Finite elements applied to panel flutter.
Author:
Affiliation:
1. National Aeronautical Establishment, Ottawa, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference16 articles.
1. Errata: "Plastic Buckling of Axially Compressed Cylindrical Shell"
2. August 1963;Leckie F. A.
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