Abstract
The paper presents an improved technique and the results of strength analysis for the aircraft structural elements with a structural defect like an arbitrary shape delamination.
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Original Russian Text © A.M. Kokurov, I.N. Odintsev, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2017, No. 1, pp. 21–25
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Kokurov, A.M., Odintsev, I.N. Analysis of structural elements made of composite materials with defects. Russ. Aeronaut. 60, 21–26 (2017). https://doi.org/10.3103/S1068799817010044
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DOI: https://doi.org/10.3103/S1068799817010044