A Finite Element Analysis for Predicting the Residual Compressive Strength of Impact-Damaged Sandwich Panels by National Aeronautics and Space Adm Nasa

A Finite Element Analysis for Predicting the Residual Compressive Strength of Impact-Damaged Sandwich Panels

National Aeronautics and Space Adm Nasa

32 pages missing pub info (editions)

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Description

A simple analysis method has been developed for predicting the residual compressive strength of impact-damaged sandwich panels. The method is tailored for honeycomb core-based sandwich specimens that exhibit an indentation growth failure mode unde...

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