NASA NTRS ยท 19840024365
Hole interaction and load introduction effects for compression-loaded laminates with holes
Abstract
The effects of hole interaction and load introduction for (+ or - 30/90) sub 8 (s) and (+ or - 45) sub 12 (s) laminates with holes was conducted. A hole interaction region was identified in some specimens, and this region was ineffective for carrying load. The membrane stiffness of a specimen with a hole interaction region is less than the membrane stiffness of a similar specimen without a hole interaction region. A load introduction effect that occurs on the sublaminate level was also observed. This effect can cause a nonuniform load diffusion into the interior of the specimen.
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Shuart, M. J.. 1984-08-01. Hole interaction and load introduction effects for compression-loaded laminates with holes. https://ntrs.nasa.gov/citations/19840024365
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