LEADER 05662nam 2200685Ia 450 001 9910784536603321 005 20200520144314.0 010 $a1-281-11872-9 010 $a9786611118723 010 $a0-08-053157-1 035 $a(CKB)1000000000365292 035 $a(EBL)305568 035 $a(OCoLC)469629765 035 $a(SSID)ssj0000152946 035 $a(PQKBManifestationID)12003435 035 $a(PQKBTitleCode)TC0000152946 035 $a(PQKBWorkID)10391352 035 $a(PQKB)10668514 035 $a(Au-PeEL)EBL305568 035 $a(CaPaEBR)ebr10188167 035 $a(CaONFJC)MIL111872 035 $a(MiAaPQ)EBC305568 035 $a(EXLCZ)991000000000365292 100 $a20071103d2004 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aFailure criteria in fibre reinforced polymer composites$b[electronic resource] $ethe World-Wide Failure Exercise /$fedited by M.J. Hinton, A.S. Kaddour, P.D. Soden 205 $a1st ed. 210 $aAmsterdam ;$aSan Diego, CA ;$aOxford $cElsevier$d2004 215 $a1 online resource (1269 p.) 300 $a"This volume contains 34 previously published papers from the journal Special issue composites science and technology and four new papers." 311 $a0-08-044475-X 320 $aIncludes bibliographical references and index. 327 $aFront Cover; Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise; Copyright Page; Contents; Preface; About the editors; Section 1: The World-Wide Failure Exercise: Its Origin, Concept And Content; Chapter 1.1 The world-wide failure exercise: Its origin, concept and content; Section 2: Test Cases, Lamina Data and Experimental Results Under Biaxial Loads; Chapter 2.1 Lamina properties, lay-up configurations and loading conditions for a range of fibre reinforced composite laminates 327 $aChapter 2.2 Biaxial test results for strength and deformation of a range of E-glass and carbon fibre reinforced composite laminates: Failure exercise benchmark dataSection 3: Description of the Individual Failure Theories by their Originators; Chapter 3.1 Prediction of composite laminate fracture: Micromechanics and progressive fracture; Chapter 3.2 Failure criteria for use in the design environment; Chapter 3.3 Stress-based Grant-Sanders method for predicting failure of composite laminates; Chapter 3.4 Predicting transverse crack formation in cross-ply laminates 327 $aChapter 3.5 Predictions of the original and truncated maximum-strain failure models for certain fibrous composite laminatesChapter 3.6 Predictions of a generalized maximum-shear-stress failure criterion for certain fibrous composite laminates; Chapter 3.7 Failure analysis of FRP laminates by means of physically based phenomenological models; Chapter 3.8 Prediction of laminate failure with the Rotem failure criterion; Chapter 3.9 Prediction of failure envelopes and stress/strain behavior of composite laminates; Chapter 3.10 A progressive quadratic failure criterion for a laminate 327 $aChapter 3.11 A strain-energy based failure criterion for non-linear analysis of composite laminates subjected to biaxial loadingChapter 3.12 The strength of multilayered composites under a plane-stress state; Chapter 3.13 Predicting the nonlinear response and progressive failure of composite laminates; Chapter 3.14 The predictive capability of failure mode concept-based strength criteria for multidirectional laminates; Chapter 3.15 Composite laminate failure analysis using multicontinuum theory 327 $aChapter 3.16 A bridging model prediction of the ultimate strength of composite laminates subjected to biaxial loadsChapter 3.17 Expanding the capabilities of the Ten-Percent Rule for predicting the strength of fibre-polymer composites; Section 4: A Comparative Study of Failure Theories and Predictions for Fibre Polymer Composite Laminates: Part (A); Chapter 4.1 A comparative study of failure theories and predictions for fibre polymer composite laminates: Part (A); Section 5: Comparison Between the Individual Theoretical Predictions and Experimental Results 327 $aChapter 5.1 Application of progressive fracture analysis for predicting failure envelopes and stress-strain behaviors of composite laminates: A comparison with experimental results 330 $aFiber reinforced polymer composites are an extremely broad and versatile class of material.Their high strength coupled with lightweight leads to their use wherever structural efficiency is at a premium. Applications can be found in aircraft, process plants, sporting goods and military equipment. However they are heterogeneous in construction and antisotropic, which makes making strength prediction extremely difficult especially compared to that of a metal. This book brings together the results of a 12year worldwide failure exercise encompassing 19 theories in a single volume 606 $aPolymeric composites$xFatigue 606 $aFibrous composites$xFatigue 606 $aLaminated materials$xFatigue 615 0$aPolymeric composites$xFatigue. 615 0$aFibrous composites$xFatigue. 615 0$aLaminated materials$xFatigue. 676 $a620.1920287 701 $aHinton$b M. J$g(Mike J.)$01500595 701 $aKaddour$b A. S$01500596 701 $aSoden$b P. D$g(Peter D.)$01500597 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910784536603321 996 $aFailure criteria in fibre reinforced polymer composites$93727333 997 $aUNINA