TWELFTH INTERNATIONAL CONFERENCE

ON COMPOSITE MATERIALS

Paris, France

5th - 9* July 1999

EXTENDED ABSTRACTS

Chairman,

Thierry Massard

1CCM12 Association loi de 1901

UB/TIB Hannover 89

121 561 364

TABLE OF CONTENTS

Plenary SessionsThe Therrno-StructuralComposite Niche: a Global Approach for PierreBitin, Senior Vice-President. SNECMA,France 1

Progress andSuccess

Recent Progress in Experimental and Computational Mechanics Isao Kimpara, Professor, University ofTokyo, JAPAN 2

Approach to Performance Assessment ofComposite MaterialsStructures

Advance in Composites Research forMarine Structures Yapa D.S. Rajapakse, Office ofNaval Research, USA 3

Advanced Cement-Based Composites SurendraP. Shah,Northwestern University, USA 4

Driving Forcesfor cost-effective composites: new demands on JanAnders E.Hanson, Professor, EcoleFid&rale 5

materials andprocesses Polytechnique de Lausanne, SWITZERLAND

Bio-CompositesModelling Laminate Recycled Polymeric Matrix Composites Antonio Avila, UniverstdadeFederal deMinas Gerais, 6

BRAZIL

The Agave Fibers in Composite Materials RldhaBen Cheikh, EcoleNationaled'Ingenieurs de 7

Tunis, TUNISIA

Analysis ofExplanted Silicone/Silica Composite Breast Implants HaroldBrandon, Washington University, USA 8

Occupational Health Aspects andRegulations onAirborne Fibrous BengtChristensson,National Institutefor WorkingLife. 9

and Non-Fibrous Dust SWEDEN

Flow Orientation of Vegetable Fibres Ignazio Crivelli Visconti, DepartmentofMaterials and 10

Production Engineering, ITALY

Surface Modification to Improve the ImpactPerformance of Natural Jayamol George, Katholieke UniversitettLeuven, 11

Fibre Composites BELGIUM

An Object-Oriented Finite Element Processing Model for Oriented Pascal Hubert,Forintek CanadaCorp., CANADA 12

Strand Board Composites

Tensile &Impact Properties ofBanana Glass Hybrid Polyester LalyAPothanKattqpurathu,Mahatma Gandhi 13

Composites University, INDIA

Biodegradable Polyester MatrixReinforced withHemp Fibres -Effect AndreasKeller, FAT, SWITZERLAND 14

ofFibre RefinementbySteam Explosion

Natural Composites Based on Cellulosic Fibres and Polypropylene HansLilhott, Rise NationalLaboratory, DENMARK 15

Matrix - Their Processingand Characterisation

Performanceofa Prosthetic Ihtevertebral Disc John Muzzy, GeorgiaInstitute ofTechnology, USA 16

Characterization of Wood-Polypropylene Composite Sandwich System Karthik Ramani, Purdue University, USA 17

Incorporation of Unsaturated Polyester Based Matrix Composites into JeanNoelReygrobellet, Ecole desMines D'Ales, 18

aPolypropylene for Recycling PRANCE

Processing and Properties ofBiodegradable Composites Basedon Analia Vazquez, Institute OfMaterial Science and 19

Materbi and Sisal Fiber Technology, ARGENTINA

Computational Model of Soft Composite Materials for Artificial Pasquale Vena, Politecnko AlMilano - DJ.S, ITALY 20

Ligaments Analysis

Ceramic Matrix and C/C CompositesPreparation and Characterization of Metal/Si02 Nanocomposite Yimin Chen,National University of Defense 21

Aerogels Technology, POP.REP. CHINA

Effects of Ethanol and Polyelectrolyte on theProcessing of Melissa Crimp,Michigan State University, USA 22

SiCW/AG03 Composites

Processing ofNextel 720/Mullite Composite Using Electrophoretio PamelaFairies, DefenceEvaluation Research Agency, 23

Deposition UNITEDKINGDOM

CUC (Hybrid) Fibers for Enhanced CreepResistance Vincent Hammond, UniversityofVirginia, USA 24

Molecular Design of Precursors and Application in CMCs Preparation HaifengHu, National University ofDefense 25

Technology, POP. REP. CHINA

Synthesis and Characterization of novel Organosilicon Precursor HaifengHu, National University ofDefense 26

Technology, POP. REP. CHINA

Near Net Shape Manufacture ofCMC Components WalterKrenkel, DIM. Stuttgart, GERMANY 27

High Temperature StableCeramic Composites Components on the EdwinKroke, TUDarmstadt, GERMANY 28

BaseofPolyborosilazane and Nano-Metallopoly(Boro)SilazanePrecursors

Development ofCyanate Ester Based Carbon/Carbon Composites for Shivakumar Kunigal, North CarolinaA&TState 29

Complex Parts University, USA

Stress-Rupture, Stress-Relaxationand Overstressing: aMonotonic and EdgarLara-Curzio, OakRidgeNational Laboratory, 30

Fatigue LoadingBehavior ofa2-D Woven Ceramics USA

Processing and Properties of Fullerene (C-60) Derived Carbon/Carbon Chen-Chi Ma, National Tsmg-Hua University, 31

Composites TAIWAN

MatrixComposite atRoom andElevated Temperatures Shankar Mall, Wright-Patterson AirForce Base, USA 32

Properties and Thermostructural Behavior ofCarbonFelt-Carbon SongheMeng, Centerfor Composite Materials, POP. 33

Composites at Ultra-High Temperature REP. CHINA

Impact Response of Innovative Sandwich Composites in Low, Uday Vaidya, Tuskegee University,At, USA 34

Intermediate Velocity and High StrainRate Scenarios

Synthesis ofa Ceramic Composite Material: SiC-(W.Mo)Si2 Francisco JavierNarcisoRomero.UmversidadDe 35

Alicante, SPAIN

High Temperature Deformation Behavior ofNanocrystalline Ceramics Yutaka Shinoda, JapanScience andTechnology 36

Composite Corporation,JAPAN

Improved Magnetization of 3Y-Zro2/Ba-Hexaferrite Composite by Yoshikazu Suzuki,National Industrial Research 37

Post-Plastic Deformation Institute ofNagoya, JAPAN

Creep ofa C/C-SiC Composite Under Interlaminar Shear Loading at BSrbel Thelicke, Fraunhofer-Institut fUr 38

High Temperatures Werkstoffmechanik, GERMANY

Preparation ofAlumina Matrix for CeramicComposites by Sol-Gel JiayuXiao, National University ofDefense Technology, 39

Method POP. REP. CHINA

Thermomechanical Characterization ofSiC Fiber Tows and HeeMann Yun,NASA LewisResearch Center, USA 40

Implications for CMC

Porosity Influence on the Characterization ofCMC(C/C-SiC) RodolfoM. Aoki, DLR (German Aerospace Center), 41

Specimens GERMANY

Effects of Fiber/Matrix Interface and its Composition on Mechanical Narottam P. Bansal, NASALewisResearch Center, 42

Properties ofHi-Nicalon/CelsianComposites USA

Thermomechanical Behaviour of2D-SiC/SiC Composites with S. Bertrand, Laboratoryfor Thermostructural 43

Nanoscale-Multilayered (PyC-SiC)N Interphases Composites UMR5801, FRANCE

Heat Treatment Effects on Tensile Strength and Microstructure of Ramakrishna Bhatt, USArmy, USA 44

BN/SiC Coated SiC Fiber Preforms

Improvement of Unidirectional Composite Strength Probabilistic ChrisMichelBoyer, Pole Universitaire Leonardde 45

Model Vinci, FRANCE

Failure of2.5DCF-SiC Composites Creep Tested in Tension SAverineDarzens.LERMAT.URA CNRSI3IZISMRA, 46

FRANCE

Factors Controlling Stress Rupture of Fiber-Reinforced Ceramic James A. Dicarlo, NASALeRC, USA 47

Composites

Mechanical Behavior of2D SiC/SiC Composite with a Multilayered Philippe Forio, Laboratoire deComposites Thermo- 48

Matrix. Structuraux,FRANCE

Mechanical Properties ofMoSi2-Al203 Composites Processedby SHs Christian Gault,EcoleNationale Supe"rieure des 49

Ceramiques Industrielles, FRANCE

Modeling ofOxidation Behavior ofCeramicCoated Carbon/Carbon HiroshiHatta, The Institute ofSpace andAstronautical 50

Composites Science, JAPAN

Evaluation ofBonding Strength Between SiC-Cating and C/C Yasuo Kogo, Science University of Tokyo, JAPAN 51

Composite

Performances ofY2Sk>5 CoatingSystem for Carbon/Carbon MasayukiKondo, JAPAN 52

Composites

Probabilistic Ceramic Matrix Composite Behavior Pappu Murthy, NASALewisResearch Center, USA 53

Damage Modelling ofa Satin Sepcarb Composite Jean-Noel Perie, LMT-ENS - Cachan, FRANCE 54

ModularDesign ofNanocomposite Structures Based on a A1203 and Van An Phan, National Centerfor Technical Progress 55

Mechanisms of Structural Transformations Therein of Vietnam, VIETNAM

Importance ofFiber/Matrix Bonding in SiC/Bn/SiC on Mechanical F. Rebillat, Laboratoire de Composites Thermo- 56

and Interfacial Properties Structuraux, FRANCE

CMC DamagePrediction byMicro-Macro Modelling ClaudeRospars, MEDYSYS, FRANCE 57

Preparation and Properties ofCeramic Matrix Composites with Mitsuhiko Sato, AdvancedMaterial Gas-Generator, 58

Tyranno Fibersas theReinforcement JAPAN

Mechanical Properties and Intcrfaoial Characterization of Nextel 312 RichardSchalek, Michigan State University, USA 59

Fiber/Bti/Blackglas Composites

CrackMicrostructureDuring the Carbonization ofCarbon Fibre JanSchulte-Fischedtck, GermanAerospace Centre 60Reinforced Plastics to Carbon/Carbon Composites (DLR), GERMANY

Composite StructuresInfluence of Curvature onFoam Core Sandwich Panels MarkBattley, Industrial Research Limited,NEW 61

ZEALAND

Mechanics of Elliptical Sandwich Shells with Elliptical Facings Victor Birman, University ofMissouri-RoUa, USA 62

Ply Wavinesson In-Plane Stiffiiess of Composite Laiiunates CiminiJunior CarlosAlberto, Federal University of 63

MinasGerais, BRAZIL

Effect of Boundary Conditions on the Ballistic Response of Fabric EMsCepus, UniversityofBritish Columbia, CANADA 64

Structures

Thermoelastic Stress Analysis ofSandwich Construction Tee- Joints JaniceDulieu-Barton, University ofLiverpool, 65

Loadedin Compression UNITEDKINGDOM

Application of a Damage Model for High Rate Deformation of HamidEskandari, McQill University, CANADA 66

Composite Structures

AThird-OrderApproach forthe Reinforcement of Concrete Shells AntonioJoaquim MendesFerreira,DEMEGI-FEUP, 67

with External Composite Laminates PORTUGAL

Exact Three-Dimensional Models forLayered Composites SergeiGalileev,RUSSIA 68

Finite Element Damage Prediction of Composite Structures LaurentGomet, EcoUt Centrale Nantes,FRANCE 69

Stress Analysis ofa Hybrid Flywheel Rotor UsingaModified SungKyu Ha, Hanyang UniversityMeckEng.,KOREA 70

Generalized Strain Assumption

Failure Prediction ofa Tapered Composite I-Beam Graham Hill University ofBristol, Aerospace 71

Department, UNITEDKINGDOM

Use of a Linear Viscoelastic Constitutive Law to Model the Time RolandHinterhoekL UniversityofInnsbruck, 72

Dependent Behaviour of Orthotropic Glassfibre Reinforced Plastic AUSTRIA

Variable Axial Compositesfor Complexly LoadedHith-Speed Rotors WernerHufenbach, Technische Universitat Dresden, 73

GERMANY

ACubic Boundary Element for Two-Dimensional Composite Plates ChyanbinHwu,NationalChengKung University, 74

Containing Holes TAIWAN

Compression After Impact (CAI)Behavior ofCF/PixaStiffened Panels Takashi Ishikawa, NationalAerospace Laboratory, 75

forHSCTEmpennage JAPAN

AnInterfaceModelfor Prediction ofInitiation and Propagation of NiklasJansson, Chalmers University ofTechnology, 76

Delamination SWEDEN

Failure of Solid andHollow S2-Glass FnWEpoxy ThickTubesUnder A.S. Kaddour, UMIST, UNITEDKINGDOM 77

Biaxial Compression

Yield Analysis ofInterfaces FrancoiseKrasuckl, Laboratoire deModeUsation en 78

Mecanique deJussleu,FRANCE

Comparison ofDamage Behaviour in Structures Reinforced by Knitted BernardLamy,EcoleCentrale de Nantes, FRANCE 79

and WovenTextile Fabrics

Design and Testing of In-Situ Consolidated Thick High Performance GeorgeLeon,ElectricBoat Corp.GeneralDynamics, 80

Thermoplastics USA

OptimumDesign ofFilamentWound Multizonal Composite Shells Evgeny V. Morozov, University ofNatal, REP. of 81

SOUTHAKRICA

Non LinearProgressive Delamination ofComposite PlatesUnder AleksanderMuc, Insitute ofMechanics andMachine 82

Cyclic Shear Loadings Design, POLAND

Experimental and Theoretical SmdyofDynamio Stochasticity Effects Oleg Naimark, Institute ofContinuousMedia 83

Under CrackPropagation in Structures. Mechanics, RUSSIA

UltralightFRP Pseudospherical Shell GX. Narasimham, Vikram Sarabhai Space Center, 84

Composites Group, INDIA

Numerical Analysis ofMicro-MacroCoupled Behaviors forFibrous Yoshihiro Ohnishi, Osaka University, JAPAN 85

Composites Under LargeDeformation

Effect of the Skin-Core Interphase Properties onthe Tensile Stress G.C. Papanicolaou, University ofPatras, GREECE 86

Distribution Field ofan Al-GFRP Sandwich Beam

^identification ofthe Through-Thickness Stiffnesses of Thick Fabrice Plerron, Ecole desMines de Saint-Etienne, 87

Laminates by Inverse Analysis FRANCE

Design and Optimisationofa NewRunComposite Bicycle Crank Marino Quaresimin, UniversityofPadova, ITALY 88

AVariationalModel for Stress Analysis in Textile Composites AjitK.Roy, AirForceResearch Laboratory, USA 89

Experimental andNumerical Investigations of the Forming of Olivier Rozant,EcolePolytechnique Fidirale de 90

Thermoplastic Sandwiches Lausanne, SWITZERLAND

Sandwich Beams with Mid-Plane Asymmetry Subjected io Lateral Nihar Satapathy, University ofDelaware, Newark, 91

Loads-Analysis andDesign USA

The Effect of Internal Liner on Mechanical Behavior ofComposite MahmoodShokrieh, IRAN UniversityofScienceand 92Pressure Vessels Technology, IRAN

Curing Stresses inThickPolymer Composites, Part 11: Management GraemeStringer, DefenceEvaluationResearch 93of Residual Stresses Agency, UNITEDKINGDOM

Damage Accumulation in Composite Laminates Due to a Hiroshi Suemasu, Sophia University, JAPAN 94Concentrated Load

Width andCurvature Effects onthe Damage Tolerance ofComposite AnthonyJ Vlzzini, University ofMaryland, USA 95Sandwich Structures

A StrenghAnalysis Method for Composite Plates with Multiple Bolted YangXu, ShenyangAircraft Research Institute, POP. 96

Joints REP. CHINA

Determination ofComposite Material Constants byDirectNumerical Jin Yeon Cho, Dept. ofAerospaceEng. SeoulNational 97

Simulation Univ.,KOREA

Two Layer Composite Shell forAnchored Refractory Lining Alain Gasser, ESEMOrleans,FRANCE 98

Computing

Transient Thermoelastic Stresses Through the Thickness of an Frid&rtc Jacquemin, Ecole desMines de Saint-Etienne 99

Anisotropic Laminated Tube , FRANCE

Fatigue of3D Sandwich-Fabric Composites Under Core Shear HermawanJudawisastra, Katholieke Universiteit 100

Loading Leuven, BELGIUM

Dynamic Stability ofa Composite Cantilever Beamwith Viscoelastic Tae-WooKim, Dept. ofAerospaceEng. SeoulNational 101Properies Under a Follower Force Univ., KOREA

PredictionoftheLongTermMechanical Behaviour ofComposite Patricia Krawczak, Ecole desMines deDouat, 102

Pipes Under Internal Pressure from ShortTerm Tests FRANCE

Discussion on the Failure Mechanism ofRe Beams Strengthened in AlexLi.IUTdeREIMS, FRANCE 103ShearbyExternally Bonded CFRP Sheets

Modelling ofthe Mechanical Behavior of Fabric-ReinforcedRubber- Pierre-YvesManach, Laboratoire GinieMicanique et 104

Like Materials Matiriaux, University de Bretagne Sud,FRANCE

Design ofSandwich Structures with Curvature VmcentManet, EcoleNationaleSup&rieure desMines 105

deSaint-Etienne, FRANCE

Determination ofComposite Effective Characteristics and Complex ValeriyMatveenko, RUSSIA 106

Modulesfor Shell Structuresfrom the Solution of Inverse Problem

Sub-Structure Method foran Assembly ofStructures Invariant inOne StephaneMeo.CNRSMarseille,FRANCE 107Direction

Flexural Behaviour of Anisotropic Composite Discs Subjectedto JoaoPedroNunes, Universidade doMinho, 108

Three-Point SupportBending Teste PORTUGAL

Folded Honeycombs- Fast and Continuous Production ofthe Core and JochenPflug, Katholieke Universiteit Leuven, 109a Reliable Core-Skin Bond BELGIUM

Analytical Discrete Model Non-Symmetric Sandwich Panels at ValeryPolyakov, Institute ofPolymerMechanics, 110

Bending LATVIA

External Pressure Testing of Large Scale Composite Pipe GuillermoRamirez, The University ofKansas, USA 111

Investigation of the Structural Damping ofthe Full-Scale Helicopter Bosko Rasuo, UniversityofBelgrade, YUGOSLAVIA 112

Main RotorBlade Made ofComposite Laminated Materials

Residual Stress Minimization to Prevent Process-Induced Damages in Eui-Sup Shin, Dept. Aeronautics& Space Eng., Tohoku 113

Thick-Walled CFRPPipes Univ., JAPAN

Compressive Failure ofNotched Composite-Honeycomb Sandwich SimonMark Spearing, Massachusetts Institute of 114

Panels Technology, USA

Failure Modes inComposites Joints, a Finite Element Study Efstathios Theotokoglou, .GREECE 115

Genei^TheoryformeModellmgofLsminatedMulti-LayerPlates OleThyboThomsen,DENMARK 116

and its Application for the Analysis ofSandwich Panels with PlyDrops

Open Hole Compression andTension Characterization ofStitched GregoryDean Tracy, University ofCalifornia, Santa 117

Hybrid Carbon Fiber Reinforced Epoxy Composite Laminate Barbara, USA

Post-Failure Modelling ofBallistically Impacted Composites Jack Van Hoof, Carleton University, CANADA 118

Analysis of Thermoelastic Laminated Composite Plates and Shells on Viktor Verijenko, University ofNatal, REP. ofSOUTH 119

the Basisof3-D Analytical Solutions and Higher-Order Theory AFRICA

Asymptotic GDQ Solutions ofUminatedCircular Conical Shells CJ>. Wu, National ChengKung University, TAIWAN 120

Study of Process-Induced Interlaminar Stress of Composite Laminates Zhenglin Yang, Dalian University qfTechnology, POP. 121

byFine Integration Method REP. CHINA

Design/OptimisationDesign of Laminated Plates with Required In-Plane, Coupling and MichelGrediac, LERMES-UniversiteBlaise Pascal, 122

Bending Stiflhesses Using Non-Standard Ply Angles FRANCE

DesignofBeam Structures with Braided Composites Tubes Hiroyuki Hamada,Kyoto Institute of Technology, 123

JAPAN

MuWcriterion Optimization of Urninate Stacking Sequencefer Petri Kere,Helsinki University ofTechnology, 124

Maximum Failure Margins FLNLAND

Predictionand Evaluation of Local and Global Optima in Strength PhilippeManne, Goodyear Technical Center, 125

Optimization of Composite Laminates LUXEMBOURG

Design Methodology for Buckling of Thin-Walled Laminated Lawrence Rehfield, University ofCalifornia, Davis, 126

Composite Beams r/SA

Design ofLarge Composite Structures UnderDynamic Loads with Jose Sancho.MTorresDlsenosIndustriaUs, SPAIN 127

Fatigue Assessment

Formability of Weft-Knitted Preforms SuleSavci, UniversityofNewSouth Wales, 128

AUSTRALIA

Validation ofCoda Software for IntegratedComposite Materials Graham Sims, National Physical Laboratory, UNTIED 129

Synthesis and Preliminary Design KINGDOM

DevelopmentofanOptimization Methodfor Composite Materials Ghislaine Terrel, ONERA-ULLEandLM2S,FRANCE 130

Design and Optimisation ofComposite Blade-Stiffened Panels with RodneyThomson, CRCforAdvancedComposite 131

Cut-Outs Structures, AUSTRALIA

Designingwith Anisotropy: Laminate without Membrane/flexure Paolo Vannucci, ISAT- Universlte deBourgogne, 132

Coupling and Quasi-HomogeneousAnisotropicLaminates FRANCE

Designing with anisotropy: Methods and General Results for Georges VercheryJSAT, FRANCE 133

Laminates

Computer-AidedLaminate Selection Using a GraphicalMethod Paul Weaver, Bristol University, UNITEDKINGDOM 134

OptimalDesign ofViscoelastic Composites with Periodic Yeong-Moo Yl, SpaceDivisionJCoreaAerospace 135

Microstructures Research Institute, KOREA

Durability andAgeingLongTermDurability Testing ofPolymer Composite Materials Cory P. Arendt, TheBoeing Company, USA 136

Influence ofVarious Defects on the Quality andtheDurability of Philippe Castaing,CETIM, FRANCE 137

Composite Pipes

Damage/Weight Loss Relationship UnderThermal Ageing ofPolymer Xavier Colin, ONERA-CHATILLON, FRANCE 138

Composite Laminates

Hygro-Theimal TransientAnalysis forHighly StableStructures Suzana DaMotaSilva,European Laboratoryfor 139

Particle Physics, CERN, SWITZERLAND

Isothermal Aging of an Advanced High Temperature CarbonFibre BronwynFox,Australian National University, 140

Composite AUSTRALIA

Mechanism ofThermal Spiking-Enhanced Moisture Absorptionby S.Karad, DepartmentofEngineering Materials, 141

Cyanate Ester CuredEpoxy Resin Matrices UNITEDKINGDOM

Monotoring the Durability of PPS, Nylon, and PVDFUsing in the Situ DavidEKranbuehl, College ofWilliam andMary, 142

Fdems SensingforExtended Use in the Field USA

Influenceof the Fibre/Matrix Interface onthe LongTermDynamic Virginle Lletard, Ecole desMines deDouai,FRANCE 143

and Environmental Stress Cracking Behaviour of Glass/Epoxy

CompositesInfluence of Matrix Cracks and Swellingon Moisture Absorption and Jan-ErikLundgren, RoyalInstitute ofTechnology, 144

Desorption in Cross-Ply GFRP Laminates SWEDEN

Acid Stress CorrosionofEandC Glassybrid Composites MachikoMaeda, KyotoInstitute ofTechnology, JAPAN 145

Influence of Temperature on the Durability of Composite Systems CelineMahieux, Virginia Tech, USA 146

Crack Propergation Propaties ofGFRP Laminates Under Acid Stress Kazuhlro Onodera, Waseda University, JAPAN 147

Environment

Environmental Effectsonthe Mechanical Properties of Plain Weft RolandReber,ETH-SWB, Swiss Federal Inst, of 148

KnittedCF/Peek and GF/Pet Composites Technology, SWITZERLAND

Sea Water Resistance ofModified Polycaprolactone M. Rutkowska, Gdynia Maritime Academy,POLAND 149

CorrosionBehavior and MechanismofGlassComposites in Acidic Tetsuya Sakai, Tokyo Institute Technology,JAPAN 150

Solutions

ShearStrength Caracteristics in Aged Polyester-Glass Fibre Francisco Segovia, UniversitadPolltecnica de 151

Composites Valencia,SPAIN

Moisture Resistance ofNew Glass/Epoxy-Aluminium Laminates Oleg V. Startsev, Altai State University, RUSSIA 152

EvaluationsoftheCoefficient ofMoisture Expansion Using Transient Takeshi Takatoya,Polymeric CompositesLaboratory, 153

Simulated Laminates Technology (TSL) USA

Hygrothemial Deformation ofComposite Snadwich Panels Ernest G. Wolff, Oregon State University, USA 154

Residual Stresses and Thermoplastic Adhesive Environmental Wenping Zhao, Purdue University, USA 155

Cracking

Physical and Mechanical Characterizations ofGlass/Vinyl Ester Yang Zhong, Prairie ViewA&M University, USA 156

Composite Under Environmental Cycling

FibresDust Emission and Strength Losses Dueto Handling of Reinforcement Carl-HakanAndersson, Dept. ofProduction & 157

Fibres Materials Enginenng, SWEDEN

Optimisation ofHollowglass Fibers and Their Composites IanBond, University ofBristol, UNITEDKINGDOM 158

Processing and Mechanical Properties ofa Plasticised PVC Reinforced Jean-Yves Cavailli, INSA-Lyon, FRANCE 159

with Cellulose Whiskers

Effects ofthe Fibre Sizing on the Damageof Unidirectional Antoine Chateauminois, Ecole Centrale deLyon, 160

Glass/EpoxyComposites: FRANCE

Chemical Plating ofChopped SiC Fiber Haifeng Cheng, National University ofDefense 161

Technology, POP. REP. CHINA

Microstructure and Mechanical Properties atHigh Temperatures of Florence Delegltse, Ecole des mines de Paris,FRANCE 162

Two Nanocomposite Oxide Fibres

Direct Evaluation of Axial Compressive Properties ofCarbon Filament KazuhiroFujita, OsakaNational Research Institute, 163

AIST, JAPAN

ProcessmgaiidQiaracterizationofNewTheriiiosetNanocomposites MireyaMatos-Ruyz, INSA-Lyon,FRANCE 164

Reinforced by Cellulose Whiskers

Oxide Fibres Produced by Internal Crystallization Method and Their Sergei T. Mileiko, SolidState PhysicsInstitute, 165

Usage inCompositeTechnology RUSSIA

Longitudinal Compressive BehaviourofCarbon Fibres Naoyuki Oya, University ofLeeds, UNITEDKINGDOM 166

Microhardness ofa Pe/Pe-Composite and Polyethylene Gradient ArturPoeppeL, Technische UmversitaetHamburg- 167

Material Harburg, GERMANY

Evaluation ofAdvanced Sic Fibers for Reinforcement ofCmc Hisashi Serizawa, JWRI, Osaka University, JAPAN 168

Effect ofNrtridation on theProperties ofSiC Monofilament Nanlin Shi, Institute ofMetalResearch, CAS, POP. 169

REP. CHINA

Effect ofFiller Aggregates Structure on Composite Elastic Properties Sergei Timan, Institute ofChemicalPhysics, RUSSIA 170

The Production ofHollowCarbon Fibre from a Special Pan Precursor Simon Travis, DefenceEvaluationResearchAgency, 171

UNITED KINGDOM

Effects of Chemical Treatment on HighPerformance PoIy(P- Gwomei Wu, Chang Gung University, TAIWAN 172

Phenylene Benzobisoxazole) Fiber

Copper-Phosphate Bonded High Strength Fiber Composite Material Yue Zhuo, National UniversityofDefense Technology, 173

POP.REP. CHINA

IndustrialApplicationsMeclianicalBelMvior ofCF/Polymer Composite Laminates Under TakahiraAoki, University ofTokyo, Dept. of 174

CryogenicEnvironment Aeronautics,JAPAN

C-130 Hercules Composite FlapsFatigue Test Program JamesAyling, Hawker de Havilland,AUSTRALIA 175

Aerospace Composite Lattice Structures VyacheslavBarynln, RUSSIA 176

Are CompositesSuitable for Reinforcement of Ship Structures 7 Ivan Grabovac, Department ofDefence,AUSTRALIA 177

Compaction of Thick Composites H. Thomas Hahn, University ofCalifornia, Los 178

Angeles, USA

Fabrication of Grid Stiffened Structures: 1990S Lessons Learned, Steven Huybrechts, USAirForceResearchLaboratory, 179

Issues Encountered and MethodsDeveloped USA

Design ofComposite Wing Access Cover Under Impact Loads Alastair Johnson, German Aerospace Center (DLR), 180

GERMANY

Evaluation of Fire Performance ofComposite Materials for Aerospace Andrew Johnston, National Research Council of 181

Structural Applications Canada, CANADA

Ultra Lightweight Satellite Antenna with Stretched Surface Shigenon Kabashima, Mitsubishi Electric Corporation, 182

JAPAN

Development ofLow CostFRM Diesel Piston Sung-Chul Kim, HyundaiMotor Company, KOREA 183

Creep Rupture of3-D Woven Si-Ti-C-O Fiber / SiC Matrix Composite Toshio Ogasawara, National Aerospace Laboratory, 184

with Glass Sealant JAPAN

Nasa Space Flight Tethered Satellite - Fabrication, Flight and Post- £ Pete Scab, Cortland Cable Co., Inc., USA 185Mortem

Design ofMultifimctional Semitrailer HeinSchellem,Eindhoven University ofTechnology, 186

NETHERLANDS

In-Plane Properties ofCFRP Uininates Containing Through- Craig Steeves. Cambridge University Engineering 187Thickness ReinforcingRods (Z-Pins) Department, UNITEDKINGDOM

Composite Risers for offshore Technology Yuri TarnopolSkii, Institute ofPolymerMechanics. 188

LATVIA

Doe Automotive Composite Materials Research: Present and Future C. David Warren, OakRidgeNationalLaboratory, 189Efforts USA

Catalytic Oxidation ofCo on the Silica Aerogels Containing JingXu,National UniversityofDefense Technology, 190Nanoclusters of Metals pop, REP. CHINA

SiCf/SiC Composites for Structural Applications in Fusion Power Giacomo AieUo, CEA Saclay DRN/DMT/SERMA/LCA, 191Reactors: the Tauro Blanket FRANCE

Fatigue Model for Steel Fiber Reinforced Concrete PauhBarreto Cachim, University ofAveiro. 192

PORTUGAL

Composite Material Advances in the Recreation Industry Jerome Berg, True Temper Sports, USA 193

Tilted Sandwich Debond(TSD Specimenas Beam on Elastic LeifA. Carlsson, Florida Atlantic University, USA 194

Foundation)

Properties ofCore Materials for Sandwich Structures RichardM. Christensen, Lawrence Livermore 193National Laboratory, USA

Effect of Strain Rate and Fiber Waviness on the Compressive Behavior Isaac M. Daniel, Robert R.McCormlckSchool of 196ofCrossply Composite Laminates EngineeringandApplication, USA

Testingand Analysis ofComposite Sandwich Beams Isaac.M. Daniel, RobertR.McCormick Schoolof 197

Engineering andApplication, USA

Failure Under Multiaxial Stresses ofComponent Materials for Fiber Steve. J. Deteresa, LawrenceLivermoreNational 198

Composite Sandwich Construction Laboratory, USA

Hard and Soft Magnetic Composites in High Speed Wheels D.Howe, University ofSheffield, UNITEDKINGDOM 199

Imperfection SensitivityofModerately Thick Composite Cylindrical George.A Kardomateas, SchoolofAerospace 200Shells Engineering, USA

Failure Analysis ofThick Composite Rings Under Diametral Hassan Mahfitz, Tuskegee University's Centerfor 201

Compression AdvancedMaterial, USA

Albero Polymeric Mortar and its Possibilities in Building Construction OlivaresManuel, Universidadde Sevilla, SPAIN 202

Glass Fiber-Reinforced Plastic Poles for Transmission and Distribution DimosPolyzois, The University ofManitoba, CANADA 203

Lines: anExperimental Investigation

Failure Mode Transition in Fiber Reinforced Composites Under G. Ravichandran, California Institute of Technology, 204

Dynamic Multiaxial Compression USA

Subsonic and Intersonic Dynamic Crack Growth in Unidirectional Ares Rosakls, California Institute ofTechnology, USA 203

Composites

Dynamic mterlaminar Fracture Toughness in Polymeric Composites C. T. Sun, Purdue University, USA 206

High Strength Right Angle Joints for Civil Engineering Applications Gerard VanErp, UniversityofSouthern Queensland, 207

AUSTRALIA

Effects of Salt Water Agingonthe Post-Impact Behavior of Polymeric DavidR Veazie, Clark Atlanta University, USA 208

Composites

Sandwich Beams with Mid-Plane Asymmetry Subjectedto Lateral JackR. Vinson, Universityof'Delaware, USA 209

Loads Analysis and Optimization

Compositesin the Sea: Sorption, Strength and Fatigue YJ, Weitsman, DepartmentofMechanical & 210

Aerospace Engineering &, USA

Interphase and InterfaceCorrelationof Micro- and Macrocomposite Properties ofAdvanced AzharAbuBakar, University ofSheffield, UNITED 211

Composites Through Fragmentation Test KINGDOM

Fibre/Matrix Interface TestingUsing the Single Fibre Broutman Test Christophe Ageorges, Insitutfur verbundwerkstoffe, 212

GERMANY

Behaviour ofthe Polymer-FiberInterface Under Various Loading Tatiana Brantseva, The Univer. ofChem. Technol. of 213

Rates Russia, RUSSIA

InfluenceofTranscrystalline Interphase on Flexural Failure of Short Ming Chen, NationalSun Yat-Sen University, TAIWAN 114

Carbon Fiber Reinforced Peek Composites

Interfacial Design for Damage Tolerant Composites VesnaDamljanovic, UniversityofIllinois, USA 215

Rheological and Morphological Influences on the Viscoelastic Roger Gaertner, GEMPPM- INSA Lyon, FRANCE 216

Behaviour of Polymer Composites

Unification ofFibre/MatrixIiiterfacial Measurements with Laser Costas Galiotis, ICE/HT-FORTH, GREECE 217

Raman Microscopy

Experimental Examination of the Effect of an Interphasewith Known SimonAntonyHayes, Sheffield University, UNITED %l 8

Properties, on FragmentationProcesses Within Polymer Matrix KINGDOM

Composite Systems.

Geometric Considerations in the Experimental and Finite Element AlmaHodzic,Department ofEngineeringFETT,ANU, 219

Analyses ofthe MicrodropletTest AUSTRALIA

OntheUse and Limitations of Concentric Cylinder Models for EdgardJacobs, Katholieke Universiteit Leuven, 220

Polymer Matrix Composites BELGIUM

Modellingthe Effectofa Discrete Interphase on Fibre Fragmentation Richard Lane, Sheffield University, UNITED 221

Processes in Polymer Matrix Composite Systems. KINGDOM

On a Role of Fibre-MatrixInterfaces in the Context of Near-Surface YuriN. Lapusta, UniversitStKarlsruhe, GERMANY 222

Stability Analysis of Composites Materials

Observation of Fiber-Fiber Interactions in Fiber/Matrix Model Steffen LUtze, Universitat StuttgartIKP, GERMANY 223

Samples

MatrixStrainField Mapping AroundEmbedded Fibres Using Anders S. Nielsen, Aalborg University, DENMARK 224

PolarisedRaman Microscopy

Adhesion ofCarbon Fibersto Vinyl Ester Matrices Michael Rich, Michigan State University, USA 225

Frictional Behaviour oftheInterface in SiC Monofilament Model Dominique Rouby, INSA de Lyon, FRANCE 226

Composites with Borosilicate Glass Matrix

Evaluating theMechanical PropertiesofGlass Fibre/EpoxyInterfaces Norihiko Taniguchi, Waseda University, JAPAN 227

Usingthe Slice Compression Test

Fiber-MatrixInterfacial Stress Analysis by UsingHeterogeneous Finite Youqi Wang,Kansas State University, USA 228

Element

Fiber Fragmentation inTwin-Fibre Composite Beams by Bending Lawrence Wu, City University ofHongKong, HONG 229

KONG

Theoretical Studies on Steady-State Fibre Pull-Out XIZhang, UniversityofSydney, AUSTRALIA 230

Micromechanical and Microscopic Effects of Preprocessing on Philippe Bartolomeo, Universite de Toulon et du Var, 231

Interfacial Shear StressofGlass Fiber-Cyanate Ester Resin Composite FRANCE

Measurement ofMicro-Mechanical Interfacial Properties of AldoRobertoBoccaccini, FG Werkstofftechnik, TU 232

SiC(Nicalon) Fibre/Borosilicate Glass Matrix Composites at Elevated Ilmenau, GERMANY

Temperatures bythe Senv-Push-OutTechniqueInfluence ofCrack-Wake DebondingonMatrix Cracking Yih-Cherng Chiang, Chinese Culture University, 233

TAIWAN

Thermal Characterization of Larc Peti-5 as a Potential High Donghwan Cho, MichiganState University, USA 234

Temperature SizingMaterial

Mechanism ofAdhesion Improvement ofAramid Fibers to Epoxy LawrenceDrzal, Michigan State University, USA 235

Matricesby Elevated Temperature Treatment

Failure at Interfaces in Composite Material System Due to Thermal Efthymios Folias, University ofUtah, USA 236

Expansion Mismatch

Crystallinity andInterphase properties ofCarbon Fibre/PEEK Matrix Shang-Lin Gao, HongKong University ofScience & 237

Composites Technology, HONGKONG

Coating Icm-Oxide Fibres in a Bundle byMetal and Compound Andrew A. Kolchin, SolidState Physics Institute, 238

Layers RUSSIA

LowVelocity Impact Damage in Glare(C) Fibre Metal Laminates JeremyLallberte, Carleton University, CANADA 239

Interfacial Effecton the Mechanical Properties of Glass/Phenolic Tohru Morii, Shonan Institute ofTechnology, JAPAN 240

Composite

Effects of Fiber Surface Treatment on the Fiber Break Behavior in Shinji Ogihara, Department qfMechanical 241

Single Fiber Composite Engineering,JAPAN

Electrically Conductive Composite: Influence ofPolypyrroleParticles Philippe Olivier, Laboratoire de GinieM&canique de 242

onDynamic Mechanical Characteristics of an Epoxy Matrix Toulouse, FRANCE

Interfacial Aspects ofTwo-Fiber Reinforced Composites Using Joung-Man Park, GyeongsangNational University, 243

Electro-Micromechanical Techniques and Electrodeposition (Ed) KOREA

Adhesive Interactions in Interphases: Competition Between Acid-Base Elena Ptsanova, Institute ofPolymerResearch 244

and Diffusion Mechanisms Dresden, GERMANY

Experimental DetectionofInterphases in Glass Fibre/Polypropylene GlselaPompe, Institute ofPolymerResearch Dresden, 245

Composites GERMANY

Polypropylene Reinforced with Glass Beads. Prediction of Interface Olga Rodriguez, Materiales Compuestos. INTA, SPAIN 246

Adhesion by LGC

Interface Adhesion in Composites. Correlations Between Igc Slxto Santa,Materiales Compuestos. INTA, SPAIN 247

Measurements and Mechanical Testing Results

Fiber/MatrixDebonding in SiC/Ti Composites -Numerical and Alain Thionnet, Ecole desMines de Paris, FRANCE 248

Experimental Analysis

Compositional ControllabilityofThin Film Metal-Organic MatrixComposite Materials Synthesizedby Variable Duty Cycle PulsedPlasma Polymerizations

Preparation ofGF/PVC Composites UsingAqueous SuspensionImpregnation Technique: the Interfacial Issues

Influence ofFibre Cross-Sectional Aspect Ratio on Mechanical

Properties of Glass Fibre/Epoxy Composites

Adhesive Pressure as Failure Criterion in Micromecbaiu'cal Tests

JointsFGMs Interlayers in Diffusion BondingJoints

Progressive Damage Modelling andUltimate Failure of Out-of-Plane

Composite Structures

Life Extension of an F/A-l8 Aileron Hinge Using Bonded CompositeReinforcement

Monitoring Adhesive Bonds Using Embedded Devices

Development ofan Adhesive Joint Design and Analysis Tool

Fracture Toughness ofAdhesive Bonded Composite Joints UnderMixed Mode Loading

An Investigation into the Structural Behavior ofMonocoqueFibre

Composite Truss Joints

Analysis of Adhesively Bonded Single Lap Joints in Srim CompositesUnder Flexural Loading

Analysis of Single LapAdhesive Composite Joints with Delaminated

Adberends

Environmental Durability ofa Thermoset Adhesive Bonding ofa

Composite to Galvanized Steel

Feasibility Study ofInsulator, Adhesive, and Y-Joint Structure for theCryogenio Propellant Tank of Reusable Launch Vehicle

Stress-Strain State Investigation of Adhesive Layer in SandwichStructure ofFlyingVehicle

Strength of Adhesive BondedComposite Lap ShearJoints with and

Without EmbeddedCracks

Stresses in Double-Lap Adhesive Joints with Laminated CompositeAdherends

Bolted Joint Fracture Modes in Glass-Fiber Reinforced Polyester

J-Integral and Constraint in Adhesive Joint

Time and Temperature Dependence ofStatic, Creep, and FatigueBehavior forFRP Adhesive Joints

MatricesDendritic-Based Additives forPolymer Matrix Composites

Crystal Forms andMelting Behavior in Cold-Crystallized Vs. Melt-

Crystallized Syndiotactio PolystyreneOn-Line Dynamics ofVoid Formation upon Curing ofEpoxy Resin

Thermoplastic Composites Based on Biodegradable Matrices and

Natural Fibres

Curing of the Epoxy Resins Under MicrowaveAnd/Or ElectronBeam

Treatment

In-Situ Polymerisation ofPal2 for Thermoplastic Composite

Processing

Ab Initio InvestigationofCarbon Fiber Reinforced Plastics ApplyingPhenolic Resins

Effect of Debonding Microprocesses onParticulate Filled PolyolefinesFlow and Fracture. I. Yield Stress

Silica Filled Pa6: a Studyon theReinforcing Role Played by

Nanoparticles

Yuliang Wu, University ofTexas atArlington, USA 249

Jiarui Xu, Zhongshan University, POP. REP. CHINA 250

Lin Ye, University ofSydney, AUSTRALIA 251

Serge Zhandarov, Institute ofPolymerResearch 252

Dresden, GERMANY

MarekBarlak, WarsawUniversity ofTechnology, 253POLAND

JamesBlake, University ofSouthampton, Highfield, 254UNLTEDKINGDOM

RichardChester, Aeronautical&Maritime Research 255

Lab, AUSTRALIA

Steven Donaldson, U. S. AirForceResearch 256

Laboratory, USA

Dan Gleich, Aerospace Department,NETHERLANDS 257

Xiao-Jing Gong, LRMA, 1SAT, Universtti de 258

Bourgogne,FRANCE

Matthew FrancisHumphreys, UniversityofSouthern 259

Queensland,AUSTRALIA

PankajMallick, University ofMichigan-Dearborn, 260USA

Minghao Qin, Department ofEngineeringMechanics, 261USA

KarthlkRamani, Purdue University, USA 262

Takayukl Shimoda, JAPAN 263

Huang Song-Jeng, Moscow State Aviation Technology 264

University, RUSSIA

Liyong Tong, University ofSydney, AUSTRALIA 265

M. Y. Tsal, Department ofMechanicalEngineering, 266

ChangGungU, TAIWAN

Bart Vangrtmde, EcolePolytechnique deMontriat, 267

CRASP, CANADA

Cheng Yan, UniversityofSydney, AUSTRALIA 268

Toshiaki Yonemori, KanazawaInstitute ofTechnology, 269

JAPAN

LouisBoogh, Laboratoire de Technologie des 270

Composites etPolymeres- EPEL, SWITZERLAND

M. Woo Eamor , Department of Chemical 271

Engineering, National Cheng, TAIWAN

YongsungEom,Ecole PolytechniqueFederate de 272

Lausanne, SWITZERLAND

SanjeevKumar Garkhail. Eindhoven University Of 273

Technology, NETHERLANDS

Horialow, Polytehnica University ofBucharest, 274

ROMANIA

Alexandre Luisier, Swiss Federal Institute of 275

Technology, SWITZERLAND

Aklndele Odeshi, Technical University ofChemnitz, 276

GERMANY

Victor Oshmyan, Institute ofChemicalPhysics, RUSSIA 277

EmmanuelleReynaud, LNSA-CNRS UMRJSIO, 278

FRANCE

PropertiesofEpoxy Resin Treatedby Strong Magnetio Field Juris Rodins,,LATVIA 279

Characterization ofPhenolic Resole ResinsforCompositeHoneycomb Jahan Shafizadeh, UniversityofWashington, USA 280

Applications

Mechanical andPhysicalPropertiesInterfacial Approach ofDelamination: Possibilities and Difficulties VincentAlbouys, CNES - Centre Spatial de Toulouse, 281

FRANCE

3D DamageAnalysis Appliedto Low-EnergyImpactson Composite OlivierAUix,LMT(ENSCachan),FRANCE 282

Miro-Macro Modelling ofthe Influence of theDiscontinuous Didier Baptiste, ENSAM, FRANCE 283

Reinforced Composites Heterogeneities on Damage and Failure

Properties

Mechanical Behaviour ofPolypropylene Composites Containing SergeBastlde, Ecole desMines dAles, FRANCE 284

Ultrafine Particles. Correlations with Granulometryand

Microstructure.

ImpactBehaviourofMixed Composite Aluminium Tubes for Jirdme Bouchet,L2M- University, FRANCE 285

Automotive Applications

The Effectof Transverse Cracks on the Characteristics ofa Laminate MohammedBoutaib, LGM.T-IJI.SA Ginie 286

Micanique Toulouse, FRANCE

The Behaviour ofColumns forthe Design ofPultrudedFrames: NigelD. Brown, University ofWarwick, UNITED 287

EccentricallyLoaded Tests KINGDOM

Development ofTests to Characterize Interlaminar Fracture in Angle- LeifA. Carlsson, Florida Atlantic University, USA 288

PlyGlass/Epoxy Cylinders

Analysis of Fracture Mechanics on Skew Crack-Tip Near Interface of Haoran Chen,Dalian University ofTechnology,POP. 289

Bimaterials REP. CHINA

General Forms of Universal Connections ofElastic Fibrous Tungyang Chen, National ChengKung University, 290

Composites TAIWAN

Impact Properties of Glass Fiber Composites with Respect to Surface Seong Sik Cheon, KoreaAdvanced Institute ofScience 291

Treatment and Fiber Volume Fraction andTechnology, KOREA

On the Transitions of SecantModulus ofGFRP Laminates for Ship Sadayoshi Chiakl, Ministry ofTransport, JAPAN 292

Structure DuringFatigue Test

Transient Elastic WavesPropagating inaComposite Layered Medium Ma Chien-Ching, National Taiwan University, TAIWAN 293

for Dynamic Loadings

Experimental Studies ofImpact on Marine Composites Dominique Choqueuse, IFREMER Centre deBrest, 294

FRANCE

5lmdVofIrnrrtu3tedCoinpositeStrucmiwbyMeansofweRespoi^ Francis Collombet, LAMEF-ENSAM, FRANCE 295

Surface Methodology.

Designing Composites for Energy Absorption Under Tensile Loading Brian Cox, Cambridge University, UNITED 296

KINGDOM

The Effect of Pores on the Compressive Failure of Highly Aligned Colin Creighton, UniversityofCambridge, UNITED 297

Carbon Fibre Reinforced Epoxy Composite Rods Produced by KINGDOM

Puttrusion

Creep and Physical Aging Characterization ofaCarbon/Polyimide IsaacDaniel,Northwestern University, USA 298

Composite

Research in Progress: Fatigue ofCFRP Composites Cornelia E. Demers, University ofArizona, USA 299

Influence ofSome Structural Parameters onBoth Theoretical and Sylvain Drapier, EcoleNationaleSupirieure des Mines 300

Experimental Compressive Strength of Laminates de Saint-Etienne,FRANCE

Inipact Resistance and Tolerance ofInterleaved Run Laminates AndreDuarte.RMIT-AerospaceEngineering, 301

AUSTRALIA

Fibre Structure Influence on the Anisotropic Rheological Behaviour of MahmoudDweib, CompositesResearch Unit, Galway, 302

Glass Reinforced Thermoplastics IRELAND

Dynamic Fracture ofNotched Multilayer Composites EvgenyEvseev, MATI-Russian State Universityof 303

Technology, RUSSIA

Postbuckling Failure ofa Blade-Stiffened Carbon-Epoxy Compression Brian Falzon, Imperial College ofScience, Technology 304

Panel andMed., UNITED KINGDOM

Residual Stress Distribution and its Influence onthe Mechanical Xlao-Lu Gong, Universiti de Technologie de Troyes, 305

Behaviour ofComposite Laminates FRANCE

Testing and Failure Analysis ofa CFRP WingboxContaininga 150J Emile Greenhalgh, Defence EvaluationResearch 306

Impact Agency, UNITED KINGDOM

Investigation of the Failure Mechanisms for Delamination Growth Emile Greenhalgh, Defence EvaluationResearch 307

from EmbeddedDefects Agency, UNITED KINGDOM

Three-Dimensional Continuum Theory of Failure Propagation in AMGuz, Ukrainian Academy ofSciences, UKRAINE 308

Composite Materials in Compression

On Continuum Approximation in Stability TheoryofNon-Linear Igor A. Guz, Department cfAeronautics,Imperial 309Composites Undergoing Large Deformations College, UNITEDKINGDOMhterlaymmLaminates: Modelling and Influence onthe Free-Edge MohamedHabousst,IM2S-mSAM, FRANCE 310

Response of Integral ArmorUnder High Velocity Impact-an MahfuzHassan, Tuskegee University, USA 311Experimental and Finite Element Study

ModellmgofTnmsverse Cracking Under Uniaxial FatigueLoadingin CatherineHenaff-Gardin,LMPM,ENSMA, FRANCE 312Cross-Pry Composite Laminates: Experimental Validation

PerdictionofWorld-Wide Failure Theories: Comaprisonwith M. J. Hinton,Defence EvaluationResearch Agency, 313Experiments UNITEDKINGDOMThe Role of mterleafiBase Lainina Interphase on Toughening of MasakiHop,Mesoscapic MaterialsRes Ctr, Kyoto 314Interleaf-Toughened CFRP University, JAPAN

Buckling Optimization of Unsymmetrically Laminated Plates Under Hsuan-TehHu, National ChengKung University, 315Transverse Loads

TAIWAN

Energy Absorption Capacity ofComposite Tubes MichaelHyer, Virginia Polytechnic Institute andState 316

University, USA

Modelling Approach ofMiwbucklmgMechaaism DuringCure ina Christian Jochum,LPMM/ISGMPUntversitedeMea, 317Carbon Epoxy Laminate FRANCE

Damage Evolution Modeling in Multidirectional Laminates and the Roberts Joffe, Lulea University ofTechnology, 318ResultingNonlinearResponse SWEDEN

Effects of Test Conditions on Mode H Ititerlaminar Fracture KamroKageyama, University ofTokyo, JAPAN 319

Toughness ofFour-Point EnfSpecimens

Impact of Ply Drops Kays Kairouz, BritishAerospaceAirbus, UNITED 320

KINGDOM

Mixed ModeI and II Stress Intenstiy Factors for Edge Cracks in GeorgeKardomateas, Georgia Institute ofTechnology, 321Anisotropic Infinite Strips USA

Damage Mechanics Model for off-Axis Fatigue Behavior of MasamichiKawai, University ofTsukuba, JAPAN 322Unidirectional Carbon Fiber-Reinforced Composites at Room and

High Temperatures

ThresholdDamage Criteria forThin add Thick Laminates Subjected AfitKelkar, North CarolinaA&TState University, USA 323to Low Velocity Impact Loads

Temperature Effect onthe DamageDevelopmentofa CFRP NizarKhemiri.ENSICA Toulouse, FRANCE 324Laminates Under Cyclic Loading

ExperimentalMeasurement andNumerical Prediction ofHail Ice HyonnyKim, UniversityofCalifornia, Santa Barbara, 323

Impact Damage on Composite Panels USA

Effects of Temperature andFiber Orientation on ModeI Interlaminar HyoungSooKim, Kyushu University, JAPAN 326Fracture Toughness ofCarbon/EpoxyComposites

Optimization ofthe Performance ofGradient Composite Armor FranckKo, Drexel University, USA 327

Delamination ofTapered Composite Laminates Subjectedto KyoheiKondo, University ofTokyo,JAPAN 328Mechanical and Hygrothermal Loadings

Delamination in Mode I and H ofCarbon Fibre Composite Materials: FridericLachaud, JUTPaul Sabatier- Toulouse, 329Fibre Orientation Influence FRANCE

Free Vibration Analysis ofClamped-Free Cylindrical Shells withan Young-ShinLee, ChungnamNational University, 330Interior RectangularPlate KOREA

Effects of Temperature on ImpactFracture Behavior of Pultruded J.Z. Liang, City University ofHongKong,HONG 331

Glass Fiber-Reinforced Polyvinyl Ester) Composite KONG

The Smooth Indentationofa Cylindrical Indentor andAngle-Ply W. C. Liao,Depart CivilEngineering -Fong Chia 332

Laminates University, TAIWAN

Characteristics of Compression Failure ofCarbon/Epoxy Laminated TianXiangMao, ChineseSociety of Composite,POP. 333

Composite REP. CHINA

Effective Properties of Non-LinearOrthotropic Porous-Ductile StefanoMariani, Politecnico ofMilano, ITALY 334

Materials

Modelization ofthe Electromagnetic Behaviour of Multi-Layer Diego Martinez, ONERA.-Chatillon, FRANCE 335

Carbon/Epoxy Materials.

Analytical Model for Debonded Interfaces Associated with Pibre Neil McCartney, NationalPhysical Laboratory, 336

Fractures or MatrixCracks UNITEDKINGDOM

Isotropic and Near Isotropic Fibre Composites NeilMcCartney,NationalPhysicalLaboratory, 337

UNITEDKINGDOM

Time andTemperature Dependence of Static, Creep, and Fatigue RyosukeNakamae, KanazawaInstitute ofTechnology, 338

Behavior forCF/Epoxy Strands JAPAN

Mode II and Mixed Mode MI Delamination ofGraphite/Epoxy SylvamsNwosu, Dillard University, USA 339

Composite UnderDynamic LoadingConditions

Dynamical Characteristics of Hybrid Fiber Composites onthe Basis of Torsten Obier, InstitutfuerTechnischeAkustik, TU 340

C/Peek Dresden, GERMANY

Time-DependentBehavior of Transverse Cracking in CFRP Cross-Ply Keiji Ogi, Research Institute forAppliedMechanics, 341

Laminates Kyushu University, JAPAN

Delaminations UnderPure Mode II LoadingShowSignificant Local Isabelle Paris, The University ofBritish Columbia, 342

Mode I Behaviour CANADA

Impact Response ofCarbon Fibre Rodand Tube, with andWithout a Kevin Potter, University ofBristol AeroEng Dept, 343

TensionedKevlarOverwind UNITEDKINGDOM

Ultrasonic MeasurementofIn-Plane Moduli of Pultruded Composites RamamurthyPrabhakaran, OldDominion University, 344

USA

Damage Strength Optimization of Laminates by a Reliability-Based Fabrice Richard, LMARC, FRANCE 345

Method

Experimental Approach and Modelling ofCFRP Laminates Creep TaniaRisson, Ecole Centrale deLyon,FRANCE 346

Influence of Thermally Induced Strains onSubsequent CreepLoading, Jan Schjoedt-Thomsen,Aalborg University, Inst, of 347

Using Micro Raman Spectroscopy Mech. Engineering, DENMARK

TheEffectofDelamination Geometryonthe Buckling and Failure of GraemeShort, University ofBristol, UNITED 348

CFRP Plates KINGDOM

Damage Accumulationin Composite Structures under Repeated Loads Peter Shyprykevich,Federal Aviation Administration, 349

USA

Automated Shift for Time-Temperature Superposition Sangwook Sihn, Stanford University, USA 350

Matrix Crackingina(0/90)2S GFRP Uminate Loaded in Flexure Paul Smith, University ofSurrey, UNITEDKINGDOM 351

Creep Design Using Fiber Contents on FRTP Satoshi Somiya, Department ofMechanical 352

Engineering, Keio University, JAPAN

Experimental Investigation of Fatigue Behaviour in Composite Bolted Roman Starikov, RoyalInstitute ofTechnology, 353

Joints SWEDEN

TheInfluence ofRubber Particle Concentration on Fracture Dejan Stevanovic, ANU, FEJT,AUSTRALIA 354

Toughness ofInterlayer-ToughenedVinyl-Ester/Glass Fibre

CompositeEffect ofPekon Fracture Toughness of Glass Fabric/Phenolics Yongqi Sun, NorthwestInstitute ofTextile SCI.&TECH., 355

Composites and Toughening Mechanisms POP. REP. CHINA

Compressive Strength of3-D Heat-Resistant Composites Ippei Susuki, National Aerospace Laboratory, JAPAN 356

Mixed Numerical and Experimental Methods forTime-Dependant Catherine Szostkiewicz, L2M- UniversityLyonI, 357

Stiffness Determination for Composite Membranes Under Biaxial FRANCELoads

OnMultiple Delamination Buckling ofComposite Structures FarldTaheri,Daltech,Dalhouste University, CANADA 358

Estimation ofElectrical Conductivity of Lcf-Pp/Pani-Complex Blends Riitta Taipalus, Institute for CompositeMaterials Ltd, 359

GERMANY

HomogenizationMethod to Predict 'Three-Dimensional Permeabilties Naob Takano, Osaka Univ., Dept.Manufacturing Sci., 360

Considering Micro-Macro and Solid-Fluid Interactions JAPAN

Influenceof Electron Radiation and Water Absorption on Impact and Kazuto Tanaka, Faculty ofEngineering,Kyoto 361

CAI Fracture Behaviour ofCarbon/Epoxy Composite University, JAPAN

Enhanced Fatigue Resistance in Carbon/Epoxy Laminates by Use of Toshio Tanlmoto, Shonan Institute ofTechnology, 362

InterleafLayers oflnterleafLayers JAPAN

Modelling of FatigueBehaviour in Composites Laminates Alain Thionnet, Ecole desMines deParis, FRANCE 363

Singularity-Free Composites T. C. T. Ting, UniversityofIllinois at Chicago, USA 364

Edge-Delamination ofComposite Laminates UnderLow Cycle Nobuhide Uda, Kyushu University, JAPAN 365

Fatigue

Modellingthe Mechanical and Thermal Properties of ShortFibre Ferrie VanHattum, University ofMinho, PORTUGAL 366

Compostes

Crack Opening Displacement as a Basic Parameter for Stiffmess Janls Varna, Lulea UniversityofTechnology, SWEDEN 367

ReductionModeling in Laminated Composites

Energy Absorption During Fracture ofGMT Jan Wahlberg, Lund University, SWEDEN 368

NewMethodology toStudy the Behaviour ofDelaminated Composite Jean Christophe Watrick O.N.E.RA-IM F.L, FRANCE 369

Structures

Interlaminar Reinforcement to Composite Laminates by Distributing Wen-Xue Wang, Kyushu University, JAPAN 370

Whiskers Along the Interface

Femand Experimental Analysis ofModeHI Fracture Behavior of Youjiang Wang, Georgia Institute ofTechnology, USA 371

Composite Laminates

Deternikiation of Interfacial Fracture Toughnessfrom the WelWu, Katholieke Universiteit Leuven, BELGIUM 372

Fragmentation Test Databy Variational Models

UiwEnei^Ima^Kt Behaviors of NonstKched and Stitched Foam Sung-HoYoon,KumohNational University of 373Cored Sandwich Structures Technology, KOREAAStudyof 0°-Fibre Microbuckling in Multidirectional Composite PierreBerbinau, Imperial College ofScience, 374kuninates Technology &Medicine, UNITEDKINGDOMDamage Detection ofCFRP Laminates byUsing Localized Flexibility OH(Goicht)£yon(Ben),NIH0N UNIVERSITY, JAPAN 375Method

DelarmnationI3elwviourofZ.pinnedIjniinates Denis Cartie, Cranfteld University, UNITED 376

KINGDOM

Some Proposed Experimental Tests for Use in Finite Element Bruce Cartwright, CooperativeResearch Centrefor 377Simulation of Composite Forming Advanced Composite, AUSTRALIA

Telescoping Composite Mechanics for Composite Behavior Oirotor C. Chamis, NASA LewisResearch Center, 378Simulation USA

Damage Detectionand Vibration ControlofaDelarninated Smart Aditi Chattopadhyay,Arizona State University, USA 379

Composite Plates

Stress Based Yield/Failure Criteria for Fiber Composites RichardM. Christensen,Lawrence Livermore 380

National Laboratory, USA

Mechanisms and Models for Delamination in the Presence of Through- Brian Cox, Cambridge, UNITEDKINGDOM 381Thickness Reinforcement

Modeling Stitch Failure and Damage Growth in Stitched Warp-Knit Edward Glaessgen, National Research Council, USA 382Stiffened Composite Structures

Composite Boundary-Effects Computational Modelling Laurent Guitard, LMT (ENS Cachan), FRANCE 383

Tensile Damage in Quaternary Melamine-Foemaldehyde Composites Per-OlaHagstrand, Chalmers Universityof 384

Technology, SWEDEN

DirectNumerical Simulation of Composite Structures JeongHoKim, SeoulNational Univ., KOREA 385

The NewFracture Plane Related Strength Criterion in Comparison JochenKopp, Institute ofPlastics Processing QKV), 386with Common Strength Criteria GERMANY

Thermomechanical Behavior ofComposite Plate UsingUnmixing- Nam SeuckKweon, SeoulNational University, KOREA 387

Mixing Scheme in Hypersonic Flight

Damage in Particulate Compositeswith Hard Particles Embeddedina YoungKwon, US.NavalPostgraduateSchool USA 388Soft Matrix

Transient Waves in aLaminated Composite plate to a Point Excitation G. J?. Liu, National University ofSingapore, 389

SINGAPORE

Bridged Delamination Cracks in Curved Beams RobertaMassabo,D1SEG - University ofGeneva, 390

ITALY

Damage Behaviour ofof Glass Polyethylene Composite After Ageing - Laurence Meylheuc, ECPM-LPMT,FRANCE 391

Tension Test and X Ray Microtomlography

Delamination in Laminates with the Presence ofR-CurveEffect Hung Nguyen-Dang, LTAS-Universlty ofLiege, 392

BELGIUM

InfluenceofSpecimen Preparationand Specimen Size on Composite Thomas O'Brien, NASALangleyResearch Center, USA 393

Transverse Tensile Strength

Adapted Progressive Failure Criterion forMulti-Directional Grp- GerardSluimer, Delft University ofTechnology, 39A

Laminates NETHERLANDS

ARate Dependent Anisotropic Damage Model forComposite George Z. Voyiadjis, CEBA 3S08B,Louisiana State 395

Materialsat Elevated Temperatures University, USA

AStrain SofteningApproach to Modelling Damage Progression in Kevin Williams, DefenceResearch Establishment 396

Composite Laminates Valcartier, CANADA

Evaluation of Stress Intensity Factors and T-Sfress in an Anisotropic F. G. Yuan, NorthCarolina State University, USA 397

Plate Subjectedto Bendingand Transverse Shear Loads

Metal Matrix CompositesTitanium Alloys with Ti3 (Si,Ga)3 andTi2Ga Strengthening Natalia Antonova, NationalAcademyofScience of 398

Ukraine, UKRAINE

Processing and Properties of Continuous Fibre Titanium Matrix Axi- Jonathan Beddoes, Department ofMechanical and 399

Symmetric Composites Aerospace Engineering, CANADA

Stable andUnstable Fatigue Crack Growth inTi Mmcs PaulBowen, The University ofBirmingham, UNITED 400

KINGDOM

Bismuth-Based Thermoelectric Nanocomposites Frederic Brochin, Ecole desMines de nancy, FRANCE 401

The MicromechanicalModelling of the Short Crack Fatigue Peter BruzziMark, National University ofIreland, 402

Behaviour of Al-SiC Mmcs IRELAND

Cast Iron - a Natural Metal MatrixComposite CaroleAnn Cooper, UMIST/ Universityof 403

Manchester, UNITEDKINGDOM

Micromechanical Modellingof Ti MMCs Subjected to Transverse WeiDing, The UniversityofBirmingham, UNITED 404

Tension Loading KINGDOM

Finite Element Modeling ofInfiltration Processing Thomas Dopier, Ecole Centrale deParis, FRANCE 405

Corrosion Protection ofMmcsby Diamond-Like Caarbon Coatings Annett Dorner, TUChemnitz, LehrstuhlfUr 406

Verbundwerkstoffe, GERMANY

SiC-CuSnSi Composites by Pressureless Melt Infiltration ChristianEnglisch, EMPA Dubendorf SWITZERLAND 407

Nanostructural Characterization ofTernary Carbides in Carbon-Fibre ArminFeldhojf.Max-Planck-InstitutfUr 408Reinforced Mg-Al Matrices and Their Influence onthe Composite Mlkrostrukturphysik, GERMANYProperties

Mechanical Strength ModelingofHigh Temperature SiC James Fragomeni, Ohio University, USA 409Discontinuously Reinforced Heat Treated Aluminum Alloys

Fatigue Properties ofSCS-6/SP700 Titanium Matrix Composite AkiraFukushima, ResearchInstitute ofAdvanced 410Material Gas-Genera,JAPAN

AModelfor Bridging Crack Growth in Titanium Metal Matrix Hamouda Ghonem, University ofRhodeIsland, USA 411

Monte CarloApproach to the Creep Rupture Lifetime of Fiber Koichi Goda, Yamaguchi University, JAPAN 412Reinforced Metal Matrix Composites

Fabrication and Wear Behaviour ofanAluminium Matrix Composite Javier GoHi, SPAIN 413Reinforced witha High Content of Silicon Carbide Particles

Comparison ofLaser Modes Using Co2 Laser to Develop Surface ChaolinHu, University ofStrathclyde, UNITED 414MMCs onTi Alloys KINGDOM

Damage Progression and Residual StrengthofFatigued Open Hole W. Steven Johnson, Georgia Institute ofTechnology, 415

Hybrid Titanium Composite Laminatese USA

The Formation of Solid SolutionBand at the Surface ofTi(CN>based ShinhooKang, SeoulNational University, KOREA 416Cermets

Thermal Conductivity of Continuous CarbonFibre Reinforced Copper JurajKorab, SlovakAcademy ofScience, SLOVAK 417Matrix Composites REP.

Mechanical Properties ofGas Pressure Infiltrated Metal Matrix MariannaKouzeli, EcolePolytechnique Fide"rale de 418

Composites Containing High Volume Fractions ofCeramic Particle Lausannne, SWITZERLANDReinforcements

Bridging Mechanisms in Fibre-Reinforced Ti MMCs Jun Liu, The UniversityofBirmingham, UNITED 419

KINGDOM

Fracture SurfaceofAl203/AI-Alloy Composites Xicong Liu, National University ofDefense 420

Technology, POP. REP. CHINA

Effects oftheOxide Layer onPressure InfiltrationofAluminium EnriqueLouis Cereceda, UniversidadDe Alicante, 421

Alloys SPAIN

Reliability ofthe Strength and Fracture ProcessofSiC/Al Composite Yun Lu, Chiba University, JAPAN 422

with Different Interfacial Shear Strength

Progress & Promise in DiscontinuouslyReinforced Aluminum BenjtMaruyama. AirForce Research Laboratory, USA 423

Microstructure and Mechanical Properties ofAl Matrix Composites Kiyoshi Mizuuchi, OsakaMunicipal Technical 424Produced by LCCS Process Research Institute, JAPAN

Design Criteria foe Continuous Fibre Reinforced Mmc Bolt EricNeussl, Giesserei-Institut, GERMANY 425Connectors

Numerical Evaluation ofThermal Field in Solidifyingof Composites PetreNica, Technical University, ROMANIA 426Materials.

Fluidity and Castability Studies on Al-SiCP Composites UmaThanuSubramoniaPillai, Regional Research 427

Laboratory, INDIA

Fracture Toughness ofStructural SiCP-6061Al/6061Al Composite Shuyi Qin, ShanghaiJiao Tong University, POP. REP. 428

CHINA

in Situ Observation of Fatigue Fracture ofMmc Gaofeng Quan, XI anJiaotong University, POP. REP. 429

CHINA

Effect ofSiCReinforcement on Mechanical PropertiesofSiC/Al Metal HoJinRyu, KoreaAdvancedInstitute ofScienceand 430Matrix Composites Technology, KOREA

Elaboration and Characterization ofSiC/TiAl Composites Djanarthany Sarala, Universiti deMarne-la-Vallie, 431

FRANCE

Electron Microscopy Analysis ofSqueeze CastAH8B4033/AZ91D Gen Sasaki,Hiroshima University, JAPAN 432

Composites

Flexural Behavior ofC/C Composites at High Temperature Yoshihiro Sawada, OsakaNational Research Institute, 433

AIST-MITI, JAPAN

Thermal Fatigue ofLocally Fiber Reinforced Magnesium with Graded Wolfgang Schaff, Department ofMaterials Science (LS 434

Structure WTM), GERMANY

The Mechanical Behavior ofCeramic/Metal Laminate Under Thermal Dov Sherman, Department ofMaterials Engineering, 435

Shock ISRAEL

ThermoMechanical Response of an in Shu CopperBase Composite Shoujin Sun, University ofLeicester, UNITED 436

KINGDOM

Ballistic Impact Behaviour of SiC Fibre Reinforced Titanium MMCs Martin Thomas, Defence Evaluation & Research 437

Agency, UNITEDKINGDOM

Tensile and Compressive Response ofParticulate Reinforced Anne Whitehouse, University ofLeicester, UNITED 438Aluminium Composites at Elevated Temperature KINGDOM

TheTransverse Response of 1140+/Ti-6-4 TMCs Under Tensile Xinhua Wu, The UniversityofBirmingham, UNITED 439

Loading-in Situ Observations KINGDOM

Fatigue Crack Growth Behaviour of Angle-Ply Ti-6Al-4V/Scs-6 Asma Yasmin, The UniversityofBirmingham. UNITED 440Metal-Matrix Composites KINGDOM

Comparison Between TOA1 and Ni3Al Intermetallics Used as VicenteAmigo, UnlversidadPolittcnicaDe Valencia, 441

Reinforcements in Aluminium AlloyMMC SPAIN

Processing ofCarbon Fiber Reinforced Titanium Matrix Composites Corinne Arvieu, ICMCB - LGM. FRANCE 442

FatigueBehaviour ofUnidirectionally Continuous Attex-Fibre OlivierBeffort, EMPA, SWITZERLAND 443

Reinforced Aluminium-Based Composites

AStudyofthe Fibre/Matrix Interace in Oxide-Fibre/Nickel- V/acheslavP. Buntushldn, Russian Institute ofAviation 444

Aluminide-Matrix Composites Materials, RUSSIA

Infiltration of Fibrous Preform by aPure Metal: Modelizationofthe MichelDanis, Laboratoire GenieMicanique - KIT 445

Deformationof the Preform BordeauxI, FRANCE

Al-SiC Improves Reliabittiy ofLGBT Power Modules H.P. Degischer, Vienna UniversityofTechnology, 446

AUSTRIA

InfluenceofReactive Alloying Elements ontheMechanical Properties Sarala Djanarthany, UniversitydeMarne-la-Vallie, 447

ofCarbon/Magnesium Composites FRANCE

Continuous Fiber Reinforced Aluminum Wires MartinDoktor,AUSTRIA 448

Composite Materials of Aluminium/Granulated Slag and OctavioDcminguez, Institute de Metallurgies 449

Aluminium/Arc-Fumace Dust Prepared by Powder Metallurgy MEXICO

TechniquesProcessing ofComposite Material Using Industrial Waste Aluminum Isao Fukumoto, Universityofthe Ryukyus,JAPAN 450

Sludge

Preparation ofLaminated Ceramic/ Metal FoamsUsing an la-Situ Vtado Gergely, UniversityofCambridge, UNITED 451

Foaming Technique KINGDOM

Acoustic Emission MonitoringUnder Fatigue Conditions of Marie Jacquesson, ONERA/DMSC-Chatillon, FRANCE 452

AluminiumMatrix CompositesReinforced by Continuous Alumina

Fibres.

Development ofMagnesium Matrix Composites forPowerTrain Karl UlrlchKainer, Technische Universitat ClausthaL, 453

Application GERMANY

Synthesis ofTiC/MgComposite by Reactive Infiltration Process MakotoKobashi, Nagoya University, JAPAN 454

Dynamic Compressive Strength and Failure ofCarbonFber Woei-Shyan Lee, National ChengKung University, 455

ReinforcedAmuliniumMetalMatrix Composite TAIWAN

Strength ofA1203/Al-Alloy Composites at Elevated Temperature Xlcong Liu, National UniversityofDefence 456

Technology,POP. REP. CHINA

Mechanical Behaviour of Layered Metal Foam / Ceramic Composites AthlnaMarkakl, University ofCambridge, UNITED 457

KINGDOM

Probing Interface Failure Mechanisms in Titanium Matrix Composites Benji Maruyama,AirForceResearch Laboratory, USA 45 8

Using

Development and CharaterisationofHighDampingMagnesium Based Christine Mayencourt, EcolePolytechnique Fidirale 459

Composites Lausanne, SWITZERLAND

ICM-Oxide-Fibre/Ni3Al-Based-Matrix Composites: Fabrication, Sergei T. Mileiko, Solid StatePhysics Institute, 460

Microstructure and Some Mechanical Properties RUSSIA

Transverse Creep Responseof SiC (Trimarcl(r))/Ti-22Al-23Nb Daniel B. Miracle, AirForce, USA 461

MMCs

Interface Modification of Polymer-Derived SiC Single Fiberand Ti Takakazu Suzuki, Nat. Inst. Mater. Chem. Res., JAPAN 462

Aluminide Composites

Chemical Compatibility Between Aluminum Base Matrices and Light Jean-Claude Viala, CNRS UniversiteLyon I, FRANCE 463

Refractoty Carbide Reinforcements

MechanicalPropertiesofan AluminaFiberReinforced Aluminium Ludger Weber,EcolePolytechniqueFidirale de 464

Wire in Tension andAfter Axial Torsion Lausannne, SWITZERLAND

Superplastie Forming& Diffusion Bonding ofSiCF / Titanium Matrix YuwetXun, NanyangTechnological University, 465

Composite SINGAPORE

Preparationand Characterizationof SiC Reinforced Alumina-Yag Makoto Yoshida, Dept. ofMech.Eng. Hiroshima 466

Eutectic Composites University, JAPAN

The Distribution andthe Diffusion of Si Above Liquidus in SiCP/Al DiZhang, Shanghai Jiao Tong University, POP.REP. 467

Composite CHINA

Non Destructive Evaluation and

ReliabilityHigh Frequency Dielectric Measurements and Destructive Testingfor Gordon Armstrong, University ofStrathclyde, UNITED 468

the Investigation ofWaterUptake in Adhesively Bonded Joints KINGDOM

Composite Materials and Structures Testing by Electronic Holography DanBona, INSA Rouen, FRANCE 469

Standardised ProceduresforUltrasonic Bill Broughton, National Physical Laboratory, 470

Inspection ofPolymer Matrix Composites UNITEDKINGDOM

3DCharacterisation ofGlassFibres in Composites byConfocal AshleyClarke, University ofLeeds, UNITED 471

Microscopy KINGDOM

Ultrasonic Study of the Anisotropic Damage ofGlass-Epoxy RachidEl Guerjouma, INSA deLYON, FRANCE 472

Composites DuringHygrothermal Ageing

Acoustic EmissionNDT ofComposites Damaged byStatic and JackHale, University ofNewcastle upon Tyne, 473

Dynamic Loadingin Aqueous Environments UNITED KINGDOM

The Determination of Inner Surfaces in Composites byX-Ray AndreasHampe, BundesanstaltfuerMatenalpruefung, 474

Refraction GERMANY

Peculiarities ofThermalMeasurements at Quasi-AdiabaticLoadings Michael Kamensky, LATVIA 475

of Aramid-Plastic Shells

Complex Permittivity ofLow Loss Thermoplastic Composites Usinga Harry Ku, University ofSouthern Queensland, 476

Resonant CavityMethod AUSTRALIA

AE Studies During Fatigue Cycling ofGFRP Elliptic Springs SantKumarMalhotra, Composites Tech. Centre, 477

INDIA

Determination of Stiffness Reduction and Damage Accumulation Philippe Margueres, Umversiti de Technologie de 478

Monitoring in Composite Materials UsingUltrasonic Techniques Compiegne, FRANCE

Application ofX-Ray Microtomography to the Study ofPolymer RyszardPyrz, Aalborg University, DENMARK 479

Composites

Continuous DamageMonitoring Techniques forLaminated Composite Marnix Surgeon, Department ofMetatlurgy and 480

Materials Materials Engineering, BELGIUM

Nondestructive InspectionandEvaluationMethods for Composites JanR Weitzenboeck,DetNorske Veritas, NORWAY 481

Used in the Marine Industry

AHibridElastic Wave Method for Measuring Elastic Constants of Tsung-Tsong Wu, Institute ofAppliedMechanics, 482

Fiber ReinforcedComposite Plate N.T.U, TAIWAN

NormalisationDetermination of Elastic Properties by an Ultrasonic Technique Stephane Baste, Laboratoire deM&caniquePhysique - 483

CNRS UPRESA 546, FRANCE

Evaluation ofthe Resistance to Crack Propagation ofCeramic Matrix Jacques Lamon, Laboratoire de Composites Thermo- 484

Composites and Carbon/Carbon Composites Structuraux, FRANCE

Determination of the ElasticModuli ofCMCs at High Temperatures W. Lins, University ofVienna,AUSTRIA 485

bythe Resonant BeamTechnique

OntheDetermination of Statistical Strength Parameters of Fibres for D. Loidl, UniversityofVienna, AUSTRIA 486

Endless -Fibre Reinforced Ceramic Matrix Composites by the Fibre -

Bundle Tension Test

Marketing ofAdvanced Materials Intellectual Property MichaelMartin, Virginia Tech Intellectual Properties, 487

Inc., USA

Measurement ofBending in Specimens of Ceramic-Matrix Composites PascalReynaud, INSA deLyon, FRANCE 488

Uniaxially Loaded inTension-Compression

Building a Composites Infrastructure Graham Sims, National Physical Laboratory, UNITED 489

KINGDOM

Standardisation on Continuous Fibre Reinforced Ceramic Matrix M. Steen, Institute forAdvancedmaterials, 490

Composites NETHERLANDS

Poster SessionsAcoustic Emission in Laminated Beams Due to Fiber Fractures MatsAberg, Department ofSolid Mechanics, KTH, 491

SWEDEN

Tensile Deformation and Fracture Behaviour ofMg Matrix Composite MohdYazidAhmad, UMIST/Umversity ofManchester, 492

UNITEDKINGDOM

New Fem Analysis ofCrack Growth Behavior in Composite Materials MotookiAndo, JWRI, Osaka University, JAPAN 493

Micromechanical Analysis ofthe Effect of Temperature on Toughness Shigetoshi Araki,Kyoto Institute ofTechnology, JAPAN 494

ofCeramic Based Composites

Three-Dimensional Finite Element AnalysisofTransverseStresses in AlainMartialAte, ISAT, FRANCE 495

Sandwich Plates

Advanced Textile Composite Fixator Ring Krishna Prasanna Baidya, Research Scholar, 496SINGAPORE

Impact Behavior ofSandwich and LajninatedComposites with EvgenyBarkanov, Riga Technical University, LATVIA 497Damping

Analytical & Numerical Simulations of Experimental Determinations CristinaE. Beldica, University ofIllinois, USA 498of Linear Viscoelastic Constitutive Relations

Use of Sensors and Simulationsto Move Towards Automationofthe Simon Bickerton, University ofDelaware, USA 499Resin Transfer MoldingProcess

DamageDevelopmentDuring ThermalCyclingof Metal and Glass Aldo RobertoBoccaccini.PCwerkstoffechnik, TU 500Matrix Composites llmenau, GERMANY

Identification of Glass Fibre Defect Density UsingMuhifragmentation Chris Michel Boyer,Pole unhersitaire Leonard de 501Test

Vinci, FRANCEThe Fractal Analysis of Interphase for Polymer Composites Olga Buryan, RUSSIA 502

Experimental and Numerical ^termination of Stress Intensity Factor Donatella Cerniglia, Dipartimento diMeccanica e 503in Composite Materials Aeronautica, ITALY

Thermal Expansion Coefficient of Composites Using Interferometer Wen Chan, University of Texasat Arlington, USA 504Data

Interaction Between a Hole andan Elastic Circular Inclusion Under a Ching-KongChao, National Taiwan University of 505Remote Uniform HeatPlow Science and Technology, TAIWANOnPredicting Elastic Moduli inFormed Metals Using Equivalent Lu-Ping Chao,DepartmentofMechanicalEngineering, 506Inclusion Method Feng Chia, TAIWAN

Damage Monitoringin CFRP Laminates byMeans ofDielectric Antoine Chateauminois,EcoleCentrale de Lyon, 507Properties FRANCE

The Research of the Precursor Preparing Methodand Electromagnetic Renchao Che, National UniversityofDefense 508Properties of Composite FinePowder Technology, POP. REP. CHINA

Preparation ofSiC Absorbent by Pyrolyzing Polycarbosilane Mixed Haifeng Cheng, National University ofDefense 509with Nano-Co (Ni) Powder Technology, POP. REP. CHINA

The Effect of Processing on Fibre Alignment and Compressive Colin Creighton, University of Cambridge, UNITED 510Strength of Carbon Fibre -Epoxy Composites KINGDOM

ProbabilisticAnalysis and Failure Mechanisms ofa Brittle Material CatherineCrestia.LMT- Cachan, FRANCE 511Under Uniaxial Loading

Preparation of Carbonaceous Farticules for Production of Cast Zn-Al Luis JavierCruz RfaHo, UniversidadPontifica 512Matrix Composites by Rhecasting Method Bolivariana, COLOMBIA

Fracture Toughness of in Shu Synthetised Tinp-Al Composite Chunxiang Cui, Hebei University ofTechnology, POP. 513REP. CHINA

Optimization ofa Composite Material Box-Beamfor Use in aHaptic Pierre Cyr.McGiUUniversity, CANADA 514Device

Scale and Size Effects in the Mechanical Characterization of Peter Davies.lFREMER-CentredeBrest, FRANCE 515

Composite and Sandwich Materials

Damage-FractureTransitions as Nonlinear Problem of Defects MarinaDavydova, Institute ofContinuousMedia 516Solution. Mechanics,RUSSIA

ElasticBehaviour of Particulate Nitride Boride Composites Martine Desmaison-Brut,LMCTS- University of 517

Limoges,FRANCE

Self-Consistent ModellingofDamaged Elastic Behavior Using Frederic Desrumaux, U.T.C.,FRANCE 518

Reliability Approach

End-Effectors for Ply Placement and Consolidation inLow Cost Due Do, RMIT, AUSTRALIA 519

Composite Manufacture

Determination ofLocal Stress Concentrations in Cracked Cross-Ply Costas Gallons, ICE/HT-FORTH, GREECE 320

Composites

Simulation ofa Fiber Pushout Test in a Model Polyester/Epoxy Philippe Geubelle,AMDept. - Univ. ofIllinois at 521

Composite Urbana, USA

Computed Tomography for Non Destructive EvaluationofMetal Mario Gonzalez, ConservatoireNational desArts et 522

MatrixComposites Metiers, FRANCE

Reliability of Composite Structures - Impact Loading - Laurent Guillaumat, LAMEF-ENSAM, FRANCE 523

Interface Prediction: Inverse Gas Chromatography (LGC) and its Maria Cruz Gutierrez, Materiales Compuestos. INTA, 524

Potential Application to Fibre-MatrixAdhesion Problems SPAIN

Model ofGrowth a Irregular Eutectic Composite in Situ ( Mmcs) Edward Guzik, UniversityofMining andMetallurgy, 525

POLAND

High Strain Rate Properties of an Alumina Dispersion Reinforced Ian Hall, University ofDelaware, USA 526

Composite

Improvement of Mechanical Properties of Composites with Flexible Hiroyuki Hamada, Kyoto Institute ofTechnology, 527

Interphase JAPAN

MathematicalStudyofLaplace andYoungEquations in theCaseof TayssirHamieh.ICSI-CNRS, FRANCE 528

the ContactBetween aDrop and Fibre

Ballistic Performance ofCeramio BackedS2-Glass/Vinyl Ester AnwarulHaque, Tuskegee University, USA 529

Composites

Effect of Rib Geometry onthe Buckling Behavior ofComposite MahfuzHassan, Tuskegee University, USA 530

Isogrid Cylinders

Relationship Between Probabilistic and Continuum Descriptions of the Francois Hild, LMT-Cachan, FRANCE 531

Mechanical Behavior of Brittle-Matrix Composites

Multi-Axial Testing of Planar Composite Specimens PeterHopgood, DefenceEvaluation ResearchAgency, 532

UNITED KINGDOM

The Optimized FiberVolume Fraction for Magnetoelectric Composites Jin H. Huang, Feng Chia University, TAIWAN 533

Time andTemperature Dependence of Flexural Fatigue Strength for Masayuki Ikeda, Kanazawa Institute ofTechnology, 534

Pitch-Based CFRP JAPAN

ImprovementofResin Impregnation into GlassCloth by Silane Nobuo Ikuta, ShonanInstitute ofTechnology, JAPAN 535

Treatment inResinTransfer Molding

Drilling ofMufti-LayerPrinted Wiring Board ofAFRP UsingC02 Hisahiro Inoue, College ofEngineering, Osaka 536

Laser Prefecture University, JAPAN

Analysis of the Endothermic Behavior in theCure Process of Resole BinJiao, POP. REP. CHINA 537

Three-Dimensional Design Analysis forHystereticBehavior of TiNi- MasamichiKawai, University ofTsukuba, Inst.Eng. 538

SMA Fiber Embedded Smart Composites Meek,JAPAN

DesignandComputerModellingofSmart Composite Materialsofthe Vladimir DmitrievichKoshur, Institute of 539

Type Laminated Metal-Ceramic Composites with Neural Network ComputatioanlModelling ofRAS, RUSSIAAdaptive ControlofElastic Waves Transformations

AContainer Design foraThermally Induced Deconfinement of Francois-XavierKromm, IUTDomaine Universitaire 540

EnergeticMatter Talence, FRANCE

Use ofAcoustic Emission on Composites Structure Control AbdelouahedLaksimi, University ofTechnology of 541

Compiegne, FRANCE

The Mechanical Property Change ofa Newly Developed Epoxy Jae-RockLee, KoreaResearch Institute ofChemical 542

System at High Temperature and Oxidative Conditions Technology,KOREA

Propagation of Bridged Cracks in Fiber-Reinforced Composites. Philippe Levasseur, ONERA-CHATILLON, FRANCE 543

Modeling ofVoid Formation During ResinTransfer Molding Seong TaekLim, SeoulNational University, KOREA 544

AGeneral Approach for the Measurement ofThermal Residual Strain Qiuyun Liu, ChineseAcademyofSciences, POP. REP. 545

and Stress in SiCW/Al Composite CHINA

TheFull Controlled Deformations of Active Composite Plates and Sergey Lurie, Institute ofSmartMaterialsMechanics, 546

Shells with Shape Memory Alloys RUSSIA

The Model ofModulus DegradationNearEdgesZones for Composite Sergey Lurie, Institute ofSmartMaterials Mechanics, 547

Materials RUSSIA

Automated Consolidation in the Manufacture ofComposite LiMa, RMIT, University,AUSTRALIA 548

Components

Influenceof the Interface Strength on Local Failure Processes in Fiber ChristianMarotzke, Fed. Inst,forMaterials Research. 549

Rein-Forced Composites & Testing, GERMANY

Compression Moulding of Thermoplastic CompositeSandwich LanceMcgarva.KunglTekniskaHOgskolan (KTH), 550

Components SWEDEN

In-Situ Ultrasonic Imaging ofGF/Peek During Delamination Closure ChiakiMiyasaka, The Pennsylvania State University, 551

at Elevated Temperature USA

Ferrocement Water Tanks: Numerical Analysis and Experimental GrayMalta,Department ofResearch andPostgrad 552

Results studies, CEFET-MG, BRAZIL

Lamb Waves GenerationUsingaTransducer Embedded in a EmmanuelMoulin, IEMN, UMR CNRS 9929, DOAE, 553

Composite Plate FRANCE

Isothermal andNon-Isothermal Consolidation ofUnidirectional Joao PedroNunes, Universidade doMinho, 554

Carbon Fibre-Thermoplastic Towpregs PORTUGAL

A Finite ElementModel for Size Effectand Heterogeneity in Concrete RoquePitangueira, DEES-UFMG, BRAZIL 555

Structures

Electrical Resistance andAcoustic Emission During Cyclic Tensile Torsten Prasse, Technical UniversityHamburg- 556

Loading ofCFRP Laminates Harburg, GERMANY

Elastic-Plastic Analysis of Interfacial Stress in Model Composites JiaPurong, Northwestern Polytechnlcal University, 557

POP. REP. CHINA

Composite Material Processing in a SingleMode Cavity with Variable Yunchang Qiu, MichiganState University, USA 558

Frequency Microwaves

Acoustic Emission for CyclicDamage Evaluation on Fiberglass Pipes GuillermoRamirez, The University ofKansas, USA 559

Fabricated Following Rtp-1 Methods and Specifications.

Methodology for Evaluating ImpactDamage on Fiber Reinforced GullUrmoRamirez, The University ofKansas USA 560Composite Tubes

CureKinetic Modeling for Liquid MoldingProcesses ofEpoxy Resin EngelRenata, The Pennsylvania State University 561Composites usa

Manufacwring Composite MateriaU withEmbedded Optical Fibres John Sabu,RMIT University,AUSTRALIA 562

Characterization and Damage Evolution ofSMC Composites MohamedSayari,ENSAMParis, FRANCE 563Materials by Ultrasonic Methods

NonDestructive Inspection ofWeak Bonds in Adhesively Bonded Krtshnakumar Shankar, Australian DefenceForce 564Jomts

Academy, UNSW,AUSTRALIA

Fatigue Life Behaviour ofSnPbAg/NiTi Composite Jean-Francois Sitvaln, ICMCB-CNRS, FRANCE 565

Design ofa Fibre Reinforced Composite Bridge Deck for offshore PaulEdwardSimpson, University ofSouthern 566Applications Queensland,AUSTRALIAANovel Method for Indentation Testing Rebecca Sinclair, Manchester MaterialsScience 567

Centre, UNITED KINGDOM

Optimum Design of Grid Cylindrical StructuresUsing Homogenized Denys Slinchenko, University ofNatal,REP. of 568Model SOUTHAFRICA

Long-Term Theoretical and Experimental Analysis of Limit States of Gntda Sossou,Pridnieprovskaya StateAcademy of 569Steel-Concrete Composite Beams for Structural Use CivilEng. & Archit., UKRAINE

Interfaces in Flax Fibre-Polymer Composites Artemis Stamboutis,Imperial College , UNITED 570KINGDOM

Thin Effects in EpoxyBindersofPolymerComposite Materials OlegV.Startsev, Altai State University,RUSSIA 571

AnExamination of Heat Conduction Effect in Infrared Stress Sunao Sugimoto,National AerospaceLaboratory, 572MeasurementofCFRP Laminates JAPAN

TheComposite Material - Steel Fiber Concrete in the Highway Klara Talantova, Altai State Technical University, 573Engineering Under Continental Climate of the Altai Region Conditions RUSSIA

Effectiveness and Optimization of Fiber Bragg Grating Sensor as Liqun Tang TheHongKong Polytechnic University, 574Embedded Strain Sensor HONGKONG

Development ofaComposite Grinding Stonefor an Use of Ultra Yoji Tomita, FacultyofEngineering, Ibaraki 575Precision Processing ofGlass University .JAPAN

Life Enhancement andRepair ofStructures Using Shape Memory KellyA. Tsoi, The University ofSydney, AUSTRALIA 576

Alloy Patches

Prototype Development andDesign/Analysis ofa Composite Cab ofa Gligorce Vrtanoski, REP. ofMACEDONIA 577

Light off-Road Vehicle

Microdroplet andFragmentation Tests for Fiber/MatrixInterfacial Atsushi Wada, Science UniversityofTokyo,JAPAN 578Strength

Dynamical Modelling for die Chain Structure Formation in Biao Wang, Nanyang Technological University, 579Electrorheological Fluids SINGAPORE

Behaviour of Inflated FabricBeams atMediumPressures Christian Wielgosz, Unlversiti de Nantes, FRANCE 580

A Study ofResin Transfer Molding ProcessUsing Experimental XinranXiao, Concordia University, CANADA 581

Design Method

Optimum Design of Composite Thin-Walled LaminatedBeam by Zhen-Ying Zhang, Zhang Wei-Min, POP. REP. CHINA 582

Laminate Ranking

Automatic Mesh Generationof Joint / Interface Elements Canh Thai Nguyen, Kyoto University, JAPAN 583

Design of Hybrid Laminated Composite Sandwich Panels for Maria Antontetta Alello, University cfLecce,ITALY 584Maximum Buckling Loads: the Influence ofThermal Actions

Strength, Crack Inhitation and Crack Propagation in Fabric Based Carl-Hakan Andersson, Dept, ofProduction& 585Flexible and Semiflexible Composites MaterialsEnginertng, SWEDEN

Screening Composite Materials Based onGraphite Fillers. SergeyBiblkov, Institute ofBioChemicalPhysics RAS, 586

RUSSIA

Three-Dimensional Variational Analysis ofImpactDeformation and AlexanderBogdanovich, 3TEK, Inc., USA 587

Failure ofThickComposite Plates

AStudy of the Damping ofa Sandwich Material Function ofthe Christian Burtin, Ecole Centrale de Nantes,FRANCE 588

Interface Core/Skin by Viscoelasticity

Thermo-Mechanical Model of2-D Braided Textile Composites Joon-HyungByun, Korea Institute ofMachinery & 589

Materials,KOREA

The Effects of Different TypesofShortFibers on the Behavior and JoseMarcio Cahxto, UFMG,BRAZIL 590

Strength of Reinforced Concrete Beams

Damage Analysis in Unidirectional Composites Using Finite Element MohammedCheikh, IUTAuxerre, FRANCE 591

Reanalysis

FT-LR Studies on Imidization and EndGroup Reaction Behaviors ofa Donghwan Cho, Michigan State University, USA 592

Phenylethynyl TerminatedImide Oligomer

Finite Element Postprocess Method forComposite Plates with General Maenghyo Cho, Inha Uinversity, KOREA 593

Layups

Study onHigh Performance SiC Fibers with Low Oxygen Content Zengyong Chu, National UniversityofDefense 594

Technology, POP. REP. CHINA

Effect of Microwave Processing Upon the Structure and Properties of Richard Day, UMIST-ManchesterMaterials Science 595

an Epoxy Resin Centre, UNITED KINGDOM

Computing Uncertainties in aDelta Wing Composite Structurewith FranckDelcroix, LM2S- Universite Pierre &Marie 596

Interval-Based Methods Curie, FRANCE

Preparation ofSi-C-O-N CeramicFibersfrom Polycarbosilane Xiaolin Fan, National University ofDefense 597

Technology,POP. REP. CHINA

A Generalised Continuum Model forTextile Jean-Francois Ganghoffer, CNRS - JCSI, FRANCE 598

Lead Glass Fibre Made from Electronic Waste Valentino Gorobinskay, Institute forProblems of 599

Material Science, UKRAINE

Continuous MineralFibre-a ReinforcedElementforComposites Valentino Gorobinskay, InstituteforProblemsof 600

Material Science, UKRAINE

Fiber Optic Sensors for Strain Monitoring in Concrete Beams Repaired Alfredo Guemes, UmversidadPolitecmcaMadrid, 601

with Composite Materials SPAIN

Crushing Performance ofBraided Composite Rods HiroyukiHamada, KyotoInstitute ofTechnology, 602

JAPAN

Numerical Simulation of the Non Linear Behaviour of Reinforced SalimaHassani-Manal, LMSC CergyPontolse, 603

Concrete Structures FRANCE

Behaviour ofAlumina Refractory Composites for Temperatures Jean-Francois Hernandez, LMT-Cachan ENS 604

Lower Than 600°C. Experimentand Modelling Cachan/CNRS/ Univ. Paris 6, FRANCE

Development ofTechniques fortheJoiningofComposite Tubes S, V. Hoa, Concordia Centrefor Composites, 605

CANADA

Damage Arrest Assesment ofHSCT Composite Sandwich Panels Nai-ChienHuang, University ofNotreDame, USA 606

Incorporation ofAlumina Fibres in Glass Matrix Composites DagmarHUlsenberg, Technical University ofllmenau, 607

GERMANY

Response of Segmented-Stiflhess Composite Cylinders MichaelHyer, Virginia Polytechnic Institute and State 608

University, USA

Stitch Parameter on wterlaminer Fracture ToughnessofCFRP YutakaIwahori, Japan AircraftMFG.Co.,LTD, JAPAN 609

Laminates

Experimental Assessment ofGRC Structural Characteristics J0S0Paulo Janeiro GomesFerrelra, Instituto Superior 610

Tecnico ofLisbon, PORTUGAL

Mathematical Model for the Creep Behavior of Kevlar49 Salah Kaci, University ofTlzi-Ouzou, ALGERIA 611

Probabilistic Computational Experiments on Composite Materials Marcin Kaminskt, Technical UniversityofLodz, 612

Effective Characteristics POLAND

Stiffness Loss Due to Transverse Cracking and Splitting in Cross-Ply MariaKashtalyan, Department ofAeronautics, 613

Laminates Under Biaxial Loading Imperial College, UNITEDKINGDOM

Plastic and Fracture Properties ofComposites ValeryKisel, Institute ofSolid State Physics, RUSSIA 614

Influence oftheThermal Dependent Matrix Properties on the Residual AndreasKlisch, GERMANY 615

Stress Distribution in a Model Composite

Effect ofStacking Sequence ontheTransverseCracking in Quasi- SatoshtKobayashi, UniversityofTokyo,JAPAN 616

Isotropic Interleaved CFRP Laminates

PolymerNanocomposites for Load-Bearing Mri-Compatible Implants Pierre Koever, ETH-BWB, SWITZERLAND 617

The Method ofComputer Multifractal Paramctrization Composite DmitriyKozitskiy, RUSSIA 618

Structures

Structure Transformations and Increasing of Mechanical Properties of SergeyKulkov,RUSSIA 619

Composites

Strength and Fatigue Life ofCarbon/Epoxy Laminates Under Biaxial ChangSoo Lee, Pohang University ofScience and 620

Loading of Tension andTorsion Technology, KOREA

The Influence of Fiber Aspect Ratio onthe Tensile and Toughness D. J. Lee. School ofMechanicalEng, Yeungnam 621

Properties of Short-Fiber Reinforced Rubber University,KOREA

Bending Vibrations of Rotating Non-Uniform Composite Timoshenko Sen YungLee, National ChengKung University, 622

Beams with an Elastically RestrainedRoot TAIWAN

Climatice Exposure Experiment ofStructural Adhesives for Helicopter BinLiang, POP. REP. CHINA 623

Infiltration and Reactivity of Tic Particulates with LiquidAluminium Enrique Louis Cereceda, UnMrsidadDe Alicante, 624SPAIN

Effect of Matrix Propertyon the Strength and its Scatter of Fiber Yun Lu, Chiba University, JAPAN 625Reinforced Metal Composites

Asymptotic Approach to Micromechanics ofComposite Materials LeonidManevitch, TheoreticalDivision, RUSSIA 626

On the Vibrations ofComposite Bar in Plan Motion Mihnea IonMann, University ofCraiovaia, ROMANIA 627

A Criteria to Predict the Initiation Along Free Edges in Laminates GwenaelMarion,LGM-lUTBordeaux I, FRANCE 628

Model ofThermomechanical Behaviour of Polymers in Glass ValeryMatveenko, RUSSIA 629Transition State and its Application to the Analysis ofTechnologicalStresses in Polymers

Improvement of Cast Iron Surface by Using Alloy Powders on the YoshisadaMlchlura, JAPAN 630Mold

Size Effects on Plain and Fiber Reinforced ConcretesatHigh Loading SidneyMindess, UniversityofBritish Columbia, 631Rates CANADA

Properties of CastMagnesiumMatrix Composites at Elevated FlorianMoll, Technical University ofClausthal, 632Temperatures GERMANY

The Weibull Moduli of Si-Zr-C-0 Fiberwith Diameter Variation TetsuyaMorimoto, National Aerospace Laboratory of 633Along theGaugeLength Japan, JAPAN

Fabrication of Titanium MetalMatrix Composite Ring KatsuyoshiMoriya, AMG,JAPAN 634The PhaseComposition Specific Surfase and Mechanical Properties of EllaMoroz,Boreskov Institute ofCatalysis, RUSSIA 635Composite Materials R2O3-A1203(R=Y,La,Ce).

Description ofFatigue Failure Process for Laminated Composites A. Muc, Institute ofMechanics andMachneDesign, 636POLAND

Systhesis ofa (WSi2,W5Si3>SiC Composite Using the Reaction Francisco JavierNarciso Romero, UniversidadDe 637BetweenWCand Si Alicante, SPAIN

Effect of Polypyromellitimide TougbeneronMechanical Properties of A/ay Nema,MacromolecularResearch Centre, INDIA 638Kevlar Fibre Reinforced Polyimide Composite

Cure Dependent Creep Compliance ofan Epoxy Resin Daniel J. OBnen, UniversityofIllinois at Urbana- 639

Champaign, USA

Compatibility ofSi-C-0 Fiber and Si-C Fiber with Aluminum JinPan, Hiroshima University, JAPAN 640

Tensile Fatigue Damage Development in Plain Weave and Knitted SuryaPandita, Katholieke Universiteit Leuven, 641Fabric Composites (GFRP) BELGIUM

Numerical Modelling ofComposite Pin-Joints and Experimental FabricePierron,EcoledesMines de Saint-Etienne, 642

Validation FRANCE

Joining Mmcs to Metals Katarzyna Pietrzak, POLAND 643

Thermal Cycling Creep of Particle Reinforced Aluminium PeterPrader, Institute ofMaterials Scienceand 644

Testing, AUSTRIA

Residual Stresses in High Volume Fraction Metal Matrix Composites JoSo Quinta DaFonseca,DepartmentofMaterials- 645

University ofLeeds, UNITEDKINGDOM

Densification ofC/C CompositesUsing Pulsed Chemical Vapor DonaldRadford, Colorado State University, USA 646

Infiltration

Tension, ompression & Flexure Properties of Pultruded Composites PrabhakaranRamamurthy, OldDominion University, 647

USA

Closed Form Solutions for the Dynamic Stress Intensity Factors at the Carlos Rubio, UniversityofNotreDame, USA 648

Tip ofUniformly Loaded Semi-Infinite Cracks in OrthotropicMaterials

Damage Progression Analysis in3-D Woven Composite Components John Sabu, RMIT, University, AUSTRALIA 649

Haro^ning ofan AluminiumAlloyMatrix Composite Reinforced with CatherineSalmon, UniversiteCathoUquedeLouvain, 650

Stainless Steel Fibres BELGIUM

Load-Ratio Dependence on Fatigue Life of Composites Joakim SchOn, The AeronauticalResearch Institute of 651

Sweden, SWEDEN

Mmcs Characterisation by Internal FrictionMeasurement Irina Severin, Politehnica University ofBucharest, 632

ROMANIA

Strain Rate Effects on the Strength ofSome Glass-Fibre Reinforced MohammedZafar Shah Khan,DefenceScience and 653

Polymer Composites Technology Organization, AUSTRALIA

Modelling and Experimental Investigation of the Ballistic Behaviour Nikhtl Sharma, Defence Clothing and TextilesAgency, 634

ofan Ultrahigh Molecular Weight Polyethylene (Uhmwpe) UNITEDKINGDOM

Thermoplastic Rubber Matrix Composite

InexpensiveDamage Propagation Analysis forComposite Laminates Yoshinobu Shimamura, Tokyo Institute ofTechnology, 655byUsing Fern with Plane Elements JAPAN

Mode I FatigueCrack Growth in Foam Core Materialsfor Sandwich Andrey Shipsha, RoyalInstitute ofTechnology, 656Structures SWEDEN

Impact Damage and Residual Compressive Strength of Multiaxial Tien-Wei Shyr, Feng-Chia University, TAIWAN 657Warp Knitted Glass Fabric Reinforced Polyester Laminate

SurfaceModification ofOrganic Composite After LaserAblation Jean-Francois Silvain, ICMCB-CNRS,FRANCE 658

Characterization of Mechanical and In-Situ Fracture Behaviors of ChangookSon, Dept. ofMetallurgicalEng. Pusan 659Reaction Squeeze Cast National Univ., KOREA

Prediction of the Elastic Tensor of3D Composites by an Analytical Christophe Tallaron, CEA LeRipault, FRANCE 660Model

Fabrication of Polycrystalline Yag/Alumina Composite Fibers and Atsuya Towata, National Industrial Research Institute 661YAO Fiber ofNagoya, JAPAN

Mechanical Behavior of Circular Composite Springs with Extended Ping-Cheung Tse, The HongKongPolytechnic 662Flat Contact Surfaces University, HONG KONG

Interphase Properties Between a Steel Strand andanEpoxy Matrix Danny Van Hemelri/ck,Free UniversityofBrussels, 663BELGIUM

Measuring Bolted Joint Bearing Deformation and Stiffness Bart Vangrlmde, Ecole Polytechnique deMontrial, 664CANADA

Investigation ofThermal Properties ofCarbon Fibre Composites with S. Varghese, MacromolecularResearch Centre, INDIA 665Phenolic - Epoxy Matrix

Design Optimisation ofLaminated Cylinders for Maximum Buckling Mark Walker, TechnikonNatal,REP. ofSOUTH 666

Strength AFRICA

ANew Vacuum Pressure Casting Technique for Fabricating Net- Hong Wan, National University ofDefense Technology, 667

Shaped Fiber Reinforced Metal Matrix Composites POP. REP. CHINA

Exploiting a New Natural Fiber Composite - Ramie Fabric / Up HM. Wang, NothwestInstitute ofTextile and Tech., 668

Composite POP.REP. CHINA

Laser Ablation Assisted Adhesive Bonding ofAutomotive Structural C. David Warren, OakRidgeNational Laboratory, 669

Composites USA

Influencing Factors on the Properties ofNatural Fibre Reinforced Bemhard Wielage, TU Chemnitz, GERMANY 670

Thermoplastics Manufactured by Injection Moulding

Micromechanical Modeling of Cross-PlyTitanium Matrix Composites ZihuiXia, University ofAlberta, CANADA 671Reinforced with Silicon-Carbide Fibres

Solid LiquidPressure Bonding for Fabricating Steel/Aluminium Alloy YuweiXun, Nanyang Technological University, 672

Laminated Composite SINGAPORE

Physico- Mechanical Characterization of Jute Fibre Composite Prakash Yadav, Macromolecular Research Centre, 673with TheimosetResin INDIA

Evaluation ofDebonding Energy Release Rate of Externally Bonded Kofi Yamaguchi, University ofTokyo, JAPAN 674FRP Sheets for Rehabilitation of Infrastructures

Thermal Deformation ofCarbon/Epoxy Laminates for Temperature K. Joon Yoon, KonKuk University, KOREA 675Variation

The Effect of Cell Configuration onthe EnergyAbsorbing Capacity of TX. Yu, Hong Kong University ofScience and 676Grid-Domed Textile Composites Technology, HONG KONG

Factors Affecting the Fibre Strength Distribution During the Fatigue Sylvia Zamperlni, The University ofBirmingham, 677LifeofTimmcs UNITEDKINGDOM

YachtPrepared from Bamboo WovenPreform Reinforced Polyester Jingcheng Zeng, National UniversityofDefense 678

Via RTM Technology, POP. REP. CHINA

Interfacial Structure and Mechanical Properties ofMgLiAVSiCw Dt Zhang, ShanghaiJiao Tong University, POP.REP. 679Composites CHINA

Temperature and Pressure Influences in Infiltration Processing of Wenwei Zheng, National University ofDefense 680

FabricatingFiber Reinforced CeramicMatrix Composite via Precursor Technology, POP. REP. CHINAImpregnation Pyrolysis

ProcessingNon Isothermal Simulation ofthe ResinTransfer MoldingProcess Vlncenza Antonucci, University ofNaples "Federico 681

//", ITALY

Effects of FabricArchitectural Heterogeneities on Effective and Christophe Binetruy,Ecole desMines deDouai, 682

Saturated Permeabilities in Run FRANCE

Integration ofPolymer and Composite Materials forEnhanced Design Pierre EtienneBourban, EPFL-Laboratoire de 683

Freedom and Cost-Efficiency Technologie des Composites, SWITZERLAND

Manufacturing Technology ofWound Structures by Transformation of Abel Cherevatsky, ISRAEL 684Wound Preforms

Compaction Behavior of Fabric Preforms in Resin Transfer Molding Tsu-Wel Chou, University ofDelaware, USA 685Process

Cost Comparisons ofWet Filament Winding Versus PrepregFilament Frederick W. Duval!, ThiokolPropulsionGroup of 686WindmgforTypcIIandTypelvCNGCylinders CordantTechnologies, USASimulation ofthe Compression MoldingofUnidirectional Composite Beatrice Gardarein, RENAULT-Research 687L^f Department, FRANCEInfluenceof Bindersin the Liquid Composite Moulding Process on the Tobias Geiger, GERMANY 688Fatigue Properties ofComposite Structures

Analysis ofthe Compaction Cycle in the Vacuum Infusion Moulding AdelHammami, UAE. University, UNITEDARAB 689ft01*** EMIRATES

AStandard Characterization of Saturatedand Unsaturated Flow Yann Henzel,EcolePolytechnique deMontrial, 690Behaviors in Porous Media CANADA

Complexity Based Cost Estimation Model for Composite Aerospace Jayanthi Kumar, RMLT, Computer Systems 691Structures.

Engineering, AUSTRALIA

The Melt Shear Viscosity of Polypropylene/Glass Bead Hybrid Ji-Zhao Liang,AP department, City U ofHongKong, 692Composites at High Extrusion Flow Rates HONGKONG

Numerical Simulation of Flow Phenoena in Composite Manufacturing Xiao Lin Liu, CRC-AdvancedComposite Structures, 693Processes AUSTRALIA

Experimental DesignApproach to off-Line QualityControl in Mieke Losste, KM. Leuven, BELGIUM 694Filament WindingIndustrialisation ofa CarbonComposite Control Rod JapieLudick, REP. ofSOUTHAFRICA 695

In-Plane Permeability Measurements: Stability, Repeatability and StaffanLmdstrOm, Chalmers University of 696Reproducibility Technology, SWEDEN

Vastly Increased Filament ProductOutput J. LowrieMclarty, TPI TechnicalGroup, Inc., USA 697

Development of Multi-Functional Sensor in Resin Transfer Molding ShinyaMotogl,Dept. ofMechanical Eng., Osaka City 698

Univ., JAPAN

Flow Induced Alignment of Fibers Charles Petty,Michigan State University, USA 699

Microwave Assisted Resin Transfer Moulding ofKevlar-Polyester AbdulRazakRahmat, UMJST, UNITED KINGDOM 700Composites

Net-Shape Processing of Endless Carbon Fibre Reinforced Roger Tognini,ETH-BWB, SWITZERLAND 701

Polyetheretherketone (Peek) for Fasteners by Transfer SqueezeForming(TSF)A Novel Manufacturing Cell for a NewGeneration ofComposite Martyn Wakeman, EcolePolytechniqueFederate de 702

Processing and Applications Lausanne, SWITZERLAND

Characterisation ofOvenCuredPmc Radome Panelfor Airborne NiranjanappaAc, CentreforAirBorne Systems, 703

Application YemalurPO, INDIA

Influence ofthe Sheet Forming Technique on the Impregnation Sofle Baeten,Katholieke UniversiteitLeuven, 704

Quality of Textile ReinforcedThermoplastic Composites BELGIUM

Advanced Composites Manufactured ViaDry PowderPrepregging Todd Bullions, Virginia Polytechnic Institute and State 70S

University, USA

Injection Screw Effect on Nickel-Coated Graphite Fiber Composites Chao-Chang A. Chen, Tamkang University, TAIWAN 706

forEMI Shielding

Computational Analysis of Fibre-Reinforced Thermoplastic Sheets in a RussellDykes, University ofAuckland,NEWZEALAND 707

Continuous Forming Process

The Effect of Tooling Material, Cure Cycle, and Tool Surface Finish GoranFemlund, Department ofMetals andMaterials 708

on Spring-in of Autoclaved Processed Curved Composite Parts Engineering, CANADA

A Prototype Research Laboratory forAutomated Fabrication ofHigh Norman J. Johnston, NASALangley Research Center, 709

Performance Composites USA

Structural-Property Relationships ofComposite Coil Springs Processed Byung-SunKim, Korea Institute ofMachinery& 710

byRTM Materials, KOREA

Development and Verificationof a ThermalModel for aNovel DonaldKlosterman, UniversityofDayton, USA 711

Automated Composite Fabrication Process: Laminated ObjectManufacturing(LOM)Laser Projection Links Composite Designs to Manual Fabrication DavidLedbetter, LockheedMartinAeronautical 712

Systems, USA

Optimize the Thickness Distribution in Thermoformed PP/CaCo3 Shih-Jung Liu, Chang Gung University, TAIWAN 713

Composites

ManufacturingEffects on Cure Consolidation in Filament Wound TroyMeink, US Air Force, USA 714

Composite Stuctures

Curing ofThick Angle-Bend Thermoset Composite Part: Curing Malak Naji, Concordia University, CANADA 715

Process Modificationfor Uniform Thickness and Uniform Fiber

Volume Fraction Distribution

Process Simulation of Multiple Material FilamentWound Pipes

Manufacture a Bend-TwistCoupled Beam

Kurt Olqfsson, Swedish Institute ofComposites(SICOMP), SWEDEN

Cheng-Huat Ong, Stanford University, USA

DonaldRadford, Colorado State University, USA

Bert Thuis, National AerospaceLaboratoryNLR,

NETHERLANDS

Francois Trochu, Ecole Polytechnique deMontreal,

CANADA

IanMWard, University ofLeeds, UNITEDKINGDOM

Craig Wilks, university qfnottingham, UNITEDKINGDOM

Michael Wisnom, University ofBristol, UNITED

KINGDOM

Measurement ofManufacturing Distortion in Flat CompositeLaminates

Development ofaCompositeTorque Link for Helicopter Landing

Gear Applications

Analysis ofMold Filling in Pressure Controlled Injection-

Conmpression

Recent Developments in Hot Compacted Fibre Composites

Rate Dependency During Processing ofGlass/Thermoplastic

Composites

Curing Stresses in Thick Polymer Composites, Part 1: Analysis

Reinforcement/Cement

CarbonFibre Shear Strengthening of Reinforced Concrete Beams BryanAdey, SwissFederalInstitute ofTechnology,SWITZERLAND

Analysis andDesignofFRP Gridsfor Concrete Reinforcement Charles Bakis, ThePennsylvania State University, USA

Rehabilitation of Concrete Structures with CFRP Strips Glued into Michael Blaschko, GERMANY

Slits

Strain Transfer ofSheet-BondedFRPto Concrete andMasonry ThomasBoothby, ThePennsylvania State University,USA

Performance of Concrete Systems Repaired Using Fiber Reinforced Oral Buyukozturk, Massachusetts Institute ofPlastics Technology, USA

Cost Versus Reliability in ReinforcedHsc Column Design SofiaMaria C. Diniz, UniversidadeFederal deMinas

Gerais, BRAZIL

716

717

718

719

720

721

722

723

724

725

726

727

728

729

Durability of External Carbon Epoxy Reinforcementfor Concrete EmmanuelFerrier, L2M- UniversityLyon I, FRANCE

Structure

Creep/StressRupture Characteristics ofa Second Generation Ductile Harry G. Harris, CivilandArchitectural EngineeringHybrid Fiber ReinforcedPolymer (D-H-FRP) for Concrete Structures Depart., USA

Behaviour ofBridge Decks Reinforced by FRP TorekHassan, The University ofManitoba, CANADA

Ultimate Shear ofBeams Strengthened with CFRP Sheetssss Ugo lanniruberto, University ofRome Tor Vergata,ITALY

730

731

732

733

StrengtheningofMasonry Structures with Fiber Reinforced JohnJai, Stanford University, USA

Composites

AStudy on Strengthening and Strain Sensor Techniques in Kin-TakLau, TheHong KongPolytechnic University,

Rectangular Concrete BeamUsing Fibreglass Composites andFibre HONGKONG

Bragg Grating Sensor

Development ofComposite Grid Tubes for the Reinforcement of Shi-WeiRicky Lee, Hong Kong UniversityofScience &

Concrete Columns Technology, HONG KONG

StrengtheningStructures Using Unstressed and PrestressedCFRP MichaelLeeming UNITED KINGDOM

Plates.

Application ofComposites in Repair of Reinforced Concrete Joints AymanMosallam, California state University,Fullerton, USA

StrengtheningofTunnelSupports UsingCarbon Fibre Reinforced StuartMoy, UniversityofSouthampton, UNITED

Composites KINGDOM

Orientation Process During Extrusion of Reactive Powder Concrete ArnaudPoitou, LMT- CACHAN, FRANCE

Reinforced with Short Metal Fibers

Repairingand Strengthening Reinforced Concrete Structures Using Torek Rizk, The George Washington University, USAFiber Reinforced Plastics

Elio Sacco, University ofCassino, ITALY

Pin Tong, AdvancedEngineeringMaterials Facility,HONGKONG

Micromechanical Damage of Fiber-Reinforced Concrete

Composite Materials for the Repair of Concrete Beam

RepairSensorTechniques to Validate the Stress Intensity in Cracked Metallic Bayram Aktepe, Aeronautical andMaritime Research

Panels Repaired with Bonded Composite Patches Laboratory, AUSTRALIA

734

735

736

737

738

739

740

741

742

743

744

The Importanceof FailureModeIdentification in Adhesive Bonded Maxwell Davis, ASI-SRS, AUSTRALIA 745Aircraft Structures and Repairs

Assessment of ElectronBeam and X-Ray Cure Adhesives for TamunoiyalaKoko,Martec United, CANADA 746Composite Repair

Reparability and Residual Mechanical Behaviour ofPultruded Profiles J&romePasquiet, BOMBARDIER Treansport -ANF- 747

Industrie, FRANCEExperimental Investigation of Vibration Behavior of Patched Wei-Chung Wang, TAIWAN 748Composite Plates

SmartMaterials

Advanced Composites for Smart Structures Georges Akhras,RoyalMilitary College of'Canada, 749CANADA

Onthe Minimisation of an Optical Fibre Sensor Obtrusivity with ElenaBarton, University ofSurrey, UNITED 750Respect to Matrix Cracking KINGDOM

Research and Development ofSmart GiantMagnetostriction Hiroshi Eda, FacultyofEngineering, Ibaraki 751Composite Materials Using Powder Metallurgic Technology and their University, JAPANApplications to Advanced Devices0-3 Ptezo-Electric Composites Design to Shape Controle of Structures ErbaFrancesco, LMARC,FRANCE 752

Relationship Between Electrical Conductivity and ElasticModulus of Masahro Funabashi,NJMC 753Polymer Gradient Composites (Nat.InstMater.&ChemRes.), JAPANSurfaceand Bulk Stress/Strain Measurements in Composite Laminates Castas Galiotis, ICE/HT-FORTH, GREECE 754witha Fibre-Optic RamanProbeSmart Sensors for Resin Flow and Composite Cure Monitoring Alfredo Guemes, UnlversldadPolitecnlcaDeMadrid, 735

SPAIN

Effect of Matrix and Reinforcement Morphology on Mechanical ChanghunHan, Dept. ofMetalL Eng. Pusan National 756Properties of AI/Tini Shape Memory Composite University, KOREA

Interfacial Strength of Optical Fibres Klas Levin,FFA, SWEDEN 757

A Minimalist Sensor System forMold Filling RichardParnas, NIST, USA 758

Vibration CharacteristicsofCFRP Laminates with Embedded Shape Masaki Satoh,Dept ofAeronautics & SpaceEng., 759

MemoryAlloyFibers Tohoku Univ.,JAPAN

Copper Electroless Deposition onNiTi Shape Memory Alloy: an XPS Jean-Francois Silvam, ICMCB-CNRS,FRANCE 760

Study ofSn-Pd-Cu Growth

Effect ofEmbedded Optical Fibers on the Structural Integrity of Arne Skontorp, FFA, SWEDEN 761Composites

Novel Dielectric Sensor Setup for Flow and Cure Monitoring in Resin Alexandras Skordos, Cranfield University, UNITED 762Transfer Moulding KINGDOM

Smart Composites Applied to Continuous In-Service Damage Cyril Tamiatto, EcoleDesMines deDouai, FRANCE 763

Monitoring ofGlass/Polymer Industrial Parts

Optical Fiber Sensor to Monitor the Chemical Degradation ofFRP Tomonori Tomlyama, Dept. Chem. Eng., Tokyo Inst. 764

Tech., JAPAN

SmaComposite Patches for Aero-Structure Repair Xiaaming Wang, The University ofSydney, 765

AUSTRALIA

Strain Capability of Optical Fibre Bragg Grating Sensing for Smart Cathy(Chunyang) Wet, CranfieldUniversity, UNITED 766Materials Under Statio and Dynamic Loading KINGDOM

Smart NdtUsing Electrical ResistanceMethod for Delamination Kaorl Yuse, CNAM-ITMA, FRANCE 767

Monitoring in CFRP

Optimal Piezo-Patch Design ofCompositeBeams Under Uncertain JohnC.BruchJr., University ofCalifornia at Santa 768

Loads for Minmax Deflection Barbara, USA

Built-in Structural Health Monitoringfor Composite Structures Fu-Kuo Chang, Stanford University, USA 769

A Flat Shell Composite Element Including Piezoelectric Actuators Jose Antonio Hernandes,Instituto Tecnologico de 770

Aeronautica, BRAZIL

Fracture Criteria for Multiple Cracked Piezoelectric Materials Jin H. Huang, Feng Cha University, TAIWAN 771

Design ofActive Composite Laminates and Structures ClemensKaiser, Technical University ofMunich, 772

GERMANY

Resonance Control of GenerallySupported SmartBeam-Plates Using Chien-ChangLm, National Chung-HsmgUniversity, 773

FourierSeriesMethod TAIWAN

Damage Evaluation of Smart Cfrp-Piezoceramic-Materials UsingNon- GerhardMook, UniversityofMagdeburg, GERMANY 774

Destructive Methods

Stady of Vibration Modal EstimationforComposite Beamwith PZT Nobuo Oshlma, Faculity ofEngmnering, Osaka City 775

Thin Film Sensor System University, JAPAN

Smart Composites with Integrated Tiny Piezoelectric Fibers Dieter Sporn, Fraunhofer-Institutfllr Silicatforschung 776

ISC, GERMANY

Fuzzy Control ofVibrationofa Smart CFRP Laminated Beam Takeshi Takawa, Setsunan University, JAPAN 777

DetectionofTransverse Cracks in Composite Laminates by Embedded Nobuo Takeda, The University ofTokyo, JAPAN 778

Plastic Optical Fibers

Test Methods

Mechanical Identification of AnisotropicProperties of Composites Michel Grediac, LERMES UniversityBlaise Pascal, 779FRANCE

Strain Measurements ofComposite Laminates Using Fiber Bragg- Chang-Sun Hong, Korea AdvancedInstitute ofScience 780

Grating Sensor and Technology, KOREA

Stress Concentration in Alumina-Fibre/Epoxy Model Composites HakimMahiou, LaRAMA-IFMA, FRANCE 781

Comparative Study onthe Deteimination ofthe Elastic Properties of Sebastien Mistou, LGP-ENIT, FRANCE 782

Composite Materials byTensile Tests and Ultrasound Measurement

Toward an Accurate Failure Criterion of Anisotropic Materials, a New RaedRachdan, Osaka University,JAPAN 783

Flexure Test Considering the Coupling Effect

Pure Tension with off-Axis Tests for Orthotropic Materials Georges Verchery, LRMA, ISAT, Umversiti de 784

Bourgogne, FRANCE

Fracture Analysis ofFilament-Wound FRP Composites Using Ring Shuichi Wakayama, TokyoMetropolitan University, 785

Burst Test JAPAN

Experimental Characterization and Stochastic Modeling of Chao Zhang, Concordia University, CANADA 786

Interlaminar Shear Strengths ofGraphie/EpoxyLaminated Composites

Mechanical Behaviour ofHigh Strength Unidirectional Composites PeterZinoviev, Institute ofComposite Technologies, 787

Under3-D State of Stress RUSSLA

Geometry Dependent Process andCost Modelling ofCommingled NicolasBemet, SwissFederal Institute ofTechnology, 788

Yarn Laminates SWITZERLAND

Spatial Braiding of Cylindrical Shape Atricles AndreyBeyle, Institute ofPolymerMechanics, LATVIA 789

Failure Behaviour of3D-Braided Composites-Modeling bya DavidBigaud, L2M- UniversityLyon I,FRANCE 790

Multiscale VariationalApproach

Investigation of Progressive andUltimate Failure for Woven-Fabric J. Blachut, The University ofLiverpool, UNITED 791

Composite Structures KINGDOM

Meso-Macro Mechanical Behaviour ofDry Fiber Fabric Philippe Boisse, LM2S,ENSAM, Paris 6, FRANCE 792

DamageModeling and Characterization ofaThree-Dimensional Pascal Casart, Faculti des Sciences et des Techniques 793

Woven Composite de Nantes, FRANCE

Analytical and Experimental Elastic Behavior ofTwill Woven PramodChaphalkar, North CarolinaA&TState 794

Laminate University, USA

Meso-Structural Behaviour ofComposite Fabric for the Simulation of Abdelhakim Cherouat, Universiti Technologique de 795

Manufacturing of Thin Compositeby ShapingProcess Troyes, FRANCE

Commingled Carbon/Peek Yarns forUse in Textile Reinforced High Bong-Don Choi, Dresden UniversityofTechnology, 796

Performance Rotors GERMANY

The Binary Model - a Computational Approachto Textile Composites Brian Cox, Cambridge University, UNITED 797

KINGDOM

Solid Mechanics Draping Simulations ofWoven Fabrics LiminDong, University ofSurrey, UNITED KINGDOM 798

F.E. Investigation ofthe Non-Crimp Fabrics Compressive and Sylvain Drapier, Ecole Nationale Supirieure desMines 799

hterlaminar Behaviours deSaint-Etienne, FRANCE

Eshelby Models Applied to Woven Fabric GertHuysmans, Katholieke Universiteit Leuven, 800

Composites: aBenchmarkStudy BELGIUM

Fabrication and Mechanical Properties of Pe/Pe Composite Mlyako Inoda, Kyoto Institut, JAPAN 801

Transient Heat Transfer and Thermal Stresees in Functionally Graded SeiichiNomura, University ofTexas at Arlington, USA 802

Materials

Analytio Descriptions of3-D Preforms Used in Composite Component John Sabu, RMTT, University, AUSTRALIA 803

Manufacturing

Moulding Analysis of3D Woven Composite Preforms: Mapping Shrikant Sharma, University ofManchesterInst. ofSci. 804

Algorithms & Technology, UNITEDKINGDOM

In-Plane Mechanical Properties ofCF/Epoxy 3-D Orthogonal Naoyuki Watanabe, Tokyo Metropolitan Institute of 805

Interlocked Fabrio Composite Technology, JAPAN

Routine Three-Dimensional Analysis ofWoven Composites John Whitcomb, TexasAdM University, USA 806

MEnergyApproachformePredictionofEffediveStiffhessof2-D Yong Yan, Concordia University, CANADA

Braided Composites

Textile

Modeling of the Behavior ofWoven Luninated Composites Until PierreAntoine Aubourg, Laboratoire deMicanique et

Rupture d'Acoustlque, FRANCE

Mechanical Properties of Glass Fibre/Pet Composites Based on Weft Gordana Bogoeva-Gaceva, FacultyofTechnology &

Knitted Preforms Metallurgy, MACEDONIA

Non-Linear Behaviour of Plain Weft-Knitted Carbon Fibre Reinforced JoopDeHaan, ETH-BWB, SWITZERLAND

Composites

Multiaxial Compound Weave Method for Preforms AngelaDurie,Design SystemsLaboratory, UNSW,

AUSTRALIA

Jeroen Hofsiee, DLR - Institute ofStructures and

Design, GERMANY

JinlianHu, TheHongKong Polytechnic University,

HONGKONG

Christian-AndriKeun, Technische UniversitSt

Hamburg-Harburg, GERMANY

Sheng YuanLei,ManchesterMaterialScience Centre,

UNITEDKINGDOM

KH.Leong, CRC-ACS, AUSTRALIA

AndrewLong, UniversityofNottingham, UNITED

KINGDOM

HenkPattyn, Katholieke Universiteit Leuven,

BELGIUM

Dirk Philips, Katholieke UniversiteitLeuven,

BELGIUM

AndreasProdromou, Katholieke UniversiteitLeuven,

BELGIUM

The Relationship BetweenFibre Architecture and Cracking Damage in CarlosRios, UniversityofSurrey, UNITEDKINGDOM

a Knitted Fabric Reinforced Composite

Modeling the Fiber Slippage During Preforming Process Wen-Bin Young,National ChengKmgUniversity,

TAIWAN

Thermoelastic Properties Analysis of3-D Textile Composites Sergei Yushanov. 3TEX, Inc., Raleigh, USA

The Effect ofSimpleShearonStiffness and Strength ofFabric

Laminates

Design of Multiaxial Warp Knitted Fabrics for Required Tensile

Properties in Composite Applications

Semiflexible Composites - Design ofan Endless Warp-KnittedReinforced Thermoplastic Elastomer

MeasurementofLocalFibre Strain Distributions inWoven

Composites

The Effects of Biaxially Deforming Knitted Glass Preforms on

Effects ofFibre Architecture on Deformation During Preform

Manufacture

Mechanical in Plane Performance of Aerotiss 4/5D

Stiffness ofthe Skinsof 3D-Knitted Composites

Stiffness and Failure Modelling ofTextile Composites Using a

Variational Approach

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