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These ABSTRACTS are standby for oral presentation in case ABSTRACTS are withdrawn from an appropriate session.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 :

ICAS2008-1.1 ST: P. R. Caixeta Jr., A. M. Abdalla, F. D. Marques, F. M. Catalano: Univ. of São Paulo, Brazil

AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN

ICAS2008-1.4 ST: P. H. A. O. Iscold, G. A. S. Pereira, L. A. B. Torres: UFMG, Brazil

DEVELOPMENT OF A SMALL UNMANNED AIR VEHICLE WITH MINIMUM SENSORS PHILOSOPHY

ICAS2008-1.5 ST: C. K. Patel, I. M. Kroo*: Acuity Technologies Inc., USA; *Stanford Univ., USA

THEORETICAL AND EXPERIMENTAL INVESTIGATION OF ENERGY EXTRACTION FROM ATMOSPHERIC TURBULENCE

2. AERODYNAMICS :

ICAS2008-2.1 ST: K. Mohamed, S. Nadarajah, M. Paraschivoiu*: McGill Univ., Canada; *Concordia Univ., Canada

KRYLOV RECYCLING TECHNIQUES FOR UNSTEADY SIMULATION OF TURBULENT AERODYNAMIC FLOWS

ICAS2008-2.1 ST: T. Kurotaki, T. Sumi, T. Atobe: JAXA, Japan

LARGE EDDY SIMULATION AROUND 2-D AIRFOIL WITH NATURAL TRANSITION AT HIGH REYNOLDS NUMBERS

ICAS2008-2.2 ST: T. Imamura, H. Ura, Y. Yokokawa, K. Tanaka*, T. Hirai*, K. Yamamoto: JAXA, Japan; *Ryoyu Systems Ltd. Co., Japan

OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL

ICAS2008-2.3 ST: B. Epstein, S. Peigin*: The Academic College of Tel-Aviv, Israel; *Israel Aerospace Industries, Israel

HYBRIDIZATION OF HETEROGENEOUS 3D CFD DISCRETIZATIONS VIA DIRECT FLUX OPTIMIZATION

ICAS2008-2.3 ST: A. Chupakhin, A. Cherevko: Lavrentyev Institute of Hydrodynamics, Russian Federation

MODERN MATHEMATICAL METHODS IN AERONAUTICAL SCIENCES

ICAS2008-2.4 ST: N. Kuratani, M. Yonezawa, H. Yamashita, S. Ozaki, T. Ogawa, S. Obayashi: Tohoku Univ., Japan

WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION

ICAS2008-2.5 ST: H. Xiao, Z. Liu, D. Wu: NPU, China

AERODYNAMICS CHARACTERISTICS OF HYPERSONIC VEHICLE IN NEAR SPACE

ICAS2008-2.64 ST: D. C. Sun, X. H. Jia*, X. G. Liang*: NPU, China; *Luoyang Opto-Electro Technology Development Center, China

CFD RESEARCH FOR AIR-TO-AIR MISSILE WITH LATERAL JET CONTROL

ICAS2008-2.7 ST: H. D. Cerón-Muñoz, F. M. Catalano, R. F. Coimbra*: EESC-USP, Brazil; *IFI-CTA, Brazil

PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION

ICAS2008-2.10 ST: S. Lee, L. Cho, J. Cho: Hanyang Univ., Korea

UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BY USING THE TIME-DOMAIN PANEL METHOD

ICAS2008-2.10 ST: G. Quaranta, A. Guardone, D. Muffo: Politecnico di Milano, Italy

COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS

ICAS2008-2.11 ST: L. Ayuso, R. Sant, L. Plágaro: Universidad Politecnica de Madrid, Spain

AERODYNAMIC OPTIMIZATION OF A BLENDED WING BODY

ICAS2008-3.1 ST: J. M. Su, B. F. Song: NPU, China

LOW REYNOLDS NUMBER TANDEM OR DIAMOND WING UAV AERODYNAMICS CENTER RESEARCH BASED ON RESPONSE SURFACE METHOD

ICAS2008-3.3 ST: M. Sohn: Korea Air Force Academy, Korea

DELTA-WING VORTEX CONTROL BY APEX STRAKE AND MICRO LEADING-EDGE FLAP

ICAS2008-3.4 ST: L. M. Shao, B. F. Song: NPU, China

EXPERIMENTAL RESEARCH OF FLAPPING-WING PROPULSION FOR MICRO AIR VEHICLES

ICAS2008-3.5 ST: T. Wan, C. K. Huang: Tamkang Univ., Taiwan

NUMERICAL SIMULATION OF FLAPPING WING AERODYNAMIC PERFORMANCE UNDER GUST WIND CONDITIONS

ICAS2008-3.5 ST: S. A. Prince, J. Bhatti: City Univ., UK

AN EXPERIMENTAL AND COMPUTATIONAL COMPARISON OF THE LOW SPEED AERODYNAMICS OF SQUARE AND CIRCULAR SECTIONED BODIES

ICAS2008-3.7 ST: E. Erdem, K. Kontis: The Univ. of Manchester, UK

THE INVESTIGATION OF DEPENDENCE OF LOW FREQUENCY MOTION ON UPSTREAM FLOW CONDITIONS IN HYPERSONIC FLOWS

ICAS2008-3.7 ST: G. Ichikawa, K. Kasai, S. Motogoe: Shizuoka Univ., Japan

ESTIMATION OF THE INFLUENCE OF PROFILE ERROR ON AERODYNAMIC PERFORMANCE FOR LOW-REYNOLDS-NUMBER AIRFOILS

ICAS2008-3.8 ST: J. M. Early, S. Raghunathan: Queens Univ. Belfast, UK

EXCRESCENCES EFFECTS IN AERODYNAMICS

ICAS2008-3.9 ST: D. Li, B. Chen: China Academy of Aerospace Aerodynamics, China

AN APPROXIMATION METHOD FOR THE NUMERICAL SIMULATION ON UNSTEADY FLOWS AROUND SMALL-DISPLACEMENT MOVING OBJECTS

ICAS2008-3.10 ST: A. Nagy, J. Rohács, T. Régert: Budapest Univ. of Technology and Economics, Hungary

INVESTIGATION ON THE EFFECT OF HYDRODYNAMIC MEMS ON AIRFOIL

3. MATERIALS AND STRUCTURES :

ICAS2008-7.3 ST: T. Urik, M. Malis: Brno Univ. of Technology, Czech Republic

INNOVATIVE COMPOSITE STRUCTURES FOR SMALL AIRCRAFT

ICAS2008-7.4 ST: A. Calabrò: CIRA, Italy

AN ORIGINAL SYSTEM TO MEASURE ADAPTIVE STRUCTURE PARAMETERS USING FIBER OPTIC

ICAS2008-7.4 ST: B. Rocha, A. Fonseca*, A. Suleman**: IDMEC/IST, Portugal; *ICCTAE/IST, Portugal; **Univ. of Victoria & IDMEC/IST, Canada

ON THE DEVELOPMENT OF METHODS AND TECHNIQUES FOR AIRCRAFT STRUCTURAL HEALTH MONITORING

ICAS2008-7.5 ST: J. Tessmer, U. Pfeiffer, A. Wetzel: DLR, Germany

IMPACT RESISTANCE, DAMAGE TOLERANCE AND NON-DESTRUCTIVE DAMAGE DETECTION FOR SANDWICH STRUCTURES: ANALYSIS AND TESTING

ICAS2008-7.6 ST: A. Ng: AeroStructures Technologies, Australia

SUITABILITY OF DIFFERENT CRACK GROWTH MODELS FOR ANALYSING MULTI-SITE DAMAGE IN AIRCRAFT STRUCTURAL CONFIGURATIONS

ICAS2008-7.7 ST: F. Marulo: Univ. of Naples, Italy

PRACTICAL AEROELASTIC CALCULATIONS FOR LIGHT AIRPLANES

ICAS2008-7.7 ST: F. Y. Wan, B. F. Song, T. X. Yu: NPU, China

HEALTH MONITORING FOR AEROCRAFT STRUCTURE SYSTEM BY HARMONIC WAVELET TRANSFORM

ICAS2008-7.9 ST: Y. Lu, S. L. Lu, G. Z. Lu: NPU, China

INTEGRATED PREDICTION OF MACROSCOPIC PROPERTIES OF COMPOSITES BASED ON FINITE ELEMENT COMPUTATIONAL MICROMECHANICS

ICAS2008-7.11 ST: S. Hernandez, A. Baldomir, J. Mendez: Univ. of Coruna, Spain

SIZE OPTIMIZATION OF AIRCRAFT STRUCTURES

ICAS2008-7.11 ST: A. Boillot: Messier-Dowty, France

FROM BEAM MODELS TO GLOBAL 3D MODELS FOR ROBUST LANDING GEAR DESIGN

ICAS2008-9.4 ST: S. Khosoussi, M. Rezaee, A. Abedian: Sharif Univ. of Technology, Iran

FEM MICRO-MECHANICAL ANALYSIS OF DELAMINATION PHENOMENON IN IMC LAMINATED COMPOSITES USING DAMAGE THEORY

ICAS2008-9.6 ST: J. T. Xiong, Z. H. D. Qiao, X. D. Yang: NPU, China

AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AEROELASTIC WING BASED ON CONTROL THEORY

ICAS2008-9.8 ST: Y. F. Hu, B. F. Song, X. Wang: NPU, China

METHODS FOR CALCULATING THE DAMAGE-RATE OF AIRCRAFT COMPONENT

4. PROPULSION :

ICAS2008-4.1 ST: A. Kargar Neghab, F. Ommi, S. M. Hoseinalipour*: Tarbiat Modares Univ., Iran; *Iran Universoty of Science and Technology, Iran

EXPERIMENTAL INVESTIGATION OF SPRAY CHARACTERISTICS OF DOUBLE-BASE SWIRL INJECTOR

ICAS2008-4.2 ST (AIAA 2008-8974): A. Seitz, K. Broichhausen, J. Seifert*, S. Donnerhack: Bauhaus Luftfahrt e. V., Germany; *MTU Aero Engines, Germany

A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY

ICAS2008-4.3 ST: T. Chatterjee, A. Gupta: Hindustan College of Engineering, India

LASER PROPELLED HYPERSONIC AIR-VEHICLE

ICAS2008-4.4 ST: M. J. Ivanov, R. Z. Nigmatullin: CIAM, Russian Federation

UNSTEADY CFD MODELING OF WHOLE GAS TURBINE ENGINE FLOW PASSAGE WITH APPLICATIONS

5. FLIGHT DYNAMICS AND CONTROL :

ICAS2008-5.2 ST: W. S. Mattos, N. C. Pereira, P. C. Greco Jr.: Univ. of São Paulo, Brazil

APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT  LONGITUDINAL STABILITY AUGMENTATION SYSTEM

ICAS2008-5.4 ST: A. L. da Silva, F. J. T. Vargas*, P. Paglione: Institute of Aeronautics and Space, Brazil; *Embraer, Brazil

A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL

ICAS2008-5.8 ST: K. Ito: CENAERO, Belgium

PARAMETRIC STUDY AND MITIGATION OF PORPOISING IN WATERBORN AIRCRAFTS

ICAS2008-5.11 ST: S. Pastorelli, A. Battezzato, G. Mattiazzo: Politecnico di Torino, Italy

FLY-BY-WIRE CONTROL OF A HELICOPTER: MULTIBODY MAIN ROTOR MODEL

6. SYSTEMS, SUBSYSTEMS AND EQUIPMENTS :

ICAS2008-6.1 ST: D. Parekh, A. Sinha: RMIT Univ., Australia

DESIGN OF A NOVEL INTELLIGENT DATA MANAGEMENT TOOL FOR HEALTH AND USAGE MONITORING SYSTEMS – DESIGN REQUIREMENTS

ICAS2008-6.2 ST: S. Steinkellner, H. Andersson, I. Lind, P. Krus*: Saab Aerosystems, Sweden; *Linköping Univ., Sweden

HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT

ICAS2008-6.2 ST: W. G. An, W. J. Li: NPU, China

A NEW EFFICIENT INTERACTIVE MULTI-OBJECTIVE EVOLUTIONARY OPTIMIZATION ALGORITHM AND APPLICATION IN ENGINEERING

ICAS2008-6.4 ST: C. P. Lawson, K. M. Lim: Cranfield Univ., UK

THE STATE-OF-THE-ART AND THE FUTURE OF WATER MANAGEMENT WITHIN FUEL TANKS

ICAS2008-6.4 ST: M. Li, R. Poovendran*, R. Falk**, A. Koepf**, M. Braun**, K. Sampigethaya, R. V. Robinson, S. Lintelman, H. Seuschek**: Boeing Phantom Works, USA; *Univ. of Washington, Germany; **Siemens Corporate Technology, USA

MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION

ICAS2008-6.5 ST: M. Arimoto, T. Kawadu*, Y. Kamiyoshihara*: ShinMaywa Industries, Ltd., Japan; *JAXA, Japan

DEVELOPMENT OF THE DISPLAY DEVICE OF POWER DISTIBUTION SYSTEM (DEVELOPMENT OF THE DEPTH FUSED 3-D DISPLAY FOR AIRCRAFT)

ICAS2008-6.6 ST: M. Birindelli, S. Chiesa*, S. Corpino*, B. Tranchero, N. Viola*: Alenia Aeronautica, Italy; *Politecnico di Torino, Italy

ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT

ICAS2008-6.6 ST: (AIAA 2008-8973): L. Phan, D. Mavris, J. -J. Charrier*, P. Thalin*, E. Garcia: Georgia Institute of Technology, USA; *Hispano-Suiza, France

PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES

7. SYSTEMS ENGINEERING AND SUPPLY CHAIN :

ICAS2008-6.10 ST: D. Cui, W. Cheng*: China Aviation Behang Univ. & AVIC II, China; *AVIC II, China

ADVANCED MANUFACTURING GRID SUPPORTING AVIATION INDUSTRY EXTENSIVE COLLABORATIVE DESIGN AND SIMULATION

8. AIR TRANSPORT SYSTEM EFFICIENCY :

ICAS2008-1.11 ST (AIAA 2008-8949): R. L. Thomas, D. G. Thomas*: Paratech Parachutes, USA; *Thomas Aerospace Corporation, USA

DESIGN ANALYSIS OF AN AIRCRAFT PARACHUTE RECOVERY SYSTEM FOR VERY LIGHT JETS

ICAS2008-8.1 ST (AIAA 2008-8967): G. P. Buoni, K. M. Howell: NASA, USA

LARGE UAS OPERATIONS IN THE NAS - THE NASA 2007 WESTERN STATES FIRE MISSIONS

ICAS2008-8.3 ST: M. Brunet, P. Malbéqui, W. Ghedaifi: ONERA, France

A NOVEL APPROACH TO AIR TRANSPORT SYSTEM ENVIRONMENTAL IMPACT EVALUATION THROUGH PHYSICAL MODELLING AND SIMULATION

ICAS2008-8.9 ST: T. Muehlhausen: DLR, Germany

THE USE OF MODELS FOR ATM VALIDATION: FROM AIRPORT EXTENSION PROGRAMS TO THE AIR TRANSPORT SYSTEM OF THE FUTURE

ICAS2008-8.11 ST: H. Lenz, S. Amelsberg*: DLR, Germany; *T U Berlin, Germany

GENERATION OF HIGH ACCURATE 4D TRAJECTORIES FOR TAKE-OFF AND DEPARTURE

ICAS2008-8.11 ST: S. R. Conway: The Boeing Company, USA

TOWARDS 4D TRAJECTORY MANAGEMENT: CONTAINMENT AND THE USE OF RNP IN CONSTRAINED TERMINAL AIRSPACE

ICAS2008-11.4 ST (AIAA 2008-8886): R. A. Paielli: NASA, USA

TACTICAL CONFLICT RESOLUTION USING VERTICAL MANEUVERS IN ENROUTE AIRSPACE 

ICAS2008-11.6 ST (AIAA 2008-8902): M. D. Tandale, P. K. Menon: Optimal Synthesis Inc., USA

RAPID PREDICTION OF AIR TRAFFIC FOR TRAJECTORY BASED OPERATIONS

ICAS2008-11.8 ST (AIAA 2008-8922): E. Smith: The MITRE Corporation, USA

OPERATIONAL ACCEPTABILITY OF ISSUING RNAV/RNP PROCEDURE CHANGES IN FUTURE TERMINAL ENVIRONMENTS

ICAS2008-11.11 ST (AIAA 2008-8961): C. Brinton, B. Wood, S. A. Engelland*: Mosaic ATM Inc., USA; *NASA, USA

MICROSCOPIC ANALYSIS OF AIRPORT SURFACE SEQUENCING

9. SAFETY AND SECURITY :

ICAS2008-9.3 ST: L. M. B. C. Campos, J. M. G. Marques: Instituto Superior Técnico, Portugal

ON THE PROBABILITY OF COLLISION FOR CLIMBING AND DESCENDING TRAJECTORIES RELEVANT TO AIR TRAFFIC MANAGEMENT

ICAS2008-9.7 ST: J. A. Herreria, J. Bueno, M. Valmorisco: ISDEFE, Spain

SAFE AUTOMATIC FLIGHT BACK AND LANDING OF AIRCRAFT (SOFIA)

10. CHALLENGE OF THE ENVIRONMENT :

ICAS2008-4.7 ST: G. Fleming, A. Malwitz, S. Balasubramanian, C. Roof, F. Grandi*, B. Kim*, S. Usdrowski*, T. Elliff**, C. Eyers***, G. Horton***, D. Lee****, B. Owen****: DOT Volpe Center, USA; *Wyle Labs. Inc., USA; **EUROCONTROL, UK; ***QinetiQ, UK; ****Manchester Metropolitan Univ., UK

TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025

ICAS2008-4.7 ST: T. J. Mulder, G. J. J. Ruijgrok: TU Delft, Netherlands

ON THE REDUCTION OF NOX-EMISSION LEVELS BY PERFORMING LOW NOX FLIGHTS