Energy effect removal technique to model circular/elliptical holes in relatively thick composite plates under in-plane compressive load
Author(s): |
S. A. M. Ghannadpour
M. Mehrparvar |
---|---|
Medium: | journal article |
Language(s): | English |
Published in: | Composite Structures, October 2018, v. 202 |
Page(s): | 1032-1041 |
DOI: | 10.1016/j.compstruct.2018.05.026 |
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10450195 - Published on:
23/10/2020 - Last updated on:
23/10/2020