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The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

The equations of the mathematical model are solved in terms of special functions. The results for the design scheme of the aircraft forebody are obtained with a guaranteed accuracy by the stable method of functional normalization.

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Authors and Affiliations

  1. Institute of Applied Mechanics, Russian Academy of Sciences, Leningradskii pr. 7, Moscow, 125040, Russia

    V. N. Bakulin

  2. Bauman Moscow State Technical University, ul. 2-ya Baumanskaya 5, Moscow, 105005, Russia

    Yu. I. Vinogradov

  3. Russian State Social University, ul. Wilhelm Pick 4, Moscow, 129226, Russia

    G. B Men’kov

Authors
  1. V. N. Bakulin
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  2. Yu. I. Vinogradov
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  3. G. B Men’kov
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Corresponding author

Correspondence to V. N. Bakulin.

Additional information

Original Russian Text © V.N. Bakulin, Yu.I. Vinogradov, G.B. Men’kov, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 2, pp. 10–17.

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Bakulin, V.N., Vinogradov, Y.I. & Men’kov, G.B. The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties. Russ. Aeronaut. 61, 156–164 (2018). https://doi.org/10.3103/S1068799818020022

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  • DOI: https://doi.org/10.3103/S1068799818020022

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