The reliability of laminated plates subjected to in-plane random static loads is derived. The Hashin failure criterion for unidirectional fiber composites is used to establish the performance function. The Hasofer-Lind method is then applied and the reliabilities associated with the various failure modes are obtained.
Reliability of laminated plates
Israel Annual Conference on Aviation and Astronautics ; 1989 ; Haifa, Israel
1989-01-01
Conference paper
No indication
English
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