NASA NTRS · 19920013724
Indentation-flexure and low-velocity impact damage in graphite/epoxy laminates
Abstract
Static indentation and low velocity impact tests were performed on quasi-isotropic and cross ply graphite/epoxy composite laminates. The load deflection relations in static tests and impact force history in the impact tests were recorded. The damage was assessed by using ultrasonic C-scanning and photomicrographic techniques. The static behavior of the laminates and damage progression during loading, unloading, and reloading were explained by a simple plate delamination model. A good correlation existed between the static and impact responses. It was found that results from a few static indentation-flexture tests can be used to predict the response and damage in composite laminates due to a class of low velocity impact events.
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Kwon, Young S., Sankar, Bhavani V.. 1992-03-01. Indentation-flexure and low-velocity impact damage in graphite/epoxy laminates. https://ntrs.nasa.gov/citations/19920013724
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