Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method
Author(s): |
Nur Azam Abdullah
Jose Luis Curiel-Sosa Mahesa Akbar |
---|---|
Medium: | journal article |
Language(s): | English |
Published in: | Composite Structures, October 2018, v. 202 |
Page(s): | 151-161 |
DOI: | 10.1016/j.compstruct.2018.01.015 |
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10450300 - Published on:
23/10/2020 - Last updated on:
23/10/2020