Compression Buckling Tests of Laminated Graphite-Epoxy Curved Panels

Dick J. Wilkins

AIAA Journal · 1975 · 27 citations · 0 references

Concepts

Abstract

Ten different orientation arrangements (in various panel thicknesses) were used in fabricating 72 panels. Eighty-four tests were performed, and the range of R/t studied was 100 to 400. All specimens had a 12-in. outside radius and were 13-in. long by 9-in. wide. The results included development of the moire grid-shadow technique and the South well plot method for nondestructive testing as well as observations of the effects of orientation and R/t on the buckling behavior and imperfection sensitivity of such shells. Satisfactory correlation was obtained with a laminated anisotropic curved panel analysis using the Rayleigh-Ritz energy method, which included a crude assumption that the thickness variations in the panels could be used to measure imperfection amplitude.