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Methods for determining the weight of a supersonic passenger administrative aircraft fuselage structure based on regression analysis

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Abstract

This paper describes the main projects for the creation of supersonic administrative aircraft and the features of the weight analysis of supersonic passenger administrative aircraft. The question of the resource and strength of the structure in operating conditions at high temperatures is considered from the point of view of weight analysis. A model is proposed for calculating the mass of the supersonic passenger administrative aircraft fuselage in the first approximation based on regression analysis.

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Authors and Affiliations

  1. Moscow Aviation Institute (National Research University), Moscow, Russia

    Gulnar Resulkulyeva & Sergey Serebryansky

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  1. Gulnar Resulkulyeva
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  2. Sergey Serebryansky
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Correspondence to Sergey Serebryansky.

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Resulkulyeva, G., Serebryansky, S. Methods for determining the weight of a supersonic passenger administrative aircraft fuselage structure based on regression analysis. AS 7, 159–166 (2024). https://doi.org/10.1007/s42401-023-00240-7

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  • DOI: https://doi.org/10.1007/s42401-023-00240-7

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