Experimental determination of stress intensity factors in patched cracked plates

Author:

Chandra Ramesh

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference34 articles.

1. N.N. Damage tolerance and fatigue evaluation of structure;FAA,1977

2. N.N. Airplane damage tolerance requirement;MIL-Spec. 83444,1974

3. Fibre composite reinforcement of cracked aircraft structure;Baker;Tech. Memo ARL/Mat. 366,1976

4. A summary of work on application of advanced fibre composite at ARL Australia;Baker;Composite,1978

5. Analytical estimation of stress intensity factors in patched cracked plates;Chandra;Engng Fracture Mech.,1985

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