| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-1.1.1 | A PROBABILISTIC METHODOLOGY FOR THE TREATMENT OF SYSTEM-OF-SYSTEMS PROBLEMS AND APPLICATION TO FUTURE AIR TRANSPORTATION ARCHITECTURES | DeLaurentis D, Pfaender H, Mavris D, Schrage D, Georgia Institute of Technology, Atlanta, GA, 30332-0150 |
1.1 Multidisciplinary Design Optimization I |  |
| ICAS 2002-1.1.2 | EVALUATION AND IMPLEMENTATION OF MULTIDISCIPLINARY DESIGN OPTIMIZATION (MDO) STRATEGIES | G. RENAUD, G. SHI, IAR/NRC, CA | 1.1 Multidisciplinary Design Optimization I | |
| ICAS 2002-1.1.3 | EVALUATION OF THREE DECOMPOSITION MDO ALGORITHMS | S. Chen, F. Zhang, M. Khalid, Institute for Aerospace Research, National Research Council Canada |
1.1 Multidisciplinary Design Optimization I | |
| ICAS 2002-1.1.4 | CONCEPTUAL AIRCRAFT DESIGN – A GENETIC SEARCH AND OPTIMIZATION APPROACH | Nicholas Ali *, Kamran Behdinan ** Department of Mechanical, Aerospace and Industrial Engineering Ryerson Polytechnic University 350 Victoria St., Toronto ON, M5B 2K3 |
1.1 Multidisciplinary Design Optimization I | |
| ICAS 2002-8.1.1 | THE INVESTIGATION OF MULTI-DISCIPLINARY AND MULTI-OBJECTIVE OPTIMIZATION METHOD FOR THE AIRCRAFT CONFIGURATION DESIGN | Xia Lu, Gao Zhenghong, Department of Aircraft Engineering, Northwestern Polytechnical University, P.R.China |
8.1 Student session I | |
| ICAS 2002-1.2.1 | PRELIMINARY DESIGN PHASE 928JET - KEEPING THE 728JET FAMILY COMMONALITY | J. HENKNER, Fairchild Dornier GmbH, DE | 1.2 Aircraft Design | |
| ICAS 2002-1.2.2 | DEVELOPMENT AND INTEGRATION OF A NEW HIGH PERFORMANCE WINGTIP DEVICE FOR TRANSONIC AIRCRAFT | G. Heller, P. Kreuzer, S. Dirmeier Fairchild Dornier GmbH, 82230 Wessling, Germany |
1.2 Aircraft Design | |
| ICAS 2002-1.2.3 | WING SHAPE OPTIMIZATION USING A CONSTRAINED NURBS SURFACE GEOMETRICAL REPRESENTATION | Anas Bentamy , Jean-Yves Trépanier , François Guibault Centre de Recherche en Calcul Appliqué (CERCA) |
1.2 Aircraft Design | |
| ICAS 2002-1.3.1 | ADVANCED TECHNOLOGIES & APPROACHES FOR NEXT GENERATION UAVS | S. Tsach, D. Penn and A. Levy (IAI Ltd.) |
1.3 Unmanned Air Vehicles | |
| ICAS 2002-1.3.2 | A SYSTEM FRAMEWORK TO AUTOMATE DESIGN DECISION SUPPORT OF RE-CONFIGURABLE UAVS | Sinha, A.K., Kusumo, R. Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Technology GPO Box 2476V, Melbourne, Victoria, 3001, Australia. |
1.3 Unmanned Air Vehicles | |
| ICAS 2002-1.3.3 | HELIPLAT®: STRUCTURAL ANALYSIS OF HIGH ALTITUDE VERY-LONG ENDURANCE SOLAR POWERED PLATFORM FOR TELECOMMUNICATION AND EARTH OBSERVATION APPLICATIONS | G. ROMEO, GIACOMO FRULLA (G.F.) Politecnico di Torino (Turin Polytechnic University), C. Duca degli Abruzzi 24, 10129 Turin, Italy |
1.3 Unmanned Air Vehicles | |
| ICAS 2002-1.3.4 | DESIGNING AND DEVELOPMENT OF UNMANNED AERIAL VEHICLE | FLT . LT ASIM Engineering Wing PAF Base Minhas, PAKISTAN DR A A KHAN National University of Science and Technology College of Aeronautical Engg Risalpur,24090, PAKISTAN |
1.3 Unmanned Air Vehicles | |
| ICAS 2002-1.4.1 | A NEW EFFECTIVE MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM | Li Weiji, Hu Yu Department of Aircraft Engineering, Northwestern Polytechnical University, Xi’an, 710072, P. R. China |
1.4 Multidisciplinary Design Optimization II | |
| ICAS 2002-1.4.2 | MULTIDISCIPLINARY OPTIMIZATION OF AIRCRAFT PARAMETERS BY THE LOCAL DISTRIBUTED CRITERIA METHOD | A.S. Filatyev, A.A. Golikov, A.P. Kosykh, G.G. Nersesov, A.N. Shanygin,
V.S. Voityshen, V.L. Yumashev, Central Aerohydrodynamic Institute (TsAGI) Zhukovsky, 140180 Moscow Region, RUSSIA |
1.4 Multidisciplinary Design Optimization II | |
| ICAS 2002-1.4.3 | WITH PUBLIC DOMAIN SOFTWARE TO INTEGRATED DESIGN AND ANALYSIS TOOLS | M.C.Haupt, W.Heinze, P.Horst Institut of Aircraft Design and Lightweight Structures, TU Braunschweig, Hermann-Blenk-Str. 35, 38108 Braunschweig |
1.4 Multidisciplinary Design Optimization II | |
| ICAS 2002-1.4.4 | CONCEPTUAL DESIGN OPTIMISATION OF A "MALE" CONFIGURATION USING A FLEXIBLE SCALING TOOL | Schieck, F., Technische Universität München Deligiannidis, N., Gottmann, T., and van Toor, J., EADS Military Aircraft |
1.4 Multidisciplinary Design Optimization II | |
| ICAS 2002-1.4.5 | A CONFIGURABLE FRAMEWORK FOR MULTIDISCIPLINARY ANALYSIS INTEGRATION AND MANAGEMENT | Jean-Yves Trépanier , François Guibault , Benoît Ozell , Djamel Bouhemhem Centre de Recherche en Calcul Appliqué (CERCA |
1.4 Multidisciplinary Design Optimization II | |
| ICAS 2002-1.5.1 | DOES THE AIR TRANSPORT MARKET NEED "UNCONVENTIONAL AIRCRAFT CONFIGURATIONS"? | Schmitt, D. and Strohmayer, A., Aeronautical Engineering, Technische Universität München |
1.5 Unconventional Aircraft | |
| ICAS 2002-1.5.2 | THE DOLPHIN: A NEW 100-SEAT AIRCRAFT IN LIFTING-FUSELAGE LAYOUT | Kalyguina G.V., Bogdanov S.I., Dzhamgarov S.G., Karklin A.M, Lysenkov
A.V. IRKUT-AviaSTEP, Moscow, Russia Birjuk V.I., Bolsunovsky A.L., Buzoverya N.P. Central Aerohydrodynamic Institute (TsAGI), Zhukovsky, Russia |
1.5 Unconventional Aircraft | |
| ICAS 2002-1.5.3 | FLYING WING CONCEPT FOR MEDIUM SIZE AIRPLANE | Tjoetjoek Eko Pambagjo , Kazuhiro Nakahashi , Kisa Matsushima Department of Aeronautics and Space Engineering, Tohoku University, Japan |
1.5 Unconventional Aircraft | |
| ICAS 2002-1.6.1 (I.L.) | SUPERSONIC EXPERIMENTAL AIRPLANE PROGRAM AND RELATED ACTIVITIES IN JAPAN | K. SAKATA, NAL, JA | 1.6 Supersonic and Military Aircraft | |
| ICAS 2002-1.6.2 | ASSESSMENT OF THE FEASIBILITY OF INNOVATIVE REUSABLE LAUNCHERS | M. POGOSYANN, SUKHOI, RU | 1.6 Supersonic and Military Aircraft | |
| ICAS 2002-1.6.3 | SUPERSONIC BUSINESS JET AIRCRAFT DESIGN | Dr Derek Bray, Dr Nick Lawson & Simon Harding Cranfield University, Dept. Of Aerospace Power and Sensors, RMCS, Shrivenham, Swindon, SN6 8LA, United Kingdom |
1.6 Supersonic and Military Aircraft | |
| ICAS 2002-1.6.4 | GRIPEN FUTURE DEVELOPMENT | Sjunnesson G - Saab Aerospace, Gripen S 581 88 Linkoping, Sweden |
1.6 Supersonic and Military Aircraft | |
| ICAS 2002-5.8.1(IL) | COMBUSTION TECHNOLOGY CHALLENGES FOR SMALL AVIATION GAS TURBINES | P. Sampath, T.C.J. Hu, H. Ozem Pratt & Whitney Canada Corp., 1801 Courtney Park Drive, Mississauga, Ontario, L5T 1J3 Canada |
5.8 Combustion | |
| ICAS 2002-8.8.1 (St) | THE CASE FOR A PRACTICAL SMALL SUPERSONIC TRANSPORT | Carmen Carreras, Mirna Daouk, Troy Downen, Laurent Jamonet, Stephane Lederle,
David Sharman, Russ Wertenberg, Massachusetts Institute of Technology |
8.8 Student session IV | |
| ICAS 2002-R16 | DEVELOPMENT OF ENVIRONMENTALLY-FRIENDLY TECHNOLOGIES AND CONFIGURATIONS FOR SUBSONIC JET TRANSPORTS | J P Fielding & H Smith Cranfield University |
Reserve paper | |
| ICAS 2002-R35 | THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM | Lee, Meng-Tse, Chang, Wen-Ying, Yang, Cheng-Chen, Lin, Kuo-Wei, Tsai, Yi-Feng, Wu, Chun-Rong, and Hsiao, Fei-Bin, Institute of Aeronautics and Astronautics, National Cheng Kung University, Tainan, TAIWAN | Reserve paper | |
| ICAS 2002-R41 | INTEGRATED PARAMETRIC AIRCRAFT DESIGN | T. Richter, H. Mechler, D. Schmitt Institute of Aeronautical Engineering of the Technische Universität München Mechler, H.; ATENA |
Reserve paper | |
| ICAS 2002-R49 | ANALYSIS OF FLIGHT PERFORMANCE AND STABILITY OF FAMILY OF TRANSPORT AIRPLANE DESIGNS WITH FUSELAGE COMMONALITIES | Hisar M. Pasaribu, Benny Wijanarko Department of Aeronautics and Astronautics Institut Teknologi Bandung Indonesia |
Reserve paper | |
| ICAS 2002-R50 | DEVELOPMENT OF A NEW GENERATION OF AIRCRAFT FOR PILOT TRAINING | A. PISTEK, Inst of Aerospace Eng, Brno University of Technology, Czech Republic | Reserve paper | |
| ICAS 2002-R70 | DESIGN ISSUES RELATING TO ULTRALIGHT HELICOPTERS WITH LARGE COMPOUND ROTORS OPERATING IN GROUND EFFECT | Zaidi Mohammad Zain Associate Professor Faculty of Mechanical Engineering Universiti Teknologi MARA Shah Alam, MALAYSIA |
Reserve paper | |
| ICAS 2002-R74 | EVALUATION AND IMPLEMENTATION OF MULTIDISCIPLINARY DESIGN OPTIMIZATION STRATEGIES | Renaud, G., Shi, G., Institute for Aerospace Research, National Research Council Canada |
Reserve paper | |
| ICAS 2002-R76 | HUMAN COGNITION PERFORMANCE MODEL BASED EVALUATION OF SAFE SPACING IN AIR TRAFFIC | Henk A.P. Blom, Sybert H. Stroeve, Mariken H.C. Everdij, Marco N.J. van
der Park National Aerospace Laboratory NLR PO Box 90502, 1006 BM Amsterdam, The Netherlands |
Reserve paper | |
| ICAS 2002-P9 | DESIGN TRENDS AND GLOBAL DEVELOPMENTS IN MODERN LTA VEHICLES | Prof. Bellur L. Nagabhushan, Mr. Luis J. Valera Saint Louis University |
Poster Session | |
| ICAS 2002-P10 | COMPUTATIONAL AND ANALYTICAL METHODS IN THE AIRCRAFT DESIGN CURRICULUM | Vladimir V. Riabov Rivier College, Nashua, New Hampshire 03060, USA |
Poster Session | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-2.1.1 | CFD ANALYSIS OF LOW SPEED AND CRUISE APIAN CONFIGURATION POWERED BY HIGH SPEED PROPELLERS | M. AMATO, CIRA, IT, M.A. AVERARDO, Alenia, IT | 2.1 Propellers and Rotors | |
| ICAS 2002-2.1.2 | COMPUTATIONAL SIMULATION OF PROPELLERS IN CRUISE | Ethan A. Romander, EAR, NASA Ames Research Center | 2.1 Propellers and Rotors | |
| ICAS 2002-2.1.3 | ROTORCRAFT AERODYNAMIC AND AEROACOUSTIC MODELLING USING VORTEX PARTICLE
METHODS |
Daniel G. Opoku, Fred Nitzsche, Carleton University, Ottawa, Canada Dimitris G. Triantos, Spyros G. Voutsinas, National Technical University of Athens, Greece |
2.1 Propellers and Rotors | |
| ICAS 2002-2.1.4 | A RAPID NUMERICAL METHOD FOR 3D AERO DYNAMICS DESIGN OF COMPRESSOR BLADE ROW (APPLICATION TO A LOW SPEED EXPERIMENTAL MULTI-IDENTICAL-STAGE COMPRESSOR DESIGN) | Naixing Chen, Hongwu Zhang, Yanji Xu, Weiguang Huang Institute of Engineering Thermophysics, Chinese Academy of Sciences |
2.1 Propellers and Rotors | |
| ICAS 2002-8.1.3 | SIMULATION OF TURBULENT AIRFOIL FLOW | A. EKMEDZIC, University of Belgrade, YU | 8.1 Student session I | |
| ICAS 2002-8.1.4 | OPTIMIZATION OF FLAPPING WING MOTION | Keiichi Ito, University of Tokyo |
8.1 Student session I | |
| ICAS 2002-2.2.1 | NUMERICAL PREDICTION OF THE AIRFOIL ICE ACCRETION GROWTH | T. WAN, Tamkang University, TW | 2.2 Low Speed Applications | |
| ICAS 2002-2.2.2 | THE EFFECT OF THE REYNOLDS NUMBER ON THE WING VORTICES | Kaarlonen K, Laine S, Helsinki University of Technology, Laboratory of Aerodynamics Salminen E , Siikonen T, Helsinki University of Technology, Laboratory of Applied Thermodynamics |
2.2 Low Speed Applications | |
| ICAS 2002-2.2.3 | NUMERICAL PREDICTIONS OF WING-TIP EFFECTS ON LIFT-INDUCED DRAG | Bourdin P. - ONERA - Applied Aerodynamics Department | 2.2 Low Speed Applications | |
| ICAS 2002-8.2.3 | EXPERIMENTAL STUDY OF THE STRUCTURE AND DEVELOPMENT OF A WINGTIP VORTEX IN THE NEAR-FIELD | C. WRIGHT, Utah State University, USA | 8.2 Student session II | |
| ICAS 2002-8.2.4 | WAVE DEVELOPMENT ON THIN LAYERS OF ANTI-ICING FLUID | J.E. DILLINGH, Twente University, NL | 8.2 Student session II | |
| ICAS 2002-2.3.1 | EFFICIENT WING DESIGN FOR COMPLEX AIRCRAFT CONFIGURATION USING CAD, UNSTRUCTURED CFD AND INVERSE PROBLEMS | Takeshi FUJITA, T.F., Tohoku University, Japan | 2.3 High Speed Applications I | |
| ICAS 2002-2.3.2 | NUMERICAL OPTIMIZATION OF THE WING OF A SUPERSONIC AIRPLANE | Takovitsky S.A., Central Aerohydrodynamic Institute (TsAGI), Russia | 2.3 High Speed Applications I | |
| ICAS 2002-2.3.3 | COMPUTATION INVESTIGATION IN REUSABLE SPACE TRANSPORT SYSTEMS AT SUPERSONIC SPEED | A. HENZE, RWTH-Aachen, DE | 2.3 High Speed Applications I | |
| ICAS 2002-2.3.4 | LVX - AN INTEGRATED AERODYNAMIC DESIGN AND ANALYSIS METHOD | Mendenhall, M. R., Hegedus, M. C., Nielsen Engineering & Research |
2.3 High Speed Applications I | |
| ICAS 2002-2.4.1 | AN OVERVIEW OF THE RTO SYMPOSIUM ON VORTEX FLOW AND HIGH ANGLE OF ATTACK AERODYNAMICS | Luckring, J. M., NASA Langley Research Center | 2.4 Low Speed Applications II | |
| ICAS 2002-2.4.2 | INVESTIGATION OF HIGH-LIFT, MILD-STALL WINGS | Kong F.M., Hua J., Xiang J.W. Beijing University of Aeronautics and Astronautics, China Zhang Z.Y. Northwestern Polytechnical University, Xian, China |
2.4 Low Speed Applications II | |
| ICAS 2002-2.4.3 | X-31A VECTOR HIGH ANGLE OF ATTACK DESCENT EULER AND NAVIER-STOKES SIMULATIONS OF UNSTEADY MANOEUVRES | Stephan M. Hitzel, Edwin van der Weide, Udo Tremel, Herbert Rieger Numerical Flow Simulation, EADS Military Aircraft, Munich, Germany |
2.4 Low Speed Applications II | |
| ICAS 2002-2.4.4 | VALIDATION OF CIRA FLOW SOLVER ZEN FOR SCT LOW-SPEED HIGH-LIFT COMPUTATIONS | Brandi, V., Amato, M., Catalano, P., CIRA - Italian Aerospace Research Center |
2.4 Low Speed Applications II | |
| ICAS 2002-2.4.5 | INVERSE DESIGN OF HIGH LIFT SYSTEMS | Jones, D., Bombardier Aerospace Fejtek, I., Bombardier Aerospace |
2.4 Low Speed Applications II | |
| ICAS 2002-2.5.1 | A CFD APPROACH TOWARDS MODELING BLADE/VORTEX IMPINGEMENT EFFECTS AND BUFFETING OVER AIRFOILS |
Mamou M., Khalid M., Institute for Aerospace Research, National Research Council Canada |
2.5 High Speed Applications II | |
| ICAS 2002-2.5.2 | RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT | Hua J., Kong F.M. , Wang J.J. , Zhan H., Sun R.Z. ,Qiu D. Beijing University of Aeronautics and Astronautics, China Fu D.W. , Liu J.C. Xi’an Aircraft Design Institute, China Zhang Z.Y. Northwestern Polytechnical Un |
2.5 High Speed Applications II | |
| ICAS 2002-2.5.3 | ADVANCED NUMERICAL SIMULATIONS ON STRUCTURED GRIDS FOR TRANSPORT AIRCRAFT, USING AN EFFICIENT OBJECT ORIENTED SOLVER | BARRERA, L. , AIRBUS FRANCE, Fr, BENOIT, CH. , ONERA, Fr, LE PAPE, M.-C. , ONERA, Fr, HOUDEVILLE, R. , ONERA, Fr, PETER, J. , ONERA, Fr, JOUHAUD, J.-C. , CERFACS, Fr |
2.5 High Speed Applications II | |
| ICAS 2002-8.5.1 (I.L.) | NOISE REDUCTION TECHNOLOGY FOR THE 21ST CENTURY | William. L. Willshire, Jr., Quiet Aircraft Technology Program Manager,
NASA Langley Research Center, Hampton, Va. 23681 Mark D. Guynn, Aerospace Engineer, NASA Langley Research Center, Hampton, Va. 23681 |
8.5 Aircraft Noise II | |
| ICAS 2002-8.5.2 | THE ACTIVE NOISE CONTROL OF PROPELLER NOISE USING A MULTIPOLE SECONDARY SOURCE | Muhammad Kusni Bandung Institute of Technology |
8.5 Aircraft Noise II | |
| ICAS 2002-8.5.3 | ADVANCED ACTIVE CONCEPTS FOR LOW NOISE ROTORCRAFT | M. GRUENEWALD, EADS CRC, DE | 8.5 Aircraft Noise II | |
| ICAS 2002-2.6.1 | EVALUATION OF THE CAPABILITIES OF CFD TO PREDICT STORE TRAJECTORIES FROM ATTACK AIRCRAFT | Cenko, A. Naval Air Systems Command Niewoehner, R. and Ryckebusch, C. United States Naval Academy |
2.6 CFD for Complex Flows | |
| ICAS 2002-2.6.2 | IAR STORES CLEARANCE CFD APPROACH: FROM DEVELOPMENT TO AUTOMATED ENGINEERING TOOL |
Fortin, F., Benmeddour, A., Tahi, A. Institute for Aerospace Research
(IAR),National Research Council of Canada (NRC) |
2.6 CFD for Complex Flows | |
| ICAS 2002-2.6.3 | THREE-DIMENSIONAL VISCOUS FLOW SIMULATIONS OVER A COMPLETE SATELLITE LAUNCHER USING OVERSET GRIDS | Edson Basso and João Luiz F. Azevedo, Instituto de Aeronáutica e Espaço - CTA/IAE/ASE-N, 12228-904 - São José dos Campos - SP - BRAZIL | 2.6 CFD for Complex Flows | |
| ICAS 2002-2.6.4 | PARAMETRIC ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF LAUNCH VEHICLES WITH STRAP-ON BOOSTERS | Arash Naghib-Lahouti, Amir Nejat, Taravat Khadivi Engineer, Aerospace Research Institute PO Box 15875-3885, Tehran, Iran |
2.6 CFD for Complex Flows | |
| ICAS 2002-3.6.1 | FLOW MECHANISMS ACTIVE IN WING ROCK OF COMBAT AIRCRAFT | Ericsson, L. E., Engineering Consultant, Mountain View, California 94040, USA Beyers, M. E., Institute for Aerospace Research, Ottawa, Ontario K1A 0R6, Canada |
3.6 Flow Mechanisms | |
| ICAS 2002-3.6.2 | NUMERICAL PREDICTIONS AND EXPERIMENTS ON SUPERSONIC JET MIXING FROM CASTELLATED NOZZLES | A. J. Saddington, N. J. Lawson and K. Knowles Cranfield University, RMCS, Shrivenham, UK |
3.6 Flow Mechanisms | |
| ICAS 2002-3.6.3 | USING OF THE LOW TURBULENCE WIND TUNNEL FOR INVESTIGATION OF THREE-DIMENSIONAL UNSTEADY FLOW IN CURVED CHANNELS | Hanus, D., Anderle, P., Department of Aerospace Engineering, Czech Technical University in Prague |
3.6 Flow Mechanisms | |
| ICAS 2002-3.6.4 | SPIRAL VORTICES DETECTION ON A ROTATING DISK | Astarita, T., University of Naples - DETEC, P.le Tecchio, 80 - 80125 Naples,
ITALY Cardone, G., University of Naples - DETEC, P.le Tecchio, 80 - 80125 Naples, ITALY Carlomagno,G.M., University of Naples - DETEC, P.le Tecchio, 80 - 80125 Naples, ITALY |
3.6 Flow Mechanisms | |
| ICAS 2002-1.7.1 | CALCULATION OF COMPRESSIBLE AND INCOMPRESSIBLE VISCOUS FLOWS BY A VISCOUS
INVISCID SPLITTING FINITE ELEMENT METHOD |
Su J., Aerodynamic Laboratory, Institute for Aerospace Research, National Research Council of Canada, Ottawa, Canada |
1.7 CFD Algorithms I | |
| ICAS 2002-1.7.2 | A HYBRID UNSTRUCTURED GRID SYSTEM FOR VISCOUS AND INVISCID AERODYNAMIC ANALYSIS | Akio OCHI, Eiji SHIMA, Kawasaki Heavy Industries, LTD |
1.7 CFD Algorithms I | |
| ICAS 2002-1.7.3 | FROM ANALYSIS TO DESIGN OF HIGH-LIFT CONFIGURATIONS USING A NEWTON-KRYLOV ALGORITHM | Nemec, M., Zingg, D. W. University of Toronto Institute for Aerospace Studies 4925 Dufferin Street, Toronto, ON, M3H 5T6, Canada |
1.7 CFD Algorithms I | |
| ICAS 2002-1.7.4 | AN ACCURATE MULTIBLOCK ENO DRIVEN NAVIER-STOKES SOLVER FOR COMPLEX AERODYNAMIC CONFIGURATIONS | Epstein, B, Academic College of Tel-Aviv Yaffo, Computer Science Dept. Rubin, T, and Seror, S, Israel Aircraft Industries Aerodynamic Dept, CFD Group |
1.7 CFD Algorithms I | |
| ICAS 2002-1.7.5 | STOCHASTIC MODELING OF LAMINAR-TURBULENT TRANSITION | Rubinstein, R, Choudhari, M, NASA Langley Research Center |
1.7 CFD Algorithms I | |
| ICAS 2002-2.7.1 | CFD SIMULATIONS OF THE UNSTEADY HIGH ALPHA AERODYNAMICS OF DELTA WINGS | Y. LE MOIGNE, A. RIZZI, Royal Institute of Technology, SE | 2.7 Unsteady Application | |
| ICAS 2002-2.7.2 | PREDICTION OF UNSTEADY FLOWS AROUND ROTATING BLADES | Jean-Marc Bousquet ONERA, Applied Aerodynamic Department 92322 Chatillon France |
2.7 Unsteady Application | |
| ICAS 2002-2.7.3 | MODELING OF UNSTEADY AERODYNAMIC CHARACTERISTCS OF DELTA WINGS | Jouannet Christopher, Krus Petter Linköpings University |
2.7 Unsteady Application | |
| ICAS 2002-2.7.4 | TRANSONIC AILERON BUZZ BOUNDARY PREDICTION USING HOPF-BIFURCATION ANALYSIS METHOD | Liu Qiangang, Department of Aircraft Engineering, Northwestern Polytechnical University, Xi'an Bai Junqiang, Department of Aircraft Engineering, Northwestern Polytechnical University, Xi'an |
2.7 Unsteady Application | |
| ICAS 2002-2.7.5 | CFD PREDICTION OF STABILITY DERIVATIVES OF A TURBOPROP AIRCRAFT USING A CARTESIAN GRID BASED EULER CODE | Waller G. Bombardier Aerospace | 2.7 Unsteady Application | |
| ICAS 2002-3.7.1 | HIGH REYNOLDS NUMBER SIMULATION IN A TRANSONIC WIND TUNNEL BY SURFACE SUCTION | Green, J.E., Elliott, M., Wong, P.W.C., Aircraft Research Association Ltd, Manton Lane, Bedford MK41 7PF, UK | 3.7 Wind Tunnel Testing and Experimental Technique | |
| ICAS 2002-3.7.2 | EXPERIMENTAL INVESTIGATIONS ON THE ADAPTATION ACCURACY OF ADAPTIVE SLOTS IN WIND TUNNEL TEST SECTION WALLS | Meyer O, Blume S, Nitsche W Institute of Aero- and Astronautics (ILR), Technical University (TU) Berlin, Germany |
3.7 Wind Tunnel Testing and Experimental Technique | |
| ICAS 2002-3.7.3 | VALIDATION OF A WALL INTERFERENCE CORRECTION PROCEDURE | G. Lombardi , M.V. Salvetti Department of Aerospace Engineering, University of Pisa M. Morelli Medium Speed Wind Tunnel, CSIR, South Africa |
3.7 Wind Tunnel Testing and Experimental Technique | |
| ICAS 2002-3.7.4 | PITCH OSCILLATIONS OF A RECTANGULAR WING SECTION IN TRANSONIC FLOW | Hillenherms, C., Schroeder, W., Limberg, W., Aerodynamisches Institut der RWTH Aachen | 3.7 Wind Tunnel Testing and Experimental Technique | |
| ICAS 2002-3.7.5 | NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE FLOWFIELD IN A BLOWDOWN WIND TUNNEL | Ali Rebaine, Mahmood Khalid, Cabot Broughton and Fred Ellis Institute for Aerospace Research, National Research Council Montreal Road, K1A 0R6, Ottawa, Ontario, Canada |
3.7 Wind Tunnel Testing and Experimental Technique | |
| ICAS 2002-4.7.1 | NOVEL INJECTION SCHEME FOR JET INTERACTION FLOWS | J. SCHETZ, V. VITI, Virginia Tech., USA | 4.7 ISOABE I | |
| ICAS 2002-8.7.1 (I.L.) | AERODYNAMIC DESIGN OPPORTUNITIES FOR FUTURE SUPERSONIC AIRCRAFT | Richard M. Wood, Steven X. S. Bauer, Jeffrey D. Flamm, NASA Langley Research Center |
8.7 Works in Supersonic Transports | |
| ICAS 2002-8.7.2 (I.L) | A RESEARCH INITIATIVE ON THE SUPERSONIC AIRCRAFT | Sebastien Candel* and Denis Jeandel+ *EM2C, CNRS, Ecole Centrale Paris, 92295 Chatenay-Malabry +LMFA, CNRS, Ecole Centrale de Lyon, 69131 Ecully, France |
8.7 Works in Supersonic Transports | |
| ICAS 2002-8.7.3 | LEADING-EDGE VORTEX FLAPS FOR SUPERSONIC TRANSPORT CONFIGURATION-EFFECTS OF FLAP CONFIGURATIONS AND ROUNDED LEADING-EDGES | RINOIE, K., MIYATA, K., University of Tokyo KWAK, D. Y., NOGUCHI, M., National Aerospace Laboratory |
8.7 Works in Supersonic Transports | |
| ICAS 2002-8.7.4 | TECHNOLOGICAL AND DESIGN CHALLENGES FOR SUPERSONIC BUSINESS JET | S. LEBOURG, DASSAULT AVIATION, FR | 8.7 Works in Supersonic Transports | |
| ICAS 2002-8.7.5 | TBD | P. HENNE, Gulfstream Aerospace Corporation, US | 8.7 Works in Supersonic Transports | |
| ICAS 2002-1.8.1 | SIMULATION TECHNIQUES IN HYPERSONIC AEROTHERMODYNAMICS | Vladimir V. Riabov Rivier College, Nashua, New Hampshire 03060, USA |
1.8 High Speed Aerodynamic Analysis | |
| ICAS 2002-1.8.2 | A STUDY ON REDUCTION OF AERODYNAMIC HEATING LOAD BY OPPOSING JET IN HYPERSONIC FLOW | K. HAYASHI, Kyushu University, JP, K. KARASHIMA, Nishinippon Institute of Technology, JP |
1.8 High Speed Aerodynamic Analysis | |
| ICAS 2002-2.8.1 | EXPERIMENTAL AND NUMERICAL STUDY ON TRANSITION CHARACTERISTICS AT SUPERSONIC SPEED | Sugiura, H, Yoshida, K, Noguchi, M, Ueda, Y, Tokugawa, N, Takagi, S, National Aerospace Laboratory of Japan (NAL) |
2.8 Flow Instabilities | |
| ICAS 2002-2.8.2 | THREE-DIMENSIONAL CO-OPERATIVE INSTABILITIES IN WAKE VORTEX PAIRS | Steijl, R., Hoeijmakers, H.W.M., University of Twente, P.O.Box 217, 7500, AE Enschede, The Netherlands, |
2.8 Flow Instabilities | |
| ICAS 2002-2.8.3 | PREDICTION OF LAMINAR-TO-TURBULENT TRANSITION IN INCOMPRESSIBLE FLOW PAST 3-D CAVITY | H. Yao, R. K. Cooper, E. Benard, and S. Raghunathan, School of Aeronautical Engineering Queen’s University Belfast, Belfast BT7 1NN, UK | 2.8 Flow Instabilities | |
| ICAS 2002-3.8.1 | TESTING OF A MODERN TRANSPORT AIRCRAFT CONFIGURATION IN ETW CLOSE TO MACH 0.9 | Quest, J, European Transonic Windtunnel GmbH Wright, M C N, European Transonic Windtunnel GmbH Rolston, S, Airbus UK |
3.8 Configuration Testing I | |
| ICAS 2002-3.8.2 | INVESTIGATIONS ON THE TURBULENT WAKE VORTEX FLOW OF LARGE TRANSPORT AIRCRAFT | Christian Breitsamter, Claudio Bellastrada, Boris Laschka, Institute for Fluid Mechanics, Technische Universitt Mnchen, Boltzmannstrasse 15, 85748, Garching, Germany |
3.8 Configuration Testing I | |
| ICAS 2002-3.8.3 | AERODYNAMIC CHARACTERISTICS OF SPIN PHENOMENON FOR DELTA WING | Nakamura, Y., Yamada, T. Nagoya University |
3.8 Configuration Testing I | |
| ICAS 2002-8.8.2 (St) | DOWNWASH FLOW INVESTIGATIONS FOR PASSANGER AIRPLANE | Nikolay N. Bragin Central Aerohydrodynamic Institute of Russia (TsAGI) |
8.8 Student session IV | |
| ICAS 2002-1.9.1 | SIMULATION OF STATISTICAL MEAN BEHAVIORS AND COHERENT STRUCTURES OF INCOMPRESSIBLE TURBULENT FLOWS USING UNILATERAL-AVERAGE BASED GOVERNING EQUATIONS | G.Gao-Beijing University of aero.& Astronautics, China Y.Yong-Florida Atlantic University, USA |
1.9 CFD Algorithms II | |
| ICAS 2002-1.9.2 | AN EVALUATION OF SEVERAL LOW-RE TURBULENCE MODELS PART 1- FLAT-PLATE BOUNDARY LAYER AND AXISYMMETRIC SEPARATING FLOWS | M. I. Yaras, A.D. Grosvenor Department of Mechanical and Aerospace Engineering Carleton University, Ottawa, Ontario, CANADA K1S 5B6 |
1.9 CFD Algorithms II | |
| ICAS 2002-1.9.3 | A FULLY COUPLED NEWTON-KRYLOV SOLVER FOR TURBULENT AERODYNAMIC FLOWS | Chisholm, T. T., Zingg, D. W., University of Toronto |
1.9 CFD Algorithms II | |
| ICAS 2002-1.9.4 | SENSITIVITY AND UNCERTAINTY ANALYSIS OF AERODYNAMIC FLOWS | Dominique Pelletier , Éric Turgeon , Jeff Borggaard Canada Research Chair École Polytechnique de Montréal P.O. Box 6079, Station Centre-ville Montréal, Canada, H3C 3A7 |
1.9 CFD Algorithms II | |
| ICAS 2002-2.9.1 | ON TRANSMISSION OF SOUND ACROSS A NON ISOTHERMAL BOUNDARY LAYER | Campos, L.M.B.C., Kobayashi, M.H., Instituto Superior Tecnico, Department of Mechanical Engineering/SMA, Av. Rovisco Pais 1, 1049-001, Lisbon, PORTUGAL. |
2.9 Design Applications and Accoustics | |
| ICAS 2002-2.9.2 | RELATIONSHIP BETWEEN INSTABILITY WAVES AND NOISE OF LOW SUPERSONIC JETS | MILLET Christophe, CASALIS Gregoire, ONERA |
2.9 Design Applications and Accoustics | |
| ICAS 2002-2.9.3 | DESIGN METHOD FOR PROBLEMS INVOLVING SHOCK BOUNDARY-LAYER INTERACTION | Cross, A.G.T, BAE SYSTEMS, Warton Aerodrome, Warton, Lancashire, PR4 1AX,
United Kingdom |
2.9 Design Applications and Accoustics | |
| ICAS 2002-2.9.4 | SIMPLIFIED DESIGN METHOD FOR A SYMMETRICAL WING-BODY FAIRING | C.B. Steenaert, B.W. van Oudheusden, L.M.M. Boermans, Delft University of Technology |
2.9 Design Applications and Accoustics | |
| ICAS 2002-3.9.1 | TRANSITION MEASUREMENT AND ANALYSIS ON A SWEPT WING IN HIGH LIFT CONFIGURATION | A. Séraudie, J. Perraud, F. Moens (*) ONERA, Centre de Toulouse, (*) : ONERA - Châtillon |
3.9 Flow Control | |
| ICAS 2002-3.9.2 | ENHANCED MANEUVERABILITY BY ACTIVE VORTEX CONTROL WITH MOVEABLE BLOWING JET | Huang, X. , Hanff, E. Institute for Aerospace Research, National Research Council Canada |
3.9 Flow Control | |
| ICAS 2002-3.9.3 | CONTROL OF CLOSED-TYPE SUPERSONIC CAVITY FLOWS | J. Zhang,, E. Morishita, T. Okunuki, and H. Itoh Department of Aeronautics and Astronautics, University of Tokyo, Japan |
3.9 Flow Control | |
| ICAS 2002-3.9.4 | FLOW CONTROL DOWNSTREAM OF A BACKWARD FACING STEP: A DPIV STUDY | Pier Giorgio SPAZZINI, IMGC - CNR Gaetano Maria DI CICCA, Gaetano IUSO, Michele ONORATO, DIASP, Politecnico di Torino Rachel KING, North Carolina State University |
3.9 Flow Control | |
| ICAS 2002-4.9.3 | DESIGN AND DEVELOPMENT OF OPTIC FIBER SMART STRUCTURES IN AEROSPACE VEHICLES | Zaffar. M. Khan Advanced Engineering Research Organization, Wah Cantt, PAKISTAN |
4.9 Structures and Materials III | |
| ICAS 2002-1.10.1 | USING COMPUTATIONAL FLUID DYNAMICS FOR AERODYNAMICS - A CRITICAL ASSESSMENT | A. JAMESON, Stanford University, US | 1.10 CFD for Design | |
| ICAS 2002-1.10.2 | LOW-SONIC-BOOM DESIGN METHODOLOGIES FOR FUTURE SUPERSONIC AIRCRAFT | S.X.S. BAUER, NASA LRC, US | 1.10 CFD for Design | |
| ICAS 2002-1.10.3 | THE elsA OBJECT ORIENTED COMPUTATIONAL TOOL FOR INDUSTRIAL APPLICATIONS | M. GAZAIX, ONERA, FR | 1.10 CFD for Design | |
| ICAS 2002-1.10.4 | NUMERICAL OPTIMIZATION DESIGN OF WINGS BY SOLVING ADJOINT EQUATIONS | Z. D. Qiao, X. D. Yang, X. L. Qin, B. Zhu, Northwestern Polytechnical University Xian, 710072, China |
1.10 CFD for Design | |
| ICAS 2002-1.10.5 | MEGAFLOW - A NUMERICAL FLOW SIMULATION TOOL FOR TRANSPORT AIRCRAFT DESIGN | Kroll, N., Rossow, C.C., Schwamborn, D., DLR, Institute of Aerodynamics
and Flow Technology Becker, K., Airbus-Deutschland Heller, G., Fairchild-Dornier |
1.10 CFD for Design | |
| ICAS 2002-2.10.1 | EXPERIMENTAL STUDY OF CHARACTERISTICS OF MICRO-HOLE POROUS SKINS FOR TURBULENT SKIN FRICTION REDUCTION | Danny P. Hwang - NASA/ Glenn Research Center, Cleveland, OH 44135 | 2.10 Flow Control by Boundary Layer | |
| ICAS 2002-2.10.2 | SIMULATION OF FLOWS WITH PASSIVE POROSITY | Frink, N.T., Bauer, S.X.S., Hunter, C.A., NASA Langley Research Center, Hampton, Virginia, USA | 2.10 Flow Control by Boundary Layer | |
| ICAS 2002-2.10.3 | ACTIVE SEPARATION CONTROL SYSTEM IMPROVED FOR CONTROL TIME AND SUPPRESSION EFFECT | Hiroaki Hasegawa, Department of Mechanical Engineering, Faculty of Engineering
and Resource Science, Univer-sity of Akita, Akita-shi, Akita 010-8502, Japan Kazuo Matsuuchi, Engineering Mechanics and Systems, University of Tsukuba, Tennoudai, Tsukuba-sh |
2.10 Flow Control by Boundary Layer | |
| ICAS 2002-2.10.4 | DPIV INVESTIGATION OF A TURBULENT BOUNDARY LAYER MANIPULATED BY TRANSVERSAL WALL OSCILLATIONS | Gaetano Maria DI CICCA, Michele ONORATO, Gaetano IUSO, DIASP, Politecnico di Torino Pier Giorgio SPAZZINI, IMGC - CNR |
2.10 Flow Control by Boundary Layer | |
| ICAS 2002-2.10.5 | FLOW CONTROL OVER THE WING OF A FIGHTER-TYPE CONFIGURATION USING BOUNDARY LAYER SUCTION | M. R. Soltani, T. Khadivi, A. R. Davari Department of Aerospace Engineering, Sharif University of Technology, Tehran, I. R. Iran |
2.10 Flow Control by Boundary Layer | |
| ICAS 2002-3.10.1 | DEVELOPMENT OF HIGH-LIFT SYSTEMS FOR THE BOMBARDIER CRJ-700 | Kafyeke, F., Pépin, F. , Kho, C. Advanced Aerodynamics, Bombardier Aerospace |
3.10 Configuration Testing II | |
| ICAS 2002-3.10.2 | THE EFFECT OF WING TIP BLOWING ON THE VORTEX DRAG | R.F.F. Coimbra Dr., EMBRAER, F.M. Catalano PhD.Aerodynamic Laboratory USP Brazil |
3.10 Configuration Testing II | |
| ICAS 2002-3.10.3 | TESTING OF A DASH 8 Q400 IN THE NASA AMES 80x120' WIND TUNNEL | Lye J.D. , Bombardier Aerospace, Buchholz S., Sverdrup Technology (under contract to NASA), Nickison D., NASA Ames |
3.10 Configuration Testing II | |
| ICAS 2002-3.10.4 | OVERVIEW OF ROTARY FLOW VISUALIZATION RESULTS ON THE F/A-18 AIRCRAFT | H. J. Cai and M. E. Beyers Aerodynamics Laboratory, Institute for Aerospace Research, National Research Council Canada |
3.10 Configuration Testing II | |
| ICAS 2002-3.10.5 | ESTIMATION OF SPIN CHARACTERISTICS OF AEROBATIC AIRCRAFT BY MEANS OF SPIN ROTATION MODELING IN HORIZONTAL WIND TUNNEL | Sohi N.P., Prudnikov Y.A., Temlyakov Y.N. Federal State Unitary Enterprise «Siberian Aeronautical Research Institute» (SibNIA) |
3.10 Configuration Testing II | |
| ICAS 2002-1.11.1 | VALIDATION OF A NAVIER-STOKES SOLVER FOR AIRFOIL HIGH-LIFT ANALYSIS | Langlois, M. and Mokhtarian, F. Advanced Aerodynamics Dept.. Bombardier Aerospace Montréal (Québec) Canada |
1.11 CFD Validation | |
| ICAS 2002-1.11.2 | SHORT TURNAROUND TIME TURBULENT FLOW COMPUTATIONS FOR COMPLETE AIRCRAFT CONFIGURATIONS | J.W. van der Burg, E.T.A. van der Weide - National Aerospace Laboratory, NLR Anthony Fokkerweg, 1059 CM Amsterdam, The Netherlands | 1.11 CFD Validation | |
| ICAS 2002-1.11.3 | A METHOD FOR DRAG DECOMPOSITION FROM CFD CALCULATIONS | Paparone L., CIRA Centro Italiano Ricerche Aerospaziali, Capua (CE), Italy Tognaccini R., Dipartimento di Progettazione Aeronautica, Universita` di Napoli Federico II, Napoli, Italy |
1.11 CFD Validation | |
| ICAS 2002-2.11.1 | OPTIMIZATIONS OF AIRFOIL AND WING USING GENETIC ALGORITHM | F. Zhang , S. Chen and M. Khalid Institute for Aerospace Research (IAR) National Research Council (NRC) Ottawa, K1A 0R6, Ontario, Canada |
2.11 Other Aerodynamic Methods | |
| ICAS 2002-2.11.2 | COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS OF AXI-SYMMETRIC BODIES IN TRANSONIC FLOW | Eddy Priyono and Harijono Djojodihardjo Departmentof Aeronautics and Astronautics, Bandung Institute of Technology Jl. Ganesha 10 Bandung, Indonesia |
2.11 Other Aerodynamic Methods | |
| ICAS 2002-2.11.3 | NUMERICAL SIMULATION OF FLOWS INTO INDUCTIVE PLASMATRONS | Utyuzhnikov, S.V., UMIST and MIPT Konyukhov, A.V., MIPT, Vasil'evskii, S.A., MIPT, Rudenko, D.V., MIPT (Moscow Institute of Physics and Technology) |
2.11 Other Aerodynamic Methods | |
| ICAS 2002-3.11.1 | WIND TUNNEL TESTING TO DETERMINE UNSTEADY LOADS ON A HELICOPTER FUSELAGE IN A SHIP AIRWAKE | Richard G. Lee, Steven J. Zan, Aerodynamics Laboratory, Institute for
Aerospace Research, National Research Council of Canada |
3.11 Unsteady Aerodynamics | |
| ICAS 2002-3.11.2 | DERIVATION OF UNSTEADY AERODYNAMIC MODELS FROM WIND TUNNEL MULTI-AXIS TEST RIGS | Lowenberg, MH, University of Bristol Kyle, HL, University of Bristol |
3.11 Unsteady Aerodynamics | |
| ICAS 2002-3.11.3 | CLARIFICATION OF UNSTEADY CHARACTERISTICS IN SEPARATED FLOW OVER AN AXISYMMETRIC PARABOLOID AT HIGH ANGLES OF ATTACK | ISHIDE,T,Kisarazu National College of Technology NISHIKAWA,N., MIKAMI,F, Chiba University |
3.11 Unsteady Aerodynamics | |
| ICAS 2002-R1 | THE EFFECT OF THE ANGLE OF THE INCLINED FLAT PLATE ON THE DEFLEXION OF A PLANE WALL JET | H Acar, Instanbul Technical University | Reserve paper | |
| ICAS 2002-R3 | AN UNSTEADY FLOW-SOLVER WITH ALGEBRAIC GRID MOTION FOR AEROELASTIC SIMULATIONS | C. B. Allen Department of Aerospace Engineering, University of Bristol, Bristol, BS8 1TR, U.K. |
Reserve paper | |
| ICAS 2002-R5 | AN ALGORITHM FOR THE CALCULATION OF AERODYNAMIC WING-PROPELLER INTERACTION | A Bengin, Faculty of Mechanical Engineering, YU | Reserve paper | |
| ICAS 2002-R6 | CENTRIFUGAL AND 3D EFFECTS ON THE NEAR TIP SECTION OF ROTATING BLADE | Berton, E., Favier, D.,Maresca, C., Nsi Mba, M., L.A.B.M. Laboratory, University of Méditerranée |
Reserve paper | |
| ICAS 2002-R7 | NORMAL FORCE CALCULATIONS FOR ROCKET-LIKE CONFIGURATIONS | Bigarelli, E.D.V., Azevedo, J.L.F. CTA/IAE/ASE-N - 12228-904 - São José dos Campos, SP, Brasil |
Reserve paper | |
| ICAS 2002-R15 | INTERACTION OF TWO PARALLEL RECTANGULAR JETS | ERDEM,D., Istanbul Technical University, Istanbul, Turkey ATLI, V., Civil Aviation School, Kayseri, Turkey |
Reserve paper | |
| ICAS 2002-R17 | DESIGN OF SURFACE ROUGHNESS FOR PASSIVE FLOW CONTROL | Floryan, J.M., Professor, Department of Mechanical and Materials Engineering, The University of Western Ontario, London, Ontario, N6A 5B9, Canada Nikumb, S.K., Group Leader, Precision Fabrication Processes, Integrated Manufacturing Technologies Insti |
Reserve paper | |
| ICAS 2002-R20 | AN ENGINEERING MODEL OF DELTA WING VORTEX BREAKDOWN | Dr GREENWELL, QinetiQ plc, UK | Reserve paper | |
| ICAS 2002-R21 | FAST AND ACCURATE SURFACE AND GRID CREATION ON A COMPLETE AIRCRAFT FOR A CARTESIAN GRID BASED EULER SOLVER | E Hansen, Bombardier Aerospace, CA | Reserve paper | |
| ICAS 2002-R23 | SEPARATION CONTROL BY ALTERNATING TANGENTIAL BLOWING/SUCTION AT MULTIPLE SLOTS | Hossein Hamdani, Muhammad Nauman &Khalid Parvez Department of Aerospace, College of Aeronautical Engineering, National University of Science and Technology, Pakistan |
Reserve paper | |
| ICAS 2002-R24 | EXPERIMENTAL STUDY OF TURBULENT WAKE FLOW DEVELOPMENT BEHIND A FINITE WING WITH HIGH ANGLE OF ATTACKS | Hsiao, Fei-Bin, Cheng, Chao-Zen, and Liu, Wen-Jay, Institute of Aeronautics
and Astronautics, National Chen Kung University, Tainan, Taiwan Hsu, Cheng-Chiang, Air Force Aeronautic Technique School, Kaohsiung, Taiwan |
Reserve paper | |
| ICAS 2002-R25 | CENTRE-BODY AND LEADING-EDGE BEVEL EFFECTS ON DELTA WING AERODYNAMICS AT HIGH INCIDENCE | X Huang, The Institute for Aerospace Research, NRC, CA | Reserve paper | |
| ICAS 2002-R29 | SOLUTION OF AIRFOIL-FLAP CONFIGURATIONS BY USING CHIMERA GRID SYSTEM | TARHAN E., OKTAY E. ROKETSAN, Missile Industries, Inc., 06780 Ankara Turkey KAVSAOGLU M. S. Middle East Technical University, 06531 Ankara, Turkey |
Reserve paper | |
| ICAS 2002-R30 | MULTI BLOCK NAVIER STOKES SOLUTIONS OF LOW ASPECT RATIO RECTANGULAR FLAT WINGS IN COMPRESSIBLE FLOW | DURMUS G., KAVSAOGLU M. S. Middle East Technical University, 06531 Ankara, Turkey |
Reserve paper | |
| ICAS 2002-R33 | THE STUDY OF MONOTONICITY OF AUSM-TYPE SCHEMES IN SHOCK DISCONTINUITIES | Kim, K., Lee, K. Sejong-Lockheed Martin Aerospace Research Center, Sejong University Kim, C., Rho, O. Department of Aerospace Engineering Seoul National University |
Reserve paper | |
| ICAS 2002-R38 | A SIMPLE AND NONLINEAR AERODYNAMIC MODELING FOR DELTA WITH WITH LEV BREAKDOWN INVOLVED | H. LOU, Polytechnic University, Turin, ItalyIT | Reserve paper | |
| ICAS 2002-R39 | TIME-LINEARISED TRANSONIC SMALL DISTURBANCE CODE INCLUDING ENTROPY AND VORTICITY EFFECTS | Eddie LY, Jiro NAKAMICHI, National Aerospace Laboratory of Japan (NAL), Tokyo, Japan |
Reserve paper | |
| ICAS 2002-R40 | IMPLEMENTATION AND VALIDATION OF THE SPALART-ALLMARAS TURBULENCE MODEL FOR HIGH SPEED FLOWS | MARSILIO, R., GRILLO, D. Dipartimento di Ingegneria Aeronautica e Spaziale Politecnico di Torino Corso Duca degli Abruzzi,24 10129 Torino, ITALY |
Reserve paper | |
| ICAS 2002-R43 | NORMAL AND SIDE FORCES AMPLIFICATION BY LATERAL JET ISSUED FROM AN OGIVE CYLINDER | JJ Miau, National Cheng Kung University, Taiwan | Reserve paper | |
| ICAS 2002-R44 | IMPROVEMENT OF TRANSONIC AEROFOIL AERODYNAMIC PERFORMANCE | Mochammad Agoes Moelyadi Aerospace Deparment Bandung Institute of Technology |
Reserve paper | |
| ICAS 2002-R46 | ON DESIGN OF UNCONVENTIONAL HIGH ASPECT RATIO "JOINED-WING" TYPE AIRCRAFT | Dr. R. K. Nangia & Dr. M. E. Palmer Nangia Aero Research Associates, WestPoint, 78-Queens Road, BRISTOL, BS8 1QX, UK. Dr. C. P. Tilmann Air Force Research Laboratory Air Vehicles Directorate, Wright-Patterson AFB, OHIO, USA |
Reserve paper | |
| ICAS 2002-R48 | ILU PRECONDITIONED MULTI-MODEL FORMULATION FOR COMPRESSIBLE FLOWS ON 3D UNSTRUCTURED MESHES | Xu T. UNIVERSITY OF TORONTO Cai X.-C. UNIVERSITY OF COLORADO AT BOULDER Paraschivoiu M. UNIVERSITY OF TORONTO |
Reserve paper | |
| ICAS 2002-R52 | THE APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER FLAP AS A FLOW CONTROL ON THE WING FOR REGIONAL AIRCRAFT FAMILY | Prasetyo Edi Indonesian Aerospace, Bandung, West Java, INDONESIA |
Reserve paper | |
| ICAS 2002-R53 | NUMERICAL SIMULATION OF NAVIER-STOKES EQUATIONS FOR HELICOPTER ROTOR IN FORWARD FLIGHT USING MOVING CHIMERA GRIDS | Z. D. Qiao, A. M. Yang , B. Zhu Northwestern Polytechnical University Xian, 710072, China |
Reserve paper | |
| ICAS 2002-R59 | NUMERICAL SIMULATION OF THE STORE SEPARATION USING UNSTRUCTURED CARTESIAN GRID | Weimin Sang, Fengwei Li , Qin E Northwestern Polytechnical University |
Reserve paper | |
| ICAS 2002-R60 | NUMERICAL INVESTIGATION ON THE FLOW CHARACTERISTICS OF A SUPERSONIC JET IMPINGING ON AN AXI-SYMMETRIC DEFLECTOR | Sankaran,S., Rajeswara Rao. M., Satyanarayana.T.N.V., Satyanarayana.N.,
Visvanathan.K., VAST, SHAR Centre, ISRO, Sriharikota, India-524124 Rupesh B. Kotapati, Research Assistant, Dept. of Mechanical & Aerospace Engineering Arizona State Unive |
Reserve paper | |
| ICAS 2002-R68 | INFLUENCE OF ACOUSTIC EXCITATION ON AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBERS | S. Yarusevych*, J.G. Kawall** and P. Sullivan* *Department of Mechanical and Industrial Engineering, University of Toronto. **Department of Mechanical, Aerospace and Industrial Eng., Ryerson University. |
Reserve paper | |
| ICAS 2002-R69 | WAVERIDER DESIGN WITH PARAMETRIC FLOW QUALITY CONTROL BY INVERSE METHOD OF CHARACTERISTICS | Yiji Qian Beijing University of Aeronautics and Astronautics Beijing, 100083, China Helmut Sobieczky DLR German Aerospace Research Center Bunsenstr.10, D-37073, Göttingen, Germany |
Reserve paper | |
| ICAS 2002-R79 | INFLUENCE OF INLET PROFILE ON HIGH-BPR TURBOFAN PERFORMANCE USING A RADIAL PROFILE MAP |
J. Yin, P.Pilidis School of Engineering, Cranfield University, Cranfield Bedfordshire, MK43 0AL, UK |
Reserve paper | |
| ICAS 2002-P1 | AN-70 STOL AIRCRAFT CHARACTERISTICS AT HIGH ANGLES OF ATTACK AND TAKEOFF AND LANDING CHARACTERISTICS | Balabuyev P.V., Bogdanov O.K., Kudryavtsev V.A., Pustovoytov V.P. ANTONOV Aeronautical Scientific/Technical Complex |
Poster Session | |
| ICAS 2002-P2 | VISCOUS AND WAVE DRAG OPTIMIZATION FOR A TRANSPORT AIRCRAFT MISSION ADAPTIVE WING | F.M. Catalano, P.C. Greco Jr - Aircraft Laboratory, University of São
Paulo-Brazil A.L. Martins - EMBRAER, Brazil |
Poster Session | |
| ICAS 2002-P4 | AERODYNAMIC MODELING AND PERFORMANCE ANALYSIS OF A SHROUDED-FAN UNMANNED AERIAL VEHICLE | de Divitiis N., Department of Mechanics and Aeronautics University of Rome "La Sapienza" ITALY | Poster Session | |
| ICAS 2002-P6 | MULTI BLOCK NAVIER STOKES SOLUTIONS OF LOW ASPECT RATIO RECTANGULAR FLAT WINGS IN COMPRESSIBLE FLOW | Gökhan Durmu ? , Mehmet ?erif Kavsaoglu Middle East Technical University, 06531 Ankara, Turkey |
Poster Session | |
| ICAS 2002-P13 | COMPARISON OF 1D AND 2D NUMERICAL MODELS FOR PREDICTING HYPERSONIC INLET FLOW STARTING | R B Tahir, Ryerson Polytechnic University, CN | Poster Session | |
| ICAS 2002-P17 | NEW TECHNOLOGY OF FLOW PATTERN CONTROL IN CASE OF AN AIRFOIL | Jozwiak, R, Kubrynski,K, Sierputowski,P, Institute of Aeronautics and Applied Mechanics, Warsaw University of Techology, Poland, |
Poster Session | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-3.1.1 | GEOMETRICALLY LINEAR/NONLINEAR SANDWICH STRUCTURES WITH ANISOTROPIC FACE SHEETS: THEORY AND BEHAVIOR | Liviu Librescu and Terry Hause Virginia Polytechnic Institute and State University, Department of Engineering Science and Mechanics, Blacksburg, Virginia 24061, USA |
3.1 Structures Materials I | |
| ICAS 2002-3.1.2 | FAILURE PREDICTION OF STRINGER STIFFENED COMPOSITE PANELS WITH IMPACT DAMAGE UNDER UNIAXIAL COMPRESSION | P. T. Curtis, Dstl, U.K. C. Soutis, Y. Zhuk, I. Guz, Imperial College of Science, Technology & Medicine, U.K. |
3.1 Structures Materials I | |
| ICAS 2002-3.1.3 | A LINEAR 3-D FINITE ELEMENT UNIT CELL MODEL FOR FIBRE WAVINESS IN COMPOSITE MATERIALS | Gunnion, A.J. Scott, M.L., The Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Technology GPO Box 2476V, Melbourne, Victoria, 3001, Australia Thomson, Rodney S. Coopera |
3.1 Structures Materials I | |
| ICAS 2002-3.1.4 | LOAD RESPONSE AND FAILURE OF THICK RTM COMPOSITE LUGS | Markus Wallin, Olli Saarela, Helsinki University of Technology Francesco Pento, FP, Patria Finavicomp |
3.1 Structures Materials I | |
| ICAS 2002-4.1.1 | NUMERICAL SIMULATION OF ACTIVE CONTROL OF TRANSONIC FLUTTER | L. Djayapertapa & C. B. Allen Department of Aerospace Engineering, University of Bristol, Bristol, BS8 1TR, U.K. (L. Djayapertapa now at Airbus UK) |
4.1 Aeroelasticity I | |
| ICAS 2002-4.1.2 | STABILITY ANALYSIS IN THE TIME-DOMAIN APPLIED TO ADAPTIVE TRANSPORT-AIRCRAFT WINGS | Send, W., Voss, R. Institute of Aeroelasticity, German Aerospace Center (DLR) 37073 Göttingen, Germany |
4.1 Aeroelasticity I | |
| ICAS 2002-4.1.3 | NONLINEAR AEROELASTIC SIGNAL ANALYSIS OF AN AIRFOIL-AILERON COMBINATION | Alighanbari, H, Ryerson University | 4.1 Aeroelasticity I | |
| ICAS 2002-4.1.4 | ON THE NONLINEAR DYNAMICS APPROACH OF MODELING THE BIFURCATION FOR TRANSONIC LIMIT CYCLE FLUTTER | H. Matsushita * , T. Miyata * , L. E. Christiansen ** , T. Lehn-Schiøler
** , and E. Mosekilde *** * Fukui University, Fukui, Japan ** Technical University of Denmark, Lyngby, Denmark |
4.1 Aeroelasticity I | |
| ICAS 2002-3.2.1 | EFFICIENT NON-LINEAR MODELLING OF FUSELAGE PANELS | A. Murphy, M. Price, A. Gibson, C.G. Armstrong* School of Aeronautical Engineering, Queens University Belfast, Belfast, N. Ireland * School of Mechanical Engineering, Queens University Belfast, Belfast, N. Ireland |
3,2 Structural Analysis Numerical Simulation | |
| ICAS 2002-3.2.2 | NONLINEAR BUCKLING PREDICTIONS OF CURVED PANELS UNDER COMBINED COMPRESSION AND SHEAR LOADING |
Domb M M Bombardier Aerospace | 3,2 Structural Analysis Numerical Simulation | |
| ICAS 2002-3.2.3 | ANALYTICAL APPROACH TO COMPOSITE BEAM ANALYSIS | Omri Rand, Faculty of Aerospace Engineering, Technion - Israel Institute of Technology Haifa 32000, Israel. Vladimir Rovenski, Faculty of Aerospace Engineering, Technion - Israel Institute of Technology Haifa 32000, Israel. |
3,2 Structural Analysis Numerical Simulation | |
| ICAS 2002-4.2.1 | FREE FLEXURAL VIBRATION OF RECTANGULAR PLATES HAVING SINGLE CRACKS | S. D. Yu Department of Mechanical, Aerospace and Industrial Engineering Ryerson University, Toronto, Ontario, Canada M5B 2K3 | 4.2 Structural Dynamics I | |
| ICAS 2002-4.2.2 | LIMIT-CYCLE OSCILLATIONS OF AN AIRFOIL WITH PIECE-WISE LINEAR RESTORING FORCES |
Lee, B.H.K., Liu, L. Aerodynamics Laboratory National Research Council, Ottawa, Ontario, Canada Wong, Y.S. Department of Mathematical and Statistical Sciences University of Alberta, Edmonton, Alberta, Canada |
4.2 Structural Dynamics I | |
| ICAS 2002-4.2.3 | APPLICATION OF AEROELASTIC TAILORING TO ARROW WING CONFIGURATION | Hitoshi Arizono, Kyushu University | 4.2 Structural Dynamics I | |
| ICAS 2002-8.2.1 | A SEMI-ANALYTICAL NUMERICAL METHOD OF DETERMINING STRESS INTENSITY FACTORS FOR MULTIPLE SITES DAMAGE STRUCTURE | Wu Ling, Sun Qin, Dept of Aircraft Eng, Northwest Polytechnic University, Shaanxi, PR China |
8.2 Student session II | |
| ICAS 2002-3.3.1 | SERVICE LIFE OF AIRPLANE STRUCTURES | Prof. Grigory I. Nesterenko Central Aerohydrodynamic Institute (TsAGI), Russia |
3.3 Structural Integrity Damage Tolerance | |
| ICAS 2002-3.3.2 | MODELING OF FULL-SCALE AIRCRAFT STRUCTURAL TESTS | Roy L. Hewitt Institute for Aerospace Research, National Research Council Canada |
3.3 Structural Integrity Damage Tolerance | |
| ICAS 2002-3.3.3* | ANALYTICALLY-EXPERIMENTAL STUDY OF DAMAGE TOLERANCE OF AIRCRAFT STRUCTURES | Boris G. Nesterenko, Moscow Institute of Physics and Technology (st.uni), Russia |
3.3 Structural Integrity Damage Tolerance | |
| ICAS 2002-3.3.4 | FATIGUE LIFE EVALUATION OF CRITICAL LOCATIONS IN AIRCRAFT STRUCTURES USING VIRTUAL FATIGUE TEST | Jarkko Tikka Patria |
3.3 Structural Integrity Damage Tolerance | |
| ICAS 2002-4.3.1 | EFFECTS OF PRETWIST AND PRESETTING ANGLES ON FREE VIBRATION OF ELASTICALLY TAILORED ROTATING THIN-WALLED BEAMS | S-Y Oh , L. Librescu, Virginia Polytechnic Institute and State University, Department of Engineering Science and Mechanics Blacksburg, Virginia 24061, USA O. Song , Chungnam National University Mechanical Engineering Department Taejon, 305-764, Kor |
4.3 Structural Dynamics II | |
| ICAS 2002-4.3.2 | REVIEW AND OUTLOOK ON ACTIVE AND PASSIVE AEROELASTIC DESIGN CONCEPTS FOR FUTURE AIRCRAFT | Kuzmina, S., Amiryants, G., Central Aerohydrodynamic Institute (TsAGI), Russia Schweiger, J., EADS-Deutschland, Germany Cooper, J., Amprikidis, M., Sensburg, O., University of Manchester, UK |
4.3 Structural Dynamics II | |
| ICAS 2002-4.3.3 | SMART SPRING CONCEPT FOR HELICOPTER VIBRATION AND NOISE CONTROL | Zimcik, D. G., Yong, C., Wickramasinghe, V. K., National Research Council, Ottawa, Canada Nitzsche, F., Carleton University, Ottawa, Canada |
4.3 Structural Dynamics II | |
| ICAS 2002-4.3.4 | TRANSONIC STATIC AEROELASTIC SIMULATIONS OF FIGHTER AIRCRAFT | Meijer, J.J., Prananta, B.B., National Aerospace Laboratory NLR, Anthony Fokkerweg 2, 1059 CM Amsterdam, NL |
4.3 Structural Dynamics II | |
| ICAS 2002-8.3.5 | LASER VIBROMETRY BASED DETECTIONS OF DELAMINATIONS IN AEROSPACE COMPOSITES | Amraoui, M.Y., Lieven, N.A.J., Department of Aerospace Engineering, University of Bristol |
8.3 Student session III | |
| ICAS 2002-3.4.1 (I.L.) | DESIGN RULES FOR A CFRP OUTER WING | Herbeck, L., Wilmes, H., DLR - Institute of Structural Mechanics |
3.4 Structural Design Optimisation | |
| ICAS 2002-3.4.2 | OPTIMAL DESIGN OF FUSELAGE STRUCTURES | Elliott, W.G., Bombardier Aerospace Kok, L.J.J., Bombardier Aerospace |
3.4 Structural Design Optimisation | |
| ICAS 2002-3.4.3 | THE CFRP SANDWICH PANEL FOR AIRCRAFT NOSE STRUCTURE | Hirose, Y, Kosugi, K, Nishitani, M, Sashikuma, H, Imuta, M, Fukagawa,
H, Kawasaki Heavy Industries Kikukawa, H, Japan Aircraft Development Corporation |
3.4 Structural Design Optimisation | |
| ICAS 2002-3.4.4 | MULTILEVEL OPTIMIZATION OF AEROSPACE AND LIGHTWEIGHT STRUCTURES |
Fischer M., Kennedy D., Featherston C.A. Cardiff School of Engineering, Cardiff University, PO Box 925, The Parade, Cardiff CF24 0YF, United Kingdom |
3.4 Structural Design Optimisation | |
| ICAS 2002-3.4.5 | SERVICE LIFE OF A TITANIUM MAIN WING BOX FOR SECOND GENERATION SUPERSONIC COMMERCIAL TRANSPORT | Dementyev A.D.,Rodchenko T.S., Shcherban K.S TsAGI, Zhukovsky, 140180, Moscow region, Russia |
3.4 Structural Design Optimisation | |
| ICAS 2002-4.4.1 (I.L.) | AILERON FLUTTER CALCULATION FOR A SUPERSONIC FUSELAGE-WING CONFIGURATION | Guowei YANG, Shigeru OBAYASHI, Institute of Fluid Science, Tohoku University, Japan Jiro NAKAMICHI, Structures and Materials Research Center, National Aerospace Laboratory of Japan |
4.4 Aeroelasticity II | |
| ICAS 2002-4.4.2 | AEROSERVOELASTIC ROBUST MODEL DEVELOPMENT FROM FLIGHT DATA | Martin J. Brenner, MJB, NASA Dryden Flight Research Center | 4.4 Aeroelasticity II | |
| ICAS 2002-4.4.3 | AN EXPERT DATA MINING SYSTEM FOR NONLINEAR AEROELASTIC RESPONSE PREDICTION | WONG, Y. S., VOITCU, O., POPESCU, C. A., Department of Mathematical and Statistical Sciences, University of Alberta, Edmonton, Alberta, Canada, T6G 2G1. |
4.4 Aeroelasticity II | |
| ICAS 2002-4.4.4 | SUPERSONIC FLUTTER AND POST-FLUTTER CONTROL OF AN AIRCRAFT WING SECTION | MARZOCCA, P, LIBRESCU, L. Virginia Polytechnic Institute and State University, Blacksburg, VA 24061-0219, SILVA, W.A., NASA Langley Research Center, Hampton, VA 23681-2199. |
4.4 Aeroelasticity II | |
| ICAS 2002-4.4.5 | INVESTIGATION OF SHOCK-INDUCED LCO OF A WING/STORE CONFIGURATIONUSING THE TRANSONIC SMALL DISTURBANCE METHOD | F. E Eastep, N. S. Khot, P. S. Beran, J. V. Zweber and R. D. Snyder Multidisciplinary Technologies Center ,AFRL/VASD Air Force Research Laboratory (AFRL), Air Vehicle Directorate Wright-Patterson AFB, Ohio,USA 45433-7531 |
4.4 Aeroelasticity II | |
| ICAS 2002-4.6.1 (I.L.) | INVESTIGATIONS OF AIRSHIP AEROELASTICITY | Amiryants G.A., Grigoriev V.D., Ishmuratov F.Z. Central Aerohydrodynamic Institute (TsAGI), Russia Bessert N., Franz A., d’Hénin E. CargoLifter Development GmbH, Germany |
4.6 Aeroelasticity III | |
| ICAS 2002-4.6.2 | FLUID-STRUCTURE COUPLING USING CFD AND MULTIBODY SIMULATION METHODS | Krueger, W.R., Heinrich, R., Spieck, M., DLR - Deutsches Zentrum für Luft- und Raumfahrt | 4.6 Aeroelasticity III | |
| ICAS 2002-4.6.3 | RIGID BODIES IMPACTS ON WATER SURFACE. NUMERICAL AND EXPERIMENTAL ACTIVITY | Marco Anghileri. Dipartimento di Ingegneria Aerospaziale. Politecnico di Milano. Italy |
4.6 Aeroelasticity III | |
| ICAS 2002-4.6.4 | IN-FLIGHT GUST AND LOAD MEASUREMENTS ON AN AIRSHIP FOR MODEL-BUILDING AND COMPARISON WITH THE TRANSPORT AIRSHIP REQUIREMENTS | Koenig, R., German Aerospace Center Wulff, G., German Aerospace Center |
4.6 Aeroelasticity III | |
| ICAS 2002-8.6.2 | AN APPROACH TO MODELLING AND PREDICTING IMPACT DAMAGE IN COMPOSITE STRUCTURES | Rajbhandari, S.P., Scott, M.L. The Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Technology GPO Box 2476V, Melbourne, Victoria, 3001, Australia Thomson, R.S. Cooperati |
8.6 Structures & Materials II | |
| ICAS 2002-8.6.3 | EB VARESTRAINT TEST METHOD AND AN APPLICATION | M. Cemal KUSHAN 1 , Mümtaz ERDEM 2 , Tamer SARAÇYAKUPO LU 3 1 Osmangazi University, Engineering & Architecture Faculty, Dept. of Mechanical Engineering, Eski ehir/TURKEY 2 TUSA Engine Industries Inc., Eski ehir/TURKEY 3 1 st Air Supply Maintanance Com |
8.6 Structures & Materials II | |
| ICAS 2002-4.8.1 | DIAGONAL TENSION IN FIBRE-METAL LAMINATES | T. N. Alexandre Jodoin, Cheung J. Poon, George Shi, Structures, Materials and Propulsion Laboratory, Institute for Aerospace Research, National Research Council Canada, Ottawa, Ontario, Canada K1A 0R6 Paul V. Straznicky, Department of Mechanical and A |
4.8 Hybrid Materials | |
| ICAS 2002-4.8.2 | PLASTICITY CORRECTION FACTORS FOR BUCKLING OF FLAT RECTANGULAR GLARE PLATES LOADED IN COMPRESSION OR SHEAR |
Wittenberg, T. C., Delft University of Technology, The Netherlands De Jonge, A., Fokker Aerostructures B.V., The Netherlands |
4.8 Hybrid Materials | |
| ICAS 2002-4.8.3 | A HIGHER-ORDER THEORY FOR FIBER-METAL LAMINATES | Wu, X.J., Structures, Materials and Propulsion Laboratory, Institute for Aerospace Research, National Research Council of Canada |
4.8 Hybrid Materials | |
| ICAS 2002-4.9.1 | EXPERIMENTAL BUCKLING TESTS AND NUMERICAL ANALYSES OF STIFFENED CYLINDRICAL SHELLS IN COMPOSITE MATERIALS | Chiara Bisagni, Potito Cordisco, Luca Lanzi Dipartimento di Ingegneria Aerospaziale Politecnico di Milano Via La Masa 34, 20156 Milano, Italy |
4.9 Structures and Materials III | |
| ICAS 2002-4.9.2 | INTEGRATED NUMERICAL ANALYSIS FOR COMPOSITE DAMAGE TOLERANCE | Guinard, S., EADS-CCR Thévenet, P., EADS-CCR Vinet, A., EADS-CCR Maison-Le Poëc, S., EADS-CCR |
4.9 Structures and Materials III | |
| ICAS 2002-4.9.4 | ANALYSIS IF TRIAX COMPOSITES FOR SATELLITE APPLICATIONS | S.V. HOA, Concordia University, CA | 4.9 Structures and Materials III | |
| ICAS 2002-4.10.1 | NEW LIGHTWEIGHT ALLOYS FOR WELDED AIRCRAFT STRUCTURES | Blanka Lenczowski, EADS CRC Germany, Munich | 4.10 | |
| ICAS 2002-4.10.2 | AN EVALUATION OF THE PHYSICAL PROPERTIES OF ND:YAG LASER WELDED HIGH STRENGTH 6000 SERIES ALUMINUM ALLOYS |
Barry R. Leigh Bombardier Aerospace, Toronto ON M3K 1Y5 Cheung Poon National Research Council Canada, Ottawa ON K1A 0R6 Hugh W. Kerr and W.H.S. Lawson University of Waterloo, Waterloo ON N2L 3G1 Norman Ferguson Ryerson Polytechnic University, Toron |
4.10 | |
| ICAS 2002-4.10.3 | NON DESTRUCTIVE INVESTIGATION TOOLS: VALUE CREATION FOR STRUCTURAL TEST MONITORING |
Pétillon O., Simonet D., European Aeronautic Defence and Space Company - Corporate Research Centre |
4.10 | |
| ICAS 2002-4.10.4 | BEARING STRENGTH OF BOLTED JOINTS IN CFRP WING FITTINGS | GIULIO ROMEO, GIACOMO FRULLA Politecnico di Torino, Dept. of Aerospace Eng., C. Duca Abruzzi 24, 10129 Turin, Italy |
4.10 | |
| ICAS 2002-4.10.5 | DEVELOPMENT APPROACH AND TESTING OF AN UNMANNED AERIAL VEHICLE | Accardo A. F., Ricci F., Bassi P., Lega M., University of Naples Dipartimento Progettazione Aeronautica |
4.10 | |
| ICAS 2002-R2 | INTEGRATED ACTIVE FIBRES IN VIBRATION CONTROL OF HELICOPTER BLADES | Afagh, F.F.; Dept. of Mechanical & Aerospace Eng., Carleton University, Ottawa, Canada | Reserve paper | |
| ICAS 2002-R10 | PRE-STRESSED SYMMETRIC COMPOSITE BEAMS IN AIRCRAFT - ANALYSIS AND DESIGN IMPLICATIONS | David H. Chester, Department 4441, Israel Aircraft Industries Ltd., Ben-Gurion International Airport, 70100, Israel | Reserve paper | |
| ICAS 2002-R11 | BEND/TWIST COUPLING EFFECTS FOR UNSYMMETRICAL & UNBALANCED LAMINATE USED IN AIRCRAFT WING STRUCTURE ANALYSIS | Degang Cui , Zhengneng Li and Yingshu Xiu Aircraft Research Center, Beijing University of Aeronautics & Astronautics Beijing China Junyi He China Aero Information Center Beijing China |
Reserve paper | |
| ICAS 2002-R14 | EXTENSION OF REPAIR LIFETIME FOR THE CP140 BY COLD WORKING OF FATIGUED HOLES | Dr DABAYEH, Senior Aero Engineer, CA | Reserve paper | |
| ICAS 2002-R18 | AN INVESTIGATION INTO THE EFFECTS OF EXPERIMENTAL ERRORS ON THE CORRELATION BETWEEN FEA AND TEST RESULTS FOR A WELDED FUSELAGE PANEL | J. Shah, A. Gibson, M. Price School of Aeronautical Engineering, Queen’s University of Belfast, Belfast, UK |
Reserve paper | |
| ICAS 2002-R32 | THE INFLUENCE OF MULTIPLE NESTED LAYER WAVINESS ON COMPRESSION STRENGTH OF CARBON FIBER COMPOSITE MATERIALS | Zaffar. M. Khan Advanced Engineering Research Organization, Wah Cantt, PAKISTAN |
Reserve paper | |
| ICAS 2002-R34 | NUMERICAL MODELLING OF LOW-VELOCITY IMPACT DAMAGE IN FIBRE-METAL-LAMINATES | Laliberté, J., Poon, C. IAR-SMPL National Research Council Canada, 1200 Montreal Road, Ottawa, ON K1A 0R6, Canada Straznicky, P.V. Department of Mechanical and Aerospace Engineering, Carleton University, 1125 Colonel By Drive, Ottawa, ON K1S 5B6, Ca |
Reserve paper | |
| ICAS 2002-R36 | SIGNAL SUBSPACE IDENTIFICATION & NOISE REDUCTION OF FLIGHT TEST DATA WITH TRUNCATED SINGULAR VALUE DECOMPOSITION | T M Lee, RMIT University, Australia | Reserve paper | |
| ICAS 2002-R42 | FATIGUE LIFE PREDICTION OF 3-D PROBLEMS BY DAMAGE MECHANICS WITH SPECTRUM LOADING | Iqbal Rasool Memon, Xing Zhang* and Deyu Cui* Department of Aerospace, College of Aeronautical Engineering, National University of Science and Technology, Pakistan *Department of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeron |
Reserve paper | |
| ICAS 2002-R47 | DYNAMIC MODELING AND TIME DOMAIN SIMULATION OF NON-LINEAR FLUTTER WITH THE EXISTENCE OF FREE-PLAY MECHANISM | C P PAGWIWOKO, University of Science Malaysia. | Reserve paper | |
| ICAS 2002-R54 | AN EXPERIMENTAL METHODOLOGY FOR EVALUATING SURVIVABILITY OF AN AERONAUTICAL CONSTRUCTIONS FROM COMPOSITE MATERIALS | Rasuo B., University of Belgrade, Aeronautical Department, Faculty of Mechanical Engineering |
Reserve paper | |
| ICAS 2002-R61 | INNOVATIVE TECHNIQUES FOR THE FINITE ELEMENT ANALYSIS AND OPTIMISATION OF COMPOSITE STRUCTURES | McMahon, C.D., Scott, M.L. The Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Technology GPO Box 2476V, Melbourne, Victoria, 3001, Australia |
Reserve paper | |
| ICAS 2002-R63 | ROBUST FLUTTER MARGINS OF A TYPICAL WING SECTION USING WINDTUNNEL EXPERIMENT DATA : A PRELIMINARY STUDY | H.Y.Sutarto, Rianto A.S., Zaki S., L.Gunawan Vibration And Control Laboratory Department of Aerospace Engineering Institute Of Technology Bandung Indonesia |
Reserve paper | |
| ICAS 2002-R65 | ACTIVE VIBRATION CONTROL OF A SMART PLATE | Yavuz Yaman, Tarkan Çaliskan Department of Aerospace Engineering, Middle East Technical University, 06531, Ankara, Turkey Eswar Prasad, David Waechter Sensor Technology Limited P. O. Box 97, Stewart Road, Collingwood, Ontario, Canada L9Y3Z4 |
Reserve paper | |
| ICAS 2002-R67 | THIRTY YEARS OF RETROGRESSION AND REAGING | Wu, X.J., Raizenne, M.D, Chen, W.R., Poon, C., and Wallace, W., Institue
for Aerospace Research, National Research Council of Canada. |
Reserve paper | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-5.8.2 | VORTEX BREAKDOWN CONTROL FOR REDUCED COMBUSTION PRESSURE PULSATIONS | C. O. Paschereit, P. Flohr, W. Geng, ALSTOM (Switzerland) Ltd, CH-5405 Baden, Switzerland E. Gutmark, Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati, OH 45221, USA |
5.8 Combustion | |
| ICAS 2002-5.8.3 | STRESS INTENSITY FACTOR CALCULATIONS FOR CRACKS EMANATING FROM BOLT HOLES IN A JET ENGINE COMPRESSOR DISC | Beres, W., Institute for Aerospace Research, National Research Council Canada, Ottawa, Ontario, Canada Koul, A.K., Life Prediction Technologies, Inc., Ottawa, Ontario, Canada |
5.8 Combustion | |
| ICAS 2002-5.9.1 | NEW TECHNOLOGIES FOR EFFICIENT AND ENVIRONMENTALLY FRIENDLY AERO ENGINES | Scheugenpflug, H., MTU Aero Engines GmbH Wilfert, G., MTU Aero Engines GmbH Pickard, N., Rolls-Royce plc Massè, B., Snecma Moteurs |
5.9 Engine Modeling and Optimization | |
| ICAS 2002-5.9.2 | CONCEPTUAL DESIGN OF AIRCRAFT ENGINE USING MULTIDISCIPLINARY DESIGN OPTIMIZATION TECHNIQUE | Tomoaki Asako, Ishikawajima-Harima Heavy Industries Co.,Ltd. Hiroshi Miyagawa, Ishikawajima-Harima Heavy Industries Co.,Ltd. Satoshi Miyata, Engineous Japan, Inc. Keiji Kudo, Engineous Japan, Inc. |
5.9 Engine Modeling and Optimization | |
| ICAS 2002-5.9.3 | MODELING PROPULSION SYSTEM OF A SUBSONIC CIVIL JET AIRCRAFT FOR MULTIDISCIPLINARY CONCEPTUAL DESIGN OPTIMIZATION | Vivek Sanghi, Engine Simulation Group, Gas Turbine Research Establishment,
Bangalore-560 093, India. S.K. Sane, Department of Aerospace Engineering, Indian Institute of Technology, Mumbai-400 076, India. |
5.9 Engine Modeling and Optimization | |
| ICAS 2002-5.9.4 | ADAPTIVE SELECTION OF PARETO OPTIMAL ENGINE TECHNOLOGY SOLUTION SETS | Roth, B. A., Graham, M., Mavris, D.N., Georgia Institute of Technology, Atlanta, GA 30332-0150 |
5.9 Engine Modeling and Optimization | |
| ICAS 2002-5.10.1 | ON HAMMERSHOCK PROPAGATION IN A SUPERSONIC FLOW FIELD | A. Robert Porro, ARP, National Aeronautics and Space Administration, Glenn Research Center, Cleveland, OH 44135, USA | 5.10 Inlets, Propellers and Compressor CFD | |
| ICAS 2002-5.10.3 | A STAGE CALCULATION IN A CENTRIFUGAL COMPRESSOR | Wallis, CV, Moussa, ZM, Srivastava, BN, General Electric Aircraft Engines |
5.10 Inlets, Propellers and Compressor CFD | |
| ICAS 2002-5.10.4 | THE AERODYNAMIC DESIGN OF AN OPTIMISED PROPELLER FOR A HIGH ALTITUDE LONG ENDURANCE UAV | Monk, J.S. , Defencetek, CSIR | 5.10 Inlets, Propellers and Compressor CFD | |
| ICAS 2002-5.10.5 | ENGINE INTAKE DOWNWASH FOR REAR FUSELAGE MOUNTED NACELLES | R. Slingerland, N.L.S. Moonen Faculty of Aerospace Engineering Department of Flight Mechanics and Propulsion Delft University of Technology P.O. Box 5058, 2600 GB Delft, The Netherlands |
5.10 Inlets, Propellers and Compressor CFD | |
| ICAS 2002-5.11.1 | RESEARCH ON APPLICATION OF CERAMIC TURBINE TO JET ENGINE | Hiroaki Hasegawa ,Yoshiaki Tsukamoto Technical Research & Development Institute, Japan Defense Agency Tadayuki Hanada Nagoya Guidance & Propulsion Systems, Mitsubishi Heavy Industries, LTD Katsuhiko Takita Nagasaki Research & Development Center, Mits |
5.11 Turbines | |
| ICAS 2002-5.11.2 | PERFORMANCE CHARACTERISTICS OF A REDUCED SOLIDITY LOW PRESSURE TURBINE | Solomon, W. J., GE Aircraft Engines | 5.11 Turbine | |
| ICAS 2002-5.11.3 | FLOWFIELD UNSTEADINESS AND TURBULENCE IN MULTISTAGE LOW PRESSURE TURBINES | D.E. HALSTEAD, GE Aircraft Engines, US | 5.11 Turbine | |
| ICAS 2002-5.11.4 | IMPACT OF FLOW QUALITY IN TRANSONIC CASCADE WIND TUNNELS: MEASUREMENTS IN AN HP TURBINE CASCADE | Corriveau, D., Carleton University Sjolander, S.A., Carleton University |
5.11 Turbine | |
| ICAS 2002-R4 | PARAMETRIC BASED AERODYNAMIC DESIGN OF PERFORMANCE ENHANCING BLADING SYSTEMS | Bayandor, J., The Sir Lawrence Wackett Centre for Aerospace Design Technology, Department of Aerospace Engineering, Royal Melbourne Institute of Technology | Reserve paper | |
| ICAS 2002-R57 | EXERGY BASED LOSS ANALYSIS OF A TURBOJET OVER A FLIGHT CYCLE | M A Rosen, Ryerson University, Canada | Reserve paper | |
| ICAS 2002-R64 | VALIDATION OF ANALYTIC TOOL FOR SUBSCALE PROPELLER TESTS | J Syms, National Research Council Canada | Reserve paper |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-5.1.1 | THE EFFECT OF AIRCRAFT BIASES ON THE DELIVERY OF AN ENHANCED LASER-GUIDED WEAPON | Ralph J. F. Department of Electrical Engineering and Electronics, The University of Liverpool, Brownlow Hill, Liverpool, L69 3GJ, United Kingdom. Edwards K. L. Avionics and Vetronics Centre, Sensors and Electronics Division, QinetiQ Ltd., Farnborou |
5.1 Flight Dynamics of Spacecraft and Missiles | |
| ICAS 2002-5.1.2 | 3D-SIMULATION OF NONLINEAR DYNAMICS FOR A REENTRY VEHICLE | Norihiro GOTO, Takashi KAWAKITA, Kyushu University, Japan |
5.1 Flight Dynamics of Spacecraft and Missiles | |
| ICAS 2002-5.1.3 | TRAJECTORY OPTIMIZATION OF SPACE PLANE USING GENETIC ALGORITHM COMBINED WITH GRADIENT METHOD | Yokoyama N. (University of Tokyo) | 5.1 Flight Dynamics of Spacecraft and Missiles | |
| ICAS 2002-5.1.4 | DESIGN OF MISSILE'S GUIDANCE SYSTEM BASED ON COMBINATION OF OPTIMAL PRESET AND A TRANSCRIPTION OF FUNCTIONAL GUIDANCE | M.R. JAHED-MOTLAGH, University of Sciences and Technology, IR | 5.1 Flight Dynamics of Spacecraft and Missiles | |
| ICAS 2002-5.2.1 | FLYING QUALITIES ANALYSIS OF A THREE SURFACES AIRCRAFT MODEL | Coiro P. D., Nicolosi F., De Marco A., Genito N., University of Naples
"Federico II", Dipartimento di Progettazione Aeronautica (DPA) Nicolosi F., De Marco A., Genito N., |
5.2 Flight Dynamics of Light Aircraft | |
| ICAS 2002-5.2.2 | A LOW COST FLIGHT TEST INSTRUMENTATION PACKAGE FOR LIGHT AIRPLANES | Eggleston B., McKinney W.D., Choi N.C., Min D. Found Aircraft of Canada |
5.2 Flight Dynamics of Light Aircraft | |
| ICAS 2002-5.2.3 | THEORETICAL, EXPERIMENTAL AND IN-FLIGHT SPIN INVESTIGATIONS FOR AN EXECUTIVE LIGHT AIRPLANE | Goraj Z., Baron A., Institute of Aviation, Warsaw, Poland |
5.2 Flight Dynamics of Light Aircraft | |
| ICAS 2002-5.3.1 | FEEDBACK STABILISED BIFURCATION TAILORING APPLIED TO AIRCRAFT MODELS | Charles, G.A., Wang, X.F., Stoten, D.P., Mechanical Engineering, University of Bristol. Lowenberg, M.H., Aerospace Engineering, University of Bristol. Di Bernardo, M., Engineering Mathematics, University of Bristol. |
5.3 Aircraft Control and Handling | |
| ICAS 2002-5.3.2 | AERODYNAMIC AND FLIGHT DYNAMIC REAL-TIME ANALYSIS DURING SPIN AND CAREFREE MANEUVERING TESTS OF THE SAAB JAS39 GRIPEN | Klas Andersson , Mats Karlsson , Mårten Staaf Saab AB (publ), S-581 88 Linköping, Sweden |
5.3 Aircraft Control and Handling | |
| ICAS 2002-5.3.3 | DEVELOPMENT OF A HANDLING QUALITIES EVALUATION TOOLBOX ON THE BASIS OF GIBSON CRITERIA | Hendarko, Institute of Technology Bandung, Indonesia | 5.3 Aircraft Control and Handling | |
| ICAS 2002-5.3.4 (I.L.) | HIGH ANGLE OF ATTACK APPROACH AND LANDING CONTROL LAW DESIGN FOR THE X-31A | B. Fischer and Dr. A. Knoll European Aeronautic Defense and Space Company Military Aircraft Flight Dynamics 81663 Munich, Germany |
5.3 Aircraft Control and Handling | |
| ICAS 2002-8.3.1 | RE-ENTRY MOTION OF AN AXIALSYMMETRIC VEHICLE AND ITS ANALYSIS BASED ON FLIGHT SIMULATION | A. Guidi Delft University of Technology, Delft, The Netherlands |
8.3 Student session III | |
| ICAS 2002-8.3.2 | CAPTIVE CARRY TESTING AS A MEANS FOR RAPID EVALUATION OF UAV HANDLING QUALITIES | Munro, C., Linkoping University, Sweden. Krus, P., Linkoping University, Sweden. Llewellyn, E., University of Bristol, England |
8.3 Student session III | |
| ICAS 2002-8.3.3 | SMALL LEADING-EDGE FLAP FOR POST-STALL FLOW CONTROL ON A 45-DEG DELTA WING | Takashi Matsuno, Shigeru Yokouchi, Yoshiaki Nakamura, Department of Aerospace Engineering, Nagoya University, 464-8603 Nagoya, JAPAN |
8.3 Student session III | |
| ICAS 2002-5.4.1 (I.L.) | LINEAR, PARAMETER-VARYING CONTROL AND ITS APPLICATION TO AEROSPACE SYSTEMS | Gary J. Balas Aerospace Engineering, University of Minnesota Minneapolis, MN 55455 |
5.4 Robust Control | |
| ICAS 2002-5.4.2 | ROBUSTIFICATION OF AN H2 AUTOPILOT FOR FLEXIBLE AIRCRAFT BY SELF-SCHEDULING BASED ON MULTI-MODEL EIGENSTRUCTURE ASSIGNMENT | Constant, G.; SUPAERO, ONERA/DCSD Chable, S.; ONERA/DCSD, SUPAERO Chiappa, C.; SUPAERO, ONERA/DCSD Doll, C.; ONERA/DCSD, SUPAERO SUPAERO : 10 av E. Belin, B.P. 4032, F-31055 Toulouse Cedex 4, France ONERA/DCSD: 2 av E. Belin, B.P. 4025, F-31055 To |
5.4 Robust Control | |
| ICAS 2002-5.4.3 | ROBUST FLIGHT CONTROL : A REAL TIME SIMULATION INVESTIGATION | D Harman and H H T Liu, Institute for Aerospace Studies, University of Toronto, Ontario, Canada | 5.4 Robust Control | |
| ICAS 2002-5.4.4 | DESIGN OF STABILIZING AND LOCALLY-ROBUST NONLINEAR CONTROLLERS FOR A CLASS OF NONLINEAR SYSTEMS | Amitabh Saraf Postgraduate Researcher, Henry Samueli School of Engineering 4200 Engineering Gateway, University of California, Irvine, CA 92697-3975 |
5.4 Robust Control | |
| ICAS 2002-5.4.5 | LATERAL FLIGHT CONTROL SYSTEM USING OPTIMAL H-INFINITY CONTROLLERS | Adrian Stoica University "Politehnica" of Bucharest, Faculty of Aerospace
Engineering, Str. Splaiul Independentei, no. 313, Ro-77206, Bucharest, Romania |
5.4 Robust Control | |
| ICAS 2002-5.5.1 (I.L.) | FLIGHT DYNAMICS OF SMALL VEHICLES | Steven Ho 1* , Hany Nassef 1 , Nick Pornsin-Sirirak 2 , Yu-Chong Tai 2
, Chih-Ming Ho 1 1 Mechanical and Aerospace Engineering Department, University of California Los Angeles 2 California Institute of Technology |
5.5 Flight Dynamics of Small Vehicles | |
| ICAS 2002-5.5.2 | MODELING OF THE NONLINEAR DYNAMIC BEHAVIOR OF A MICRO-AERIAL-VEHICLE (MAV) IN AN ENVIRONMENT OF A TURBULENT ATMOSPHERE | Kordes, T.,Buschmann, M.,Vörsmann, P., Institute of Aerospace Systems, Technical University of Braunschweig, Braunschweig, Germany |
5.5 Flight Dynamics of Small Vehicles | |
| ICAS 2002-5.5.3 | A STUDY OF FLIGHT DYNAMICS AND AUTOMATIC CONTROL OF AN ANIMALOPTER | Lasek M., Pietrucha J., Zlocka M. Warsaw University of Technology, Nowowiejska 24, 00-665 Warsaw; Sibilski K. Air Force Institute of Technology, Ks. Boleslawa 6, 01-495 Warsaw |
5.5 Flight Dynamics of Small Vehicles | |
| ICAS 2002-5.6.1 (I.L.) | APPLICATION OF ESTOL FLIGHT CONTROL TECH-NOLOGY TO UCAV DESIGN | A. Knoll, B. Fischer EADS Military Aircraft |
5.6 Flight Dynamics of UAV’s | |
| ICAS 2002-5.6.2 | AN AUTONOMOUS CONTROL TECHNIQUE FOR LAUNCHING SHIP BASED UNMANNED AIR VEHICLES (UAVS) IN EXTREME CONDITIONS | Crump, M.R., Bil, C., Sir Lawrence Wackett Center for Aerospace Design Technology, RMIT University |
5.6 Flight Dynamics of UAV’s | |
| ICAS 2002-5.6.3 | DESIGN OF A SHIPBOARD RECOVERY SYSTEM FOR A SHROUDED-FAN UAV | G. Avanzini, Turin Polytechnic G. de Matteis, University of Rome "La Sapienza" | 5.6 Flight Dynamics of UAV’s | |
| ICAS 2002-5.6.4 | REAL TIME SHIP MOTION CRITERIA FOR MARITIME HELICOPTER OPERATIONS | Colwell, J.L., Defence R&D Canada - Atlantic | 5.6 Flight Dynamics of UAV’s | |
| ICAS 2002-5.7.1 | MINIMISING THE RISK OF COLLATERAL DAMAGE WITH THE KALMAN-LEVY FILTER | Sims S. W., Ralph J. F. Department of Electrical Engineering and Electronics, The University of Liverpool, Brownlow Hill, Liverpool, L69 3GJ, United Kingdom. Edwards K. L. Avionics and Vetronics Centre, Sensors and Electronics Division, QinetiQ Ltd |
5.7 Flight Control | |
| ICAS 2002-5.7.2 | NONLINEAR CONTROL LAW DESIGN FOR AUTO-FLARE | F. MORA-CAMINO, LAAS-CNRS and ENAC, FR | 5.7 Flight Control | |
| ICAS 2002-5.7.3 | DETECTION AND ISOLATION OF CONTROL SURFACE EFFECTIVENESS LOSS IN AIRCRAFT BY USING FILTER BANK APPROACH | Zongji Chen & Weiqee Li Beijing University of Aeronautics and Astronautics 100083, Beijing, China |
5.7 Flight Control | |
| ICAS 2002-5.7.4 | CONTROL LAW SYNTHESIS FOR AIRCRAFT AUTOPILOT WITH NONLINEAR ELEMENTS | SZABOLCSI Róbert, Miklós Zrínyi National Defense University, Department of Aircraft Onboard Systems, H-5008 Szolnok, POB 1, Hungary | 5.7 Flight Control | |
| ICAS 2002-5.7.5 | A FUZZY LOGIC AUTOPILOT DEVELOPMENT FOR A LIGHT TWIN ENGINE AIRCRAFT IN THE APPROACH FLIGHT CONDITION | Ceruti A. , Rossi V., Saggiani G. M. Aerospace Engineering Department - University of Bologna |
5.7 Flight Control | |
| ICAS 2002-3.9.5 | MATHEMATICAL MODELLING AND ACTIVE CONTROL OF OSCILLATORS. APPLICATION TO BUFFET AND TO COMPRESSOR SURGE. | Alain Le Pourhiet, Michel Corrège, Daniel Caruana, ONERA, 2 av. Édouard-Belin, 31400 Toulouse, France |
3.9 Flow Control | |
| ICAS 2002-R12 | NUMERICAL MODEL OF SINGLE MAIN ROTOR HELICOPTER DYNAMICS | Dragan Cvetkovi?, Ivan Kosti?, ?aslav Mitrovi?, Aleksandar Bengin, Faculty
of Mechanical Engineering, University of Belgrade, 27. Marta St. 80, 11000
Belgrade, Yugoslavia Duko Radakovi?, Federal Bureau for Measures and Precious Metals, Mike Alasa St. 1 |
Reserve paper | |
| ICAS 2002-R19 | EXTREME LOADS OF A TRAINER JET FOLLOWING A SUDDEN DEFLECTION OF CONTROL SURFACE | Goraj Z., Warsaw University of Technology, Warsaw, Poland Olejnik A., Military University of Technology, Warsaw, Poland |
Reserve paper | |
| ICAS 2002-R22 | AERODYNAMIC MODEL IDENTIFICATION OF THE N-250 AIRCRAFT BASED ON FLIGHT | Dr H MUHAMMAD, Aerospace Eng.Dept.,Inst. Of Tech. Bandung, ID | Reserve paper | |
| ICAS 2002-R26 | RECONFIGURABLE CONTROL OF AN EXPERIMENTAL UNMANNED AIR VEHICLE (UAV) | M. HUZMEZAN, Deprtament of Electricam and Computer Engineering, University of British Columbia, CA | Reserve paper | |
| ICAS 2002-R31 | FLIGHT TRAJECTORIES OPTIMIZATION | Sherzada Khan College of Aeronautical Engineering, PAF Academy, Risalpur, National University of Science and Technology, Pakistan |
Reserve paper | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-8.1.2 | HYBRID TWO-LEVEL GENETIC OPTIMIZATION ALGORITHM WITH DIFFERENT FIDELITY MODELS FOR AERODYNAMIC DESIGN PROBLEMS | Ivan L. Chernyshev Central Aerohydrodynamic Institute (TsAGI), Zhukovsky, Russia |
8.1 Student session I | |
| ICAS 2002-8.3.4 | THERMODYNAMIC DESIGN OF AN ALTERNATIVE MONOPROPELLANT FOR EMERGENCY POWER UNITS | Shin Matsumura, John J. Rusek, Department of Aeronautics and Astronautics Purdue University |
8.3 Student session III | |
| ICAS 2002-6.4.1 (I.L.) | ULTRA EFFICIENT ENGINE TECHNOLOGY PROGRAM | R Shaw, Nasa, US | 6.4 ISOABE II | |
| ICAS 2002-6.4.2 (I.L.) | PROGRAM OVERVIEW AND INTERMEDIATE ACHIEVEMENTS OF "RESEARCH AND DEVELOPMENT
OF ENVIRONMENTALLY COMPATIBLE PROPULSION SYSTEM FOR NEXT-GENERATION SUPERSONIC TRANSPORT(ESPR PROJECT) |
Yuji Tokumasu, Medical and Welfare Equipment Technology Dept. Industrial Science and Technology Policy and Environment Bureau, Ministry of Economy, Trade and Industry(METI) Yukihiro Hata, Applied Technology Development Dept., New Energy and Industr |
6.4 ISOABE II | |
| ICAS 2002-6.4.3 (I.L.) | AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN | Gérard LARUELLE, EADS LAUNCH VEHICLES | 6.4 ISOABE II | |
| ICAS 2002-6.4.4 (I.L.) | MODELING OF NOX FORMATION IN GAS TURBINE COMBUSTORS | N. RIZK, ROLLS ROYCE, US | 6.4 ISOABE II | |
| ICAS 2002-6.4.5 (I.L.) | T.B.D | W. SMITH, PRATT & WITHNEY, US | 6.4 ISOABE II | |
| ICAS 2002-7.4.1 (I.L.)+C672 | A FAST AND PRECISION INITIAL ALIGNMENT METHOD FOR SINS ON STATIONARY BASE | Xinlong Wang, Gongxun Shen Beijing University of Aeronautics and Astronautics, Beijing, P.R. China |
7.4 Avionic Systems I | |
| ICAS 2002-7.4.2 | FAST CALIBRATION TECHNIQUE FOR A GIMBALLED INERTIAL NAVIGATION SYSTEM | Shin, Y. J., Park, J. H., Agency for Defense Development Kim, C. J., Korea Aerospace Research Institute |
7.4 Avionic Systems I | |
| ICAS 2002-7.4.3 | NON-LINEAR STRUCTURES FOR STABILISATION- AND PRECESSION AXIS COUPLING OF THE ORIENTATION AND STABILISATION GYROSYSTEMS | Lungu, R. -Avionics Division, University of Craiova, Romania | 7.4 Avionic Systems I | |
| ICAS 2002-7.4.4 | SIMULATION OF TERRAIN REFERENCE NAVIGATION SYSTEM BASED ON IMAGE MATCHING FROM DIGITAL VIDEO CAMERA | ZASUWA M., NARKIEWICZ J., Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology, Warsaw, Poland |
7.4 Avionic Systems I | |
| ICAS 2002-7.4.5 | LOW-COST 3D-DISPLAY SYSTEM FOR LIGHT AIRCRAFT | Sachs, G., Sperl, R., Technische Universitt Mnchen, Boltzmannstr. 15, 85748 Garching, Germany | 7.4 Avionic Systems I | |
| ICAS 2002-6.5.4 | FOSTERING INNOVATION ACROSS SUPPLIER NETWORKS CHALLENGES AND OPPORTUNITIES | K. BOZDOGAN, MIT, US | 6.5 Management of R & D | |
| ICAS 2002-6.7.1 | AN INTEGRATED MODULAR TEST RIG FOR LANDING GEAR FATIGUE AND STRENGTH TESTING | Schmidt, RK, Messier-Dowty Inc. | 6.7 System Testing | |
| ICAS 2002-6.7.2 | VIRTUAL LABORATORIES FOR SPACE ROBOTICS | K. SCHILLING, Univ. of Applied Sciences, DE | 6.7 System Testing | |
| ICAS 2002-6.7.3 | LOAD SIMULATOR BASED ON THE PRINCIPLE OF HYDROSTATIC SECONDARY CONTROL | Zongxia Jiao, Xiaodong Wang Automation Science and Electric Engineering College Beijing University of Aeronautics and Astronautics, Beijing 100083, China Monika Ivantysynova Institute for Aircraft Systems Engineering, Technische Universität Hamburg |
6.7 System Testing | |
| ICAS 2002-6.8.1 | OPTICAL DESIGN OF TWO FIELD OF VIEW INFRA-RED OBJECTIVE IN 3-5 MICRON BAND FOR FOCAL PLANE ARRAY DETECTOR | MUHAMMAD HAMMAD ASGHAR, ADVANCE ENGINEERING RESEARCH ORGANIZATION (AERO), E-5, OFFICERS COLONY, WAH CANTT 47040. PAKISTAN | 6.8 Avionic Systems II | |
| ICAS 2002-6.8.2 | A MISSION PLANNER AND NAVIGATION SYSTEM FOR THE ARARA PROJECT | Trindade, Jr. O; Barbosa, L. C. P; Neris, L.O; Jorge, L.A.C. ICMC - Math and Computer Science Institute University of São Paulo - Brazil |
6.8 Avionic Systems II | |
| ICAS 2002-6.8.3 | SEMI-AUTOMATIC 3D FLIGHT SIMULATORSCENARIOS RECONSTRUCTION FROM GEOREFERENCED AERIAL PHOTOS AND TERRESTRIAL MAPS | A. Liverani, F. Persiani, G. Piraccini, M. Tappi DIEM - Università di Bologna, v.le Risorgimento, 2, 40136 Bologna – Italy |
6.8 Avionic Systems II | |
| ICAS 2002-6.8.4 | ROBUST INTEGRATED INS/RADAR ALTIMETER ACCOUNTING FAULTS AT THE MEASUREMENT CHANNELS | Chingiz Hajiyev, Remzi Saltoglu, Istanbul Technical University |
6.8 Avionic Systems II | |
| ICAS 2002-5.10.2 | COMPRESSOR TECHNOLOGY FROM INNOVATION TO ECONOMICS | K. BROICHHAUSEN, MTU, DE | 5.10 Inlets, Propellers and Compressor CFD | |
| ICAS 2002-6.10.1 | MULTIDISCIPLINARY DESIGN OPTIMISATION FOR EMBEDDED SENSOR DESIGNS | Abbott, E.A., Scott, M.L. The Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Technology GPO Box 2476V, Melbourne, Victoria, 3001, Australia |
6.10 System Design I | |
| ICAS 2002-6.10.2 | ACTIVE FAULT-TOLERANT CONTROL SYSTEM DESIGN FOR A TWO-ENGINE BLEED AIR SYSTEM OF AN AIRCRAFT | Bao, G., Jiang, J.,The University of Western Ontario, London, Ontario,
Canada Liu, G., Ryerson University, 350 Victoria Street, Toronto, Ontario, Canada Lam, C. H., Honeywell Engines & Systems (Toronto), Ontario, Canada |
6.10 System Design I | |
| ICAS 2002-6.10.3 | THE DESIGN AND DEVELOPMENT OF THE AIRBUS A380 MAIN LANDING GEARS | P. VANDERPOL, Landing Gear Goodrich Corporation, CA | 6.10 System Design I | |
| ICAS 2002-6.10.4 | SYSTEMS INTEGRATION – AIRBUS APPROACH | R. SMYTH, AIRBUS France, FR | 6.10 System Design I | |
| ICAS 2002-8.11.1 | ENVIRONMENTAL ISSUES ADDDRESSED AND PROGRESS MADE UNDER THE HIGH SPEED CIVIL TRANSPORT (HSCT) PROGRAM | A. WILHITE, University of Alabama, US | 8.11 SAE Session II | |
| ICAS 2002-R28 | A METHOD TO DERIVE THE USAGE OF HYDRAULIC ACTUATORS FROM FLIGHT DATA | H. Kannemans, H.W. Jentink National Aerospace Laboratory, NLR Anthony Fokkerweg 2, 1059 CM Amsterdam, The Netherlands |
Reserve paper | |
| ICAS 2002-R37 | CONTROL INTEGRATION PROCESS IN AIRCRAFT SYSTEMS DEVELOPMENT | Hugh H T Liu and Anton de Ruiter, Inst for Aerospace Studies, University of Toronto, Ontario, Canada. | Reserve paper | |
| ICAS 2002-R45 | TRAJECTORY MODELING ACCURACY FOR AIR TRAFFIC MANAGEMENT DECISION SUPPORT TOOLS | Stephane Mondoloni, Mike Paglione, Steve Green (CSSI Inc., FAA WHJTC, NASA Ames) |
Reserve paper | |
| ICAS 2002-R55 | TORQUE CONTROL SYSTEM BASED ON COMPOUND CONTROL STRATEGIES FOR AERODYNAMIC LOAD SIMULATOR | Z. REN, Beijing Univ. of Aeronautics and Astronautics, PRC | Reserve paper | |
| ICAS 2002-R71 | ADAPTIVE MODELING AND OPTIMIZATION OF PILOT HELMETS FOR DIFFERENT KINDS OF IMPACTS WITH HARD OBSTACLES | ?aslav Mitrovi ? , Ivan Kosti ? , Dragan Cvetkovi ? , Aleksandar Bengin Faculty of Mechanical Engineering, University of Belgrade Aeronautical Engineering Department, 27.marta St. 80 11 000 Belgrade, F.R. of Yugoslavia |
Reserve paper | |
| ICAS 2002-R73 | A SYSTEM FRAMEWORK FOR THE DESIGN OF AN AVIONICS ARCHITECTURE WITH UPGRADE POTENTIAL – AVIONICS ARCHITECTURE ANALYSIS MODULE | Rao, N., Sinha, A.K., Kusumo, R. Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Technology GPO Box 2476V, Melbourne, Victoria, 3001, Australia. |
Reserve paper | |
| ICAS 2002-R75 | SPEED CONTROL ISSUES OF 3D-TUNNEL/PREDICTOR DISPLAYS | Sachs, G., Sennes, U., Technische Universitt Mnchen Boltzmannstr. 15, 85748 Garching, Germany |
Reserve paper | |
| ICAS 2002-R77 | PROPOSALS AND COMPARATIVE EVALUATION OF SYNTHETIC NONLINEAR MODELS IN FLIGHT CONTROLS SIMULATION | Borello L., Villero G. Department of Aerospace Engineering - Politecnico di Torino Corso Duca degli Abruzzi 24 – 10129 TORINO |
Reserve paper | |
| ICAS 2002-R78 | HELICOPTER HYDRAULIC SYSTEM (Design, Component Selection, Modular Construction, Integration & Testing) |
VISWANATH. S, NAGARAJAN. R, Hydraulics Group, Rotary Wing Research & Design Centre, Hindustan Aeronautics Limited, Bangalore, India |
Reserve paper | |
| ICAS 2002-R80 | APPLICATION OF FAULT DIAGNOSIS EXPERT SYSTEM FOR AIRCRAFT ELECTRIC POWER SYSTEM | ZHU XinYu (China Civil Aviation Flight College, Guanghan City 618307) SHEN SongHua (Beijing University of Aeronautical and Astronautical, Beijing City 100083) |
Reserve paper | |
| ICAS 2002-P5 | USING DATA MINING METHOD FOR ANALYZING OTS CAPTURE ZONE | Jinsong GAO (Department of Electronic Engineering, Northwest Polytechnical University, Xi’an 710072, China ) Longhe SUN and Guangshan LU (Electro-Optical Equipment Research Institute, Luoyang 471009, China) |
Poster Session | |
| ICAS 2002-P7 | REAL-TIME, DISTRIBUTED, PARALLEL SIMULATION OF HYDRAULIC SYSTEM BASED ON LINUX IN THE NETWORK | Li Kun, Jiao Zongxia College of Automation Science and Electrical Engineering Beijing University of Aeronautics and Astronautics Beijing 100083 P. R. China |
Poster Session | |
| ICAS 2002-P8 | THE VERFICATION OF FLIGHT TEST FOR AIORBORNE ELECTRO-OPTICAL DETECTING SYSTEM | Li Zhaohui Chinese Flight Test Establishment |
Poster Session | |
| ICAS 2002-P11 | AVIONICS DATA COMMUNICATION NETWORK MODELING AND ANALYSING | Song Hailang., Flight Test Establishment of China | Poster Session | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-6.1.1 (I.L.) | JOINT STRIKE FIGHTER (JSF) DEVELOPMENT FOCUSING ON REDUCED LIFECYCLE COSTS | M.L. FORTSON, Lockheed Martin Aeronautics Company, US | 6.1 Integrated Product Development I | |
| ICAS 2002-6.1.2 | A FRAMEWORK FOR ACHIEVING LIFECYCLE VALUE IN AEROSPACE PRODUCT DEVELOPMENT | Alexis Stanke, Earll Murman Massachusetts Institute of Technology |
6.1 Integrated Product Development I | |
| ICAS 2002-6.1.3 | COMMON DEVELOPMENT TOOLS FOR AN INTEGRATED DECISION SUPPORT SYSTEM FOR MID-LIFE UPGRADE ANALYSIS | Kusumo, R., Sinha, A.K. Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Technology GPO Box 2476V, Melbourne, Victoria, 3001, Australia. |
6.1 Integrated Product Development I | |
| ICAS 2002-6.2.1 (I.L.)+C546 | SOME MANUFACTURING ACTIVITIES IN JAPANESE AIRCRAFT INDUSTRIES (JAI) | Yoichi Sugimura, Japan Aircraft Development Corporation | 6.2 Manufacturing I | |
| ICAS 2002-6.2.2 | A HOLISTIC APPROACH TO MANUFACTURING SYSTEM DESIGN IN THE DEFENSE AEROSPACE INDUSTRY | Vaughn, A.F., Shields, J.T., Lean Aerospace Initiative, MIT |
6.2 Manufacturing I | |
| ICAS 2002-6.2.3 | COST AND CYCLES REDUCTION BASED ON MANUFACTURING PROCESS SIMULATION | Dominique DELOISON, Didier GUEDRA-DEGEORGES Albert ABISROR, Gilles MARIN,
EADS CCR |
6.2 Manufacturing I | |
| ICAS 2002-6.3.1 | DEVELOPMENT AND TESTING OF FRICTION STIR WELDING (FSW) AS A JOINING METHOD FOR PRIMARY AIRCRAFT STRUCTURE | B. CHRISTNER, Eclipse Aviation, US | 6.3 Manufacturing II | |
| ICAS 2002-6.3.2 | CREEP FORMING OF AlMgSc ALLOYS FOR AERONAUTIC AND SPACE APPLICATIONS | Jambu, S., Lenczowski, B., Rauh, R., EADS Deutschland GmbH, 81663 Munich Juhl, K., Airbus Germany GmbH, 28183 Bremen |
6.3 Manufacturing II | |
| ICAS 2002-6.3.3 | A UNIQUE SPRAY FORMING PROCESS FOR HIGH TEMPERATURE MATERIALS FOR AEROSPACE APPLICATIONS | Zhang, G., Li, Z., Tian, S., Yan, M., Beijing Institute of Aeronautical Materials, China |
6.3 Manufacturing II | |
| ICAS 2002-6.3.4 | NEW APPROACHES IN TEXTILE AND IMPREGNATION TECHNOLOGIES FOR THE COST EFFECTIVE MANUFACTURING OF CFRP AEROSPACE COMPONENTS | Brandt, J., Gessler, A., Filsinger, J., EADS Deutschland GmbH, CRC Germany, LG-WF, D-81663 Munich |
6.3 Manufacturing II | |
| ICAS 2002-6.5.3 | BALANCING ACCURACY OF CALCULATIONS AND PROBABILITY OF ASSUMPTIONS IN THE TECHNOLOGY INTEGRATION | G.A. DIRKS, EADS Airbus GmbH, DE | 6.5 Management of R & D | |
| ICAS 2002-8.6.1 | PATCH REPAIR OF CRACKS IN THE UPPER LONGERON OF AN F-16 AIRCRAFT OF THE ROYAL NETHERLANDS AIR FORCE (RNLAF) | W.G.J. Hart, J.A.M. Boogers National Aerospace Laboratory (NLR), the Netherlands |
8.6 Structures & Materials II | |
| ICAS 2002-8.8.3 (St) | ACCESSIBILITY AND MAINTAINABILITY STUDIES THROUGH DIGITAL HUMANS IN A DIGITAL MOCK-UP CONTEXT | Gallizio, M., Sembenini, G. L., Politecnico di Torino, Italy |
8.8 Student session IV | |
| ICAS 2002-6.9.3 | VALUE STREAM ANALYSIS AND MAPPING FOR PRODUCT DEVELOPMENT | Hugh L. McManus, Richard L. Millard, Massachusetts Institute of Technology |
6.9 Integrated Product Development II | |
| ICAS 2002-6.9.4 | A VALUE-BASED APPROACH FOR COMMERCIAL AIRCRAFT CONCEPTUAL DESIGN | Markish J., Willcox, K., Massachusetts Institute of Technology |
6.9 Integrated Product Development II | |
| ICAS 2002-R27 | SYSTEM APPROACH TO IDENTIFY AEROSPACE RESEARCH CAPABILITIES AT UNIVERSITY | S. KAINIKARA, RMIT University, Australia | Reserve paper | |
| ICAS 2002-R51 | MATRIX FORMULATION OF WING LOADING DISTRIBUTION | A. PISTEK, Inst of Aerospace Eng, Brno University of Technology, Czech Republic | Reserve paper | |
| ICAS 2002-R55 | PREDICTING CURE KINETICS FOR A NON-ISOTHERMAL CURE PROCESS WITH A CONVENTIONAL ISOTHERMAL DSC TECHNIQUE. | A D Rogers, Dept of Mech Eng, University of New Brunswick, Canada | Reserve paper | |
| ICAS 2002-R62 | CALCULATING THE COST OF A CARBON FIBRE COMPOSITE STRUCTURE FROM WITHIN A FINITE ELEMENT MODEL | Barlow, D.A. Clayton, G. Hawker de Havilland 226 Lorimer Street, Port Melbourne, Victoria, 3207, Australia Scott, M.L. Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Te |
Reserve paper | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-4.7.2 | NASA'S FUTURE AEROPROPULSION VISION | A. SEHRA, NASA GRC, USA | 4.7 ISOABE I | |
| ICAS 2002-4.7.3 | CLEAN : THE EUROPEAN ENVIRONMENTALLY FRIENDLY ENGINE DEMONSTRATOR | BROICHHAUSEN, G. WILFERT, MTU-AE, DE |
4.7 ISOABE I | |
| ICAS 2002-4.7.4 | DIAGNOSTICS OF LEAKAGES IN GAS TURBINES | Y.I. LI, P. PILIDIS, E. KLEINAKIS, P. KOTSIOPOULOS, Cranfield University, UK | 4.7 ISOABE I | |
| ICAS 2002-7.7.1 | A CONTRIBUTION TO PROACTIVELY PLANNING AND MANAGING AIRPORT GROUND TRAFFIC USING A STOCHASTIC MODELLING APPROACH | TORSTEN BUSACKER, Berlin University of Technology PROF. MANFRED FRICKE, Berlin University of Technology |
7.7 Development in ATM | |
| ICAS 2002-7.7.2 | AN OBJECT-ORIENTED METHODOLOGY FOR MANAGING THE COMPLEXITY OF ATM SYSTEMS | Michel LEMOINE and Pierre DARBON ONERA Centre de Toulouse 2 avenue E. Belin 31055 Toulouse CEDEX |
7.7 Development in ATM | |
| ICAS 2002-7.7.3 | A COST/BENEFIT ANALYSIS OF AFAS FUNCTIONALITIES FOR A FUTURE ATM-SYSTEM | Dey, D., Schnieder, H., Schäfer, D., AIRBUS |
7.7 Development in ATM | |
| ICAS 2002-7.7.4 | PATS PERSONAL AIR TRANSPORTATION SYSTEM | Dr. Jozsef Rohacs Department of Aircraft and Ships Budapest University of Technology and Economics |
7.7 Development in ATM | |
| ICAS 2002-7.9.1 | CAPACITY AND WAKE VORTICES | Hallock, J. N., US DOT Volpe National Transportation Systems Center Tung, C., US Army Aero-Flight Dynamics Directorate, NASA Ames Sampath, S., US Army Research Laboratory, European Research Office |
7.9 Wake Vortex | |
| ICAS 2002-7.9.3 | A MODEL FOR SIMULATION OF FLIGHT PASSAGES THROUGH TRAILING TIP VORTICES | Sedin, Y. C-J. , Gråsjö, I. , Kullberg, E., Larsson, R., Saab Aerospace |
7.9 Wake Vortex | |
| ICAS 2002-7.9.4 | ON WAKE VORTEX RESPONSE FOR SEVERAL COMBINATIONS OF LEADING AND FOLLOWING AIRCRAFT |
Campos, L.M.B.C., Marques, J.M.G., Instituto Superior Técnico, Portugal |
7.9 Wake Vortex | |
| ICAS 2002-8.9.1 | DARPA’S QUIET SUPERSONIC PLATFORM (QSP) PROGRAM | R. WLEZIEN, NASA, US | 8.9 SAE Session I | |
| ICAS 2002-8.9.2 | NASA’S SUPERSONIC COMMERCIAL AIRCRAFT TECHNOLOGY DEVELOPMENT – BACKGROUND AND CURRENT STATUS | R.A. MERCURE EM2C, CNRS, FR | 8.9 SAE Session I | |
| ICAS 2002-8.9.3 | NORTHRUP GRUMANN’S FLIGHT TEST ON SONIC BOOM MITIGATION | C. BOCCADORO, Northrop Grumman, US | 8.9 SAE Session I | |
| ICAS 2002-8.9.4 | LOCKHEED MARTIN’S HISTORY OF SUPERSONIC AIRCRAFT | R. BAUMGARTNER, Lockheed Matrin, US | 8.9 SAE Session I | |
| ICAS 2002-7.10.1 | DEVELOPMENT OF APPROACH PROCEDURE DESIGN CRITERIA FOR SYSTEMS BASED ON GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) WITH GROUND BASED AUGMENTATION SYSTEM (GBAS) | Dipl.-Ing. Ren Doerries Prof. Dr.-Ing. Manfred Fricke Dipl.-Ing. Holger Schulz Technical University of Berlin Institute of Aeronautics and Astronautics Section Flight Guidance and Control / Air Transportation Marchstrae 14, 10587 Berlin, Germany |
7.10 Mission Management Issues | |
| ICAS 2002-7.10.2 | RELATIONAL MODEL AND DATA LINK FOR AIRCRAFT CONTROL DURING LANDING AND TAKE-OFF | K. Yazdanian, Office National d'Etudes et de Recherches Aérospatiales Département Prospective et Synthèse 2 av. Ed Belin 31055 Toulouse cedex France |
7.10 Mission Management Issues | |
| ICAS 2002-7.10.3 | A SYSTEM FRAMEWORK FOR THE DESIGN OF AIRCRAFT MISSION SYSTEMS FROM AN OPERATOR’S PERSPECTIVE | Kainikara, S., Sinha, A.K., Kusumo, R. Sir Lawrence Wackett Centre for Aerospace Design Technology, Department of Aerospace Engineering, Royal Melbourne Institute of Technology, Melbourne, Australia. |
7.10 Mission Management Issues | |
| ICAS 2002-7.10.4 | AN AUTOMATED SYSTEM FRAMEWORK FOR PRE-MISSION SUCCESS EVALUATION OF MEDICAL EMERGENCY HELICOPTERS OPERATIONS – DEFINED MISSION CAPABILITY SUB-MODULE | Sinha, A.K and Kusumo, R Sir Lawrence Wackett Centre for Aerospace Design Technology Department of Aerospace Engineering Royal Melbourne Institute of Technology GPO Box 2476V, Melbourne, Victoria, 3001, Australia. Hogan, P and Laycock, K.. Air Amb |
7.10 Mission Management Issues | |
| ICAS 2002-7.10.5 | AN OPERATIONAL EVALUATION OF A TAKE-OFF PERFORMANCE MONITORING ALGORITHM | Zammit-Mangion David, Dr. Ing. (University of Malta) Eshelby Martin, Dr. (Cranfield University) |
7.10 Mission Management Issues | |
| ICAS 2002-4.11.1 (I.L.) | DISCOVERING THE SECRETS OF THE WRIGHT BROTHERS | K. HYDE, The Wright Experience, US | 4.11 History | |
| ICAS 2002-4.11.2 (I.L.) | TEST AND EVALUATION OF THE WRIGHT BROTHERS AIRCRAFT, PROPELLERS AND ENGINES | K. KOCHERSBERGER, Rochester Institute of Technology, US | 4.11 History | |
| ICAS 2002-8.11.2 | SONIC BOOM PREDICTION AND MITIGATION | K.J. PLOTKIN, Wyle Lab. US | 8.11 SAE Session II | |
| ICAS 2002-8.11.3 (I.L.) | NASA’S ULTRA EFFICIENT ENGINE TECHNOLOGY (UEET) PROGRAM – ENVIRONMENTAL ELEMENTS | C.L. PEDDIE, NASA GRC, US | 8.11 SAE Session II | |
| ICAS 2002-8.11.4 (I.L.) | CONCORDE’S LEGACY : CHANGES IN THE ENVIRONMENTAL SCENE. FROM 1976 TO TODAY | G.M. LILLEY, NASA LRC, US | 8.11 SAE Session II | |
| ICAS 2002-R8 | ON THE CALCULATION OF COLLISION PROBABILITIES AS AN ASSURANCE OF SAFE SEPARATION BETWEEN AIRCRAFT | Campos, L.M.B.C.,Marques, J.M.G., Instituto Superior Técnico, Portugal |
Reserve paper | |
| ICAS 2002-R66 | FLIGHT TEST MANAGEMENT AND COMMAND GUIDANCE SYSTEM FOR FLIGHT TEST | T Wan, Department of Aerospace Engineering, Tamkang University, PRC | Reserve paper | |
| ICAS 2002-R72 | GENERATION OF SU-27 FIGHTER | Mickhail A. Pogossyan, Mickhail P. Simonov, German I. Zagainov, Alexy
Z. Tarasov Sukhoi Aircraft Design Bureau, Russia |
Reserve paper | |
| ICAS 2002-P3 | ANALYSIS OF PREVENTIVE MAINTENANCE PROGRAM IMPROVEMENT FOR IN-SERVICE AIRCRAFT | Cui Yi-yong, Ding Li-ping, Zhu Kai Beijing Aeronautical Technology Research Center, China |
Poster Session | |
| ICAS 2002-P16 | REDUCED THRUST TAKEOFF | Yan Chenghong Flight Tech Department ,China Civil Aviation Fight College, Guanghan,Sichuan,China 618307 |
Poster Session | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-7.1.1 | ASSESMENT OF EXPLICIT F.E. CAPABILITIES FOR FULL SCALE COUPLED FLUID/STRUCTURE AIRCRAFT DITCHING SIMULATIONS | Ortiz, R. , ONERA/DMSE Portemont, G. , ONERA/DMSE Charles, J.L., ONERA/DMSE Sobry, J.F. , ONERA/DMSE |
7.1 Structures and Safety | |
| ICAS 2002-7.1.2 | RELIABILITY-BASED CALENDRIC INSPECTION SCHEDULE FOR AIRCRAFT STRUCTURES WITH CORROSION FATIGUE | 1,2 Bintuan Wang and 2 Seiichi Ito 1 Japan Society for the Promotion of Science Fellow 2 Structures and Materials Research Center, National Aerospace Laboratory of Japan |
7.1 Structures and Safety | |
| ICAS 2002-7.1.3 | SECURING OF THE SAFETY AND ECONOMY OF ACROBATIC AIRPLANE SERVICE | MALER, Z., Private advisor in the strength and the fatigue life of small airplanes | 7.1 Structures and Safety | |
| ICAS 2002-8.2.2 | HYPOTHESIS ON THE ENHANCING OF THE PROBABILITY OF SURVIVAL OF SPACE AND TRANSATMOSPHERIC VEHICLES IN SPACE DEBRIS AND MICROMETEOROIDS CONTAMINATED ENVIRONMENT | M. Gallizio, G. Sembenini, N. Viola Department of Aerospace Engineering Politecnico di Torino, Italy |
8.2 Student session II | |
| ICAS 2002-7.3.1 | RECENT DEVELOPMENTS IN SCALING METHODS FOR ICING WIND TUNNEL TESTING AT REDUCED SCALE | Richard J. Kind, Carleton University, Ottawa, Canada K1S 5B6 Myron M. Oleskiw, National Research Council of Canada, Ottawa, Canada K1A 0R6 |
7.3 Weather and Natural Hazards | |
| ICAS 2002-7.3.2 | COPING WITH WAKE VORTEX | Hahn, K.-U., Institute of Flight Research, German Aerospace Center (DLR) | 7.3 Weather and Natural Hazards | |
| ICAS 2002-7.3.3 | ON ICE BLOCKAGE OF VENT TUBES IN THE WING FUEL TANKS OF THE EPSILON AIRCRAFT | J.M.M. Sousa - Instituto Superior Técnico, TU Lisbon, Av. Rovisco Pais, 1049-001 Lisboa, Portugal O.D.C.S. Ferreira, B.M.M. Fundanga - Academia da Força Aérea, Granja do Marqês, 2710 Sintra, Portugal |
7.3 Weather and Natural Hazards | |
| ICAS 2002-7.3.4 | EXPERIMENTAL INVESTIGATION OF SIMULATED ICE ACCRETION ON TURBOPROP AIRCRAFT | Patek, Z., VZLU (Aeronautical Research and Test Institute), Czech Republic Holl, M., VZLU (Aeronautical Research and Test Institute), Czech Republic |
7.3 Weather and Natural Hazards | |
| ICAS 2002-8.4.1 (I.L.) | FLOW AND NOISE CONTROL: TOWARD A CLOSER LINKAGE | Thomas, R.H., Choudhari, M.M., NASA Langley Research Center, USA Joslin, R.D., Office of Naval Research, USA |
8.4 Aircraft Noise I | |
| ICAS 2002-8.4.2 | JET NOISE REDUCTION TECHNOLOGY DEVELOPMENT AT GE AIRCRAFT ENGINES | Martens, S., GE Aircraft Engines | 8.4 Aircraft Noise I | |
| ICAS 2002-8.4.3 | OPTIMIZATION OF ACOUSTIC LINER DESIGN FOR AXISYMMETRIC MIXER-EJECTOR NOZZLES UNDER ESPR PROGRAM | Mohammed Salikuddin, Sr. Engineer, GE Aircraft Engines, MD A411, One Neumann Way, Cincinnati, Ohio 45215, USA | 8.4 Aircraft Noise I | |
| ICAS 2002-8.4.4 | ON THE ACOUSTIC MODES IN A CYLINDRICAL NOZZLE WITH AN ARBITRARY IMPEDANCE DISTRIBUTION | Campos, L. M. B. C., Oliveira, J. M. G. S., Secção de Mecânica Aeroespacial,
ISR, Instituto Superior Técnico, 1049-001 Lisboa Codex Portugal |
8.4 Aircraft Noise I | |
| ICAS 2002-8.4.5 | COMPARISON OF TWO CFD-BASED METHODS FOR THE PREDICTION OF THE TONE-NOISE GENERATED BY THE FAN-OGV INTERACTION CASE | D.Berge, Snecma Moteurs, France. | 8.4 Aircraft Noise I | |
| ICAS 2002-7.5.1 | AUTOMATIC AIRCRAFT COLLISION AVOIDANCE SYSTEM FOR AIR COMBAT MANEUVERING | Bengt-Göran Sundqvist, Andreas Persson, Johan Pellebergs, Krister Fersan SAAB AB |
7.5 Safety - Flight Control Systems | |
| ICAS 2002-7.5.2 | TRAJECTORY GENERATION AND DISPLAY FOR RELATIVE NAVIGATION OF TRANSPORTATION AIRCRAFT | B OUATTARA, EAMAC, NE, A.K. ACHAIBOU, F. MORA-CAMINO, CNRS, J. SLAMA, COPPE/UFRJ |
7.5 Safety - Flight Control Systems | |
| ICAS 2002-7.5.3 | THE HIERARCHICAL AVAILABILITY ANALYSIS FOR FLIGHT CONTROL SYSTEM | S. WANG, M. CUI, D. KONG, Beijing, University of Aeronautics & Astronautics, CN | 7.5 Safety - Flight Control Systems | |
| ICAS 2002-7.6.1 | EXPANDED ACCOMMODATION ANALYSIS AND RAPID PROTOTYPING TECHNIQUE FOR THE DESIGN OF A CREW STATION COCKPIT |
Winkler, E., The Boeing Company Onyebueke, L., Ameye, O., Tennessee State University |
7.6 Safety - Human Factors | |
| ICAS 2002-7.6.2 | EFFICIENT EYE-SCANNING FOR REDUCING PILOT WORKLOAD-SINGLE PILOT IFR AND VFR FLIGHT TESTS- | RINOIE, K., University of Tokyo SUNADA, Y., University of Tokyo |
7.6 Safety - Human Factors | |
| ICAS 2002-7.6.3 | PROMOTING AUTONOMOUS CONTROL IN CIVIL TRANSPORTS AS A PROPOSAL FOR THE FLIGHT COMMAND SYSTEM | Junichiro Sumita Nishinippon Institute of Technology 1-11 Aratsu, Kanda, Miyako, Fukuoka-Pref. Japan |
7.6 Safety - Human Factors | |
| ICAS 2002-7.6.4 | RELATIONSHIP BETWEEN QUALITY ASSURANCE AND SAFETY | O. TURCSANYI, MALEV, HU, R. MALIK, University ELTE, HU | 7.6 Safety - Human Factors | |
| ICAS 2002-7.8.1 (I.L.) | HELICOPTER FLIGHT SAFETY ENHANCEMENT: A EUROCOPTER CONTINUING ACTION | Jean-Marc Pouradier Eurocopter |
7.8 Safety as a Global Issue | |
| ICAS 2002-7.8.2 (I.L.) | Aging Military Aircraft | GARCIA, .L., garcia@lmco.com | 7.8 Safety as a Global Issue | |
| ICAS 2002-7.8.3 | KING AIR 350 FLIGHT-TEST DATA GATHERING AND LEVEL-D SIMULATOR AERODYNAMIC MODEL DEVELOPMENT | Kenneth Hui, Ramesh Srinivasan, Lorenzo Auriti, Joseph Ricciardi, National Research Council, Ottawa, Ontario, Canada K1A 0R6. Kimberly Blair, Devesh Pokhariyal, NLX Corporation, Sterling, VA, USA. |
7.8 Safety as a Global Issue | |
| ICAS 2002-7.9.2 | SAFETY-SEPARATION ASSESSMENT OF SATELLITE-BASED EN-ROUTE ATC VERSUS CONVENTIONAL EN-ROUTE ATC | S. STROEVE, M.H.C. EVERDIJ, M.N.J. VAN DER PARK, NLR, NL | 7.9 Wake Vortex | |
| ICAS 2002-7.11.1 | PROPULSION SYSTEM OPTIMISATION FOR MINIMUM GLOBAL WARMING POTENTIAL | Whellens M W, Cranfield University Singh R, Cranfield University |
7.11 Aircraft Emission | |
| ICAS 2002-7.11.2 | EMISSION SCATTERING SIMULATION FOR AIR-PORT REGION | Dr. Jozsef Rohacs Department of Aircraft and Ships Budapest University of Technology and Economics |
7.11 Aircraft Emission | |
| ICAS 2002-7.11.3 | ENVIRONMENTAL, ECONOMICAL AND TECHNICAL ASPECTS OF A CRYOPLANE IN THE PRELIMINARY DESIGN PHASE | Krijnen, J.A. , Astaburuaga, M.F. , Delft University of Technology Faculty of Aerospace Engineering, Netherlands |
7.11 Aircraft Emission | |
| ICAS 2002-R22/1 | TECHNOLOGICAL TRENDS IN SIMULATION TECHNOLOGY IN AVIATION & PILOT TRAINIG | Dr JANICEK, Unstitute of Aerospace, CZ | Reserve paper | |
| ICAS 2002-P12 | EXPERIMENTAL ASSESSMENT AND ANALYSIS OF THE CREW WORKLOAD | Giuseppe Surace, Polytechnic of Turin, Aerospace Department Juri Barollo, Alenia Aeronutica S.p.A |
Poster Session | |
| ICAS 2002-P15 | A METHOD OF ESTIMATING AIRPLANE TURBULENCE USING WIND DATA | Yongzhong Wang Department of Air Traffic Management, China Civil Aviation Flight College, Guanghan, Sichuan, P.C. 618307,P.R.China |
Poster Session | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| Special | ICAS , History of THE INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES, A BRIEF HISTORY |
J Green | Invited | |
| ICAS2002-0.1 | THE DANIEL AND FLORENCE GUGGENHEIM MEMORIAL LECTURE. CIVIL PROPULSION; THE LAST 50 YEARS |
H.I.H. Saravanamuttoo Carleton University and GasTOPS |
Invited | |
| ICAS 2002-0.2 | AEROSPACE IN 2020 : EUROPEAN VISION | H. VON BOSE, European Commission, BE | Invited | |
| ICAS 2002-0.3 | The John Green Lecture CFD IN CANADIAN AEROSPACE |
F. MAVRIPLIS, Bombardier Inc., CA | Invited | |
| ICAS 2002-0.4 | DEVELOPMENT AND APPLICATION OF TECHNOLOGY FOR THE SONIC CRUISER | D.P. MOONEY, Boeing Commercial, US | Invited | |
| ICAS 2002-0.5 | MARKET DRIVERS AND INNNOVATION BEHIND THE AIRBUS PRODUCTS | JARRY Philippe, Vice-President, Aircraft Evaluation, AIRBUS | Invited | |
| ICAS 2002-0.6 | THE CANADIAN AND AUSTRALIAN F/A-18 INTERNATIONAL FOLLOW-ON STRUCTURAL TEST PROJECT | D. L. Simpson, Institute for Aerospace Research, National Research Council of Canada Ottawa, Ontario, Canada N. Landry Directorate of Technical Airworthiness Department of National Defence Ottawa, Ontario, Canada Jean Roussel Military Aviation Se |
Invited | |
| SESSION | TITLE | AUTHORS | SESSION NAME | LINK |
| ICAS 2002-7.2.1 (I.L.) | THE WAY OF HARMONIZATION AND COOPERATION IN AEROSPACE EDUCATION IN EUROPE | A. Pernpeintner Institute for Fluid Mechanics TU Muenchen Boltzmannstr. 15, 85748 Garching, Germany |
7.2 Aerospace Education Systems and International Cooperation | |
| ICAS 2002-7.2.2 (I.L.) | THE CONTRIBUTION OF UNIVERSITY TO THE AEROSPACE RESEARCH AND TECHNOLOGIES | E. VALLERANI, P. SANTINI, Univ. La Sapienza, IT | 7.2 Aerospace Education Systems and International Cooperation | |
| ICAS 2002-7.2.3 (I.L.) | THE GLOBAL ROLE OF THE US-TOP UNIVERSITIES FOR THE PROVISION OF THE HUMAN RESOURCES IN ENGINEERING SCIENCE TO THE AEROSPACE COMMUNITY | B. LUSIGNAN, Center for International Cooperation in Space, US | 7.2 Aerospace Education Systems and International Cooperation |