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
By: by Jagannath Giri.
Publisher: s.n.]
Published: 1975
Place of publication: [Atlanta
Language: eng
Number of pages: 147
Subjects: Shells (Engineering); Cylinders.; Torsion.; Airplanes -- Motors -- Cylinders.; Structural stability.
Notes: Vita.

"November 1975."

Thesis (Ph.D.)--Georgia Institute of Technology, 1975. Directed by George J. Simitses. (U.M. order no. 76-16,281)

Bibliography: leaves 143-146.