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Matrix cracking evolution in open-hole laminates subjected to thermo-mechanical loads

  • Published:2018-01 Issue: Volume:183 Page:510-520
  • ISSN:0263-8223
  • Container-title:Composite Structures
  • language:en
  • Short-container-title:Composite Structures

Author:

Moure M.M.,García-Castillo S.K.,Sánchez-Sáez S.,Barbero E.,Barbero E.J.

Funder

Ministry of Economy and Finance of Spain

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference39 articles.

1. Response of pre-loaded laminate composite plates subject to high velocity impact;García-Castillo;J Phys IV,2006

2. Roy S, Utturkar A, Benjamin M. Modeling of permeation and damage in graphite/epoxy laminates at cryogenic temperatures. In: 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. Palm Springs-California, April 2004.

3. Hodge AJ. Evaluating of microcraking in two carbon-fiber/epoxy-matrix composite cryogenic tanks. NASA/TM-2001-211194; 2001.

4. Damage evolution and characterisation of crack types in CF/EP laminates loaded at low temperatures;Lundmark;Eng Fract Mech,2008

5. Constitutive relationships for laminates with ply cracks in-plane loading;Lundmark;Int J Damage Mech,2005
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