A simplified method of elastic-stability analysis for thin cylindrical shells
This paper develops a new method for determining the buckling stresses of cylindrical shells under various loading conditions. In part I, the equation for the equilibrium of cylindrical shells introduced by Donnell in NACA report no. 479 to find the critical stresses of cylinders in torsion is appli...
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| Main Author | |
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| Corporate Author | |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
U.S. G.P.O.,
1947.
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| Series | Report (United States. National Advisory Committee for Aeronautics) ;
no. 874. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156454 1680156454 |
| Physical Description | 1 online resource (25 pages) |
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| Summary: | This paper develops a new method for determining the buckling stresses of cylindrical shells under various loading conditions. In part I, the equation for the equilibrium of cylindrical shells introduced by Donnell in NACA report no. 479 to find the critical stresses of cylinders in torsion is applied to find critical stresses for cylinders with simply supported edges under other loading conditions. In part II, a modified form of Donnell's equation for the equilibrium of thin cylindrical shells is derived which is equivalent to Donnell's equation but has certain advantages in physical interpretation and in ease of solution, particularly in the case of shells having clamped edges. -- |
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| Bibliography: | Includes bibliographical references. |
| ISBN: | 9781680156454 1680156454 |
| 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 (25 pages) |