An experimental and numerical investigation on low velocity impact response of a composite structure inspired by dragonfly wing configuration

Published 2018 View Full Article

Authors

Keywords

Bio-inspired sandwich structure, Low velocity impact, Progressive damage model, Cohesive zone elements, Foam core, VUMAT

Journal

COMPOSITE STRUCTURES

Volume 184, Issue -, Pages 327-336

Publisher

Elsevier BV

Online

2017-10-11

DOI

10.1016/j.compstruct.2017.10.006

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