NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Compression-Failure Mechanisms in Composite LaminatesFailure mechanisms observed using transparent fiberglass/epoxy birefringent materials. Technique based on use of transparent fiberglass/epoxy birefringent material. Transparency allows visual observation of location of initial laminate failure and of subsequent failure propagation; birefringence allows laminate stress distribution to be observed during test and also after test if permanent residual stresses occur. Nondestructive technique developed to observe failure as it develops and as propagates within laminate.
Document ID
19860000129
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Shuart, M. J.
Williams, J. G.
Cooper, P. A.
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 2
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LAR-13345
ISSN: 0145-319X
Report Number: LAR-13345
Accession Number
86B10129
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

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