Minimum-weight stiffened shells with slight meridional curvature designed to support axial compressive loads.
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5438
Reference5 articles.
1. Some recent advances in the investigation of shell buckling.
2. Computer analysis of various shells of revolution
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