PRELIMINARY PROGRAMME

ICAS2010-3.7 ST1: A. Touyeras: Snecma, France
FLOW-CONTROL CONCEPTS FOR COMPRESSORS
ICAS2010-3.7 ST2: Y. L. Li, D. Li, Y. Yang: NPU, China
THE STUDIES OF OPTIMUM WAVELENGTH CHOICE IN DISTRIBUTED ROUGHNESS LAMINAR FLOW CONTROL TECHNIQUE
ICAS2010-3.8 ST1: 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
ICAS2010-3.9 ST1: T. Atobe, T. Ikeda: JAXA, Japan
FLOW INSTABILITY AROUND A 2D AIRFOIL INDUCED BY ACOUSTIC DISTURBANCES AT LOW REYNOLDS NUMBERS
ICAS2010-9.9 ST1: F. AREVALO, H. CLIMENT*, P. GARCIA-FOGEDA**: AIRBUS MILITARY & UNIV. POLITECNICA DE MADRID;
*AIRBUS MILITARY; **UNIV. POLITECNICA DE MADRID, Spain
NONLINEAR TIME-DOMAIN STRUCTURE/AERODYNAMICS COUPLING IN SYSTEMS WITH CONCENTRATED STRUCTURAL
NONLINEARITIES
ICAS2010-9.9 ST2: W. P. Song, R. F. Xu, Z. H. Han: NPU, China
STUDY ON THE IMPROVED KRIGING-BASED OPTIMIZATION METHOD FOR AERODYNAMIC DESIGN
ICAS2010-2.10 ST1: H. Kawazoe, S. Abe, T. Matsuno, et al: Tottori Univ., Japan
LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A BUSEMANN-TYPE SILENT SUPERSONIC BIPLANE
ICAS2010-2.11 ST1: A. Cenko: NAVAIR, USA
LESSONS LEARNED IN 30 YEARS OF USING CFD FOR STORE SEPARATION
ICAS2010-3.10 ST1: L. Popelka, D. Simurda, M. Matejka, et al: Institute of Thermodynamics, Czech Republic
BOUNDARY LAYER TRANSITION, SEPARATION AND FLOW CONTROL ON AIRFOILS AND BODIES IN CFD, WIND-TUNNEL AND IN-
FLIGHT STUDIES
ICAS2010-3.11 ST1: O. Almeida, B.S. Aflalo, R. Lauterjung Queiroz, et al: ITA, Brazil
NUMERICAL INVESTIGATION OF A HELMHOLTZ RESONATOR
ICAS2010-6.10 ST1: J. S. Jang, S. Y. Wie, D. J. Lee: KAIST, Korea
EXPERIMENTAL AND NUMERICAL STUDY OF DUCTED FAN UAV
ICAS2010-6.10 ST2: 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
ICAS2010-4.4 ST: P. R. Pamidi, J. Maronick, X. Chen*, et al: MSC.Software Corp, USA; *GE Research, USA
AIRCRAFT CABIN NOISE COLLABORATIVE STUDY USING FRF-BASED ASSEMBLY OF ROTORDYNAMIC SYSTEM
ICAS2010-8.2 ST1: M. Tehrani, A. Abedian: Sharif Univ. of Technology, Iran
A FEM STUDY OF THE OVERLAPPING RATIO EFFECT ON SUPERPLASTIC FORMATION OF METAL MATRIX COMPOSITES
ICAS2010-8.3 ST P. Hintikka, M. Wallin, O. Saarela: Helsinki Univ. of Technology, Finland
THE EFFECT OF MOISTURE ON THE INTERLAMINAR FRACTURE TOUGHNESS OF CFRP LAMINATE
ICAS2010-8.4 ST1: M. T. Heitzmann, C-T. Ng, B. Lindenberger*: Univ. of Queensland, Australia; *Univ. of Stuttgart, Germany
SINGLE PLANT BASED NATURAL FIBRE COMPOSITE FOR AIRCRAFT CABIN INTERIOR MATERIALS MADE SOLELY FROM THE
CASTOR PLANT
ICAS2010-8.4 ST2: J. W. Lee, J. W. Kim, H. G. Kim: Korea Aerospace Research Institute, Korea
FULLY ISOTROPIC LAMINATES WITH UP TO TWENTY SEVEN PLIES
ICAS2010-8.5 ST1: R. Pullin, J. J. Hensman*, M. J. Eaton, et al: Cardiff School of Engineering, UK; *Univ. of Sheffield, UK
AUTOMATED FATIGUE FRACTURE DETECTION, IDENTIFICATION AND LOCATION IN STEEL STRUCTURES USING ACOUSTIC
EMISSION
ICAS2010-8.6 ST1: E Dubovikov: TsAGI, Russian Federation
INFLUENCE OF COMPOSITE WING ELASTICITY PARAMETERS ON STRUCTURE WEIGHT
ICAS2010-8.6 ST2: H. Cui, Y. Li: NPU, China
NUMERICAL SIMULATION OF THE FAILURE OF COMPOSITE T-JOINTS BASED ON COHESIVE ZONE MODEL
ICAS2010-8.7 ST1: S. Wang, M. Liu, X. Wang*: Xian Jiaotong Univ.; *The First Aircraft Design Institute, AVIC, China
EFFECT OF STRESS ON MULTIPLE SITE DAMAGE
ICAS2010-8.8 ST1: M. G. Zielonka: MSC.Software Corp, USA
ADAPTIVE MESH REFINEMENT: ADVANCES AND APPLICATIONS TO THE ANALYSIS OF AEROSPACE STRUCTURES.
ICAS2010-8.9 ST1: A. Abedian, H. Dastoom Latleily: Sharif Univ. of Technology, Iran
NONLINEAR RESPONSE ANALYSIS OF FGM PLATES UNDER THERMO-MECHANICAL LOADS USING HIGHER ORDER SHEAR
DEFORMATION THEORIES
ICAS2010-8.9 ST2: M. Leite Ribeiro, R. Afonso Angélico, V. Tita: Univ. of São Paulo, Brazil
PROGRESSIVE FAILURE STUDY OF COMPOSITE CYLINDRICAL STRUCTURES
ICAS2010-9.1 ST1: P. Xue, C. F. Qiao, J. J. Tian, et al: NPU, China
CRASHWORTHINESS STUDY OF A CIVIL AIRCRAFT SUB-FLOOR STRUCTURE
ICAS2010-9.2 ST1: S. Hernandez, A. Baldomir, J. Diaz, et al: Univ. of La Coruña, Spain
DESIGN OPTIMIZATION OF STRUCTURES CONSIDERING UNDAMAGED AND
ICAS2010-9.3 ST1: J. Liu, Y. Li: NPU, China
OPTIMIZATION INVERSION ON CONSTITUTIVE MODEL PARAMETERS OF BIRD IN THE SIMULATION OF BIRD STRIKE ON THE
AIRCRAFT
ICAS2010-9.4 ST1: A. Pistek: Brno Univ. of Technology, Czech Republic
ANALYTICAL METHOD FOR LIMIT LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES
ICAS2010-9.5 ST1: M. G. Zielonka, S. C. Rennich: MSC.Software Corp, USA
A GENERAL APPROACH FOR THE COUPLING OF EXISTING SIMULATIONS COMPONENTS INTO A GENERAL MULTIPHYSICS
ENVIRONMENT.
ICAS2010-9.6 ST2: T Ahmad, R Varatharajoo: Univ. Putra Malaysia, Malaysia
BIRD IMPACT TESTS ON F5 AIRCRAFT CANOPY
ICAS2010-9.7 ST1: V. Weissberg: Israel Aerospace Industries, Israel
TOWARDS AN ALL COMPOSITE FASTENERLESS COMPOSITE WING
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