TY  - JOUR

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

JO  - Composite Structures

PY  - 2018/10/15

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  - 2025/11/06

ER  -