NASA NTRS ยท 19940015686
Compression strength of composite primary structural components
Abstract
Two projects are summarized in this report. The first project is entitled 'Stiffener Crippling Initiated by Delamination', and the second is entitled 'Pressure Pillowing of an Orthogonally Stiffened Cylindrical Shell.' The objective of the first project 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 objectives of the second project are to analyze the concentration of interacting loads at the stiffener intersection and to study the pillowing of the skin.
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Johnson, Eric R.. 1993-10-01. Compression strength of composite primary structural components. https://ntrs.nasa.gov/citations/19940015686
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