Computational experiment in the problem of supersonic flow around a blunt body with tail expansion
Matematičeskoe modelirovanie, Tome 31 (2019) no. 10, pp. 117-129

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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.
Keywords: supersonic flows, unstructured spatial grids.
Mots-clés : quasi-gas-dynamic equations
@article{MM_2019_31_10_a9,
     author = {I. A. Shirokov and T. G. Elizarova},
     title = {Computational experiment in the problem of supersonic flow around a blunt body with tail expansion},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {117--129},
     publisher = {mathdoc},
     volume = {31},
     number = {10},
     year = {2019},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2019_31_10_a9/}
}
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I. A. Shirokov; T. G. Elizarova. Computational experiment in the problem of supersonic flow around a blunt body with tail expansion. Matematičeskoe modelirovanie, Tome 31 (2019) no. 10, pp. 117-129. http://geodesic.mathdoc.fr/item/MM_2019_31_10_a9/