Title The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion / Harold Crate, S.B. Batdorf, and George W. Baab

Published Washington, D.C. : National Advisory Committee for Aeronautics, [1944]

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Description 1 online resource (15 pages, 9 unnumbered pages) : illustrations Series Wartime Report / National Advisory Committee for Aeronautics ; number L67 Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L67 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 Notes 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 Notes Print version record Subject Cylinders. Loads (Mechanics) Shear (Mechanics) Buckling (Mechanics) Strains and stresses. Charts, diagrams, etc. cylinders (solids) shear stress. warping. buckling. strain. stress. diagrams. Buckling (Mechanics) Charts, diagrams, etc. Cylinders. Loads (Mechanics) Shear (Mechanics) Strains and stresses. Form Electronic book Author Batdorf, S. B., author. Baab, George W., author United States. National Advisory Committee for Aeronautics. Langley Aeronautical Laboratory. ISBN 9781680156362 1680156365

Other Titles NACA Wartime Reports. Series L

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