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Instability-related delamination growth of embedded and edge delaminationsCompressive loads can cause local buckling in composite laminates that have a near surface delamination. This buckling causes load redistribution and secondary loads, which in turn cause interlaminar stresses and delamination growth. The goal of this research was to enhance the understanding of this instability-related delamination growth in laminates containing either an embedded or an edge delamination.
Document ID
19900014178
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Whitcomb, John D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1988
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:100655
NASA-TM-100655
Accession Number
90N23494
Funding Number(s)
PROJECT: RTOP 505-63-01-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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