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Compression strength of composite primary structural componentsTwo projects are summarized. The first project is entitled 'Stiffener Crippling Inititated by Delaminations' and its objective is to develop a computational model of the stiffener specimens that includes the capability to predict the interlaminar stress response at the flange free edge in postbuckling. The second is entitled 'Pressure Pillowing of an Orthogonally Stiffened Cylindrical Shell'. A paper written on this project is included.
Document ID
19940014877
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Johnson, Eric R. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-194562
NAS 1.26:194562
Report Number: NASA-CR-194562
Report Number: NAS 1.26:194562
Accession Number
94N19350
Funding Number(s)
CONTRACT_GRANT: NAG1-537
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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