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]
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