|
ACCEPTED ABSTRACTS - CATEGORY
B These ABSTRACTS are standby
for oral presentation in case ABSTRACTS are withdrawn from an appropriate
session. Full ABSTRACTS will appear
in the congress CD-Rom proceedings They may also be presented
as posters in the Poster area |
| |
| 1. AIRCRAFT AND SYSTEMS INTEGRATION |
|
ICAS 2006-1.1S
; H. R. Saeedipour, B. J. Guztyne, W. J. Chan: Univ. of Science Malaysia (USM), Malaysia THE DESIGN OF A HIGH-MANEUVERABLE SINGLE- MINI-JET
ENGINED REMOTELY PILOTED VEHICLE (RPV) |
|
ICAS 2006-1.2S
; H. Liu, Z. Wu*: Beihang Univ., China; *Beijing Univ. of Aeronautics
and Astronautics, China EVOLUTIONAL DESIGN SUPPORT STRATEGY
ORIENTED TO AIRCRAFT CONCEPTUAL DESIGN |
|
ICAS 2006-1.3S
; N. Kehayas: Hellenic Air
Force Academy, Greece |
|
ICAS 2006-1.4S
; H. R. Saeedipour: Univ. of Science Malaysia (USM), Malaysia ON THE DESIGN OPTIMIZATION OF A THRUST-VECTORED HIGH-SUBSONIC
JET TRANSPORT AIRCRAFT |
|
ICAS 2006-1.4S
; A. Mirzoyan: CIAM, Russian
Federation MULTIOBJECTIVE OPTIMIZATION OF ENGINE & A/C MATCHING
ON MISSION AND ENVIRONMENTAL CRITERIA AT SSBJ CONCEPTUAL DESIGN |
|
ICAS 2006-1.6S
; R. K. Cooper, E. Benard, G. Bourgouin*:
Queen's Univ. Belfast, UK; *ENSMA Poitiers, France ELECTRIC POWERED COMMUTER AIRCRAFT |
|
ICAS 2006-1.6S
; B. Goeksel, M. Fischer*: TU Berlin, Germany; *FESTO AG & Co PULSED PLASMA PROPULSION AND FLOW CONTROL FOR BIONIC
AIRSHIPS |
|
ICAS 2006-1.7S
; D. Kubo, S. Suzuki, T. Kagami*: Univ. of Tokyo, Japan; *Solekia Limited DEVELOPMENT OF EXPERIMENTAL
SMALL UAV EQUIPPED WITH CELLULAR PHONE DATA LINK SYSTEM |
|
ICAS 2006-1.9S
; X. Li, W. Li*: Beijing Institute
of Technology, China; *Northwestern Polytechnical Univ., China A PRACTICAL MULTIDISCIPLINARY
DESIGN OPTIMIZATION ALGORITHM BASED ON THE UNIFORM DESIGN THEORY |
|
ICAS 2006-1.9S
; K. S. Jeon, J. W. Lee, Y. H. Byun: Center for Advanced e-System Integration Technology,
Korea REPETITIVE RESPONSE SURFACE ENHANCEMENT TECHNIQUE THROUGH
DESIGN SPACE TRANSFORMATION AND SUB-OPTIMIZATION |
|
ICAS 2006-1.10S
; J. Blacklock, L. Zalcman*: Australian Defence Dept., Australia; *Zalcman Consulting,
Australia |
|
ICAS 2006-1.10S
; J. Khreish, A. Sinha: RMIT, Australia |
|
ICAS 2006-1.11S
; K. S. Zhang, W. J. Li, H. Y. Wei, Z. H. Han:
Northwestern Polytechnical Univ., China A NEW METHOD FOR OPTIMUM ALLOCATION
OF DESIGN REQUIREMENTS IN AIRCRAFT CONCEPTUAL DESIGN |
| 2. AERODYNAMICS |
|
ICAS 2006-2.1S
; C. Georgantopoulou, G. A. Georgantopoulos*, S. Tsangaris:
National Technical Univ. of Athens(NTUA), Greece; *Hellenic
Air Force Academy, Greece INCOMPRESSIBLE NAVIER STOKES
EQUATIONS SOLUTION USING BLOCK NESTED CARTESIAN GRID |
|
ICAS 2006-2.2S
; D. Sun, X. Jia, X. Liang: Northwestern Polytechnical Univ., China NUMERICAL SIMULATION OF THE
FLOWFIELD AROUND MISSILE WITH LATERAL JET INTERACTION |
|
ICAS 2006-2.2S
; Y. C.- J. Sedin, I. Persson, H. Åslund:
Saab Aerosystems, Sweden COMPUTATIONAL AERODYNAMIC ANALYSIS
ON A GENERIC UCAV/URAV CONFIGURATION |
|
ICAS 2006-2.3S
; L. J. Johnston: Univ. of Salford, UK PREDICTION OF HIGH-LIFT SYSTEM AERODYNAMICS USING UNSTRUCTURED-GRID
FLOW SOLVERS AND TRANSPORT EQUATION TURBULENCE MODEL |
|
ICAS 2006-2.5S
; E. Iuliano, V. Brandi, C. De Nicola*:
CIRA, Italy; *Università di Napoli "Federico II" EULERIAN WATER IMPINGEMENT PREDICTION ON MULTI-ELEMENT
AIRFOILS WITH VISCOUS AND INVISCID FLOW |
|
ICAS 2006-2.5S
; G. Imai, K. Fujii*, A. Oyama*: Univ. of Tokyo, Japan; *JAXA, Japan COMPUTATIONAL ANALYSES OF SUPERSONIC
FLOWS OVER A DELTA WING AT HIGH ANGLES OF ATTACK |
|
ICAS 2006-2.6S
; S. B. Hazra: Univ. of Trier,
Germany ONE-SHOT PSEUDO-TIMESTEPPING METHOD FOR AERODYNAMIC
SHAPE OPTIMIZATION |
|
ICAS 2006-2.7S
; S. Zahir, S. Raza*, Z. Ye: Northwestern Polytechnical Univ., China; *NESCOM, Pakistan |
|
ICAS 2006-2.7S
; C. Han, H. Lee*, J. Cho**: Konkuk Univ., Korea; *Sindorico; **Hanyang Univ. PROPULSIVE CHARACTERISTICS OF
BIOMORPHING AIRFOILS IN GROUND EFFECT |
|
ICAS 2006-3.2S
; A. R. Davari, M. R. Soltani*, A. Mohammadi:
Azad Univ., Iran; *Sharif Univ., Iran IMPACT OF MODEL PLUNGING MOTION
ON WIND TUNNEL WALL PRESSURE FLUCTUATIONS |
|
ICAS 2006-3.2S
; M. R. Hassani Ahangar, M. R. Kangavari, R. Berangi:
Iran Univ. of Science and Technology (IUST), Iran INVESTIGATION OF ERROR SOURCES
ON THE BALANCE AND THE STANDARD DYNAMIC MODEL IN THE WIND TUNNEL |
|
ICAS 2006-3.4S
; M. R. Soltani, A. Mamaghani, A. Bakhshalipour:
Sharif Univ. of Technology, Iran |
|
ICAS 2006-3.4S
; R. Sosovicka, M. Kouril, J. Friedl: Brno Univ. of Technology, Czech Republic GROUND MOBILE LABORATORY FOR
MEASUREMENT OF AIRFOIL AERODYNAMIC CHARACTERISTICS |
|
ICAS 2006-3.5S
; Z. Pátek, M. Zabloudil: Aeronautical Research and Test Institute, Czech Republic |
|
ICAS 2006-3.5S
; K. Ogawara, S. Mochizuki, T. Higuchi:
Yamaguchi Univ., Japan DIRECT MEASUREMENT OF WALL-SHEAR
STRESS OF PLANE SHEAR LAYER WITH PLASMA SYNTHETIC JET ACTUATOR |
|
ICAS 2006-3.6S
; H. Nobahari, S. Y. Nabavi, S. H. Pourtakdoust:
Sharif Univ. of Technology, Iran |
|
ICAS 2006-3.7S
; T. Wan, H.- C. Chou, K.- W. Lien: Tamkang Univ., Taiwan |
|
ICAS 2006-3.8S
; F. M. Catalano, G. L. Brandt: Univ. of Sao Paulo, Brazil EXPERIMENTAL AND NUMERICAL STUDY
OF A TWO-ELEMENT WING WITH GURNEY FLAP |
|
ICAS 2006-3.9S
; S. Calvo, E. Rodriguez, C. Gallego: EADS-CASA, Spain AEROLOADS. A TOOL TO GENERATE PRESSURE LOAD MODELS
OF AN AIRCRAFT FITTED TO AN AERODYNAMIC DATA BASE |
|
ICAS 2006-3.10S
; F. D. Marques, A. R. Simoni, V. A. Oliveira:
Univ. of Sao Paulo, Brazil |
|
ICAS 2006-3.10S
; K. Ito, S. Suzuki*: Hiyoh Aircraft Manufacturing and Development Co., Japan;
*Univ. of Tokyo, Japan CONIC CURVE DESCRIPTION OF FLAPPING WING PLANFORMS
AND PARAMETRIC INVESTIGATION OF THEIR PERFORMANCE |
|
ICAS 2006-3.11S
; H. Li, J. Stewart*, R. S. Figliola: Clemson Univ., USA; *General Electric EXERGY BASED DESIGN METHODOLOGY
FOR AIRFOIL SHAPE OPTIMIZATION AND WING ANALYSIS |
| 3. MATERIALS AND STRUCTURES |
|
ICAS 2006-4.1S
; J. E. Schut, R. C. Alderliesten: TU Delft, Netherlands DELAMINATION GROWTH RATE AT
LOW AND ELEVATED TEMPERATURES IN GLARE |
|
ICAS 2006-4.2S
; M. Calomfirescu, A. S. Herrmann, C. König*, J. Müller**:
Faserinstitut Bremen e.V. (FIBRE), Germany; *Bremer
Institut für Konstruktionstechnik (BIK), Germany; **Bremer Institut
für Angewandte Strahltechnik (BIAS), Germany INVESTIGATION OF WAVE PROPAGATION
IN COMPOSITES AS REQUIREMENT FOR IMPACT DETECTION |
|
ICAS 2006-4.3S
; Y. He, F. Li, H. Zhang: Air Force Engineering Univ., China A GENERALIZED LOCAL STRAIN APPROACH
TO CONSIDERING THICKNESS EFFECT ON FATIGUE PERFORMANCE |
|
ICAS 2006-4.6S
; S. A. Bolsunovsky, V. D. Vermel*, V. V. Zinyaev*:
Moscow Institute of Physics and Technology (MIPT),
Russian Federation; *Central Institue of Aerodynamics (TsAGI), Russian
Federation COMPUTATIONAL AND EXPERIMENTAL ASSESSMENT OF CONDITIONS
FOR CUTTING OF ALLOYED STEEL IN HIGH SPEED MILLING |
|
ICAS 2006-4.8S
; G. Frulla: Politecnico
di Torino, Italy STRUCTURAL BEHAVIOR OF DAMAGED
ANISOTROPIC STIFFENED PANELS UNDER COMPRESSIVE LOADS |
|
ICAS 2006-4.8S
; R. Poul, D. Hanus: Czech Technical Univ. in Prague, Czech Republic |
|
ICAS 2006-4.9S
; A. Abedian, H. Farahpour: Sharif Univ. of Technology, Iran 3-D FEM ANALYSIS OF PLASTIC
BEHAVIOR INSIDE MMC COMPOSITES CONSIDERING DAMAGE THEORY |
|
ICAS 2006-4.10S
; H. Baier, M. Huber, J. Klammer: TU Munich, Germany |
|
ICAS 2006-4.10S
; R. M. Grothaus, S. Junghannß, T. Seung*:
EAST-4D GmbH Lightweight Structures, Germany; *LIEBHERR-Aeropsace
Lindenberg GmbH, Germany ADVANCED CONCEPTS FOR NOVEL LANDING GEAR STRUCTURES
USING HIGHLY ANISOTROPIC COMPOSITES |
|
ICAS 2006-4.11S
; P. Linde, H. de Boer*, J. Pleitner: Airbus, Germany; *Advanced Lightweight Engineering,
Netherlands SIMULATION OF STRUCTURAL BEHAVIOUR
OF FIBRE METAL LAMINATE JOINTS |
|
ICAS 2006-10.1S
; Y. Zhang, H. Wang: Northwestern Polytechnical Univ., China |
|
ICAS 2006-10.1S
; P. Konstanzer, M. Grunewald, P. Jänker, S. Storm:
EADS Corporate Research Centre, Germany AIRCRAFT INTERIOR NOISE REDUCTION
THROUGH A PIEZO TUNABLE VIBRATION ABSORBER SYSTEM |
|
ICAS 2006-10.2S
; E. Camilo, F. D. Marques, J. L. F. Azevedo*:
Univ. of Sao Paulo, Brazil; *Aerospace Technical Center-
CTA/IAE/ASE-N, Brazil AEROELASTIC ANALYSIS OF TYPICAL
SECTIONS WITH STRUCTURAL AND AERODYNAMIC NONLINEARITIES |
|
ICAS 2006-10.3S
; S. Shams, H. Haddadpour*, M. H. Sadr Lahidjani, M.
Kheiri*: Amirkabir Univ. of Technology, Iran; *Sharif Univ.
of Technology, Iran AN ANALYTICAL METHOD IN COMPUTATIONAL
AEROELASTICITY BASED ON WAGNER FUNCTION |
|
ICAS 2006-10.4S
; D. Kennedy, D. C. Patel, C. A. Featherston:
Cardiff Univ., UK |
|
ICAS 2006-10.6S
; T. Gausz, Z. Gausz: Budapest Univ. of Technology and Economics, Hungary |
|
ICAS 2006-10.6S
; E. M. Gruppioni, F. D. Marques: Univ. of São Paulo, Brazil AEROELASTIC CONTROL OF A FLEXIBLE WING WITH EMBEDDED
PIEZOELECTRIC ACTUATORS |
|
ICAS 2006-10.7S
; A. J. Gunnion, H. Körber*, D. J. Elder, R. S. Thomson:
CRC for Advanced Composite Structures Ltd., Australia;
*Univ. of Stuttgart, Germany DEVELOPMENT OF FASTENER MODELS
FOR IMPACT SIMULATION OF COMPOSITE STRUCTURES |
| 4. PROPULSION |
|
ICAS 2006-5.1S
; J. Zeng, J. Zhang, K. C. Huang: China Gas Turbine Establishment, China COMPUTATION OF FLOW AND HEAT TRANSFER IN A PRESWIRL
ROTOR-STATOR SYSTEM |
ICAS 2006-5.4S
; E. Janke, F. Haselbach: Rolls Royce Deutschland, Germany THE AITEB PROGRAMME: EUROPEAN RESEARCH FOR IMPROVED
HIGH PRESSURE TURBINES |
|
ICAS 2006-5.5S
; N. Pegemanyfar, M. Pfitzner: Univ. of the Federal Armed Forces, Germany DEVELOPMENT OF A COMBUSTION
CHAMBER DESIGN METHODOLOGY AND AUTOMATION OF THE DESIGN PROCESS |
|
ICAS 2006-5.5S
; A. Saharan, Q. J. Khan, R. R. Pant: Hindustan College of Engineering, India |
|
ICAS 2006-5.6S
; M. Swoboda, A. Huppertz, A. Keskin*, D. Otto*, D. Bestle*:
Rolls Royce Deutschland, Germany; *BTU-Cottbus |
|
ICAS 2006-5.6S
; A. R. Wadia, D. Christensen, J. V. R. Prasad*:
GE Aircraft Engines, USA; *Georgia Tech., USA |
| 5. Flight Dynamics and Control |
|
ICAS 2006-6.1S
; F. Al-thobaiti, A. Al-bahi: King AbdulAziz Univ., Saudi Arabia FULL ENVELOPE MISSILE AUTOPILOT DESIGN |
|
ICAS 2006-6.2S
; P. H. Iscold, F. Mol, N.S. Brasil*, B. C. O. Maciel:
Federal Univ. of Minas Gerais- UFMG, Brazil; *Instituto Tecnológico de Aeronáutica-
ITA |
|
ICAS 2006-6.2S
; I. Jebacek: Brno Univ.
of Technology, Czech Republic POSSIBILITIES AND METHODS OF IN FLIGHT LOADING MEASUREMENTS |
|
ICAS 2006-6.3S
; T. Sharma, C. Bil, A. Eberhard: RMIT, Australia OPTIMUM FLIGHT TRAJECTORIES
AND SENSITIVITY ANALYSIS FOR TERRAIN COLLISION AVOIDANCE SYSTEMS |
|
ICAS 2006-6.7S
; A.- M. Stoica: Univ. Politehnica
of Bucharest, Romania ROBUST FLIGHT CONTROL SYSTEM DESIGN WITH GUARANTEED
H-INFINITY TYPE PERFORMANCE |
|
ICAS 2006-6.8S
; M. Cook, S. Erbsloeh: Cranfield Univ., UK DEVELOPMENT OF A LOW COST FLIGHT DYNAMIC TEST CAPABILITY
FOR UAV |
| 6. SYSTEMS, SUBSYSTEMS AND EQUIPMENTS |
|
ICAS 2006-7.1S
; T. Sawata, L. Paskell, A. Dinu, J. Roadley-Battin,
M. Holme, S. Webster*, M. Royle**, J. Harris**: Goodrich Corporation, Electromagnetic Systems Technical
Centre, UK; *Goodrich Engine Control Systems; **Goodrich Power Systems |
|
ICAS 2006-7.2S
; J.- Y. Routex: Hispano-Suiza,
France AN INNOVATIVE TOOL FOR AIRCRAFT EQUIPMENT SYSTEMS INTEGRATION
AND ELECTRICAL NETWORK CHARACTERISATION |
|
ICAS 2006-7.5S
; M. Torabzadeh-Tari, L. Austrin*, S. Tidblad-Lundmark**:
Royal Institute of Technology (KTH), Sweden; *Saab
AB/Aerosystems, Sweden; **Chalmers Univ. of Technology, Sweden SIMULATION AND ANALYSIS OF A
NEW HIGH POWER DENSITY GENERATOR |
|
ICAS 2006-7.5S
; J. M. Blineau: LABINAL, France LABINAL CURRENT WORK TOWARDS THE MORE ELECTRICAL AIRCRAFT
THROUGH THE POA EUROPEAN PROGRAMME |
|
ICAS 2006-7.7S
; T. Sivarajah, A. Smith: Airbus UK, UK THE NEED FOR A MORE EFFICIENT ALTERNATIVE TO THE ENGINE
BLEED AIR OPERATED WING ICE PROTECTION SYSTEM |
|
ICAS 2006-7.9S
; J. Shi, C. Zhang, J. Duan: Beihang Univ., China HIGH SPEED OPTICAL FIBER TRANSMISSION
TECHNOLOGY FOR AVIONICS APPLICATIONS |
|
ICAS 2006-7.10S
; B. Lantto, M. Jareland: Saab Aerosystems, Sweden MODEL-BASED DIAGNOSIS STUDIES
OF COMPLEX FLUID MECHANICAL AIRCRAFT SYSTEMS |
|
ICAS 2006-7.10S
; D. Naderi, B. Dehghan, A. Abedian: Sharif Univ. of Technology, Iran OPTIMIZATION OF A SPUR GEAR PROFILE FOR MINIMUM TRANSMISSION
ERROR OF A GEAR SET USING GENETIC ALGORITHM |
| 7. SYSTEMS ENGINEERING AN SUPPLY CHAIN |
|
ICAS 2006-9.2S
; M. Gallizio, G. P. De Poli, M. Usseglio*:
Avio SpA, Italy; *Politecnico di Torino, Italy TOP DOWN CAD MODELING METHODOLOGY
FOR LOW PRESSURE TURBINE DESIGN |
| 8. AIR TRANSPORT SYSTEM EFFICIENCY |
|
ICAS 2006-8.2S
; V. P. W. Gollnick: TU Munich, Germany POTENTIAL FOR TRANSPORT EFFICIENCY
IMPROVEMENTS OF AVIATION TRANSPORTATION SYSTEMS |
|
ICAS 2006-8.3S
; M. Wagner, M. Fricke*: TU Berlin, Germany; *Berlin Univ. of Technology, Germany ESTIMATION OF DAILY UNSCHEDULED
LINE MAINTENANCE EVENTS IN CIVIL AVIATION |
|
ICAS 2006-8.5S
; M. D. Guenov: Cranfield Univ.,
UK |
|
ICAS 2006-8.5S
; J. Stankunas, K. Vaitonyte: Vilnius Gediminas Technical Univ., Lithuania |
| 9. SAFETY AND SECURITY |
|
ICAS 2006-8.1S
; Y. C. Sun: Nanjing Univ.
of Aeronautics and Astronautics, China ENTROPY METHOD OF RELIABILITY
ASSESSMENT FOR AIRCRAFT SYSTEMS |
|
ICAS 2006-9.6S
; W. Lam, C. Bil: RMIT, Australia |
|
ICAS 2006-9.7S
; H. Eißfeldt: DLR, Germany INCREASING AVIATION SAFETY BY
ASSESSING ENGLISH LANGUAGE PROFICIENCY AMONG AVIATION POFESSIONALS
|
|
ICAS 2006-9.7S
; K.- H. Keller, T. Juergensohn, M. Hunold*:
HFC Human-Factors-Consult GmbH, Germany; *Fraport AG-
Frankfurt Airport Services, Germany INTRODUCTION OF DUAL THRESHOLD OPERATION IN FRANKFURT/MAIN-
EVALUATION OF HUMAN-FACTORS FROM THE PILOT’S PERSPECTIVE |
|
ICAS 2006-9.8S
; M. Gröning: Innovint Aircraft
Interior GmbH, Germany SAFETY FOR LITTLE TRAVELERS- CHILD RESTRAINT SYSTEMS- GETTING SAFELY OFF THE GROUND |
|
ICAS 2006-9.9S
; H.- U. Doehler, B. Korn: DLR, Germany |
|
ICAS 2006-9.9S
; L. Hatfaludy: Budapest Univ.
of Technology and Economics, Hungary VIRTUAL CO-PILOT SYSTEM IN GENERAL AVIATION |
|
ICAS 2006-9.10S
; K. Rambhatla: Univ. of Ottawa
, Canada, Canada AIRCRAFT SECURITY : EVOLUTION OF COCKPIT RESOURCE MANAGEMENT
& COCKPIT VIDEO TRANSMISSION |
| 10. CHALLENGE OF THE ENVIRONMENT |
|
ICAS 2006-5.9S
; F. Noppel, R. Singh, M. Taylor*: Cranfield Univ., UK; *Rolls Royce, UK |
|
ICAS 2006-5.9S
; J. Hendricks, B. Kärcher, U. Lohmann*, M. Ponater:
DLR, Germany; *ETH-Zurich, Switzerland DO AIRCRAFT BLACK CARBON EMISSIONS
AFFECT CIRRUS CLOUDS ON THE GLOBAL SCALE ? |
|
ICAS 2006-5.10S
; L. Chaudron, J. B. Chaudron: ONERA, France AN ALGEBRAIC APPROACH TO AGGREGATE SUBJECT RESPONSE
IN AIRCRAFT NOISE MANAGEMENT |