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Analysis of instability-related growth of a through-width delaminationThe effect of various parameters on instability related delamination growth was studied. The configuration studied consisted of a thick composite laminate with a single through width delamination located near one surface. Both mechanical and thermal loads were considered. It is assumed that GI and GII govern delamination growth. An approximate superposition stress analysis was developed which gives closed form expressions for GI and GII. It is found that both GI and GII are very sensitive to delamination length and location through the thickness and that the magnitude of GI is also sensitive to initial imperfection. Critical loads for delamination growth are calculated based on three growth criteria. Large differences in the predictions highlight the need for a verified mixed mode delamination growth criterion.
Document ID
19840025453
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Whitcomb, J. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1984
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:86301
NASA-TM-86301
Accession Number
84N33524
Funding Number(s)
PROJECT: RTOP 534-06-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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