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Investigation of the buckled state of ribbed cylindrical shells subjected to axial compression

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Literature Cited

  1. I. Ya. Amiro, “Investigation of the stability of a ribbed cylindrical shell in axial compression,” Prikl. Mekhan.,6, No. 3 (1960).

  2. I. Ya. Amiro, “Investigation of the stability and postbuckling deformation of ribbed cylindrical shells in axial compression,” Prikl. Mekhan.,1, No.10 (1965).

  3. A. S. Vol'mir, Flexible Plates and Shells [in Russian], GITTL, Moscow, (1956).

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  4. O. I. Terebushko, “Calculation of the carrying capacity of a circular cylindrical panel reinforced with ribs,” in: Design of Three-Dimensional Structures [in Russian], Vol. 4, Gosstroiizdat, Moscow, (1958).

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  5. N. J. Hoff, W. A. Madsen, and J. Mayers, “Postbuckling equilibrium of circular cylindrical shells in axial compression,” Rocket Technology and Astronautics [Russian translation], No. 1, Fourth Edition (1966).

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Institute of Mechanics, Academy of Sciences of the Ukrainian SSR, Kiev. Translated from Prikladnaya Mekhanika, Vol. 5, No. 9, pp. 34–39, September, 1969.

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Pryadko, A.A. Investigation of the buckled state of ribbed cylindrical shells subjected to axial compression. Soviet Applied Mechanics 5, 929–933 (1969). https://doi.org/10.1007/BF00885775

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  • DOI: https://doi.org/10.1007/BF00885775

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