Geodesic
Application of kinetically consistent finite difference schemes for turbulent supersonic jet noise prediction
Matematičeskoe modelirovanie, Tome 13 (2001) no. 10, pp. 56-76 Cet article a éte moissonné depuis la source Math-Net.Ru

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The results of supersonic jet noise prediction are represented. Numerical simulation procedure includes two main stages. At the first stage, a steady flow field for turbulent supersonic jet is calculated with the help of Reynolds averaged Navier–Stokes equations closed by $k-\varepsilon$ turbulence model. At the second stage, the data on mean flow parameters and turbulent characteristics obtained at the previous stage are used at solving the linearized Navier-Stokes equations with specially constructed source terms. Kinetically consistent finite difference (KCFD) schemes are taken as a basic numerical algorithm. 
@article{MM_2001_13_10_a4,
     author = {I. V. Abalakin and A. N. Antonov and M. A. Antonov and T. K. Kozubskaya and B. N. Chetverushkin},
     title = {Application of kinetically consistent finite difference schemes for turbulent supersonic jet noise prediction},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {56--76},
     year = {2001},
     volume = {13},
     number = {10},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2001_13_10_a4/}
}
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I. V. Abalakin; A. N. Antonov; M. A. Antonov; T. K. Kozubskaya; B. N. Chetverushkin. Application of kinetically consistent finite difference schemes for turbulent supersonic jet noise prediction. Matematičeskoe modelirovanie, Tome 13 (2001) no. 10, pp. 56-76. http://geodesic.mathdoc.fr/item/MM_2001_13_10_a4/