Search NASA⌕ Search

NASA NTRS · 19890015919

Vibration testing of impact-damaged composite laminates

Abstract

A new test is described that can be used to measure changes in the vibration properties of impact damaged composite materials. Impact-induced delamination was observed to significantly affect natural frequencies of vibration and damping properties in cross-ply graphite/epoxy laminates. Natural frequencies are shown to drop by as much as half of their original value, and modal damping ratios can increase by a factor of up to eight when large amounts of damage are present. A simple finite element model of the damaged impact specimens was used to predict the effect of delamination on certain vibration properties. A comparison of the finite element calculations with the experimental measurements suggests that delamination was the dominant mechanism of flexural stiffness loss resulting from the transverse impact.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Grady, Joseph E., Meyn, Erwin H.. 1989-06-01. Vibration testing of impact-damaged composite laminates. https://ntrs.nasa.gov/citations/19890015919

Cite the original work for its findings. Save a collection to share your selection of sources.