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
Author(s)
Giri, Jagannath
Advisor(s)
Simitses, George J.
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Date Issued
1975-12
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Resource Type
Text
Resource Subtype
Dissertation