The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion
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| Main Authors | , , |
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| Corporate Authors | , |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1944]
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| Series | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L67. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156362 1680156365 |
| Physical Description | 1 online resource (15 pages, 9 unnumbered pages) : illustrations |
Cover
| 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. |
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| 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 |
| Physical Description: | 1 online resource (15 pages, 9 unnumbered pages) : illustrations |