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Approximate analysis of postbuckled through-width delaminationsAn approximate analysis was developed to analyze the postbuckling behavior of through-width delaminations in a laminated coupon. The analysis contains two parameters which are determined using a finite element analysis. After calculating the parameters for a few configurations, the approximate analysis was used to analyze many other configurations. Lateral deflections and mode I strain-energy release rates obtained with the approximate analysis were compared with results from the finite element analysis. For the configurations analyzed, the approximate analysis agreed very well with the finite element results.
Document ID
19810018664
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
June 1, 1981
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-83147
Report Number: NASA-TM-83147
Accession Number
81N27202
Funding Number(s)
PROJECT: RTOP 506-53-23-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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