Affiliation:
1. Delft University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Cited by
2 articles.
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1. Reduction Method for Finite Element Nonlinear Dynamic Analysis of Shells;AIAA Journal;2011-10
2. Finite Element Based Initial Post-Buckling Analysis of Shells of Revolution;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07