Abstract:
The results of direct numerical simulation of supersonic flow around a cylindrical blunt
body with tail expansion are presented. The data obtained are compared with the results
of laboratory experiments for the Mach numbers 3 and 4 and the angles of attack of 10
and 20 degrees. The results are obtained by using the quasi-gas-dynamic equations.
Citation:
I. A. Shirokov, T. G. Elizarova, “Computational experiment in the problem of supersonic flow around a blunt body with tail expansion”, Mat. Model., 31:10 (2019), 117–129; Math. Models Comput. Simul., 12:3 (2020), 433–444
\Bibitem{ShiEli19}
\by I.~A.~Shirokov, T.~G.~Elizarova
\paper Computational experiment in the problem of supersonic flow around a blunt body with tail expansion
\jour Mat. Model.
\yr 2019
\vol 31
\issue 10
\pages 117--129
\mathnet{http://mi.mathnet.ru/mm4122}
\crossref{https://doi.org/10.1134/S0234087919100095}
\elib{https://elibrary.ru/item.asp?id=41137484}
\transl
\jour Math. Models Comput. Simul.
\yr 2020
\vol 12
\issue 3
\pages 433--444
\crossref{https://doi.org/10.1134/S2070048220030163}
Linking options:
https://www.mathnet.ru/eng/mm4122
https://www.mathnet.ru/eng/mm/v31/i10/p117
This publication is cited in the following 2 articles:
S. V. Polyakov, V. O. Podryga, N. I. Tarasov, “Modeling of Supersonic Flow around Bodies of Revolution of Different Shapes”, Math Models Comput Simul, 16:S2 (2024), S250
I. A. Shirokov, “Chislennoe issledovanie aerodinamicheskikh kharakteristik treugolnogo kryla pri razlichnykh uglakh ataki i bolshikh chislakh Makha”, Preprinty IPM im. M. V. Keldysha, 2021, 056, 24 pp.
Citation in format AMSBIB
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