TY  - CONF

T1  - Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method

JO  - Proceedings of the 3rd International Conference on Mechanics of Composites

PY  - 2017/07/04

AU  - Abdullah NA

AU  - Curiel-Sosa JL

AU  - Akbar M

ED  - 

Y2  - 2024/12/25

ER  -