Comparative Study on Optimal Stiffener Placement for Curvilinearly Stiffened Panels
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C000234
Reference23 articles.
1. General Panel Sizing Computer Code and Its Application to Composite Structural Panels
2. Panda—Interactive program for minimum weight design of stiffened cylindrical panels and shells
3. PANDA2—Program for minimum weight design of stiffened, composite, locally buckled panels
4. Theoretical basis of the PANDA computer program for preliminary design of stiffened panels under combined in-plane loads
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