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  4. Non-linear random response of stiffened aerospace panels using a combined finite element / modal technique
 
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Non-linear random response of stiffened aerospace panels using a combined finite element / modal technique

Author(s)
Leung, Andrew Yee Tak  
Author(s)
McEwan, M. I.
Wright, J. R.
Cooper, J. E.
Date Issued
2001
Publisher
American Institute of Aeronautics and Astronautics
Related Publication(s)
Proceedings of the International Forum on Aeroelasticity and Structural Dynamics (IFASD 2001), Volume 3
Start page
1
End page
12
URI
https://repository.sfu.edu.hk/handle/sfu/3034
SFU Affiliated Publication
No
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