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

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Authors
Giri, Jagannath
Authors
Advisors
Simitses, George J.
Advisors
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Supplementary to
Abstract
Sponsor
Date Issued
1975-12
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Resource Type
Text
Resource Subtype
Dissertation
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