Cover Image

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

Show other versions (1)
Bibliographic Details
Main Authors: Crate, Harold (Author), Batdorf, S. B. (Author), Baab, George W. (Author)
Corporate Authors: Knovel (Firm), United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Format: Government Document eBook
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L67.
Subjects:
Cylinders.
Loads (Mechanics)
Shear (Mechanics)
Buckling (Mechanics)
Strains and stresses.
Charts, diagrams, etc.
Electronic books.
Online Access:Connect to the full text of this electronic book
Description
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.
Physical Description:1 online resource (15 pages, 9 unnumbered pages) : illustrations.
Bibliography:Includes bibliographical references.
ISBN:9781680156362
1680156365