BEM analysis of damage progress in 0/90 laminates
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Publication:443507
DOI10.1016/J.ENGANABOUND.2009.01.004zbMath1244.74139OpenAlexW2083216705WikidataQ64017065 ScholiaQ64017065MaRDI QIDQ443507
Federico París, N. L. Mccartney, Vladislav Mantič, A. Blázquez
Publication date: 7 August 2012
Published in: Engineering Analysis with Boundary Elements (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.enganabound.2009.01.004
contact problemcomposite materialsdelaminationenergy release ratecross-ply laminatetransversal crack
Boundary element methods applied to problems in solid mechanics (74S15) Composite and mixture properties (74E30) Brittle damage (74R05)
Uses Software
Cites Work
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- Stress state characterization of delamination cracks in [0/90 symmetric laminates by BEM]
- Integral kernels in the 2D Somigliana displacement and stress identities for anisotropic materials
- BEM solution of two-dimensional contact problems by weak application of contact conditions with nonconforming discretizations
- Delamination cracks originating from transverse cracking in cross-ply laminates under various loadings
- Application of BEM to generalized plane problems for anisotropic elastic materials in presence of contact
- The Interface Crack
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