| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8059076 | Progress in Aerospace Sciences | 2018 | 18 Pages |
Abstract
This paper outlines an approach for demonstrating the crashworthiness characteristics of the airframe performing a drop test at low velocity impact to validate a numerical model obtained by assembling structural components and materials' properties previously obtained by testing coupons and sub-elements.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
M. Guida, F. Marulo, S. Abrate,