NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Delaminations in composite plates under transverse impact loads - Experimental resultsTests were performed measuring the locations and geometries of delaminations in Fiberite T300/976 graphite/epoxy, Fiberite IM7/977-2 graphite-toughened epoxy, and ICI APC-2 graphite/PEEK plates subjected to transverse impact loads. The data provide specific information on the effects of impactor velocity, impactor mass, material, thickness of back ply group, difference in fiber orientation between adjacent ply groups, plate thickness, and impactor nose radius. The data were compared to the results of the Finn-Springer model. The model was found to describe the data with reasonable accuracy.
Document ID
19930048650
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Finn, Scott R.
(NASA Langley Research Center Hampton, VA, United States)
He, Ye-Fei
(NASA Langley Research Center Hampton, VA, United States)
Springer, George S.
(Stanford Univ. CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: Composite Structures
Volume: 23
Issue: 3
ISSN: 0263-8223
Subject Category
Structural Mechanics
Accession Number
93A32647
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available