Buckling of thin-walled cylinder under axial compression and internal pressure
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| Main Author | |
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| Corporate Author | |
| Other Authors | , |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 2021. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156195 1680156195 |
| Physical Description | 1 online resource (29 pages) : illustrations |
Cover
| Abstract: | An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results. |
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| Item Description: | "January 1950." NACA TN No. 2021. |
| Bibliography: | Includes bibliographical references. |
| ISBN: | 9781680156195 1680156195 |
| 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 (29 pages) : illustrations |