A simplified method of elastic-stability analysis for thin cylindrical shells

This paper develops a new method for determining the buckling stresses of cylindrical shells under various loading conditions. In part I, the equation for the equilibrium of cylindrical shells introduced by Donnell in NACA report no. 479 to find the critical stresses of cylinders in torsion is appli...

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Bibliographic Details
Main Author Batdorf, S. B.
Corporate Author United States. National Advisory Committee for Aeronautics
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : U.S. G.P.O., 1947.
SeriesReport (United States. National Advisory Committee for Aeronautics) ; no. 874.
Subjects
Online AccessFull text
ISBN9781680156454
1680156454
Physical Description1 online resource (25 pages)

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