Weight Comparisons of Optimized Stiffened, Unstiffened, and Sandwich Cylindrical Shells
Author:
Affiliation:
1. Northrop Corp., Hawthorne, Calif.
2. Westinghouse Electric Corp., Madison, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58885
Reference19 articles.
1. MINIMUM WEIGHT POTENTIALS FOR STIFFENED PLATES AND SHELLS
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