journal article·2001-01

On a Formulation and Solutions for Doubly Periodic Cracking in hhh Laminates

Yuri Lapusta

International Journal of Fracture· Volume 107· Issue 2
Publisher page

Abstract

Problem formulation and simple analytical procedure are presented for the determination of the distribution of averaged through the thickness displacements, strains and stresses in layers for the case of doubly periodic matrix cracking in [α1m,α2n ]s composite laminates. The modeling accounts for the coupling between tensile and shear stresses in the layers.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Epoxy Resin Curing Processes · Synthesis and properties of polymers

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References (5)

Show source-provided references
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2. Henaff-Gardin, C., Lafarie-Frenot, M.C. and Gamby D. (1996) Doubly periodic matrix cracking in composite laminates. Part 1: General in-plane loading. Composite Structures 36, 113-130.10.1016/S0263-8223(96)00071-2 ↗
3. Kashtalyan, M. and Soutis, C. (2000). Stiffness degradation in cross-ply laminates damaged by transverse cracking and splitting. Composites: Part A 31, 335-351.10.1016/S1359-835X(99)00077-9 ↗
4. Lapusta Yu.N. and Henaff-Gardin C. (2000). An analytical model for periodic αΰ-layer cracking in composites laminates. International Journal of Fracture, 102, L73-L76.10.1023/A:1007696725543 ↗
5. Tsai C.L., Daniel I.M. and Lee J.-W. (1990) Progressive matrix cracking of crossply composite laminates under biaxial loading. In: Winter Annual Meeting of the ASME (Edited by G.J. Dvorak and D.C. Lagoudas), ASME, Dallas, TX, 9-18.