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Study of thermohumid aging of aircraft fiberglass plastic

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Abstract

The thermohumid aging of aircraft fiberglass plastic over 5.5 years is studied. It is shown that, under conditions that simulate a tropical climate, the controlled parameters (maximal water saturation, moisture diffusion coefficient, shear modulus along the sheet plane) vary to the greatest extent after 1 year of aging, after which they stabilize. The molding conditions under which fiberglass plastic preserves high parameters under long-term exposure to a moist environment are determined.

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Authors and Affiliations

  1. Altai State University, pr. Lenina 61, Barnaul, 656049, Russia

    O. V. Startsev, K. O. Prokopenko, A. A. Litvinov & A. S. Krotov

  2. OOO Tekhpolikom, Nizhne Syromyatnicheskaya ul. 11, Moscow, Russia

    L. I. Anikhovskaya

  3. Federal State Unitary Enterprise All-Russian Institute of Aircraft Materials, ul. Radio 17, Moscow, 105005, Russia

    L. A. Dement’eva

Authors
  1. O. V. Startsev
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  2. K. O. Prokopenko
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  3. A. A. Litvinov
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  4. A. S. Krotov
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  5. L. I. Anikhovskaya
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  6. L. A. Dement’eva
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Corresponding author

Correspondence to O. V. Startsev.

Additional information

Original Russian Text © O. V. Startsev, K.O. Prokopenko, A.A. Litvinov, A.S. Krotov, L.I. Anikhovskaya, L.A. Dement’eva, 2009, published in Klei. Germetiki. Tekhnologii, 2009, No. 8, pp. 18–21.

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Startsev, O.V., Prokopenko, K.O., Litvinov, A.A. et al. Study of thermohumid aging of aircraft fiberglass plastic. Polym. Sci. Ser. D 3, 58–61 (2010). https://doi.org/10.1134/S1995421210010107

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  • DOI: https://doi.org/10.1134/S1995421210010107

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