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Problem of Multiparametric Optimization of the Construction of the Joint Between the Ceramic Hull and Metallic Fuselage of an Airplane

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Refractories and Industrial Ceramics Aims and scope

An approach to the solution of the problem of determining the optimal design of the connector assembly between the ceramic hull of a high-speed airplane and its metallic fuselage is presented. Definitions of the parameters that exert an effect on the bearing capacity of this assembly are given. An example illustrating the solution of the problem of finding the optimum of the parameters of a construction for the case of a three-layer axisymmetric model is presented.

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Authors and Affiliations

  1. GNTs Russian Federation OAO ONPP Tekhnologiya, Obninsk, Kaluga District, Russia

    D. A. Rogov & P. V. Kovalenko

Authors
  1. D. A. Rogov
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  2. P. V. Kovalenko
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Correspondence to D. A. Rogov.

Additional information

Translated from Novye Ogneupory, No. 10, pp. 24 – 30, October, 2014.

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Rogov, D.A., Kovalenko, P.V. Problem of Multiparametric Optimization of the Construction of the Joint Between the Ceramic Hull and Metallic Fuselage of an Airplane. Refract Ind Ceram 55, 396–402 (2015). https://doi.org/10.1007/s11148-015-9733-4

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  • DOI: https://doi.org/10.1007/s11148-015-9733-4

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