Geodesic
Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 56 (2016) no. 6, pp. 1034-1048 Cet article a éte moissonné depuis la source Math-Net.Ru

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Modern differential turbulence models are validated by computing a separation zone generated in the supersonic flow past a compression wedge lying on a plate of finite width. The results of three- and two-dimensional computations based on the $(q-\omega)$, SST, and Spalart–Allmaras turbulence models are compared with experimental data obtained for 8$^\circ$, 25$^\circ$, and 45$^\circ$ wedges by A. A. Zheltovodov at the Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences. An original law-of-the-wall boundary condition and modifications of the SST model intended for improving the quality of the computed separation zone are described. 
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     title = {Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge},
     journal = {\v{Z}urnal vy\v{c}islitelʹnoj matematiki i matemati\v{c}eskoj fiziki},
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A. A. Babulin; S. M. Bosnyakov; V. V. Vlasenko; M. F. Engulatova; S. V. Matyash; S. V. Mikhailov. Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 56 (2016) no. 6, pp. 1034-1048. http://geodesic.mathdoc.fr/item/ZVMMF_2016_56_6_a9/

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