Design optimization of stiffened composite panels with buckling and damage tolerance constraints
Author:
Affiliation:
1. National Aerospace Lab., Amsterdam, Netherlands
2. Porto, Univ., Portugal
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1750
Reference24 articles.
1. "VICONOPT: Program for Exact Vibration and Buckling Analysis or Design of Prismatic Plate Analysis", F. W. Williams. D. Kennedy. R. Butler. M. S. Anderson. AIAA Journal, 29, No.11, 1991.
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