The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion

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Bibliographic Details
Main Authors Crate, Harold (Author), Batdorf, S. B. (Author), Baab, George W. (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, [1944]
SeriesWartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L67.
Subjects
Online AccessFull text
ISBN9781680156362
1680156365
Physical Description1 online resource (15 pages, 9 unnumbered pages) : illustrations

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Abstract:The results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a simple interaction formula was derived.
Item Description:NACA Wartime Report L-67.
Originally issued as NACA as Advance Restricted Report L4E27 (May 1944).
Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Bibliography:Includes bibliographical references.
ISBN:9781680156362
1680156365
Access:Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty
Physical Description:1 online resource (15 pages, 9 unnumbered pages) : illustrations