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Estimating the limit state of sealants in aircraft structures

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Abstract

A computational and experimental study of the mechanical properties of the Viksint U-2-28NT sealant under uniaxial elongation and shear is carried out. The possibility of strength calculation of the sealant in terms of the elongation ratio limit value measured by the tension test results is shown.

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Authors and Affiliations

  1. Blagonravov Mechanical Engineering Institute, Russian Academy of Sciences, Maly Kharitonievskii per. 4, Moscow, 101990, Russia

    A. M. Dumanskii & A. V. Terehin

  2. OAO ONPP Technologiya, Kievskoe sh. 15, Obninsk, Kaluga oblast, 249035, Russia

    V. I. Nepovinnykh, M. Yu. Rusin & A. V. Terehin

  3. Bauman Moscow State Technical University, Gospital’nyi per. 10, Moscow, 107005, Russia

    A. M. Dumanskii

Authors
  1. A. M. Dumanskii
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  2. V. I. Nepovinnykh
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  3. M. Yu. Rusin
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  4. A. V. Terehin
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Corresponding author

Correspondence to A. M. Dumanskii.

Additional information

Original Russian Text © A.M. Dumanskii, V.I. Nepovinnykh, M.Yu. Rusin, A.V. Terehin, 2014, published in Klei. Germetiki. Tekhnologii, 2014, No. 2, pp. 31–38.

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Dumanskii, A.M., Nepovinnykh, V.I., Rusin, M.Y. et al. Estimating the limit state of sealants in aircraft structures. Polym. Sci. Ser. D 7, 201–207 (2014). https://doi.org/10.1134/S1995421214030046

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  • DOI: https://doi.org/10.1134/S1995421214030046

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