Low velocity perforation behaviour of polymer composite sandwich panels

Volume: 21, Issue: 10, Pages: 855 - 879
Published: Nov 1, 1998
Abstract
null null The paper describes low-velocity impact tests on square panels made from two polymer composite sandwich constructions, namely woven glass vinyl ester skins with Coremat core and woven glass epoxy pre-preg skins with honeycomb core. The impact velocity was up to 8 m s -1 null with an impact mass of up to 30 kg giving a maximum impact energy of 882 J. This maximum energy gives full perforation of the panels. The panels were 0.5 m by...
Paper Details
Title
Low velocity perforation behaviour of polymer composite sandwich panels
Published Date
Nov 1, 1998
Volume
21
Issue
10
Pages
855 - 879
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