Optimization of stiffened panels in which mode jumping is accounted for
Author:
Affiliation:
1. Lockheed Martin Palo Alto Research Lab., CA
2. Delft Univ. of Technology, Netherlands
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1141
Reference70 articles.
1. Panda—Interactive program for minimum weight design of stiffened cylindrical panels and shells
2. Theoretical basis of the PANDA computer program for preliminary design of stiffened panels under combined in-plane loads
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