Title:
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

dc.contributor.advisor Simitses, George J.
dc.contributor.author Giri, Jagannath en_US
dc.contributor.department Engineering mechanics en_US
dc.date.accessioned 2008-03-13T11:30:50Z
dc.date.available 2008-03-13T11:30:50Z
dc.date.issued 1975-12 en_US
dc.description.degree Ph.D. en_US
dc.identifier.bibid 253731 en_US
dc.identifier.uri http://hdl.handle.net/1853/20496
dc.publisher Georgia Institute of Technology en_US
dc.subject.lcsh Shells (Engineering) en_US
dc.subject.lcsh Cylinders en_US
dc.title 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 en_US
dc.type Text
dc.type.genre Dissertation
dspace.entity.type Publication
local.contributor.corporatename George W. Woodruff School of Mechanical Engineering
local.contributor.corporatename College of Engineering
relation.isOrgUnitOfPublication c01ff908-c25f-439b-bf10-a074ed886bb7
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
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