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Linear and geometrically nonlinear structural dynamic analysis using reduced basis finite element technique
File(s)
Author(s)
Yao, Ming-Sheng
Type
Thesis
Version
Open Access
Date Issued
1990
Date Awarded
1990
URI
Copyright Statement
Attribution NoDerivatives 4.0 International Licence (CC BY-ND)
License URL
Creator
Yao, Ming-Sheng
Publisher Department
Department of Aeronautics
Publisher Institution
Imperial College London
Qualification Level
Doctoral
Qualification Name
PhD