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Part of the book series: Solid Mechanics and Its Applications ((SMIA,volume 18))

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Abstract

Shells in which the middle surface is generated by rotating a generator about an axis are called shells of revolution. A closed cylindrical shell is the simplest case, and the analysis of stresses and deformations in such cylindrical shells was treated in Chapter 3. Due to Reissner, Meissner, and Naghdi, a generalized method of analysis can be employed for all shells of revolution subjected to axially symmetric loads without dealing with each shell geometry specifically. This treatment is presented below, because of its extreme usefulness.

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References

  1. Reissner, E., “On the Theory of Thin Elastic Shells,” H. Reissner Anniversary Volume, J. W. Edwards, Ann Arbor, Michigan, 1949, pp. 231–247.

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  2. Naghdi, P. M., and C. N. De Silva, “On the Deformation of Elastic Shells of Revolution,” Quarterly Journal of Applied Mathematics, Volume 12, 1954.

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Other suggested reading for shells of revolution subjected to asymmetric loads

  1. Steele, C. R., “Shells of Revolution with Edge Loads of Rapid Circumferential Variation”, Journal of Applied Mechanics, Vol. 29, pp. 701–707, 962.

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  2. Schile, R. D., “Asymptotic Solution of Nonshallow Shells of Revolution Subjected to Nonsymmetric Loads”, Journal of the Aerospace Sciences, Vol. 29, pp. 1375–1379, 1962.

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  3. Kalnins, A., “Analysis of Shells of Revolution Subjected to Symmetrical and Nonsymmetrical Loads, Journal of Applied Mechanics, 1964.

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© 1993 Springer Science+Business Media Dordrecht

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Vinson, J.R. (1993). Shells of Revolution Subjected to Axially Symmetric Loads. In: The Behavior of Shells Composed of Isotropic and Composite Materials. Solid Mechanics and Its Applications, vol 18. Springer, Dordrecht. https://doi.org/10.1007/978-94-015-8141-7_4

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  • DOI: https://doi.org/10.1007/978-94-015-8141-7_4

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-90-481-4237-8

  • Online ISBN: 978-94-015-8141-7

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