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NASA NTRS · 19920051954

Impact damage in small diameter graphite/epoxy composite struts

Abstract

An investigation was performed to study impact induced damage in small-diameter struts made of a composite material with a brittle matrix system. The major focus is on characterizing the impact behavior associated with the barely visible damage. An experimental procedure including ultrasonic inspection, instrumented impact testing, and delamination buckling and residual strength measurements is presented. From the ultrasonic inspection, it is found that for the strut specimens under investigation, the impact energy level for barely visible damage threshold is above that of the internal damage threshold. A 60- to 65-percent reduction in compressive strength was typical for struts subjected to the barely visible impact damage threshold.

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BibTeXRIS

Chen, G.-S., Bidinger, G. M., Cho, S., Lou, M. C.. 1992-01-01. Impact damage in small diameter graphite/epoxy composite struts. https://ntrs.nasa.gov/citations/19920051954

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