Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue

An edition of Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue (1995)

Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue

By Timothy W. Coats

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Publish Date

1995

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Crack propagation, Aircraft structures, Delaminating, Stiffness, Resin matrix composites, Fiber composites, Finite element method