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

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 si...

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Bibliographic Details
Main Author: Crate, Harold (Author)
Format: Electronic eBook
Language:English
Published: Washington, D.C National Advisory Committee for Aeronautics 1944
Series:Wartime report L-67
Subjects:
Online Access:Volltext
Summary: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:Includes bibliographical references. - 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
Physical Description:1 Online-Ressource (15 p., 9 unnumbered pages)
ISBN:9781680156362

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