Geodesic
One numerical technique to solve a three-dimensional supersonic jets
Matematičeskoe modelirovanie, Tome 14 (2002) no. 12, pp. 105-116 Cet article a éte moissonné depuis la source Math-Net.Ru

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The numerical technique is proposed to solve three-dimensional supersonic jet exhausts into the coflow with supersonic and subsonic zones. The simulation based on the parabolized Navier–Stokes equations. As a sample of simulation efficiency an exhausts of supersonic air jets into the supersonic and subsonic co-flow is given. 
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A. Zh. Kaltaev; A. Zh. Naimanova. One numerical technique to solve a three-dimensional supersonic jets. Matematičeskoe modelirovanie, Tome 14 (2002) no. 12, pp. 105-116. http://geodesic.mathdoc.fr/item/MM_2002_14_12_a9/

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