Reliability of uncertain laminated shells due to buckling and supersonic flutter
Author:
Affiliation:
1. Purdue University, West Lafayette, Indiana 47907
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10793
Reference43 articles.
1. Advances of thin shell finite elements and some applications—version I
2. Finite-Element Analysis of Vibration and Flutter of Cantilever Anisotropic Plates
3. Flutter and Buckling of General Laminated Plates
4. Free vibration and flutter of laminated quadrilateral plates
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