Geodesic
Mathematical simulation of turbulent separated transonic flows about the bodies of revolution
Matematičeskoe modelirovanie, Tome 23 (2011) no. 5, pp. 71-80.

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The properties of the turbulent separated flows around boat-tailed objects, especially in transonic regimes, are very complex and understood to date not very well. With variation of free-stream Mach number the flow structure: the size and location of separation areas, internal supersonic regions, the position and intensity of internal shocks – varies significantly. These flow properties determine the complexity of the numerical modeling problem and high demands on the algorithms used. The paper presents a comparison of numerical results obtained on the basis of different mathematical models with experimental data. The investigation of fundamental properties of transonic flow transformation are presented also.
Keywords: transonic flow, flow separation, the shock wave-boundary layer interaction, turbulence model. 
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I. Yu. Kudryashov; A. E. Lutsky. Mathematical simulation of turbulent separated transonic flows about the bodies of revolution. Matematičeskoe modelirovanie, Tome 23 (2011) no. 5, pp. 71-80. http://geodesic.mathdoc.fr/item/MM_2011_23_5_a4/

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