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Georgia Institute of Technology
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
Abstract
Ph.D.
Degree
thesis:*- Department dc:contributor.department
- Engineering mechanics
- Grantor dc:publisher
- Georgia Institute of Technology
- Year dc:date.issued
- 1975
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Giri, Jagannath
- Advisor dc:contributor.advisor
-
- Simitses, George J.
Identifiers
dc:identifier.*- Handle dc:identifier.uri
- http://hdl.handle.net/1853/20496
- OAI identifier oai:identifier
- oai:repository.gatech.edu:1853/20496