NASA NTRS · 19960010548
Impact damage in composite plates
Abstract
The objective of this research paper was to link two computer codes, PDCOMP (for Progressive Damage Analysis for Laminated Composites) and 3DIMPACT (for the prediction of the extent of delaminations in laminated composites resulting from point impact loads), in order to predict impact damage by taking into account local damage and material degradation and to estimate residual stiffness of composites after impact. The resulting graphs and analysis versus test results are presented along with the conclusive results of the codes' performances.
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Shahid, I., Lee, S., Chang, F. K., Shah, B. M.. 1995-10-01. Impact damage in composite plates. https://ntrs.nasa.gov/citations/19960010548
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