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Matematicheskoe modelirovanie, 2025, Volume 37, Number 2, Pages 45–62
DOI: https://doi.org/10.20948/mm-2025-02-04 (Mi mm4596) 		 
Optimization method for aerodynamic layout of supersonic passenger aircraft with the aim of reducing drag force and sonic boom loudness

A. V. Wolkov, U. G. Ibragimov, O. V. Karas, M. A. Meniailov, I. L. Chernyshyov

Central Aerohydrodynamic Institute named after prof. N.E. Zhukovsky
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DOI: https://doi.org/10.20948/mm-2025-02-04
Abstract: Optimization method for aerodynamic layout of supersonic passenger aircraft with the aim of reducing drag force and sonic boom loudness is presented. By the process of optimal solution search with fixed lift coefficient the wing twist, the shape of centerline and V-angle of the wing are varied. Wing planform and its volume are unaltered. Examples of optimization for test wing-body type aerodynamic layout are presented.
Keywords: supersonic civil aircraft, optimization, sonic boom.
Funding agency Grant number
Ministry of Science and Higher Education of the Russian Federation 15-2022-1023
Received: 21.02.2024
Revised: 24.06.2024
Accepted: 09.09.2024
Document Type: Article
Language: Russian
Citation: A. V. Wolkov, U. G. Ibragimov, O. V. Karas, M. A. Meniailov, I. L. Chernyshyov, “Optimization method for aerodynamic layout of supersonic passenger aircraft with the aim of reducing drag force and sonic boom loudness”, Mat. Model., 37:2 (2025), 45–62
Citation in format AMSBIB
\Bibitem{VolIbrKar25}
\by A.~V.~Wolkov, U.~G.~Ibragimov, O.~V.~Karas, M.~A.~Meniailov, I.~L.~Chernyshyov
\paper Optimization method for aerodynamic layout of supersonic passenger aircraft with the aim of reducing drag force and sonic boom loudness
\jour Mat. Model.
\yr 2025
\vol 37
\issue 2
\pages 45--62
\mathnet{http://mi.mathnet.ru/mm4596}
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    		Математическое моделирование
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