The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion
By: Harold Crate, S.B. Batdorf, and George W. Baab
Contributors: Batdorf, S. B., author; Baab, George W., author; United States. National Advisory Committee for Aeronautics; Langley Aeronautical Laboratory
Series: Wartime Report / National Advisory Committee for Aeronautics -- number L67; Wartime Reports (United States. National Advisory Committee for Aeronautics) -- no. L67.
Publisher: National Advisory Committee for Aeronautics
Published: 1944
Place of publication: Washington, D.C
Language: eng
Number of pages: 15
ISBN-13: 9781680156362
Subjects: Cylinders; Loads (Mechanics); Shear (Mechanics); Buckling (Mechanics); Strains and stresses; Charts, diagrams; Cylindres; Charges; Cisaillement (Mécanique); Flambage (Résistance des matériaux); Contraintes (Mécanique); Tableaux, graphiques; Cylinders (solids); Shear stress; Warping; Buckling; Strain; Stress; Diagrams
Other titles: NACA Wartime Reports. Series L.
Description: 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.

Includes bibliographical references.