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Measurements of matrix cracking and delamination caused by impact on composite platesTests were performed measuring the locations and extents of delaminations and matrix crackings in 3-in. by 3-in. Fiberite T300/934 graphite/epoxy plates impacted by 1/2-in. diameter aluminum spheres. Plates with six ply orientations were tested. The impactor speeds ranged from 700 to 1300 in/sec. The plates were inspected by C-scan both before and after impact. The plates were also dissected after impact and examined visually for damage. In addition, the longitudinal and transverse tensile, compressive, and shear properties of the material were measured.
Document ID
19880061836
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Wu, Hsi-Yung T.
(Stanford Univ. CA, United States)
Springer, George S.
(Stanford University CA, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1988
Publication Information
Publication: Journal of Composite Materials
Volume: 22
ISSN: 0021-9983
Subject Category
Composite Materials
Accession Number
88A49063
Distribution Limits
Public
Copyright
Other

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