Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method
This paper presents an investigation on flutter speed of cracked composite plates. This work is divided into two sections: (a) variation of crack length at a fixed location on the plate, and (b) variation of crack location on the plate with a fixed crack length, modelled as a unidirectional compos...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Elsevier
2018
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/73583/ http://irep.iium.edu.my/73583/ http://irep.iium.edu.my/73583/ http://irep.iium.edu.my/73583/7/73583%20Aeroelastic%20assessment%20of%20cracked%20composite.pdf http://irep.iium.edu.my/73583/8/73583%20Aeroelastic%20assessment%20of%20cracked%20composite%20SCOPUS.pdf |
Internet
http://irep.iium.edu.my/73583/http://irep.iium.edu.my/73583/
http://irep.iium.edu.my/73583/
http://irep.iium.edu.my/73583/7/73583%20Aeroelastic%20assessment%20of%20cracked%20composite.pdf
http://irep.iium.edu.my/73583/8/73583%20Aeroelastic%20assessment%20of%20cracked%20composite%20SCOPUS.pdf