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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Bibliographische Detailangaben
Beteilige Person: Crate, Harold (VerfasserIn)
Format: Elektronisch E-Book
Sprache:Englisch
Veröffentlicht: Washington, D.C National Advisory Committee for Aeronautics 1944
Schriftenreihe:Wartime report L-67
Schlagwörter:
Links:http://app.knovel.com/hotlink/toc/id:kpEIPBSTW3/effect_of_internal_pressure_on_the_buckling_stress_of_thinwalled_circular_cylinders_under_torsion_naca_wartime_report_l67
Zusammenfassung: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
Beschreibung: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
Umfang:1 Online-Ressource (15 p., 9 unnumbered pages)
ISBN:9781680156362