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Calculating the stiffness of formers in longitudinally compressed ribbed cylindrical shells

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Soviet Applied Mechanics Aims and scope

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References

  1. I. Ya. Amiro, “Investigation of stability of a ribbed cylindrical shell under longitudinal compression”, Prykladna mekhanika, vol. 6, no. 3, 1960.

  2. Waingarten, Morgan, and Seid, “Stability of elastic thin-walled cylindrical and conical shells under axial compression,” Raketnaya tekhnika i kosmonavtika, no. 3, 1965.

  3. A. S. Pal'chevskii, “Analysis of cylindrical minimum weight shells provided with stringers under axial compression,” Prikladnaya mekhanika [Soviet Applied Mechanics], vol. 2, no. 9, 1966.

  4. G. Fisher, “The effect of boundary conditions on the stability of thin-walled cylindrical shells under axial compression and internal pressure,” Raketnaya tekhnika i kosmonavtika, no. 4, 1965.

  5. F. R. Shanley, Weight and Strength Analysis of Aircraft Structures [Russian translation], Oborongiz, Moscow, 1957.

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  6. B. Saelman, “Optimum spacing of shell frames,” J. Aircraft, vol. 1, no. 4, 1964.

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Authors and Affiliations

  1. Institute of Mechanics, AS UkrSSR, Kiev

    A. S. Pal'chevskii

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  1. A. S. Pal'chevskii
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Prikladnaya Mekhanika, Vol. 4, No. 2, pp. 67–71, 1968

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Pal'chevskii, A.S. Calculating the stiffness of formers in longitudinally compressed ribbed cylindrical shells. Soviet Applied Mechanics 4, 39–41 (1968). https://doi.org/10.1007/BF00887296

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  • DOI: https://doi.org/10.1007/BF00887296

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