Minimum-Weight Design of Stiffened Cylinders under Axial Compression
- 1 June 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (6), 750-755
- https://doi.org/10.2514/3.60432
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
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