ACCEPTED PAPERS - CATEGORY B – STANDBY These papers are standby for oral presentation in case papers are withdrawn from an appropriate session. Full papers will appear in the congress CD-Rom proceedings They may also be presented as posters in the Poster area
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1. AIRCRAFT AND SYSTEMS INTEGRATION
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ICAS2010-1.2ST1: K. Sibilski, J. Zurek, A. Zyluk: Air Force Institute of Technology, Poland |
ICAS2010-1.5ST1: D. D. Smith, A. T. Isikveren, R. M. Ajaj*, et al: Univ. of Bristol, UK; *Swansea Univ., UK MULTIDISCIPLINARY DESIGN OPTIMIZATION OF AN ACTIVE NONPLANAR POLYMORPHING WING |
ICAS2010-1.6ST1: F. Buysschaert, M. Yacoubi*, A. Alami*, et al: Univ. Libre de Bruxelles ULB, Belgium; *Univ. Libre de Bruxelles, Belgium |
2. AERODYNAMICS
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ICAS2010-2.2ST1: T. Ishida: Tohoku Univ., Japan FLOW COMPUTATIONS AROUND MOVING AND DEFORMING BODIES ON BLOCK STRUCTURED CARTESIAN MESHES |
ICAS2010-2.3ST1: J. A. de Oliveira Neto, E. Basso*, J. L. F. Azevedo: ITA, Brazil; *Instituto de Aeronautica e Espaco, Brazil CALCULATION OF HIGH-LIFT FLOWS USING STRUCTURED AND UNSTRUCTURED GRIDS |
ICAS2010-2.4ST1: M. R. Chiarelli, M. Cagnoni, M. Ciabattari, et al: Univ. of Pisa, Italy HIGH ASPECT RATIO WING WITH CURVED PLANFORM: CFD AND FE ANALYSES |
ICAS2010-2.4ST2: J. M. Hospers, H. W. M. Hoeijmakers: Univ. of Twente, Netherlands |
ICAS2010-2.5ST1: K. Zhang, W. P. Song: NPU, China INFINITE SWEPT-WING REYNOLDS-AVERAGED NAVIER-STOKES COMPUTATIONS WITH FULL eN TRANSITION CRITERION |
ICAS2010-2.7ST1: M. Kanazaki, S. Jeong*: Tokyo Metropolitan Univ., Japan; *Tohoku Univ., Japan DATA MINING BASED MULTIPOINT DESIGN OF NEXT GENERATION TRANSONIC WING WITH SMALL SWEEP BACK |
ICAS2010-2.7ST2: N. Wood, G. Schrauf*: Airbus Operations Ltd, UK; *Airbus Operations GmbH, Germany NATURAL LAMINAR FLOW FOR TRANSPORT AIRCRAFT APPLICATIONS |
ICAS2010-2.8ST1: A. Sigal: Shehafim R&D, Israel AN ENGINEERING LEVEL PREDICTION METHOD FOR NORMAL-FORCE INCREASE DUE TO WEDGE SECTIONS |
ICAS2010-3.1ST1: M. Koike, T. Wakamatsu: Akashi National College of Technology, Japan EFFECTS OF TURBULATORS ON WINGS AT LOW REYNOLDS NUMBERS |
ICAS2010-3.1ST2: Y. F. Zhang, Z. Li, W. Song, et al: NPU, China LIFT AND THRUST CHARACTERISTICS OF THE FLAPPING WING MICRO AIR VEHICLE |
ICAS2010-3.2ST1: M. Matejka, P. Pick, L. Popelka*, et al: Czech Technical Univ. in Prague, Czech Republic; *AS CR, Czech Republic |
ICAS2010-3.2ST2: F. Rasi Marzabadi, M. R. Soltani, M. Masdari: Sharif Univ. of Technology, Iran EXPERIMENTAL INVESTIGATION OF THE LEADING-EDGE ROUGHNESS ON THE BOUNDARY LAYER OF A PLUNGING AIRFOIL |
ICAS2010-3.4ST1: A. Mazelet: Snecma, France DEVELOPMENT OF A CONTRA ROTATIVE PROPELLERS AEROACOUSTIC RIG |
ICAS2010-3.5ST1: R. Bura: Institut Teknologi Bandung, Indonesia LARGE-EDDY SIMULATION OF TRANSITIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS (SWBLIS) IN HYPERSONIC FLOWS |
ICAS2010-3.8ST1: O. Almeida, J. Roberto Barbosa, R. H. Self*, et al: ITA, Brazil; *Institute of Sound and Vibration, UK AEROACOUSTICS OF SINGLE SUBSONIC JETS: VALIDATION AND INDUSTRIAL APPLICATION |
ICAS2010-9.9ST1: B. Zhu, Z. D. Qiao, W. P. Song: NPU, China NUMERICAL SIMULATION OF WING FLUTTER BASED ON MULTIGRID METHOD |
ICAS2010-9.9ST2: W. P. Song, R. F. Xu, Z. H. Han: NPU, China STUDY ON THE IMPROVED KRIGING-BASED OPTIMIZATION DESIGN METHOD |
ICAS2010-2.10ST1: H. Kawazoe, S. Abe, T. Matsuno, et al: Tottori Univ., Japan LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A BUSEMANN-TYPE SILENT SUPERSONIC BIPLANE |
ICAS2010-2.11ST1: A. Cenko: NAVAIR, USA |
ICAS2010-6.10ST1: H. M. Choi, M. H. Ryu, J. S. Cho: Hanyang Univ., Korea AERODYNAMIC DESIGN AND EXPERIMENTAL STUDY ON THE DUCTED FAN VTOL MAV |
3. MATERIALS AND STRUCTURES
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ICAS2010-8.3ST1: P. Hintikka, M. Wallin, O. Saarela: Aalto University, School of Science and Technology, Finland THE EFFECT OF MOISTURE ON THE INTERLAMINAR FRACTURE TOUGHNESS OF CFRP LAMINATE |
ICAS2010-8.4ST1: L. Ferrer: Snecma, France USE OF STEEL IN AERONAUTIC JET ENGINES AND EQUIPMENTS FOR SAFRAN GROUP |
ICAS2010-8.4ST2: J. -W. Lee, J. -W. Kim, H. -G. Kim: Korea Aerospace Research Institute, Korea |
ICAS2010-8.6ST: H. Cui, Y. Li, S. Koussios*, et al: NPU, China; *DUT, Netherlands PARAMETRIC EVALUATION ON THE CURVED PART OF COMPOSITE T-JOINTS BASED ON NUMERICAL SIMULATION |
ICAS2010-8.9ST1: M. Leite Ribeiro, R. Afonso Angélico, V. Tita: Univ. of São Paulo, Brazil PROGRESSIVE FAILURE STUDY OF COMPOSITE CYLINDRICAL STRUCTURES |
ICAS2010-9.6ST1: T Ahmad, R Varatharajoo: Univ. Putra Malaysia, Malaysia BIRD IMPACT TESTS ON F5 AIRCRAFT CANOPY |
ICAS2010-9.7ST1: V. Weissberg, A. Green, H. Mey-Paz: Israel Aerospace Industries, Israel |
ICAS2010-9.7ST2: R. Doubrava, V. Strnad: VZLU, Czech Republic |
ICAS2010-9.8ST1: B. Li, J. P. Wen, Z. C. Yang, et al: NPU, China |
ICAS2010-10.6ST1: M. Liu, F. Hu*, H. Gao**, et al: Xi'an Jiaotong Univ. & MOE Key Lab. for Strength and Vibration, China; *Xi'an Jiaotong Univ., China; **Xi'an Jiao-tong Univ., China THE CRACK-DETECTED COATING SENSOR AND ITS APPLICATIONS IN R&M OF AIRCRAFTS |
ICAS2010-9.10ST1: B. Landkof, H. Abramovich, O. Igudisman: Technion, Israel |
ICAS2010-9.10ST2: Y. Li, Z. C. Yang: NPU, China PROBABILISTIC FLUTTER ANALYSIS AND RISK ASSESSMENT OF AN AIRFOIL |
4. PROPULSION
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ICAS2010-4.1ST1: A. Zammit, M. Kim, J. Bayandor: RMIT Univ., Australia BIRD-STRIKE DAMAGE TOLERANCE ANALYSIS OF COMPOSITE TURBOFAN ENGINES |
ICAS2010-4.3ST1: W. Y. K. Chan, D. J. Mee, M. K. Smart, et al: Univ. of Queensland, Australia BOUNDARY LAYER COMBUSTION FOR VISCOUS DRAG REDUCTION IN PRACTICAL SCRAMJET CONFIGURATIONS |
ICAS2010-4.4ST1: H. Fleischer: EADS Deutschland GmbH, Germany AERODYNAMIC AND AEROACOUSTIC INVESTIGATION OF ROUND AND RECTANGULAR FREE JET CHARACTERISTICS |
ICAS2010-4.6ST1: H. Lalit, V. Chernoray, J. Larsson*: Chalmers Univ. of Technology, Sweden; *Volvo Aero Corporation, Sweden |
5. FLIGHT DYNAMICS AND CONTROL
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ICAS2010-5.4ST1: D. P. T. Ferreira, P. Paglione*, C. D. P. S. Silva**: EMBRAER & ITA, Brazil; *ITA, Brazil; **EMBRAER, Brazil DESIGN OF FLIGHT CONTROL SYSTEMS CONSIDERING THE MEASUREMENT AND CONTROL OF STRUCTURAL MODES |
ICAS2010-5.6ST1: L. M. B. C. Campos, J. M. G. Marques*: CCTAE/IST, Portugal; *CCTAE/ULHT, Portugal ON THE MAXIMIZATION OF CONTROL POWER IN LOW-SPEED FLIGHT FOR A FLYING-WING CONFIGURATION |
ICAS2010-6.3ST1: A. Maqsood, T. H. Go: Nanyang Technological Univ., Singapore |
ICAS2010-6.4ST1: H. van Dijk, A. de Reus: NLR, Netherlands |
ICAS2010-6.6ST1: P. Garrec, P. Cornic: THALES, France MAGIC ATOLS : MICROWAVE AND GPS INTEGRATED COOPERATIVE AUTOMATIC TAKE-OFF AND LANDING SYSTEM |
ICAS2010-6.7ST1: H. Xiao, C. Liu: Chinese Flight Test Establishment, China THE SIMULATION RESEARCH OF THE LOW ALTITUDE PENETRATION FLIGHT TESTING TECHNOLOGY |
ICAS2010-6.7ST2: Z. Li, Y. Hou*, C. Liu**: Chinese Flight Test Establishment, China; *Northwestern Polytechnical University Xi’an, China; **Shanghai Aircraft Design Institute, China THE FUSION FOR COMPOSED NAVIGATION INFORMATION AND ACCURACY ESTIMATION IN FLIGHT TEST |
ICAS2010-6.8ST1: D. Greer, R. Mudford, D. Dusha, et al: ARCAA, Queensland Univ. of Technology, Australia |
ICAS2010-5.10ST1: A. R. da Silva Filho, F. R. F. Reis, G. A. Santana, et al: Federal Univ. of Minas Gerais, Brazil DEVELOPMENT AND EVALUATION OF STRATEGIES FOR PILOTING ASSISTANCE FOR LIGHT AIRCRAFT |
6. SYSTEMS, SUBSYSTEMS AND EQUIPMENT
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ICAS2010-7.1ST1: J. Gauci, D. Zammit-Mangion: Cranfield Univ., UK |
ICAS2010-7.4ST1: G. Balducci, T. Prado, P. O. Bousquet*: Messier-Bugatti, France; *DGA Techniques Aéronautiques, France PRESENTATION OF TEST RESULTS ON ELECTRICALLY ACTUATED NOSE LANDING GEAR |
7. SYSTEMS ENGINEERING AND SUPPLY CHAIN
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ICAS2010-7.9ST1: J. -L. Voirin: THALES, France METHOD & TOOLS TO SECURE AND SUPPORT COLLABORATIVE ARCHITECTING OF CONSTRAINED SYSTEMS |
ICAS2010-7.11ST1: B Nagel, T Zill, M Hepperle: DLR, Germany CHALLENGES ARISING FROM THE ADVANCED INTEGRATION OF TECHNOLOGIES AIMING AT SYSTEM LEVEL IMPROVEMENTS |
8. AIR TRANSPORT SYSTEM EFFICIENCY
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ICAS2010-11.1ST1: D. Troegner: DLR, Germany |
ICAS2010-11.3ST1: Z. Michaelides: The Univ. of Liverpool, UK THE DEVELOPMENT OF FUTURE AIR TRANSPORT SECTOR MODELS: A PARADIGM SHIFT |
ICAS2010-11.5ST1: A. Andreeva, S. Suzuki, E. Itoh*: Univ. of Tokyo, Japan; *Electronic Navigation Research Inst., Japan GUIDELINES FOR FLIGHT TIME MANAGEMENT AND SUSTAINABLE AIRCRAFT SEQUENCING |
ICAS2010-11.7ST1: K. Kageyama, Y. Fukuda: ENRI, Japan STUDY ON ANALYSIS METHOD OF HORIZONTAL FLIGHT DISTANCE FOR ATM PERFORMANCE ASSESSMENT |
ICAS2010-11.7ST2: O. Techakesari, J. J. Ford: Queensland Univ. of Technology, Australia AUTOMATED CENTRALISED SEPARATION MANAGEMENT WITH ONBOARD DECISION SUPPORT |
ICAS2010-11.10ST1: D. Karikawa, M. Takahashi, H. Aoyama*: Tohoku Univ., Japan; *ENRI, Japan PERFORMANCE VISUALIZATION IN AIR TRAFFIC CONTROL USING COGNITIVE SYSTEMS SIMULATION |
ICAS2010-11.10ST2: P. U. Lee, N. M. Smith*, T. Prevot, et al: San Jose State Univ., USA; *NASA Ames, USA |
9. SAFETY AND SECURITY
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ICAS2010-10.8ST1: M. Tanaka: Trust Tech JAPAN, Japan FLIGHT TAXIING GUIDANCE SYSTEM FOR AIRCRAFT ON BOARD AIRCRAFT CARRIER |
10. CHALLENGE OF THE ENVIRONMENT
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ICAS2010-5.2ST1: K. Chircop, M. Xuereb, D. Zammit-Mangion*, et al: Univ. of Malta, Malta; *Cranfield Univ., UK A GENERIC FRAMEWORK FOR MULTI-PARAMETER OPTIMISATION OF FLIGHT TRAJECTORIES |
ICAS2010-5.7ST1: M. Battipede, A. Della Corte, M. Vazzola, et al: Politecnico di Torino, Italy INNOVATIVE AIRPLANE GROUND HANDLING SYSTEM FOR GREEN OPERATIONS |
ICAS2010-5.7ST2: S. Bagassi, D. Francia, C. A. Persiani: Univ. of Bologna, Italy TERMINAL AREA "GREEN" OPTIMIZATION USING JOB-SHOP SCHEDULING TECHNIQUES |