.-F. Liu¹, Y.-W. Liu¹; ¹CAAA, China
NUMERICAL INVESTIGATION OF UNSTEADY INTERACTION CHARACTERISTIC INDUCED BY IMPULSIVE JET
ICAS2016_0389: T.A. Berk¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands
EXPERIMENTAL STUDY ON AERODYNAMIC LOAD CONTROL USING SYNTHETIC JET ACTUATORS
ICAS2016_0391: Z.-Y. Ni¹, N. Cao¹, L. Xu¹; ¹CAAA, China
EXPERIMENTAL INVESTIGATION OF LATERAL PULSE JET INTERACTION FLOWFIELD IN HYPERSONIC FLOW
ICAS2016_0407: X. Li¹, W. Zhang ¹; ¹School of aeronautics, Northwestern Polytechnical University, China
UNSTEADY AERODYNAMICS MODELLING AND ITS APPLICATION IN AEROELASTIC STABILITY ANALYSIS
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
ICAS2016_0455: W. Stalewski¹, K. Surmacz¹, J. Sznajder¹; ¹INSTITUTE of AVIATION, Poland
EFFECTS OF LAMINAR-TURBULENT TRANSITION ON BUFFET ONSET AND TRANSONIC CHARACTERISTICS OF LAMINAR AIRFOIL
ICAS2016_0484: J. Huh¹, S. Lee¹; ¹Inha univ., South Korea
COMPUTATIONS OF SUPERSONIC LATERAL JET
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_0536: A.V. Novikov¹, I.V. Egorov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
DIRECT NUMERICAL SIMULATION OF DISTURBANCES IN A THREE-DIMENSIONAL HYPERSONIC NEAR-WALL FLOW OVER FLAT PLATE AND COMPRESSION CORNER
ICAS2016_0560: P.A. Polivanov¹, A.A. Sidorenko¹, A.A. Maslov¹; ¹ITAM SB RAS, Russia
STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS
ICAS2016_0577: H.S. Mudhar, City University London, United Kingdom
EFFECTIVENESS OF VORTEX GENERATORS IN HIGHLY 3D FLOWS
ICAS2016_0578: H. Xu¹, S. Mughal¹, E.R. Gowree, Centre of Aeronautics,City University London, United Kingdom; S.-J. Sherwin, Department of Aeronautics, Imperial College London, United Kingdom; ¹Department of Mathematics,Imperial College London, United Kingdom
EFFECT OF A 3D INDENTATION ON BOUNDARY LAYER INSTABILITY
ICAS2016_0606: E.R. Gowree¹, C.J. Atkin¹; ¹City University London, United Kingdom
STAGGERED THREE-DIMENSIONAL CAVITIES AS A POSSIBLE METHOD FOR SKIN FRICTION DRAG REDUCTION
ICAS2016_0718: A. Jahangirian¹, R. Khoshkhoo¹; ¹Amirkabir University of Technology, Iran
NUMERICAL SIMULATION OF FLOW SEPARATION CONTROL OVER A HUMP USING DBD PLASMA ACTUATOR
ICAS2016_0724: J. Pellicer, City University London, United Kingdom
EXPERIMENTAL INVESTIGATION OF FLOW AROUND AIRFOILS WITH UNDULATING LEADING EDGES
ICAS2016_0730: M. Herr, German Aerospace Center (DLR), Germany
BROADBAND TRAILING-EDGE NOISE: A STATUS REPORT ON CURRENT PREDICTION CAPABILITIES

2.4 - Applied Aerodynamics

ICAS2016_0003: V.D. Tavernari¹, F.M. Catalano¹; ¹Aeronautical Engineering Department _EESC-USP, Brazil
LOW REYNOLDS PROPELLER META-MODEL FOR MULTIDICIPLYNARY OPTIMIZATION
ICAS2016_0025: P. Czekalowski, Air Force Institute of Technology, Poland; K.-S. Sibilski, Institute of Aviation, Poland; A. Zyluk, Air Force Academy, Poland
AN EXPERIMENTAL STUDY OF MICRO-ELECTROMECHANICAL FLYING INSECT FLAPPING WINGS AERODYNAMIC PERFORMANCE
ICAS2016_0074: K. Wang¹, X.P. Zhu¹, Z. Zhou¹; ¹NWPU University, China
DISTRIBUTED PROPELLERS SLIPSTREAM EFFECTS ON WING AT LOW REYNOLDS NUMBER
ICAS2016_0075: H.-B. Wang¹, X.-P. Zhu, UAV Laboratory, Northwestern Polytechnical University, China; Z. Zhou¹; ¹School of Aeronautics, Northwestern Polytechnical University, China
NUMERICAL SIMULATION OF THE PROPELLER/WING INTERACTIONS AT LOW REYNOLDS NUMBER
ICAS2016_0094: W. Yuan¹, R. Lee¹, A. Wall¹; ¹National Research Council Canada, Canada
SIMULATION OF UNSTEADY SHIP AIRWAKES USING OPENFOAM
ICAS2016_0151: J. Park¹, S. Choi¹, P. Raj¹; ¹Virginia Tech, United States
ON MORE EFFECTIVE AERODYNAMIC DATA GENERATION FOR SIMULATION BASED AIRCRAFT CONCEPTUAL DESIGN
ICAS2016_0220: A.V. Grachev¹, A.N. Kraiko, CIAM, Russia; S.A. Takovitskii¹; ¹TsAGI, Russia
AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD
ICAS2016_0242: B. McCartney¹, S. Prince¹, N. Qin, University of Sheffield, United Kingdom; ¹Cranfield University, United Kingdom
THE EFFECT OF LEADING EDGE ROUNDING ON A CARET WAVERIDER CONFIGURATION AT MACH 8.2
ICAS2016_0267: L. Prince Raj¹, R.S. Myong¹; ¹Gyeongsang National University, South Korea
NUMERICAL SIMULATION OF DROPLET IMPINGEMENT ON A MULTI-ELEMENT HIGH-LIFT AIRFOIL
ICAS2016_0281: Z.-H. Han, Northwestern Polytechnical University, China
SURROOPT: A GENERIC SURROGATE-BASED OPTIMIZATION CODE FOR AERODYNAMIC AND MULTIDISCIPLINARY DESIGN
ICAS2016_0283: N. Ban, Nagaoka University of Technology, Japan
LOW-DRAG / LOW-BOOM SHAPE OPTIMIZATION OF A BIPLANE WING / TWIN-BODY FUSELAGE SST CONFIGURATION
ICAS2016_0299: W. Yang¹, B. Song¹, D. Xue¹; ¹Northwestern Polytechnical University, China
THE PROPULSIVE EFFICIENCY OF FLEXIBLE FLAPPING-WING
ICAS2016_0345: S. Görtz¹, C. Ilic¹, M. Abu-Zurayk¹, R. Liepelt¹, J. Jepsen¹, T. Führer¹, R. Becker¹, J. Scherer¹, T. Kier¹, M. Siggel¹; ¹German Aerospace Center (DLR), Germany
COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT
ICAS2016_0347: D. Florjancic¹, D. Steenhuizen¹, L.L.M. Veldhuis¹; ¹TU Delft, Netherlands
IMPROVED DESIGN OF A HIGH LIFT SYSTEM FOR GENERAL AVIATION AIRCRAFT
ICAS2016_0353: J. Steelant¹, V. Villace¹, M. Marini², G. Pezzella², B. Reimann, DLR, Germany; S.L. Chernyshev³, A.A. Gubanov³, V.A. Talyzin³, N.V. Voevodenko³, N.V. Kukshinov*, A.N. Prokhorov*, A.J. Neelyº, C. Kennellº, D. Verstraete, University of Sydney, Australia; D. Buttsworth, Univ. of Southern Queensland, Australia; ¹ESA-ESTEC, Netherlands; ²CIRA, Italy; ³TsAGI, Russia; *CIAM, Russia; ºUniv. of New South Wales, Australia
NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF A HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT
ICAS2016_0380: V.Y. Aleksandrov¹, M.K. Danilov¹, O.V. Gouskov¹, S.V. Gusev¹, N.V. Kukshinov¹, A.N. Prokhorov¹, V.S. Zakharov¹; ¹CIAM, Russia
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE
ICAS2016_0383: N.V. Voevodenko¹, A.A. Gubanov¹, D.Y. Gusev¹, M.A. Ivankin, TsAGi, Russia; D.S. Ivanyushkin¹, V.Y. Lunin¹, P.A. Meshennikov¹, Y.G. Shvalev¹, V.A. Talyzin¹, V.A. Yakovleva¹; ¹TsAGI, Russia
BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE
ICAS2016_0384: O. Rand¹, V. Khromov¹; ¹Israel Institute of Technology, Israel
EXTRACTION OF LINEAR INFLOW MODEL FOR MANEUVERING HELICOPTER FROM FREE-WAKE ANALYSIS
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
ICAS2016_0459: K.P. Garry¹, J.C. Holt¹, G. Tanguy¹, S.A. Prince¹; ¹Cranfield University, United Kingdom
THE INFLUENCE OF A LOCAL CHANGE IN WING DIHEDRAL ON THE LOW SPEED FLOW CHARACTERISTICS OF RECTANGULAR PLANFORM WINGS
ICAS2016_0515: N.A. Musa¹, S. Mansor¹, A. Ali¹, W.Z. Wan Omar¹; ¹AeroLAB, Universiti Teknologi Malaysia, Malaysia
IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN
ICAS2016_0527: W. Stalewski, INSTITUTE of AVIATION, Poland
FLOW CONTROL ON HELICOPTER-ROTOR BLADES VIA ACTIVE GURNEY FLAP
ICAS2016_0598: D. Nam¹, J. Lee¹, B. KIim¹; ¹Chungnam National University, South Korea
STUDY ON THE SYSTEM INTEGRATION FOR MULTI-ELEMENT AIRFOIL AERODYNAMIC ANALYSIS
ICAS2016_0627: M.M. Entezari, Aerospace Research Institute, Iran; M. Mohammadi-Amin, Aerospace Research Institue, Iran
CFD-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A MANNED RE-ENTRY VEHICLE
ICAS2016_0712: Y.M. Jo ¹, S.H. Park¹, D.J. Lee¹, S. Choi, Virginia Polytechnic Institute and State University, United States; ¹Korea Advanced Institute of Science and Technology, South Korea
DEVELOPMENT OF A THREE-DIMENSIONAL TIGHTLY COUPLED EULER/POTENTIAL FLOW SOLVER FOR TRANSONIC FLOW
ICAS2016_0714: Z. Seifollahi Moghadam ¹, A. Jahangirian¹; ¹Amirkabir University of Technology, Iran
NUMERICAL STUDY OF ACTIVE SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION CONTROL FOR TRANSONIC AERODYNAMICS
ICAS2016_0717: A. Jahangirian¹, M. Ebrahimi¹; ¹Amirkabir University of Technology, Iran
AERODYNAMIC SHAPE OPTIMIZATION WITH A NEW PARALLEL EVOLUTIONARY ALGORITHM AND NUMERICAL FLOW MODELLING
ICAS2016_0754: A.T. Bode-Oke¹, S. Zeyghami, Lehigh University, United States; H. Dong¹; ¹University of Virginia, United States
STRATEGIES FOR ACHIEVING BACKWARD FLIGHT BY A DRAGONFLY
ICAS2016_0755: C. Atkin, City University London, United Kingdom
AFLONEXT – ACTIVE FLOW_LOADS AND NOISE CONTROL ON NEXT GENERATION ACTIVE WING

3.1 - Materials issues, Fatigue and Damage Tolerance

ICAS2016_0146: M. Lee, Agency for Defense Development, South Korea; J. Kim, Chungnam National University, South Korea
PREDICTION OF FRACTURE STRENGTH FOR NOTCHED LAMINATE SUBJECTED TO COMPRESSION LOADING
ICAS2016_0193: I. Rivero Arevalo¹, J. Gomez-Escalonilla Martin¹, V. Ramirez Gonzalez², A. Garcia Martinez-Pardo², D. Garijo Hernandez, IMDEA Materials Institute, Spain; ¹Airbus Defence and Space, Spain; ²Safran Engineering Services, Spain
XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES
ICAS2016_0274: M. Kanerva¹, E. Sarlin, Tampere University of Technology, Department of Material Science, Finland; A. Hållbro, Plansee SE, Sweden; J. Jokinen¹; ¹Aalto University, Department of Mechanical Engineering, Finland
PLASTIC DEFORMATION OF POWDER METALLURGY TUNGSTEN ALLOY FOILS FOR SATELLITE ENCLOSURES
ICAS2016_0277: T. Bach, German Aerospace Center (DLR), Germany
NUMERICAL ASSESSSMENT OF DAMAGE TOLERANCE ALLOWABLES FOR NEW DESIGN CONCEPTS OF STIFFENED COMPOSITE PANELS
ICAS2016_0288: R. de Moura Pinho¹, D. Soria¹, L. Dimithe Aboumou¹; ¹Safran Aircraft Engines, France
A STRESS INTENSITY FACTOR SOLUTION INSPIRED BY SOAP BUBBLES FRAMEWORK
ICAS2016_0291: Q. Wei-qi¹, Z. Yu¹; ¹CARDC, China
ESTIMATION OF TEMPERATURE-DEPENDANT THERMAL CONDUCTIVITY OF MATERIAL WITH GENETIC ALGORITHM
ICAS2016_0303: A.V. Pankov¹, V.V. Konovalov¹; ¹TsAGI, Russia
VERIFICATION OF CFRP COMPONENTS FATIGUE EVALUATION PROCEDURE UNDER IRREGULAR CYCLING LOADING
ICAS2016_0308: C. Li¹, Y. He¹, T. Zhang¹, X. Li¹, S. Zhang¹; ¹Air Force Engineering University, China
LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER CORROSION ENVIRONMENT
ICAS2016_0368: K. Kuruliuk, Central Aerohydrodynamic Institute named after Zhukovsky, Russia
INVESTIGATION OF DEFORMATION FIELDS IN AIRCRAFT PANELS BY NON-CONTACT OPTICAL VIDEOGRAMMETRY METHOD
ICAS2016_0443: E. Dubovikov¹, V. Fomin¹, M. Glebova¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
DAMAGE TOLERANCE AND REPAIR OF UD-RIBS OF LATTICE COMPOSITE FUSELAGE STRUCTURES
ICAS2016_0457: M. Wojtas¹, A. Sobieszek¹, L. Czajkowski¹, R. Zurawski¹; ¹Institute of Aviation, Poland
MODERN MATERIALS IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER
ICAS2016_0522: J.Y. Choung¹, J.W. Kim¹, I.H. Hwang¹; ¹Korea Aerospace Research Institute, South Korea
DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES
ICAS2016_0639: A.A. Sviridov¹, I.G. Khlebnikova¹; ¹TsAGI, Russia
PREDICTION OF WFD OCCURRENCE IN LONGITUDINAL JOINTS OF A FUSELAGE FOR COMMERCIAL AIRPLANE
ICAS2016_0640: B. Alem¹, A. Abedian¹, M. Nasiri¹; ¹Sharif University of Technology, Iran
INSTANTANEOUS BASELINE MULTIPLE DAMAGE DETECTION AND LOCALIZATION IN AN ALUMINIUM PLATE USING LAMB WAVES
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_0021: C.-G. Pak, NASA Armstrong Flight Research Center, United States
UNSTEADY AERODYNAMIC FORCE SENSING FROM MEASURED STRAIN
ICAS2016_0037: R. Degenhardt, DLR, Germany
NEW DESIGN SCENARIO FOR FUTURE COMPOSITE LAUNCHER STRUCTURES
ICAS2016_0040: X.J. Zhao¹, B. Ai¹; ¹China Academy of Aerospace Aerodynamics, China
PANEL VIBRO-ACOUSTIC RESPONSE PREDICTION BASED ON TURBULENT BOUNDARY LAYER MEASUREMENT
ICAS2016_0068: D.A. Akhmedzyanov¹, A.E. Kishalov¹, K.V. Markina¹; ¹USATU, Russia
AUTOMATED SELECTION OF THE MATERIAL A FAN BLADE PS-90A
ICAS2016_0095: P. Gustafsson, SAAB AB, Sweden; A. Linderholt, Linnaeus University, Sweden
A STUDY OF THE ACCURACY OF GROUND VIBRATION TEST DATA USING A REPLICA OF THE GARTEUR SM-AG19 TESTBED STRUCTURE
ICAS2016_0098: A.I. Danilin, Samara State Aerospace University, Russia
DESIGNING OF AIRFRAMES HAVING MINIMUM MASS UNDER SEVERAL LOADINGS (NOT ONLY FULLY STRESSED)
ICAS2016_0123: H. Cho¹, N. Lee², S.J. Shin¹, S. Lee², S.Y. Kim, Agency for Defense Development, South Korea; ¹Seoul National Univ., South Korea; ²Inha Univ., South Korea
FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING
ICAS2016_0135: K. Ye¹, Z.Y. Ye¹, Z.H. Chen¹, Z. Qu¹; ¹Northwestern Polytechnical University, China
UNCERTAINTY QUANTIFICATION AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC AEROTHERMOELASTIC ANALYSIS
ICAS2016_0166: M. Radestock¹, J. Riemenschneider¹, H.P. Monner¹, O. Huxdorf¹, N.P.M. Werter², R. De Breuker²; ¹German Aerospace Center, Germany; ²Delft University of Technology, Netherlands
DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN UAV LEADING EDGE WITH A MORPHING MECHANISM
ICAS2016_0178: H. Huang, China; M. Zhao, China; W. Wang, China
MODELING AND ANALYSIS METHOD ON CRASHWORTHINESS OF CIVILIAN AIRCRAFT FUSELAGE STRUCTURES
ICAS2016_0189: J. Qin¹, B.-W. Wang¹; ¹ASRI, China
RESEARCH ON VIBRATION CHARACTERISTIC FOR VARIABLE ROTATING VELOCITY BLADES
ICAS2016_0198: W. Hu¹, Z.C. Yang¹, Y.S. Gu¹; ¹Northwestern Polytechnical University, China
THE INFLUENCE OF MORPHING PROCESS ON THE AEROELASTIC CHARACTERISTICS OF A FOLDING WING
ICAS2016_0201: Y.I. Dudarkov¹, E.A. Levchenko¹, M.V. Limonin¹, A.S. Dzuba¹; ¹TsAGI, Russia
EXPERIENCE OF USING NONLINEAR NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT PRIMARY STRUCTURE STRENGTH
ICAS2016_0206: M. Winter¹, C. Breitsamter¹; ¹Technische Universität München, Germany
SENSITIVITY ANALYSIS OF UNSTEADY AERODYNAMIC REDUCED-ORDER MODELS ROBUST TO FREESTREAM PARAMETER VARIATIONS
ICAS2016_0209: S.-F. Lung, Jacobs, United States; W.L. Ko, NASA, United States
APPLICATIONS OF DISPLACEMENT TRANSFER FUNCTIONS TO DEFORMED SHAPE PREDICTIONS OF THE G-III SWEPT-WING STRUCTURE
ICAS2016_0226: K.A. Balunov¹, V.V. Chedrik¹, S.A. Tuktarov¹, V.M. Uskov¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS
ICAS2016_0232: J. Kim¹, C. Kim, Korea Advanced Institute of Science and Technology, South Korea; S. Jun¹; ¹Agency for Defense Development, South Korea
AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS
ICAS2016_0248: K. Li¹, L. Zhang¹, K. Pan¹, W. Huang¹; ¹Aircraft strength research institute of China, China
SEMI-A VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZOELECTRIC ACTUATOR WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE
ICAS2016_0266: Y.-Y. Hou¹, Z.-Q. Liu¹, C. Ji¹; ¹China Academy o f Aerospace Aerodynamics , China
SOLAR UAV GUST LOAD AMENDMENT
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_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_0282: R. Zhang, Chinese Aeronautical Establishment, China; D.-G. Cui, Aviation of China, China; G. Song, Beihang University, China
FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE
ICAS2016_0335: K.H. Nguyen¹, V.H. Truong¹, J.H. Kweon¹; ¹Gyeongsang National University, South Korea
A STUDY ON FAILURE BEHAVIORS OF REPAIRED COMPOSITE STRUCTURES WITH SCARF BONDED PATCH
ICAS2016_0337: L.-J. Dong, Chinese Aeronautical Establishment, China; G. Song, Beijing University of Aeronautics and Astronautics, China; D.-G. Cui, Aircraft Design and Research Institute of Shenyang, China
APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS
ICAS2016_0354: G. Kowaleczko¹, T. Gorecki¹; ¹Air Force Institute of Technology , Poland
THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER'S CONSTRUCTION SCHEMATICS WITH SPECIAL EMPHASIS ON GROUND RESONANCE PHENOMENON
ICAS2016_0393: T. Matsuda¹, K. Mizutani¹, S. Enomoto¹, M. Nishida², T. Moroe², K. Yamada²; ¹CHURYO ENGINEERING CO., LTD., Japan; ²Nagoya Institute of Technology, Japan
FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO PROJECTILE IMPACTS
ICAS2016_0436: G.A. Amiryants, Russia; A.V. Grigorev, Russia; Y.A. Nayko, Russia; S.E. Paryshev, Russia
THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT
ICAS2016_0467: E.M. Amato¹, C. Polsinelli¹, E. Cestino¹, G. Frulla¹, R. Carrese², P. Marzocca²; ¹Politecnico di Torino, Italy; ²RMIT University, Australia
ELASTO-STATIC AND MODAL MODELING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES
ICAS2016_0500: B. Talebi¹, A. Abedian¹, S. Firooz¹; ¹Aerospace Engineering, Sharif University of Technology, Iran
OPTIMIZATION OF COMPOSITE PATCH REPAIR FOR INCLINED CRACK ON ALUMINUM PLATE USING GENETIC ALGORITHM
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_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_0519: W. Qian¹, Y.-G. Bai¹, D. Wang, AVIC Aerodynamics Research Institute, China; ¹Dalian University of Technology, China
DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY
ICAS2016_0551: A. Dzuba¹, A. Shanygin¹, I. Kondakov¹, A. Razin², V. Vassiliev²; ¹Central Aerohydrodynamic Institute (TsAGI), Russia; ²Central Research Institute for Special Machinery (CRISM), Russia
NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES
ICAS2016_0596: B. van de Kamp¹, S. Kalow¹, J. Riemenschneider¹, R. Bartels¹, H. Mainz¹; ¹German Aerospace Center (DLR), Germany
MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES
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_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_0620: A.N. Shanygin¹, A.V. Chernov¹, D.Y. Fomin¹, V.I. Grishin, TsAGI, Russia; I.N. Kacharava¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS
ICAS2016_0622: I. Mareskin, DAFE MIPT, Russia
MULTIDISCIPLINARY OPTIMIZATION OF PRO-COMPOSITE STRUCTURAL LAYOUTS OF HIGH LOADED AIRCRAFT CONSTRUCTIONS
ICAS2016_0633: E.S. Dias, Brazil; C.A. Cimini Jr., Brazil
BEARING STRENGTH ASSESSMENT OF COMPOSITE MATERIAL THROUGH NUMERICAL MODELS
ICAS2016_0670: B. Horton¹, J. Bayandor¹; ¹Virginia Tech, United States
NUMERICAL INVESTIGATION OF FAN-BLADE OUT USING MESO-SCALE COMPOSITE MODELING
ICAS2016_0673: M. Alfano, Politecnico di Milano, Italy; C. Bisagni, Delft University of Technology, Netherlands
CHAOS THEORY APPLIED TO BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELL
ICAS2016_0676: F. Fonte¹, L. Riccobene¹, S. Ricci¹, S. Adden², M. Martegani²; ¹Politecnico di Milano, Italy; ²IBK Technologie, Germany
DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL
ICAS2016_0685: N. Arai¹, W. Harasani, King Abdruaziz Univ., Saudi Arabia; K. Hiraoka¹; ¹Tokai Univ., Japan
EVALUATION OF CONCEPTUAL DESIGN BASED ON MANUFACTURED ACTUAL UNMANNED SOLAR PLANE
ICAS2016_0708: M. Beerhorst¹, C. Hühne¹; ¹DLR, Germany
WEIGHT REDUCTION OF CYLINDRICAL GRID STRUCTURES USING AXIAL-HELICAL-DESIGN
ICAS2016_0716: M. Candon¹, R. Carrese¹, H. Ogawa¹, P. Marzocca¹; ¹RMIT University, Australia
CHARACTERIZATION OF THE NONLINEAR AEROELASTIC BEHAVIOR OF AN AIRFOIL WITH FREEPLAY AND AERODYNAMIC NONLINEARITY
ICAS2016_0720: S. Bagassi¹, F. Lucchi¹, F. De Crescenzio¹, F. Persiani¹; ¹University of Bologna, Italy
GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS
ICAS2016_0746: I.K. Park¹, T.-U. Kim¹, S.-H. Kim¹; ¹KARI, South Korea
NONLINEAR DAMAGE MODELING AND ANALYSIS OF VISCOPLASTIC COMPOSITE MATERIALS

4 - Propulsion

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_0060: L. Veldhuis¹, T. Stokkermans¹, T. Sinnige¹, G. Eitelberg, TU Delft / DNW, Netherlands; ¹TU Delft, Netherlands
ANALYSIS OF SWIRL RECOVERY VANES FOR INCREASED PROPULSIVE EFFICIENCY IN TRACTOR PROPELLER AIRCRAFT
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
ICAS2016_0100: J. Jiao¹, Y.-G. Zhang¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China
MULTI-OBJECTIVE OPTIMAL DESIGN OF THE PROPELLER FOR HIGH ALTITUDE AIRSHIPS BASED ON HIGH EFFICIENCY AND LIGHT WEIGHT
ICAS2016_0163: O.S. Gurevich¹, A.I. Gulienko¹; ¹Central Institute of Aviation Motors (CIAM), Russia
METHODS FOR IMPROVING THE RELIABILITY OF FUEL SUPPLY SYSTEM OF GAS TURBINE ENGINES WITH USING ELECTRICALLY DRIVEN PUMPS
ICAS2016_0165: Y.M. Shchurovskiy, Central Institute of Aviation Motors (CIAM), Russia
INVESTIGATION OF CHARACTERISTICS OF THE OIL SYSTEM WITH ELECTRICALLY DRIVEN PUMPS FOR GAS TURBINE ENGINE
ICAS2016_0172: S. Qiu¹, X.Y. Deng¹; ¹AVIC Commercial Aircraft Engine CO.LTD, China
MULTI-POINT DESIGN OPTIMIZATION OF A HIGH BYPASS RATIO FAN BLADE
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_0234: X. Li¹, Z. Guo¹, Z. Hou¹; ¹National University of Defense Technology, China
THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMIC CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES
ICAS2016_0259: T. Otten¹, T. Lengyel-Kampmann¹; ¹German Aerospace Center (DLR), Germany
MISSION BASED COMPARISON OF SINGLE- AND COUNTER-ROTATING FAN DESIGNS
ICAS2016_0261: S.V. Pankov, CIAM , Russia; V.I. Mileshin¹, I.K. Orekhov¹, V.A. Fateev¹; ¹CIAM, Russia
DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED
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_0276: A.D. Nepomnyashchiy¹, S.V. Suntsov ¹, S.Y. Danilkin¹, V.P. Maslov¹; ¹Central Institute of Aviation Motors (CIAM), Russia
EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT
ICAS2016_0296: X.-W. Liu, China; A.-L. Gong, China; M. Yan, China; W.-J. Zhou, China
NUMERICAL INVESTIGATION OF INLET STARTING CHARACTERISTICS
ICAS2016_0344: M. Ryemill¹, C. Bewick¹, J.K. Min, Pusan UTC, South Korea; ¹Rolls-Royce plc, United Kingdom
THE ROLLS-ROYCE PLC ULTRAFAN HEAT MANAGEMENT CHALLENGE
ICAS2016_0366: F. Haselbach, Rolls-Royce plc, United Kingdom
KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES
ICAS2016_0406: S. Joo¹, J. Yoon¹, J. Kim¹, S. Kim¹, Y. Yoon¹; ¹seoul national university, South Korea
COMBUSTION INSTABILITY FREQUENCY MODE SHIFT OF H2/CH4 RATIO AND COMBUSTOR LENGTH IN A MODEL GAS TURBINE
ICAS2016_0418: T. Yatsufusa¹, K. Takatani¹, S. Miyata¹; ¹Hiroshima Institute of Technology, Japan
APPLICATION OF FLAME MEASUREMENT TECHNIC BY DENSELY INSTALLED ION-PROBES ON 2-STROKE GASOLINE ENGINE
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_0458: M.A. Ivankin¹, A.A. Nikolaev¹, V.A. Talyzin¹, O.V. Voloschenko¹; ¹TsAGI, Russia
INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT
ICAS2016_0481: A.N. Startsev¹, Y.M. Temis¹, E.G. Steshakov¹, D.A. Yakushev¹; ¹CIAM, Russia
MULTI-DISCIPLINARY DESIGN OF HIGH-SPEED COMPRESSORS FOR PROSPECTIVE TURBO-SHAFT ENGINE
ICAS2016_0542: A. Lanshin¹, A. Mirzoyan¹, A. Polev¹; ¹CIAM, Russia
DEVELOPMENT OF TECHNOLOGY ADVANCE FOR FUTURE PROPULSION SYSTEMS OF HAUL AIRCRAFT
ICAS2016_0548: T. Kächele¹, T. Schneider, MTU Aero Engines AG, Germany; R. Niehuis¹; ¹Universität der Bundeswehr, Germany
STUDY ON EFFICIENT FULL ANNULUS URANS COMPUTATIONS OF AN INTAKE COMPRESSOR CONFIGURATION
ICAS2016_0566: V. Baklanov, Russia
DYNAMICS AND VIBRATION OF NEW GENERATION AVIATION ENGINES
ICAS2016_0583: K. Anisimov¹, A.A. Savelyev¹; ¹TsAGI, Russia
AERODYNAMIC OPTIMIZATION OF AIRPLANE PROPULSION SYSTEM WITHIN THE FRAMEWORK OF AGILE PROJECT
ICAS2016_0595: M. Strack¹, T. Zill¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
INTEGRATION OF HYBRID PROPULSION SYSTEM IN A CS23 COMMUTER DESIGN
ICAS2016_0611: K. Stremousov¹, M. Arkhipov¹, S. Serokhvostov¹; ¹Moscow Institute of Physics and Technology, Russia
SMALL HEIGHT DUCT DESIGN FOR MULTICOPTER FAN
ICAS2016_0623: R.P.M. Rademakers¹, J.P. Haug¹, R. Niehuis¹, M. Stoeßel, Wehrtechnische Dienststelle für Luftfahrzeuge u Luftfahrtgeräte, Germany; ¹Institute of Jet Propulsion (UniBwM), Germany
DESIGN AND DEVELOPMENT OF A MILITARY ENGINE INLET RESEARCH DUCT
ICAS2016_0628: Y.K. Song¹, J. Bayandor¹; ¹Virginia Tech, United States
CHARACTERIZATION OF DISTORTED FLUID FLOW ALONG ADVANCED HIGH-BYPASS PROPULSION SYSTEM
ICAS2016_0629: Y.K. Song¹, K. Schroeder¹, B. Horton¹, J. Bayandor¹; ¹Virginia Tech, United States
ADVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AERIAL SYSTEM INGESTION
ICAS2016_0659: P. Ruchala¹, K. Bogdanski, Politechnika Warszawska, Poland; W. Stryczniewicz¹; ¹Instytut Lotnictwa, Poland
ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV METHOD
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_0737: O. Otto, Siemens AG, Germany
ELECTRIC PROPULSION FOR AIRCRAFT

5.1 - Flight Dynamics and Control (Control & Modelling)

ICAS2016_0019: P.V. Kuzmin¹, B.A. Meleshin¹, Y.F. Shelyukhin¹, D.V. Shukhovtsov¹; ¹TsAGI, Russia
HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACK
ICAS2016_0026: R. Mori, Electronic Navigation Research Institute, Japan
NOVEL PILOT CONTROL MODEL WITH STOCHASTIC AND PERIODICAL MOVEMENT
ICAS2016_0043: A.V. Efremov ¹, M.S. Tyaglik¹, A.S. Tyaglik¹, V.V. Aleksandrov¹; ¹Moscow aviation institute, Russia
THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS
ICAS2016_0073: J. Diepolder¹, J.Z. Ben-Asher, Faculty of Aerospace Engineering - Technion, Israel; A. Gabrys¹, S. Schatz¹, M. Bittner¹, M. Rieck¹, B. Grüter¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics - TUM, Germany
FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS
ICAS2016_0087: Y. Ochi, National Defense Academy, Japan
PILOT'S CG LOCATION AND ATTITUDE CONTROL FOR LATERAL MANEUVER OF A HANG GLIDER
ICAS2016_0091: F. Cen¹, Q. Li¹, B.-W. Nie², Z.-T. Liu², H.-S. Sun²; ¹Tsinghua University, China; ²China Aerodynamics Research and Development Center, China
WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS
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
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_0195: H. Fukumoto¹, S. Ueno¹; ¹Yokohama National University, Japan
MINIMUM-TIME FORMATION USING OPTIMAL SOLUTIONS OF SINGLE FIXED-WING AIRCRAFT
ICAS2016_0197: A.K. Khatri¹, V. Kumar¹; ¹CSIR-NAL, India
BIFURCATION ANALYSIS OF A GENERIC PUSHER TYPE TRANSPORT AIRCRAFT CONFIGURATION IN NEAR-STALL FLIGHT
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_0251: S. Oh¹, I. Cho¹, C. McLaughlin, The University of Kansas, United States; ¹Korea Aerospace Industries, LTD, South Korea
AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH HORIZONTAL TAIL ACTUATOR FAILURE
ICAS2016_0258: K. Grinev¹, S. Sorokin¹; ¹The Central Aerohydrodynamic Institute (TsAGI), Russia
EFFECT OF FEEL SYSTEM CHARACTERISTICS ON PILOT MODEL PARAMETERS
ICAS2016_0269: H.-G. Kim¹, H.-J. Kim¹; ¹Seoul National University, South Korea
IMPACT ANGLE CONTROL GUIDANCE CONSIDERING GRAVITY EFFECT
ICAS2016_0290: N. Siepenkötter¹, D. Moormann¹; ¹RWTH Aachen University, Germany
PRECISION LANDING BASED ON ATMOSPHERIC DISTURBANCE MONITORING AND MODEL PREDICTIVE CONTROL
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_0325: D.I. Ignatyev ¹, M.E. Sidoryuk¹, K.A. Kolinko¹, A.N. Khrabrov¹; ¹Central Aerohydrodynamic Institute named after N.E. Zhukovsky, Russia
WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION
ICAS2016_0355: G.-H. Moon¹, S.-W. Shim¹, M.-J. Tahk¹; ¹KAIST, South Korea
AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS
ICAS2016_0379: M.K. Kim¹, M.-H. Cho¹, M.-J. Tahk¹; ¹KAIST, South Korea
TRAJECTORY DESIGN WITH PATH PREDICTION FOR TERRAIN FOLLOWING
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_0412: Y. Kim¹, G. Seo¹; ¹Gyeongsang National University, South Korea
ON STABILITY MARGIN OF A LQR-BASED VEHICLE NETWORK
ICAS2016_0437: M. Naruoka, Japan Aerospace Exploration Agency, Japan
A WAVELET BASED FLIGHT DATA PREPROCESSING METHOD FOR FLIGHT CHARACTERISTICS ESTIMATION AND FAULT DETECTION
ICAS2016_0449: A. Sobron¹, D. Lundström¹, I. Staack¹, P. Krus¹; ¹Linköping University, Sweden
DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL AND DATA ACQUISITION SYSTEM FOR UNSTABLE SUBSCALE AIRCRAFT
ICAS2016_0474: H.-H. Kwon¹, H.-L. Choi¹; ¹KAIST, South Korea
MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL
ICAS2016_0475: N.K. Wickramasinghe¹, S. Fukushima¹, H. Hirabayashi¹; ¹Electronic Navigation Research Institute, Japan
BENEFITS ASSESSMENT ON TIME-BASED OCEANIC ARRIVALS TO THE TOKYO METROPOLITAN AREA
ICAS2016_0498: J.G. Park¹, J.H. Moon¹, J.E. Jang¹, M.S. Park¹; ¹Koreanair, South Korea
MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER
ICAS2016_0501: N. Yokoyama, National Defense Academy of Japan, Japan
INFERENCE OF FLIGHT INTENT BASED ON INVERSE OPTIMAL CONTROL
ICAS2016_0528: R. Rodríguez Robles¹, A. Sanz de Blas¹; ¹Airbus Defence & Space, Spain
ELASTIC MODES ADAPTIVE CANCELLATION ALGORITHM FOR THE A330 MRTT FLYING BOOM CONTROL LAWS
ICAS2016_0532: L. Wang, China; C. Tang, China
FLIGHT DYNAMIC STABILITY ANALYSIS OF A FLEXIBLE FLYING WING
ICAS2016_0545: Y.G.J. Park¹, C.G. Park¹; ¹Seoul National University, South Korea
WIND VELOCITY ESTIMATION WITHOUT AN AIR SPEED SENSOR USING KALMAN FILTER UNDER THE COLORED MEASUREMENT NOISE
ICAS2016_0568: S.-M. Hong¹, M.-G. Seo¹, M.-J. Tahk¹; ¹KAIST, South Korea
TERMINAL IMPACT ANGLE AND ANGLE-OF-ATTACK CONTROL GUIDANCE FOR SURFACE-TO-AIR MISSILE USING TVC
ICAS2016_0586: A. Anton Diez¹, F. Asensio Nieto¹; ¹AIRBUS DEFENCE & SPACE, Spain
ADVANCED REFUELING BOOM SYSTEM (ARBS) DEVELOPMENT AND HANDLING QUALITIES EVALUATION
ICAS2016_0723: S. Bae¹, H.-S. Shin¹, A. Tsourdos¹; ¹Cranfield University, United Kingdom
MULTI-STEP TRAJECTORY OPTIMIZATION FOR ATM BASED ON APPROXIMATED OPTIMAL PATH

5.2 - Flight Dynamics and Control (UAV related)

ICAS2016_0062: C.-S. Yoo¹, E.-Y. Jang¹, B.-S. Song¹, A. Cho¹, B.-J. Park¹, Y.-S. Kim¹, Y.-S. Kang¹, S.-O. Koo¹; ¹Korea Aerospace Research Institute, South Korea
LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV
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
ICAS2016_0096: B.-Y. Lee¹, S. Han¹, H.-J. Park², D.-W. Yoo², M.-J. Tahk¹; ¹Korea Advanced Institute of Science and Technology, South Korea; ²Agency for Defense Development , South Korea
ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME
ICAS2016_0101: R. Wang¹, X.P. Zhu¹, Z. Zhou¹, Z.P. Wang¹; ¹Northwestern Polytechnical University, China
MODELING AND CONTROL OF HIGHLY FLEXIBLE FLYING-WING UAV WITH MULTIPLE ELEVONS AND PROPELLERS
ICAS2016_0121: A.-T. Nguyen¹, J.-K. Kim¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea
THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT
ICAS2016_0128: N. Cho, South Korea; Y. Kim, South Korea
APPROXIMATE THREE-DIMENSIONAL PATH GENERATION FOR UAV PATH-FOLLOWING
ICAS2016_0129: S. Lee¹, Y. Kim¹, T.-Y. Um, Agency for Defense Development, South Korea; ¹Seoul National University, South Korea
CAPTURE REGION ANALYSIS FOR MISSILE GUIDANCE WITH FIELD-OF-VIEW CONSTRAINT AGAINST MOVING TARGET
ICAS2016_0158: Y.B. Been¹, Y.J. Kang¹, S.J. Shin¹; ¹Seoul National Univ., South Korea
A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE
ICAS2016_0203: D. Ding¹, W.Q. Qian¹, Q. Wang¹; ¹Computational Aerodynamics Institute of CARDC, China
ANALYSIS ON OFFLINE AND ONLINE IDENTIFICATION METHODS FOR AIRCRAFT STABILITY AND CONTROL DERIVATIVES
ICAS2016_0207: R.K. Rangel, BRVANT / BRV UAV& Flight Systems, Brazil
DEVELOPMENT OF PEST\'S BIOLOGICAL CONTROL TOOL USING VTOL UAV SYSTEMS
ICAS2016_0231: O. Tekinalp, Middle East Tecnical University, Turkey; S. Kumbasar, Middle East Technical University, Turkey
A NOVEL FLIGHT CONTORL ALGORITHM FOR MULTICOPTERS
ICAS2016_0237: H.I. Kim¹, H.B. Lee¹, H.J. Kim¹; ¹Seoul National Univ., South Korea
SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION
ICAS2016_0256: S.W. Ryu¹, J.G. Lee¹, H.J. Kim¹; ¹Seoul National University, South Korea
OPTICAL FLOW ON A FLAPPING WING-MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER
ICAS2016_0313: C. Galinski¹, W. Stalewski¹, M. Lis¹, J. Hajduk, Air Force Institute of Technology, Poland; ¹Institute of Aviation, Poland
OVERVIEW OF THE INVERTED JOINED WING SCALED DEMONSTRATOR PROGRAMME
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_0334: S.Y. Han¹, B.Y. Lee¹, J.M. Ahn¹, M.J. Tahk¹; ¹KAIST, South Korea
PERCH LANDING ASSISTED BY THRUSTER (PLAT): SIX D.O.F. TRAJECTORY OPTIMIZATION
ICAS2016_0370: Y. Watanabe¹, A. Manecy¹, A. Amiez¹, C. Lesire¹, C. Grand¹; ¹ONERA, France
NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION
ICAS2016_0373: S. Cho¹, Y. Jung, Korea Aerospace Research Institute, South Korea; D.H. Shim¹; ¹Korea Advanced Institute of Science and Technology, South Korea
FLIGHT TESTS OF THE VISION-BASED TARGET SENSING AND APPROACHING
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_0399: J. Moon¹, S. Choi¹, S. Cho¹, H. Kim¹; ¹KOREANAIR, South Korea
GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV
ICAS2016_0401: J. Jeong¹, S. Kim¹, J. Suk¹; ¹Chungnam National University, South Korea
ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR RECONFIGURATION OF ORGANIC FLIGHT ARRAY
ICAS2016_0413: V. Golubev¹, P. Kazarin¹, W. MacKunis¹, S. Borener², D. Hufty²; ¹ERAU, United States; ²FAA, United States
ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS
ICAS2016_0414: C. Göttlicher¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TU Munich, Germany
FLIGHT PATH RECONSTRUCTION FOR AN UNMANNED AERIAL VEHICLE USING LOW-COST SENSORS
ICAS2016_0415: H. Shin¹, H. Kim¹, J. Lee¹, D.H. Shim¹; ¹Korea Advance Institute of Science and Technology, South Korea
DESIGN THE GUIDANCE LAW FOR FORMATION FLIGHT OF MULTIPLE UAVS
ICAS2016_0444: T. Fricke¹, F. Holzapfel¹; ¹Technische Universität München, Germany
STRATEGIES FOR MANUAL LANDING OF REMOTELY PILOTED AIRPLANES WITH LARGE TIME DELAY
ICAS2016_0445: T.M. Shim¹, Y.J. Kim¹, H.C. Bang¹; ¹KAIST, South Korea
OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM
ICAS2016_0477: K. Fujita¹, H. Nagai, Tohoku University, Japan; A. Oyama¹; ¹ISAS/JAXA, Japan
EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANE
ICAS2016_0485: S.-H. Park, LIG Nex1., South Korea; K.-K. Park¹, S.-S. Park¹, C.-K. Ryoo¹; ¹Inha Univ., South Korea
REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY
ICAS2016_0497: C. Tang, China; L. Wang, China
FLIGHT DYNAMIC RESPONSE ANALYSIS OF THE FLEXIBLE AIRCRAFT FLYING THROUGH THE WIND FIELD OVER COMPLEX TERRAINS
ICAS2016_0503: S.Y. Park¹, D.H. Shim¹; ¹KAIST, South Korea
DEPTH IMAGE BASED DIRECT SLAM FOR SMALL UAVS
ICAS2016_0516: K.J. Kim¹, J.M. Ahn, Agency for Defense and Development, South Korea; S.K. Kim¹, J.Y. Suk¹; ¹Chungnam national university, South Korea
ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR BLENDED-WING UAV WITH COMPLEX DAMAGE
ICAS2016_0613: B. Gati, Budapest University of Technology and Economics, Hungary
MOBILE LAUNCHING TREBUCHET FOR UAVS
ICAS2016_0637: E. D\'Amato¹, G. Tartaglione, University of Naples Parthenope, Italy; L. Blasi¹, M. Mattei¹; ¹Second University of Naples, Italy
NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV
ICAS2016_0686: F.C. Reis¹, E.M. Belo¹; ¹Escola de Engenharia de São Carlos - USP, Brazil
SYSTEM IDENTIFICATION OF A SCALE HELICOPTER IN HOVERING FLIGHT
ICAS2016_0700: R. Hun¹, N.K. Sinha¹, D. Chakraborti, ADRDE, India; P. Balasubramanian, RIC, India; ¹Indian Institute of Technology,Madras, India
DYNAMIC MODELING AND STABILITY ANALYSIS OF A HIGH ALTITUDE AIRSHIP

6 - Systems, Subsystems and Equipment

ICAS2016_0049: G. Di Rito¹, R. Galatolo¹, F. Schettini¹; ¹Università di Pisa - Dip. Ingegneria Civile ed Industriale, Italy
EXPERIMENTAL AND SIMULATION STUDY OF THE DYNAMICS OF AN ELECTRO-MECHANICAL LANDING GEAR ACTUATOR
ICAS2016_0105: F. Mahiddini¹, M. Ridel¹, P. Reulet¹, D. Donjat¹, P. Millan¹; ¹ONERA, France
COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT"
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_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_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
ICAS2016_0184: F. Sanchez, Institut Clément Ader/Paul Sabatier University, France; S. Delbecq, Institut Clément Ader/Safran Electronics & Defense, France
SURROGATE MODELING TECHNIQUE FOR THE CONCEPTUAL AND PRELIMINARY DESIGN OF EMBEDDED ACTUATION SYSTEMS AND COMPONENTS
ICAS2016_0188: R. Hällqvist¹, M. Eek¹, R. Braun², P. Krus²; ¹Saab Aeronautics, Sweden; ²Linköping University, Sweden
METHODS FOR AUTOMATING MODEL VALIDATION: STEADY-STATE IDENTIFICATION APPLIED ON GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM MEASUREMENTS
ICAS2016_0215: S. Gafurov¹, L. Rodionov¹, A. Kryuchkov¹, H. Handroos, Lappeenranta University of Technology, Finland; ¹Samara National Research University, Russia
HIL TEST BENCH FOR ENGINE'S FUEL CONTROL SYSTEMS INVESTIGATION
ICAS2016_0318: R. Fusaro¹, Z. Goraj, Warsaw University of Technology, Poland; N. Viola¹; ¹Politecnico di Torino, Italy
SELECTION OF AN UAV CONFIGURATION LAYOUT FOR OPTIMISATION OF TELEDETECTION MISSION USING HYPERSPECTRAL SENSORS
ICAS2016_0321: X. Chen¹, H. Ren¹, J. Wang, University of Illinois at Urbana-Champaign, United States; Y. Chen¹, J. Chen¹, L. Zhi¹; ¹COMAC, China
A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM
ICAS2016_0535: H.-J. Kim¹, O.-K. Ha¹, Y.-K. Jun¹; ¹Gyeongsang National University, South Korea
GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE
ICAS2016_0554: J. Fu¹, Y. Fu¹, J.-C. Mare, Institut Clément Ader, INSA-Toulouse, France; ¹Beihang University, China
SPECIAL CONSIDERATIONS TO THERMAL BEHAVIOR MODELING AND SIMULATION OF AN AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEM
ICAS2016_0585: P. Shiva Prakasha¹, P.D. Ciampa¹, B. Nagel¹, L. Boggero², M. Fioriti²; ¹German Aerospace Center, Germany; ²Politecnico di Torino, Italy
COLLABORATIVE SYSTEMS DRIVEN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION
ICAS2016_0619: Y.S. Chati¹, H. Balakrishnan¹; ¹Massachusetts Institute of Technology, United States
STATISTICAL MODELING OF AIRCRAFT ENGINE FUEL FLOW RATE
ICAS2016_0707: H. Liu, China
STRATEGIES TO ENHANCE A CONFIGURATION FOR HIGH-PRECISION MULTI DISCIPLINARY OPTIMIZATION

7 - Systems Engineering and Supply Chain

ICAS2016_0722: H.-I. Lee¹, H.-S. Shin¹, A. Tsourdos¹; ¹Cranfield University, United Kingdom
EVOLUTIONARY GAME BASED MULTI-OBJECTIVE OPTIMIZATION FOR MULTI-AGENT NETWORK RESILIENCE
ICAS2016_0728: W. Roberts¹, K. Griendling¹, A. Gray¹, D.N. Mavris¹; ¹Georgia Tech, United States
UNMANNED VEHICLE COLLABORATION RESEARCH ENVIRONMENT FOR MARITIME SEARCH AND RESCUE
ICAS2016_0729: K. Griendling¹, O.J. Pinon¹, D.N. Mavris¹; ¹Georgia Tech, United States
VIRTUAL EXPERIMENTATION AND VISUAL ANALYTICS IN SUPPORT OF SYSTEMS ENGINEERING AND SYSTEMS OF SYSTEMS ENGINEERING EFFORTS
ICAS2016_0732: S.X. Ying, COMAC, China
REPORT FROM ICAS WORKSHOP ON COMPLEX SYSTEMS INTEGRATION IN AERONAUTICS
ICAS2016_0751: X.G. Zhang, Aviation Industry Corporation of China (AVIC), China
CO-EVOLUTION OF COMPLEX AERONAUTICAL SYSTEM & COMPLEX SYSTEM ENGINEERING
ICAS2016_0752: P. Krus, Linköping University, Sweden; L. Pereira, Federal University of ABC, Brazil
SYSTEMS ENGINEERING: AN INTERDISCIPLINARY CHALLENGE

8 - Air Transport System Efficiency

ICAS2016_0027: S. Ramasamy¹, R. Sabatini¹, Y. Lim¹, A. Gardi¹; ¹RMIT University, Australia
AUTOMATED SEPARATION ASSURANCE AND COLLISION AVOIDANCE FUNCTIONS IN THE CNS+A CONTEXT
ICAS2016_0033: Y.K. Hong¹, Y.D. Kim¹, K.J. Lee, Korea Aerospace University, South Korea; ¹Seoul National University, South Korea
NONLINEAR OPTIMAL CONFLICT RESOLUTION SOLVED WITH PARTICLE SWARM OPTIMIZATION
ICAS2016_0048: R. Mori, Electronic Navigation Research Institute, Japan
IMPROVEMENT OF PUSHBACK TIME ASSIGNMENT UNDER UNCERTAINTIES
ICAS2016_0051: M. Bittner¹, M. Rieck¹, B. Grüter¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany
OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES
ICAS2016_0055: P. Choroba¹, L. van der Hoorn¹; ¹Eurocontrol, France
TOWARDS A MORE HARMONISED AND WIDER USE OF SHORT-TERM ATFCM MEASURES (STAM)
ICAS2016_0059: T. Erlandsson, University of Skövde, Sweden
PLANNING AIR TEAM MISSIONS WITH MULTIPLE OBJECTIVES
ICAS2016_0063: T. Dubot¹, J. Bedouet¹, S. Degrémont, DSNA, France; ¹ONERA, France
MODELLING, GENERATING AND EVALUATING SECTOR CONFIGURATION PLANS - METHODOLOGY REPORT OF THE SESAR VP-755 EXERCISE
ICAS2016_0080: T. Bernatzky¹, S. Baumann¹, U. Klingauf¹; ¹Technische Universitaet Darmstadt, Germany
AN INTERFACE CONCEPT TO SUPPORT THE COCKPIT CREW DURING TRAJECTORY-BASED DISPATCH TOWING
ICAS2016_0147: T. Dautermann¹, T. Ludwig¹, R. Geister¹, T. Blase, MBDA Systems, Germany; ¹DLR Institute of Flight Guidance, Germany
ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A320
ICAS2016_0160: H. Hirabayashi¹, M. Brown¹, S. Nagaoka¹; ¹Electronic Navigation Research Institute, Japan
VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY
ICAS2016_0185: J. Jung¹, S.N. D\'Souza¹, M.A. Johnson¹, A.K. Ishihara², H.C. Modi², B. Nikaido³, H. Hasseeb³; ¹NASA Ames Research Center, United States; ²SGT Inc., United States; ³Science & Technology Corp., United States
APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AIRCRAFT SYSTEMS
ICAS2016_0202: S.R. Conway¹, M.B. Lapis¹, J.D. Musiak¹, M.L. Ulrey¹, C. Hanses, German Aerospace Center, Germany; ¹Boeing, United States
AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR SIMULTANEOUS PARALLEL APPROACH OPERATIONS
ICAS2016_0230: F. Rooseleer¹, V. Treve¹, I. De Visscher, Wake Prediction Technologies (WaPT), Belgium; R. Graham¹; ¹EUROCONTROL, Belgium
WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT
ICAS2016_0287: B. Grüter¹, M. Bittner¹, M. Rieck¹, J. Diepolder¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TU München, Germany
OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH
ICAS2016_0331: A. Andreeva-Mori¹, H. Ishii¹; ¹Japan Aerospace Exploration Agency (JAXA), Japan
IMPACT OF WEATHER UNCERTAINTIES ON NOISE CONTOURS AND NOISE ABATEMENT DESCENT TRAJECTORIES
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
ICAS2016_0402: W.J. Pan¹, X. Wang¹, X.L. Luo, NORTHWEST AIR TRAFFIC CONTROL BUREAU OF CIVIL AVIATION OF CHINA, China; ¹CIVIAL AVIATION FLIGHT UNVIERSITY OF CHINA, China
TAXIING ROUTE PLANNING BASED ON AIRPORT HOTSPOTS
ICAS2016_0463: C. Posse, United States; K. Rein-Weston, United States
AN IN-FLIGHT AID TO NEGOTIATE A MORE EFFICIENT FLIGHT PATH
ICAS2016_0490: A. Kan¹, V. Kanadin¹; ¹GosNIIAS, Russia
INTEGRATED RESEARCH SIMULATION STAND ADVANCED AIR TRAFFIC CONTROL SYSTEMS
ICAS2016_0530: S. Frank¹, P.M. Schachtebeck¹, P. Hecker¹; ¹TU Braunschweig, Institute of Flight Guidance, Germany
SENSOR CONCEPT OF HIGHLY-AUTOMATED AIRPORT TUGS FOR REDUCED EMISSION TAXI OPERATIONS
ICAS2016_0592: T. Marks¹, V. Gollnick¹; ¹German Aerospace Center, Germany
INFLUENCE OF AIRCRAFT TYPE AND ORDER ON FUEL SAVINGS GAINED BY TWO-AIRCRAFT FORMATIONS
ICAS2016_0621: A. Harada, Kochi University of Technology, Japan
AIR TRAFFIC EFFICIENCY EVALUATION BY TRAJECTORY OPTIMIZATION AND ADS-B DATA
ICAS2016_0662: D. Rohacs¹, I. Jankovics¹, J. Rohacs¹; ¹Budapest University of Technology and Economics, Hungary
DEVELOPMENT OF AN ADVANCED ATCO WORKSTATION
ICAS2016_0672: Y. Wu, University of Missouri St. Louis D of Maths and Computer Science, United States; T.A. Lauderdale, NASA Ames Research Center / Aviation Systems Division, United States; H. Chen, Johnson C. Smith University Computer Science & Engineering Dept., United States
A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM
ICAS2016_0674: J.-H. Lewe¹, K. Song¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS
ICAS2016_0682: Y. Higuchi¹, N. Kitazume¹, T. Kozuka¹, K. Tamura¹, Y. Miyazawa¹, M. Brown, Electronic Navigation Research Institute, Japan; ¹Kyushu University, Japan
EFFICIENT CONTROL OF ARRIVAL TIME AT A CONGESTED AIRPORT'S TERMINAL AREA
ICAS2016_0688: K. Song¹, J.-H. Lewe¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States
A REVIEW AND A CLASSIFICATION SCHEME FOR AIR TRANSPORTATION NETWORK RESEARCH
ICAS2016_0691: A. Gardi¹, Y. Lim¹, T. Kistan, THALES Australia, Australia; R. Sabatini¹; ¹RMIT University, Australia
PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORIES IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS
ICAS2016_0719: S. Bagassi¹, F. De Crescenzio¹, F. Lucchi¹, N. Masotti¹; ¹University of Bologna, Italy
AUGMENTED AND VIRTUAL REALITY IN THE AIRPORT CONTROL TOWER

9 - Safety and Security

ICAS2016_0010: M. Tanaka, Nagoya Univ, Japan; T. Okubo, iisec, Japan; S. Yamada¹, G. Idei¹, M. Takase¹, R. Hosomi¹; ¹Kyoto Institute of Technology, Japan
THE DRONE AVIATION NAVIGATION SYSTEMS
ICAS2016_0030: Z. Wang, NEIAS-AVIC, China
DISPATCH RELIABILITY ORIENTED MMEL FORMULATION TECHNOLOGY RESEARCH
ICAS2016_0082: C.A. Niermann, German Aerospace Center (DLR), Institute of Flight Guidance, Germany
CAN 3D-AUDIO IMPROVE STATE-OF-THE-ART PILOT-ASSISTANCE SYSTEMS?
ICAS2016_0115: L. Wang¹, Y. Li¹; ¹Civil Aviation University of China, China
STUDY ON THE SAFETY RISK AND CAPACITY OF THE ONE-WAY CIRCULATION AIR ROUTE IN CHINA
ICAS2016_0176: J. Alfredson, Saab/LiU, Sweden; P. Hagström, Saab, Sweden
DETECT AND AVOID FOR REMOTELY PILOTED AIRCRAFT IN AIR TRAFFIC CONTROL SIMULATIONS
ICAS2016_0181: J. Chen¹, J. Zhang¹, J. Li, Siemens Industry Software (Beijing), Germany; ¹Beihang University, China
RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING
ICAS2016_0190: B.J. Yang¹, P. Dutta¹, I. Hwang, Purdue University, United States; ¹Optimal Synthesis Inc., United States
FORMAL VERIFICATION OF AUTOPILOTS IN UMANNED AIRCRAFT SYSTEMS
ICAS2016_0205: T. Hu¹, L. Jin¹; ¹China Aero-Polytechnology Establishment, AVIC, China
RESEARCH ON AIRWORTHINESS REQUIREMENTS OF SUPERCOOLED LARGE DROP ICING PROTECTION FOR AIRCRAFT (§25.1420)
ICAS2016_0221: Q. Hu¹, Y.H. Chang, Oregon Health and Science University, United States; C.J. Tomlin¹; ¹University of California Berkeley, United States
SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES AGAINST ADVERSARIAL ATTACKS
ICAS2016_0295: J. Lee¹, E. Hyeon¹, M. Kim¹, J. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea
VERTICAL POSITION ERROR BOUNDING FOR INTEGRATED GPS/BAROMETER SENSORS TO SUPPORT UNMANNED AERIAL VEHICLE (UAV)
ICAS2016_0322: E. Norde¹, E.T.A. van der Weide¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands
EULERIAN METHOD FOR IN-ENGINE ICING: WITH APPLICATION TO ICE CRYSTAL TRAJECTORIES AND IMPACT IN A GENERIC TURBOFAN COMPRESSOR
ICAS2016_0338: J.O. Entzinger¹, T. Uemura¹, T. Iijima², N. Matayoshi², S. Suzuki¹; ¹The University of Tokyo, Japan; ²JAXA (Japan Aerospace Exploration Agency), Japan
OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS
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
ICAS2016_0435: Y. Tian¹, C. Lu¹, Z.-L. Wang¹; ¹School of Reliability and Systems Engineering,Beihang University, China
AIRCRAFT SECURITY ENHANCEMENT: ROTATING MACHINERY FAULT DIAGNOSIS AND HEALTH ASSESSMENT USING MANIFOLD LEARNING AND DYNAMIC TIME WARPING
ICAS2016_0465: L. Peters¹, C. Bil¹; ¹RMIT University, Australia
THE DESIGN OF AN AUTOMATIC BEACON EJECTING SYSTEM FOR AIRCRAFT
ICAS2016_0466: C. Bil, RMIT University, Australia; G. Hanlon, Five Rings Aerospace, Australia
INFLUENCE OF ETHNICITY ON PASSENGER STANDARD WEIGHT
ICAS2016_0513: C. Wang¹, L. Drees¹, F. Holzapfel¹; ¹Technische Universität München, Germany
FUEL STARVATION CAUSED BY HUB CLOSURE
ICAS2016_0655: M. Kowalski¹, A. Jankowski¹, J. Rajchel, Polish Air Force Academy, Poland; ¹Air Force Institute of Technology, Poland
RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY
ICAS2016_0661: J. Rajchel, Polish Air Force Academy, Poland; J. Zurek¹, R. Kaleta¹; ¹Air Force Institute of Technology, Poland
EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY

10 - Challenge of the Environment

ICAS2016_0097: P. Glowacki¹, M. Kawalec¹; ¹Institute of Aviation, Poland
QUANTITATIVE EMISSIONS OF NOX, CO AND CO2 DURING AIRCRAFT OPERATIONS
ICAS2016_0211: A. Spiteri¹, K. Chircop¹, D. Zammit-Mangion¹, A. Muscat², K. Falzon², J. Degiorgio³, F. Bezzina³; ¹University of Malta, Malta; ²Quaero Ltd., Malta; ³Malta Air Traffic Services Ltd., Malta
CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY OPTIMISATION
ICAS2016_0357: O. Oguntona, Munich Aerospace e.V., Germany; A. Cui, Technische Universität München, Germany; K. Ploetner¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
FLEET DEVELOPMENT PLANNING OF AIRLINES: INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR
ICAS2016_0454: K. Hein¹, S. Baumann¹; ¹TU Darmstadt, Germany
ACOUSTICAL COMPARISON OF CONVENTIONAL TAXIING AND DISPATCH TOWING - TAXIBOT´S CONTRIBUTION TO GROUND NOISE ABATEMENT
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_0031: S.-Y. Lee, Korean Air, South Korea
LCC ESTIMATION AND CASE STUDY USING RELIABILITY AND MAINTAINABILITY ANALYSIS
ICAS2016_0039: H. Xiao, China; M. Zhao, China; M. Yao, China; J. Liu, China; H. Chen, China; M. Li, China; M. Du, China
3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION
ICAS2016_0088: A. Andreeva-Mori¹, K. Kobayashi¹, M. Shindo¹, Y. Okuno¹; ¹Japan Aerospace Exploration Agency, Japan
DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF
ICAS2016_0192: A.M. Gareyev¹, Y.P. Zlobina¹, I.A. Popelniuk¹; ¹Samara State Aerospace University, Russia
IMPROVING THE EFFICIENCY AND RELIABILITY ASSESSMENT TECHNICAL STATE LIQUID SYSTEMS AIRCRAFT DURING ACCEPTANCE TESTS
ICAS2016_0218: M. Schmidt, Munich Aerospace e.V., Germany; M. Engelmann¹, R. Rothfeld¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany
BOARDING PROCESS ASSESSMENT OF NOVEL AIRCRAFT CABIN CONCEPTS
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
ICAS2016_0404: E. Neu¹, F. Janser¹, A.A. Khatibi², A.C. Orifici²; ¹FH Aachen UAS, Germany; ²RMIT University, Australia
IN-FLIGHT VIBRATION-BASED STRUCTURAL HEALTH MONITORING OF AIRCRAFT WINGS
ICAS2016_0452: E. Fouladi¹, F. Farkhondeh¹, N. Khalili¹, A. Abedian¹; ¹Sharif University of Technology, Iran
AIRLINES MAINTENANCE COST ANALYSIS USING SYSTEM DYNAMICS MODELING
ICAS2016_0514: S. Cresto Aleina¹, R. Fusaro¹, N. Viola¹; ¹Politecnico di Torino, Italy
INVESTIGATIONS OF GROUND INFRASTRUCTURES FOR UAS FLIGHT MONITORING
ICAS2016_0555: J. van der Vorst¹, P.J.A. Booij¹, J.F. Hakkaart¹, T.I. Lee, KAI, South Korea; ¹NLR, Netherlands
QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH
ICAS2016_0726: M. Liao¹, M. Yanishevsky¹, P. Patnaik¹; ¹Aerospace, National Research Council Canada, Canada
RESEARCH ADVANCES ON AIRCRAFT STRUCTURAL INTEGRITY AND SUSTAINMENT AT NRC
ICAS2016_0733: K.E. Cramer, NASA, United States
RESEARCH DEVELOPMENTS IN NONDESTRUCTIVE EVALUATION AND STRUCTURAL HEALTH MONITORING FOR THE SUSTAINMENT OF COMPOSITE AEROSPACE STRUCTURES AT NASA
ICAS2016_0734: D. Holmes¹, A. Goodwin¹, R. Vodicka¹; ¹DSTG, Australia
TRANSFORMING MILITARY AEROSPACE SUSTAINMENT

12 - Host nation

ICAS2016_0035: D.-M. Ahn, Hanseo University, South Korea; W.-H. Kang, Yanbian University, China; S.-Y. Lee, KM Engineering, Former Head of Aircraft Sys. Int. Div. ADD, South Korea
HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY
ICAS2016_0069: A.R. Gorbushin, Central Aerohydrodynamic Institute, Russia
THE ORIGIN OF WIND TUNNELS IN RUSSIA
ICAS2016_0301: J.B. Yim, Agency for Defense Development, South Korea
FROM 500MD TO LAH - CHALLENGE TOWARD VERTICAL LIFT IN KOREA
ICAS2016_0526: C.H. Lim¹, W.G. Kang¹, J.W. Kim¹; ¹KARI, South Korea
DEVELOPMENT OF SMART TILT-ROTOR UAS AND THE BEGINNINGS OF KOREAN CIVILIAN DRONES

14 - Guest lecture

ICAS2016_0735: I. Potter, National Research Council Canada, Canada
RTO\'S AND TECHNOLOGY DE-RISKING
ICAS2016_0736: R. Singh, Emeritus Cranfield University, United Kingdom
THE FUTURE JOURNEY OF CIVIL AEROSPACE: WEATHER, ENVIRONMENT AND CLIMATE
ICAS2016_0738: F. Collier, United States
ENVIRONMENTALLY RESPONSIBLE AVIATION PROJECT OVERVIEW
ICAS2016_0739: A. Velicki, United States
STITCHED, RESIN-INFUSED, HWB AIRCRAFT STRUCTURAL DEVELOPMENTS
ICAS2016_0740: A. Epstein, United States
FUEL-FLEXIBLE, COMBUSTOR AND FAN DEVELOPMENTS FOR UHB ENGINES
ICAS2016_0741: J.T. Bonet, United States
UHB ENGINE INTEGRATION FOR HYBRID WING BODY AIRCRAFT
ICAS2016_0742: D.N. Mavris¹, K.G. Schwartz¹, J. Tai¹; ¹Georgia Institute of Technology, United States
TECHNOLOGY INTEGRATION AND SYSTEM ASSESSMENTS WITH UNCERTAINTY MODELLING
ICAS2016_0745: A. Epstein, Pratt & Whitney, United States
THE FUTURE OF SUSTAINABLE COMMERCIAL PROPULSION