Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM
In this paper, a novel procedure to analyse dynamic crack under aeroelastic loading by means of XFEM and Doublet Lattice Method (DLM) - FEM coupling is presented. The present work performed a new investigation on the crack propagation on the composite plate exerted by the unsteady aerodynamic loadi...
| Main Authors: | , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English English |
| Published: |
2018
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/74973/ http://irep.iium.edu.my/74973/1/7207.pdf http://irep.iium.edu.my/74973/7/74973_Program.pdf |