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Analysis of structural elements made of composite materials with defects

  • Structural Mechanics and Strength of Flight Vehicles
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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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References

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Author information

Authors and Affiliations

  1. PAO Tupolev, naberezhnaya Akademika Tupoleva 17, Tupolev, 105005, Russia

    A. M. Kokurov

  2. A. Blagonravov Mechanical Engineering Research Institute of the Russian Academy of Sciences (IMASH RAN), Malyi Kharitonovskii pereulok 4, Moscow, 101990, Russia

    A. M. Kokurov & I. N. Odintsev

Authors
  1. A. M. Kokurov
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  2. I. N. Odintsev
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Corresponding author

Correspondence to A. M. Kokurov.

Additional information

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

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