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