Critical-stress of thin-walled cylinders in axial compression

Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axial compression. These curves are plotted in terms of nondimensional parameters of small-deflection theory and are compared with theoretical curves derived for the buckling of cylinders with simply sup...

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Bibliographic Details
Main Authors Batdorf, S. B. (Author), Schildcrout, Murry (Author), Stein, Manuel (Author)
Corporate Authors United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; 1343.
Subjects
Online AccessFull text
ISBN9781680156119
168015611X
Physical Description1 online resource (17 pages) : illustrations

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