TY  - JOUR

T1  - Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method

JO  - Composite Structures

UR  - http://eprints.whiterose.ac.uk/126643/

PY  - 2018/01/09

AU  - Abdullah NA

AU  - Curiel-Sosa JL

AU  - Akbar M

ED  - 

DO  - DOI: 10.1016/j.compstruct.2018.01.015

VL  - 202

SP  - 151

EP  - 161

Y2  - 2024/12/22

ER  -