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NASA NTRS ยท 19880010991

Delamination stresses in semicircular laminated composite bars

Abstract

Using anisotropic elasticity theory, delamination stresses in a semicircular laminated composite curved bar subjected to end forces and end moments were calculated, and their radial locations determined. A family of design curves was presented, showing variation of the intensity of delamination stresses and their radial locations with different geometry and different degrees of anisotropy of the curved bar. The effect of anisotropy on the location of peak delamination stress was found to be small.

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BibTeXRIS

Ko, William L.. 1988-01-01. Delamination stresses in semicircular laminated composite bars. https://ntrs.nasa.gov/citations/19880010991

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