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Minimum weight design of fuselage type stiffened circular cylindrical shells subjected to pure torsion and combined torsion with axial compression with and without lateral pressure

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1. http://hdl.handle.net/1853/20496
2. 253731

Identifer	oai:union.ndltd.org:GATECH/oai:smartech.gatech.edu:1853/20496
Date	12 1900
Creators	Giri, Jagannath
Publisher	Georgia Institute of Technology
Source Sets	Georgia Tech Electronic Thesis and Dissertation Archive
Detected Language	English
Type	Dissertation
Rights	Access restricted to authorized Georgia Tech users only.