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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Bibliographic Details
Main Authors: Crate, Harold, (Author), Batdorf, S. B., (Author), Baab, George W., (Author)
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Format: 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.
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ISBN: 9781680156362
1680156365
Physical Description: 1 online resource (15 pages, 9 unnumbered pages) : illustrations

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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.
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.
Bibliography: Includes bibliographical references.
ISBN: 9781680156362
1680156365
Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty