Last edited by Kajigami
Friday, April 17, 2020 | History

2 edition of 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 found in the catalog.

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

Jagannath Giri

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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Published by s.n.] in [Atlanta .
Written in English

    Subjects:
  • Shells (Engineering),
  • Cylinders.,
  • Torsion.,
  • Airplanes -- Motors -- Cylinders.,
  • Structural stability.

  • Edition Notes

    Statementby Jagannath Giri.
    Classifications
    LC ClassificationsTA350.G45 G5 1975
    The Physical Object
    Paginationxvi, 147 leaves :
    Number of Pages147
    ID Numbers
    Open LibraryOL21241109M


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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 Jagannath Giri Download PDF EPUB FB2