NASA NTRS · 19940014877
Compression strength of composite primary structural components
Abstract
Two 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.
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Johnson, Eric R.. 1993-10-01. Compression strength of composite primary structural components. https://ntrs.nasa.gov/citations/19940014877
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