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
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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