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Surface crack analysis applied to impact damage in a thick graphite/epoxy compositeThe residual tensile strength of a thick graphite/epoxy composite with impact damage was predicted using surface crack analysis. The damage was localized to a region directly beneath the impact site and extended only part way through the laminate. The damaged region contained broken fibers, and the locus of breaks in each layer resembled a crack perpendicular to the direction of the fibers. In some cases, the impacts broke fibers without making a visible crater. The impact damage was represented as a semi-elliptical surface crack with length and depth equal to that of the impact damage. The maximum length and depth of the damage were predicted with a stress analysis and a maximum shear stress criterion. The predictions and measurements of strength were in good agreement.
Document ID
19900050860
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Poe, Clarence C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Harris, Charles E.
(NASA Langley Research Center Hampton, VA, United States)
Morris, Don H.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Meeting Information
Meeting: Surface-Crack Growth: Models, Experiments, and Structures
Location: Sparks, NV
Country: United States
Start Date: April 25, 1988
Sponsors: ASTM
Accession Number
90A37915
Distribution Limits
Public
Copyright
Other

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