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Minimal weight design of longitudinal cylindrical shells under joint axial compression and internal pressure

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Soviet applied mechanics Aims and scope

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Literature Cited

  1. I. Ya. Amiro, “Boundary conditions for a ribbed cylindrical shell subject simultaneously to axial forces and internal pressure,” Prikl. Mekhan.,7, No. 5, (1961).

  2. M. M. Stepanov, M. M. Tsvétkov, and L. I. Manevich, “Thickness of reinforcing ribs for a cylindrical shell,” Prikl. Mekhan.,9, No. 1 (1963).

  3. W. Flügge, “Die Stabilität der Kreiszylinderschale,” Ing. Archiv.,3, No. 5 (1932).

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Authors and Affiliations

  1. Institute of Mechanics, Academy of Sciences of the Ukrainian SSR, Russia

    A. S. Pal'chevskii

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  1. A. S. Pal'chevskii
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Translated from Prikladnaya Mekhanika, Vol. 6, No. 10, pp. 49–54, October, 1970.

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Pal'chevskii, A.S. Minimal weight design of longitudinal cylindrical shells under joint axial compression and internal pressure. Soviet Applied Mechanics 6, 1079–1083 (1970). https://doi.org/10.1007/BF00888908

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  • DOI: https://doi.org/10.1007/BF00888908

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