RESERVE ABSTRACTS

ICAS 2004-1.1.R: ADVANCED COMBAT AIRCRAFT DESIGN FOR LOW SUPPORT COST, V. Serghides
ICAS 2004-2.1.R.1: FIELD-PANEL METHOD FOR TRANSONIC AEROELASTICITY, P. C. Chen, X. W. Gao, L. Tang
ICAS 2004-2.1.R.2: A FAST VISCOUS CORRECTION METHOD APPLIED TO SMALL DISTURBANCE POTENTIAL TRANSONIC FLOWS IN THE FREQUENCY DOMAIN, P. C. Greco Jnr, L. Y. Sheng
ICAS 2004-2.1.R.3: THE USE OF UNSTEADY CFD DATA ON AEROELASTIC ANALYSIS FOR GENERIC LARGE TRANSPORT AIRCRAFT, L. Djayapertapa
ICAS 2004-3.1.R.1: ROLL DAMPING MEASUREMENTS OF A FREE SPINNING BOMB, F. Dionisio, I. Johnson
ICAS 2004-3.1.R.2: KAWASAKI WAKE SURVEY SYSTEM, H. Ogoshi, Y. Yamaguchi, S. Suzuki
ICAS 2004-4.1.R.1: VORTEX INTERACTION AND BREAKDOWN OF A DOUBLE-DELTA WING AT SIDESLIP, M. H. Sohn
ICAS 2004-4.1.R.2: CONTROL OF THE VORTEX BREAKDOWN ON A DELTA WING BY BLOWING, S. Okada, S. Seiya, K. Hiraoka
ICAS 2004-5.1.R.1: ROTOR BLADE AIR LOADS EVALUATIONBASED ON STRUCTURAL DEFORMATION, T. Gausz, D. Szilagyi
ICAS 2004-5.1.R.2: WEIGHT ESTIMATION OF COMPOSITE SECONDARY STRUCTURE, Y- C. Cheng
ICAS 2004-6.1.R.1: DESIGN PROCEDURE AND EXPERIMENTAL EVALUATION OF PRESSURE-SWIRL ATOMIZERS, P. T. Lacava, A. P. Pimenta, D. Bastos-Netto
ICAS 2004-6.1 (St.).R.2: VORTEX DYNAMICS IN STARTING SQUARE WATER JETS, A. W-K. Law, S. Yu, J. ai
ICAS 2004-7.1.R: THE RESEARCH ON IR IMAGING TERMINAL-GUIDING TECHNOLOGY FOR AN AIR-TO-AIR MISSILE IN CLUTTER BACKGROUND, Z. LI ZHAOHUI, C. Chen
ICAS 2004-8.1.R: PRELIMINARY VALIDATION OF THE SMALL AIRCRAFT TRANSPORTATION SYSTEM HIGHER VOLUME OPERATIONS (SATS HVO) CONCEPT, D. Williams, M. Consiglio, J. Murdoch, C. Adams
ICAS 2004-1.2.R: A VISION FOR THE FUTURE EVOLUTION OF AIRCRAFT, S. Tsach, D. Penn, D. Budianu
ICAS 2004-2.2.R.1: A VISCOUS-INVISCID INTERACTION FOR AERODYNAMIC AND AEROELASTIC CALCULATION, W. K. Sekar, C. Weishäupl, B. Laschka
ICAS 2004-2.2.R.2: NUMERICAL PREDICTION FOR AIRFOIL STALL, L. Dong, I. Men'shov, Y. Nakamura
ICAS 2004-4.2.R.1: THE AERODYNAMIC PERFORMANCE OF THE CASCADE WITHIN A THRUST REVERSER, H. Hui Yao, J. Butterfield, S. Raghunathan, R. Cooper, E. Benard
ICAS 2004-4.2.R.2: PERFORMANCE OF A FLAPPED DUCT EXHAUSTING INTO A COMPRESSIBLE EXTERNAL FLOW, J. K. Watterson, P. R. Pratt, E. Benard, S. Hall
ICAS 2004-5.2 (St.).R: MULTI OBJECTIVE DESIGN STUDY OF A FLAPPING WING GENERATOR, E. Shimizu
ICAS 2004-7.2.R: NONLINEAR MODEL MATCHING FLIGHT CONTROL SYSTEM FOR LIFT/CRUISE FAN AIRCRAFT, Y. Osa, S. Take, S. Uchikado*, K. Tanaka**
ICAS 2004-2.3.R: CFD VALIDATION STUDY OF NEXST-1 NEAR MACH 1, K. Takenaka, K. Kazuomi Yamamoto, R. Ryoji Takaki
ICAS 2004-3.3.R: THE INFLUENCE OF STREAMWISE MODULATION ON THE EVOLUTION OF THREE-DIMENSIONAL WAVETRAINS IN BOUNDARY LAYERS, M. Medeiros
ICAS 2004-5.3.R.1: RESIDUAL STRENGTH PREDICTION OF IMPACT DAMAGED, J. Yap, R. Rodney S., D. Hachenberg
ICAS 2004-6.3.R: AERODYNAMIC ANALYSIS OF PROPELLER-WING INTERACTION FOR THE DEVELOPMENT OF A CUSTER CHANNEL WING, C. Han, W. Mason, J. Cho
ICAS 2004-1.4.R.1: THE AIRBUS / ENGINE & NACELLE MANUFACTURERS RELATIONSHIP: TOWARDS A MORE INTEGRATED, ENVIRONMENTALLY FRIENDLY ENGINEERING DESIGN, S. Remy
ICAS 2004-1.4.R.2: MULTI-DISCIPLINARY AIRCRAFT DESIGN OPTIMIZATION USING PARALLEL COMPUTER ARCHITECTURES, C. Peebles, C. Bil
ICAS 2004-2.4.R.1: STUDY OF VARIOUS NUMERICAL TECHNIQUES FOR THE COMPUTATION OF DIFFUSIVE TERMS IN TWO-DIMENSIONAL NAVIER-STOKES EQUATIONS, J-M. Vaassen, J.
ICAS 2004-2.4.R.2: A GENERAL METHOD FOR STRUCTURED GRID GENERATION USING, F. Sabetghadam, K. Hejranfar
ICAS 2004-2.4 (St.).R.3: MIXED ELEMENT TYPE UNSTRUCTURED GRID GENERATION AND ITS APPLICATION TO VISCOUS FLOW SIMULATION, G. Wang, Z- Y. Ye
ICAS 2004-2.4.R.4: DEVELOPMENT OF A SIMPLE AND FAST COMPUTATIONAL ROUTINE TO SOLVE THE FULL POTENTIAL EQUATION OF THE TRANSONIC AXI-SYMMETRIC FLOW, H. Djojodihardjo, A. F. Widodo
ICAS 2004-3.4.R (St.).1: INVESTIGATION OF ROTOR NOISE PREDICTION USING DIFFERENT AEROACOUSTIC METHODS IN TIME DOMAIN, Z. Han, W. Song, Z. Qiao
ICAS 2004-3.4.R.2: WALL MEASUREMENTS IN A CAVITY FLOW, P. Spazzini, R. Malvano, G. Iuso
ICAS 2004-4.4.R.1: AERODYNAMIC LOW SPEED BUFFET BOUNDARY CHARACTERISTICS OF A HIGH SPEED BUSINESS JET, A. P. Brown
ICAS 2004-5.4.R.1: VIRTUAL TESTING OF AIRCRAFT FUSELAGE STIFFENED PANELS, P. Linde, J. Pleitner, W. Rust
ICAS 2004-5.4.R.2: OPERATIONAL LOAD REGRESSION EQUATION DEVELOPMENT FOR ADVANCED FIGHTER AIRCRAFT, H. Kaneko, T. Furukawa
ICAS 2004-6.4.R: PARAMETRIC STUDY OF LIQUID ROCKET ENGINE SYSTEM USING LIQUEFIED NATURAL GAS/LIQUID OXYGEN AS PROPELLANTS, L. Sung-Woong, L. Sung-Woong, C. Yong-Ho
ICAS 2004-8.4.R.2 (I.L.): CONFLICT DETECTION AND ALERTING IN NON-TOWERED NON-RADAR TERMINAL AIRSPACE, M. Consiglio, V. Carreno, C. Munos
ICAS 2004-3.5 (St.).R: TURBULENT FORCED CONVECTIVE HEAT TRANSFER, J. Murray, E., S.
ICAS 2004-5.5 (St.).R.1: THE BEHAVIOR OF RUBBER DURING PRESSURE FORMING OF THERMOPLASTIC COMPOSITES, V. Antonelli, B. Weteringe, H. Bersee
ICAS 2004-5.5.R.2: TOUGHNESS IMPROVEMENT OF GLASS/EPOXY FILAMENT WOUND TUBES BY RUBBER MODIFICATION, R. Bagheri, H. Haddadpour, M. Abadian
ICAS 2004-7.5.R.1: SPECIFIC FEATURES OF HIGH PRESSURE WATER SEPARATION IN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEMS, Y. M. Shustrov
ICAS 2004-7.5.R.2: DEVELOPMENT OF ICE ACCRETION AND ANTI-ICING SYSTEM SIMULATION CODE, S. Nishio, S. Kato
ICAS 2004-1.6.R.1: TAIL-SITTER VTOL-UAV ~ FULL-SCALE HOVER PROTOTYPE SYSTEM, H. Hirose, K. Kamo, T. Udagawa
ICAS 2004-1.6.R.2: DEVELOPMENT APPROACH TO THE PW_103 - AN INCREASED RELIABILITY MALE UAV - UNDER THE CAPECON PROJECT WITHIN THE V FR OF EU, Z. Goraj, A. Frydrychewicz
ICAS 2004-2.6.R.1: NUMERICAL SIMULATION OF SUPERSONIC INTAKE PERFORMANCE FOR NEXST2 USING STRUCTURED-UNSTRUCTURED ZONAL APPROACH, M. Kanazaki, H. Fujiwara, Y. Ito, T. Fujita, S. Obayashi, K. Nakahashi
ICAS 2004-2.6.R.2: NUMERICAL SIMULATION OF FLOW FIELD IN AN ANNULAR TURBINE STATOR WITH FILM COOLING, J. Zeng, B. Wang, Y. Kang*
ICAS 2004-3.6.R: EFFECT OF STATIONARY VORTEX TO HEAT TRANSFER ON DELTA WING, S. Srigrarom, N. Lewpiriyawong
ICAS 2004-4.6 (St.).R: AUDIOVISUAL FLIGHT ADVISORY SYSTEM, L. Hatfaludy
ICAS 2004-5.6.R.1: RESIDUAL STRENGTH ANALYSIS OF STIFFENED PANELS USING R-CURVES, B. G. Nesterenko
ICAS 2004-5.6 (St.).R.2: AIRCRAFT EQUIVALENT VULNERABLE AREA CALCULATION METHODS, Y. Pei, B. Song, Y. Qin
ICAS 2004-6.6.R: NUMERICAL SIMULATION OF THE SPREAD OF ROCKET PLUME, S. Enomoto, R. Yanagi
ICAS 2004-7.6.R.1: ICAS_ENG_MZ, M. Zboinski
ICAS 2004-7.6.R.2: SOME CONCEPTS ON THE SEPARABLE LANDING SYSTEM OF AIRPLANE, B. Liu, J. Zhou
ICAS 2004-8.6.R: APPLICATION OF MILITARY AND AEROSPACE RAMS STANDARDS IN LARGE INFRA-STRUCTURE PROJECTS – RAILWAY CASE STUDY, A. Saleem, S. Barhey
ICAS 2004-2.7.R.1: NUMERICAL STUDY OF SHOCK GENERATION AT THE AFTER-BODY OF SLENDER BODY OF REVOLUTION USING NAVIER-STOKES EQUATION, E. Prijono, L. R. Zuhal, H. Djojodihardjo
ICAS 2004-2.7 (St.).R.2: NUMERICAL STUDY OF HIGH L/D OBLIQUE FLYING WING, T. Hamaki
ICAS 2004-3.7.R.1: NUMERICAL PREDICTION OF STAGNATION-POINT SHOCK-DETACHMENT DISTANCE FOR HYPERSONIC LOW DENSITY FLOW OVER BLUNT NOSE SHAPES, W. F. N. Santos
ICAS 2004-3.7.R.2: ESTIMATION OF SKIN SURFACE TEMPERATURE OF SPACE VEHICLES DURING WHOLE FLIGHT ENVELOPE, S. R. Chaudhry, N. U. Saqib, F. Umar
ICAS 2004-5.7.R: AEROELASTIC MODELING OF VERTICAL TAIL BUFFET, O. Levinski
ICAS 2004-7.7.R.1: THE DEVELOPMENT OF THE SYNAMEC A DESIGN TOOL FOR AERONAUTICAL MECHANISMS, APPLIED TO LEADING EDGE DEVICES, J. P. Fielding, V. Lajux
ICAS 2004-7.7.R.2: DESIGN FOR CUSTOMER - AIRCRAFT, A. K. Kundu, R. Curran
ICAS 2004-8.7.R.1: DEFINITION OF AN OPTIMAL DAMPER FOR HELICOPTER CRASHWORTHY, R. Denni, L. de Filippis
ICAS 2004-1.8.R: FUTURE INTER-THEATRE MULTI-ROLE AIRCRAFT CONCEPT, D. Bray, P. Tolhurst
ICAS 2004-3.8 (St.).R: STRUCTURE OF UNDER EXPANDED JET FROM RECTANGULAR NOZZLE, S. Tsutsumi
ICAS 2004-8.8.R: EQUIVALENT CORROSION FACTORS FOR ASSESSING CALENDAR LIFE OF AIRCRAFT STRUCTURES, B. Wang, Q.
ICAS 2004-1.9.R: SYSTEM METHODOLOGY FOR PRE-MISSION ANALYSIS OF HELICOPTER EMERGENCY MEDICAL OPERATIONS, A. K. Sinha, R. Kusumo, P. Hogan, K. Laycock, S. Atyeo
ICAS 2004-2.9.R.1: AN UNSTEADY AND TIME-AVERAGED STUDY OF A GROUND VORTEX FLOW, N. J. Lawson, J. M. Eyles, K. Knowles
ICAS 2004-2.9.R.2: BLEED PERTURBATION TO FORE-BODY ASYMMETRIC VORTICES, X. Deng, X. Chen, Y. Wang
ICAS 2004-3.9.R: DRAG REDUCTION AND VORTEX STRUCTURE MODIFICATION IN THE WAKE OF A CIRCULAR CYLINDER BY ELECTROHYDRODYNAMIC FORCES, F. Martini Catalano, J.
ICAS 2004-5.9.R.1: PROCESSING AND PROPERTIES OF NEW HIGH TEMPERATURE COMPOSITES USING SUPERIOR POLYIMIDE "TRI-A PI", T. Toshio Ogasawara, R. Rikio Yokota, J. Jun Gotoh
ICAS 2004-5.9 (St).R.2: INFLUENCE OF THE DIAMETER OF TYRANNO ZMI FIBER, K. Yamamoto, T. Morimoto, S. Ogihara
ICAS 2004-5.9.R.3: DEVELOPMENT OF SAFE AND ENVIRONMENT FRIENDLY SEAT CUSHION FOR AIRPLANE INTERIOR, S. Watanabe, S. Fujita
ICAS 2004-6.9.R: THE CONTRIBUTION OF THE AIR TRANSPORT SECTOR ON THE ATMOSPHERIC POLLUTION OF GREATER ATHENS AREA, J. Kaldellis, A. Paliatsos, E. Chelmi
ICAS 2004-8.9.R: THERMAL CONDUCTIVITY MEASUREMENT OF THERMAL INSULATION UNDER HIGH TEMPERATURE, T. Ohmura, M. Tsuboi, T. Tomimura
ICAS 2004-2.10.R.1(St.): EXPERIMENTAL ANALYSIS OF THE CONFLUENT BOUNDARY LAYER BETWEEN A FLAP AND A MAIN ELEMENT WITH SAW-TOOTHED TRAILING EDGE, R. C. Lemes, F. M. Catalano
ICAS 2004-2.10.R.2: THE INTAKE-DUCT FLOW CORRECTION BY CFD FOR JET-POWERED SUPERSONIC EXPERIMENTAL AIRPLANE WIND TUNNEL TEST DATA, A. Sannou, Y. Makino, H. Hujiwara
ICAS 2004-4.10.R: SIX COMPONENTS OF AERODYNAMIC FORCES AND MOMENTS OF FREE FLIGHT AIRPLANE MODEL IN WIND TUNNEL MEASURED BY SINGLE VIDEO CAMERA, H. Iwata, Y. Nagao, H. Kawazoe
ICAS 2004-5.10.R.1: TRANSONIC AND SUPERSONIC AEROELASTIC COMPUTATION CONSIDERING, K. Dong-Hyun, K. Kyo-Nam, K. Jin-Hae
ICAS 2004-5.10.R.2: EMBRAER170 WING BIRD STRIKE TEST, I. Isoe, T.. Okamoto, T. Taki
ICAS 2004-6.10.5.R.1: PIEZOELECTRIC ACTUATED FLAPS FOR ACTIVE ROTOR CONTROL, P. Janker, V. Kloeppel
ICAS 2004-6.10.5.R.2: INTERIOR NOISE PREDECTION FOR GENERIC CFRP AND METAL FUSELAGES, A. Peiffer, S. Brühl, S. Tewes
ICAS 2004-6.10.5.R.3: INTEGRATED ACTIVE SYSTEMS FOR AIRCRAFT INTERIOR NOISE CONTROL, R. Maier, B. Petitjean
ICAS 2004-1.11.R.1: CONCEPTUAL FEASIBILITY OF FLIGHT DEMONSTRATOR, K. Mizobata, H. Kimura, H. Sugiyama
ICAS 2004-2.11.R: GRID PATTERN EFFECTS ON AERODYNAMIC CHARACTERISTICS OF GRID FINS, F. Hiroshima, K. Tatsumi
ICAS 2004-6.11.R.1: PARALLEL CHIMERA COMPUTATIONS OF HELICOPTER FLOWS, G. Jeanfaivre, X. Juvigny, C. Benoit
ICAS 2004-6.11.R.2: NUMERICAL INVESTIGATION OF BVI, X. K. Zioutis, A. I. Spyropoulos, D. P. Margaris, D. G. Papanikas
ICAS 2004-7.11.R: FLIGHT DEMONSTRATION OF A NEW OPERATIONAL CONCEPT USING TDMA DATA LINK SYSTEM, T. Nojima, K. Funabiki, T. Iijima
ICAS 2004-8.11.R.1: AEROSERVOELASTIC STABILITY OF GUIDED MISSILES, H. Haddadpour
ICAS 2004-8.11.R.2: AIRCRAFT CONTROL USING THE ENGINES, R. Lungu, A. N. Tudosie