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Failure characteristics of graphite-epoxy structural components loaded in compressionFailure characteristics of compressively loaded graphite-epoxy components are described. Experimental results for both strength-critical laminates and structural components with postbuckling strength are presented. Effects of low speed impact damage and circular holes on compressive strength are discussed. Delamination and shear crippling failure mechanisms that limit the performance of strength-critical laminates are described. Transverse shear and skin-stiffener separation failure mechanisms that limit the performance of components with postbuckling strength are also described. The influence of matrix properties on compressive strength improvements for impact damaged laminates is discussed. Experimental data and results from a failure analysis for strength-critical laminates with cutouts are discussed and compared with impact damage results. Typical postbuckling test results are compared with analytical predictions. Previously announced in STAR as N83-12174
Document ID
19840050603
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Starnes, J. H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Williams, J. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1983
Subject Category
Composite Materials
Accession Number
84A33390
Distribution Limits
Public
Copyright
Other

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