Fracture toughness of transverse cracks in graphite/epoxy laminates at cryogenic conditions

Author:

Choi Sukjoo,Sankar Bhavani V.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference14 articles.

1. NASA. Final report of the X-33 liquid hydrogen tank test investigation team, George C. Marshall Space Flight center, Huntsville, AL, NASA Report, May 2000.

2. Choi S, Sankar BV. A micromechanics method to predict the micro-cracking of the LH2 composite tank at cryogenic temperature. In: Proceedings of the fifth international congress on thermal stresses and related topics, Blacksburg, VA, June 2003. p. WM441–444.

3. On the stress distribution at the base of a stationary crack;Willams;J Appl Mech,1957

4. Crack deflection at an interface between two orthotropic media;Gupta;J Appl Mech,1992

5. Crack point singularities at a bi-material interface;Zak;ASME J Appl Mech,1963

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