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...
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| Main Authors: | , , , |
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| Format: | Proceeding Paper |
| Language: | en en |
| Published: |
2018
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/74973/1/7207.pdf http://irep.iium.edu.my/74973/7/74973_Program.pdf http://irep.iium.edu.my/74973/ |
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