Effects of Size and Location of a Circular Cutout on Buckling and Failure of a Cylindrical Shell in Bending
Author:
Affiliation:
1. National Defense University
2. University of South Carolina, Columbia
3. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0433
Reference8 articles.
1. Data Report," 2011.
2. Failure Criteria for Unidirectional Fiber Composites
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