Finite element simulation of PMMA aircraft windshield against bird strike by using a rate and temperature dependent nonlinear viscoelastic constitutive model
Author(s): |
Jun Wang
Yingjie Xu Weihong Zhang |
---|---|
Medium: | journal article |
Language(s): | English |
Published in: | Composite Structures, February 2014, v. 108 |
Page(s): | 21-30 |
DOI: | 10.1016/j.compstruct.2013.09.001 |
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10454803 - Published on:
23/10/2020 - Last updated on:
23/10/2020