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ACCEPTED ABSTRACTS – CATEGORY C - POSTERS These ABSTRACTS will be presented in the Poster area
(manned Tuesday). Most ABSTRACTS will also appear in the congress CD-Rom
proceedings |
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1. AIRCRAFT
AND SYSTEMS INTEGRATION |
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ICAS 2006-P1.1;
G. Lee, Y. Gao: , First Aircraft Design and Research Institute,
China AN INTEGRATED PLATFORM
FOR AIRCRAFT DESIGN: FLIGHT ENGINEERING SIMULATOR |
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ICAS 2006-P1.2;
P. Mardanpour, W. R. Krüger, H. Haddadpour*, D.
Hoffmann: DLR, Germany; *Sharif Univ. of Technology, Iran DESIGN AND TESTING OF A
MODEL WING SECTION FOR A HUMAN POWERED AIRCRAFT |
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ICAS 2006-P1.3;
J. Gao, G. Lu, L. Sun: Luoyang Institute of Electro-Optical Equipment,
China |
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ICAS 2006-P1.4;
P. H. Iscold, C. A. Cimini, R. P. Ribeiro:
Federal Univ. of Minas Gerais, Brazil |
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2.
AERODYNAMICS |
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ICAS 2006-P2.1;
Y. G. Xu: XI'AN
AERO-ENGINE (GROUP) LTD., China NUMERICAL CALCULATION
OF CONFINED COAXIAL TURBULENT SWIRLING JETS |
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ICAS 2006-P2.2;
W. J. Lee, I. Ahn: Korea Aerospace Research Institute, Korea |
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ICAS 2006-P2.3;
L. S. Hao, Z. D. Qiao: Northwestern Polytechnical Univ., China |
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ICAS 2006-P2.4;
V. V. Riabov: Rivier College,
USA NUMERICAL SIMULATION OF
KINETIC EFFECTS IN LOW-DENSITY HYPERSONIC AERODYNAMICS
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ICAS 2006-P2.5;
Z. D. Wang, M. H. Zhang, J. H. Wang: THE FIRST AIRCRAFT INSTITUTE of AVIC 1, China |
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ICAS 2006-P2.6;
J. Ding, W. Li, Y. Zhang*: Northwestern Polytechnical Univ., China; *China
Aerodynamics Research and Development Center ROBUST AIRFOIL OPTIMIZATION BASED ON RESPONSE
SURFACE METHOD (RSM) |
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ICAS 2006-P2.7;
J. Si, H Zhan*, J Bai*: First Aircraft Design and Research Institute, China;
*Northwestern Polytechnical Univ., China |
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ICAS 2006-P2.8;
L. A. Moreno, R. S. Palma, L. P. Pascual:
Universidad Politecnica de Madrid, Spain AERODYNAMIC STUDY OF A
BLENDED WING BODY; COMPARISON WITH A CONVENTIONAL TRANSPORT AIRPLANE
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ICAS 2006-P2.9;
A. Cenko, D. Grove, J. Lee: NAVAIR, USA |
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ICAS 2006-P2.10;
A. Baig, A. Ahmed, S. Zahir: NESCOM, Pakistan |
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ICAS 2006-P2.11;
M. Jabbal, H. Tang, S. Zhong: Univ. of Manchester, UK THE EFFECT OF GEOMETRY
ON THE PERFORMANCE OF SYNTHETIC JET ACTUATORS |
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ICAS 2006-P2.12;
C. C. Perez, S. B. Ferreira, L. F. Figueira Da
Silva, A. B. de Jesus*, G. L. Oliveira*: Pontificia Universidade Catolica do Rio de Janeiro,
Brazil; *Empresa Brasileira de Aeronáutica SA, Brazil NUMERICAL STUDY OF THE
PERFORMACE IMPROVEMENT OF SUBMERGED AIR INTAKES USING VORTEX GENERATORS
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ICAS 2006-P2.13;
M. Lasek, J. Pietrucha*, K. Sibilski**, M. Zlocka*:
State Committee of Aircraft Accident Investigation,
Poland; *Warsaw Univ. of Technology, Poland; **Air Force Institute of
Technology & Wroclaw Univ. of Technology, Poland |
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ICAS 2006-P2.14;
T. F. G. Costa, E. M. Belo: Univ. of Sao Paulo, Brazil PREDICTION OF
AERODYNAMICS CHARACTERISTICS AND AIRLOADS OF A GENERIC GEOMETRY WING.
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ICAS 2006-P2.15;
R. Hafiz, A. Majeed*, S. Zahir, M. A. Khan:
NESCOM, Pakistan; *Pakistan Institute of Engineering
and Applied Sciences, Pakistan |
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ICAS 2006-P2.16;
Q. Z. Yang, Y. Zheng, T. Streit*: Northwestern Polytechnical Univ., China; *DLR,
Germany |
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ICAS 2006-P2.17;
R. Qian, Z. Zhu*, Z. Duan, J. Wei: First Aircraft Design and Research Institute, China;
*Beijing Univ. of Aeronautics and Astronautics, China |
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ICAS 2006-P2.18;
S. Crippa, A. Rizzi: Royal Institute of Technology (KTH), Sweden INITIAL STEADY / UNSTEADY CFD ANALYSIS OF VORTEX FLOW OVER
THE VFE-2 DELTA WING |
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ICAS 2006-P2.19;
S. Srigrarom, N. Lewpiriyawong: Nanyang Technological Univ., Singapore MODIFICATION OF DELTA WINGS TO CONTROL VORTEX
BREAKDOWN |
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ICAS 2006-P2.20;
J. Cho, C. Han: Hanyang Univerisity, Korea UNSTEADY AERODYNAMIC ANALYSIS OF WINGS FLYING OVER
NONPLANAR GROUND SURFACES |
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ICAS 2006-P2.21;
K. AsfarK.
Asfar, D. El-ani: Jordan Univ. of Science & Technology, Jordan WING ROCK CONTROL VIA EXTERNAL EXCITATION
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ICAS 2006-P2.22;
V. Diederichs, M. Lapolla, L. Lorefice, R. Malvano,
B. Palio, P. G. Spazzini, M. Onorato, C. Haigermoser, L. Vesley:
Politecnico di Torino, Italy |
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ICAS 2006-P2.23;
J. Alexandre, M. Frédéric*: Airbus, France; *EEA – Airbus COMPUTATION OF EQUIVALENT ACOUSTIC SOURCES USING AN
INVERSE METHOD |
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3.
MATERIALS AND STRUCTURES |
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ICAS 2006-P3.1;
X. Wang, L. Wang*: Beihang Univ., China; *Agricultural Univ. of Hebei,
China MEASURES AND TEST
TECHNIQUES OF FUNGUS RESISTANCE TO AIRCRAFT MATERIALS AND EQUIPMENT
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ICAS 2006-P3.2;
X. W. Liu, Y. Z. Mu, X. J. Zhang: Northwestern Polytechnical Univ., China FINITE ELEMENT ANALYSIS OF FRICTION STIR WELDING
TEMPERATURE FIELD |
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ICAS 2006-P3.3;
C. Cao, T. Cai: Northwestern Polytechnical Univ., China |
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ICAS 2006-P3.4;
F. Benmeddour, S. Grondel, J. Assaad: IEMN-DOAE, France STUDY OF FUNDAMENTAL
LAMB MODES BEHAVIOUR WITH A SHARP CHANGE OF SECTION IN A PLATE |
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ICAS 2006-P3.5;
X. Ficquet, C. E. Truman, E. Kingston, D. J. Smith:
Univ. of Bristol, UK MEASUREMENT OF RESIDUAL
STRESSES IN ALUMINIUM ALLOY AEROSPACE COMPONENTS |
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ICAS 2006-P3.6;
Y. J. Sun, D. S. Wang, C. A. Sha: Chinese Flight Test Establishment, China MULTI-DIMENSION LAPLACE
WAVELET AND THE APPLICATIONS IN FLIGHT FLUTTER TEST |
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ICAS 2006-P3.7;
I. Pavelko, V. Pavelko: Aviation Institute of Riga Technical Univ., Latvia CROSS-PLY BENDING AND
STABILITY OF COMPRESSED BAR WITH CRACK |
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ICAS 2006-P3.8;
K.- H. Byun, S.- M. Jun: Agency for Defense Development, Korea FLUTTER ANALYSIS OF
KF-16 AIRCRAFT UTILIZING TEST MODAL DATA |
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ICAS 2006-P3.9;
A. Fonseca, L. Reis, M. Freitas: Instituto Superior Tecnico, Portugal |
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ICAS 2006-P3.10;
S. B. Luo, J. M. Zhang, H. Yang, Y. Y. Bu*:
China Precision Engineering Institute, China;
*Central South Univ., China THE MANUFACTURING
TECHNOLOGY OF AN ULTRA-PRECISION AEROSTATIC SPINDLE SYSTEM
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ICAS 2006-P3.11;
H. Pfeiffer, F. Fransens*, W. Hillger**, U.
Pfeiffer**, M. Wevers*, C. Buelens: Metalogic
nv, Belgium; *K. U. Leuven, Belgium; **DLR, Germany PROGRESS ON AIRCRAFT
INTEGRATED SAFETY HEALTH ASSESSMENT (AISHA) |
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ICAS 2006-P3.12;
A. Abedian, A. Barakati, A. Malekpour:
Sharif Univ. of Technology, Iran EFFECTS OF GEOMETRY
ASPECTS ON THE SIMULATION OF SUPERPLASTICITY IN MMC COMPOSITES
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ICAS 2006-P3.13;
M. Plhal, J. Šplíchal: Brno Univ. of Technology, Czech Republic |
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ICAS 2006-P3.14;
R. Tiberkak, S. Rechak*, M. Bachen**: Université Saad Dahleb, Algeria; *Ecole Nationale
Polytechnique, Algeria; **Université de Médéa, Algeria THE DYNAMIC RESPONSE OF
LAMINATE COMPOSITE PLATE UNDER LOW-VELOCITY IMPACT |
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ICAS 2006-P3.15;
T. Mahrholz, U. Riedel*, M. Sinapius*:
DLR, Germany; *German Aerospace Center, Germany |
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ICAS 2006-P3.16;
D. Bakavos, P. B. Prangnell, F. Eberl*:
Manchester Materials Science Centre, UK; *Alcan
Centre de Recherches de Voreppe THROUGH THICKNESS MICROSTRUCTURAL GRADIENTS IN 7475
AND 2022 AGEFORMED BEND COUPONS FOR FUSELAGE AND LOWER WING SKIN APPLICATIONS
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ICAS 2006-P3.17;
S. Drawin, M. Heilmaier*, P. Jéhanno**, X. Wu***, P.
Belaygue****, P. Tsakiropoulos', M. Vilasi'', J. -Y. Guédou''', P. Novak'''',
F. Delabrouille+, N. Jones++, S. Sabbadini+++: ONERA-DMPP, France; *Univ. of Magdeburg; **Plansee
SE, REUTTE; ***Univ. of Birmingham, UK; ****Turboméca; 'Univ. of Surrey, UK;
''Univ. of Nancy, France; '''Snecma; ''''Walter Engines a.s.; +EDF R&D;
++Rolls-Royce plc; +++AVIO S.p.A. THE EU-FUNDED “ ULTMAT
” PROJECT: ULTRA HIGH TEMPERATURE MATERIALS FOR TURBINES
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4.
PROPULSION |
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ICAS 2006-P4.1;
A. Saharan, Q. J. Khan, R. R. Pant: Hindustan College of Engineering, India |
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ICAS 2006-P4.2;
P. T. L. Teixeira Lacava, H. M. S. Meira Da Silva,
J. V. F. R. Fontenele Romero: Instituto Tecnológico de Aeronáutica (ITA), Brazil THE INFLUENCE OF FLAME HOLDER GEOMETRY ON THE THRUST
INSTABILITY IN A LABORATORIAL SCALE RAMJET ENGINE |
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ICAS 2006-P4.3
S. A. Vasudev: Gas Turbine
Research Establishment, India EFFECTS OF GAS RADIATION IN SCALED COOLING
EFFECTIVENESS TESTS OF TURBINE VANES |
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5. FLIGHT
DYNAMICS AND CONTROL |
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ICAS 2006-P5.1;
S. J. Song, Y. Z. Zhang, J. H. Deng: Northwestern Polytechnical Univ., China |
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ICAS 2006-P5.2;
K. Sibilski, W. Wroblewski*: Air Force Institute of Technolgy, Poland; *Wroclaw
Technical Univ., Poland |
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ICAS 2006-P5.3;
L. M. B. C. Campos, J. M. G. Marques: Instituto Superior Técnico, Portugal ON THE EFFECT OF
DAMPING AND CONTROLS ON AN AIRCRAFT WAKE ENCOUNTER |
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ICAS 2006-P5.4;
A. Khan, C. Bil, K. E. Marion: RMIT, Australia REAL TIME PREDICTION OF
SHIP MOTION FOR THE AID OF HELICOPTER AND AIRCRAFT DEPLOYMENT AND RECOVERY
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ICAS 2006-P5.5;
J. P. G. Perez, J. L. Otero, A. M. L. de Sabando, I.
G. Perez: Universidad Politécnica de Madrid, Spain ROBUST CONTROLLERS
DESIGN STRATEGIES FOR UNMANNED AIR VEHICLES |
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ICAS 2006-P5.6;
G. Kopecki: Rzeszów
Univ. of Technology, Poland AIRCRAFT HEADING CONTROL IN CASE OF INCOMPLETE
MEASUREMENT INFORMATION FOR FLY-BY-WIRE CONTROL SYSTEM |
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ICAS 2006-P5.7;
V. Marefat, M. Rahim: Sharif Univ. of Technology, Iran NONLINEAR MODELING AND SIMULATION OF SMALL-SIZE
HELICOPTER DYNAMICS AND MODEL VALIDATION |
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6. SYSTEMS, SUBSYSTEMS AND EQUIPMENTS |
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ICAS 2006-P6.1;
Y. Zhu, P. G. Wang, A. L. Yu: Beijing Aeronautical Technology Research Center,
China ENVIRONMENTAL CHALLENGE
TO AIRBORNE ELECTRONIC EQUIPMENT MAINTENANCE |
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ICAS 2006-P6.2;
H. Long, X. M. Wang*: Beijing Union Univ., China; *Northwestern
Polytechnical Univ., China AIRCRAFT FUEL SYSTEM
DIAGNOSTIC FAULT DETECTION THROUGH EXPERT SYSTEM |
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ICAS 2006-P6.3;
H. Yuan, F. L. Tian: Chinese Flight Test Establishment, China |
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ICAS 2006-P6.4;
Y. Wang, G. L. Luo, G. P. Lin*: Beihang Univ.& BATRC, China; *Beihang Univ.,
China THE DESIGN OF A SERIES
OF ELECTROTHERMAL ICE PROTECTION SYSTEMS |
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ICAS 2006-P6.5;
D. Darnis: TECHNOFAN,
France AN INNOVATIVE CABIN RECIRCULATION FAN DEMONSTRATOR
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7. SYSTEMS
ENGINEERING AN SUPPLY CHAIN |
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ICAS 2006-P7.1;
K. Cheng, K. Liu: First Aircraft Institute, China |
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8. AIR
TRANSPORT SYSTEM EFFICIENCY |
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ICAS 2006-P8.1;
A. R. Nejad: Civil
Aviation Organization, Iran |
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ICAS 2006-P8.2;
Q. X. Ding, R. G. Zhu, Z. Y. Zhao: Luoyang Institute of Electro-Optical Equipment,
China IMAGE PROCESSING
TECHNOLOGY OF FLIR-BASED ENHANCED VISION SYSTEM |
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ICAS 2006-P8.3;
V. J. Rohács: Budapest
Univ. of Technology and Economics, Hungary CHANGES IN AIRPORT TERMINAL DESIGN |
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9. SAFETY
AND SECURITY |
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ICAS 2006-P9.1
G. Li, T. Jiang: Beijing Univ. of Aeronautics and Astronautics, China SELECTION OF PARAMETERS
IN FIXED-DURATION RELIABILITY QUALIFICATION TEST SCHEME
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ICAS 2006-P9.2;
R. Sayfi, F. Leblond*: Civil Aviation Organization of Iran, Iran; *French
DGAC DEVELOPEMENT OF A
PRODUCTION ORGANIZATION EXPOSITION SCHEME TAKING INTO ACCOUNT EN9100
REQUIREMENTS |
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ICAS 2006-P9.3;
A. R. Nejad: Civil
Aviation Organization, Iran ELECTRONIC SYSTEM FOR
DEACTIVATION OF CLOCK-ACTIVATED BOMBS WITH THE HELP OF LIQUID NITROGEN
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ICAS 2006-P9.4;
G. Klein, T. Elliger, B. Zapf: TÜV Industrie Service GmbH, Germany HYDROGEN TECHNOLOGY –
READY FOR TAKE-OFF – HYDROGEN APPLICATIONS IN AEROSPACE INDUSTRY
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ICAS 2006-P9.5;
S. Gu: CARERI,
China ENHANCEMENTS OF FLIGHT
MANAGEMENT SYSTEM WITH INTEROPERABILITY |
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ICAS 2006-P9.6;
J. J. Qiao, G. L. Tian*, Y. D. Yuan*: Xi'an Aviation Brake Technology Co.Ltd,*, China;
*Northwestern Polytechnical Univ., China RESEARCH ON RELIABILITY
GROWTH TECHNOLOGY OF ELECTROMECHANICAL-HYDRAULIC SYSTEM
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10.
CHALLENGE OF THE ENVIRONMENT |
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ICAS 2006-P10.1;
A. Junior: DLR, Germany AERONET III “AIRCRAFT EMISSIONS AND REDUCTION
TECHNOLOGIES”, A EUROPEAN FUNDED COORDINATION ACTION |
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ICAS 2006-P10.2
S. Matthes, The ECATS Management Team*:
DLR, Germany; *ECATS Network Office, DLR, Germany ECATS- A
EUROPEAN NETWORK OF EXCELLENCE FOR AN ENVIRONMENTAL AIR TRANSPORT SYSTEM |