A procedure for an analytical solution of the problem of the nonlinear deformation of composite cylindrical shells with initial surface imperfections in the form of various deflections and imperfections of the fibrous material in the form of imperfect bonding between the matrix and fibers is developed. The effect of these factors on the critical loads and the post-critical state of shells under axial compression is analyzed.
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Translated from Prykladna Mekhanika, Vol. 58, No. 3, pp. 68–81, May–June 2022.
* This study was sponsored by the budget program “Scientific and technical activities of scientific institutions of the National Academy of Sciences of Ukraine” (KPKVK 6541030).
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Semenyuk, M.P., Zhukova, N.B. Stability of Composite Cylindrical Shells with Geometrical and Structural Imperfections Under Axial Compression*. Int Appl Mech 58, 307–319 (2022). https://doi.org/10.1007/s10778-022-01156-z
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DOI: https://doi.org/10.1007/s10778-022-01156-z