RUS  ENG
Full version
JOURNALS // Matematicheskoe modelirovanie // Archive

Mat. Model., 2015 Volume 27, Number 10, Pages 32–46 (Mi mm3656)

This article is cited in 3 papers

On the accuracy of numerical calculation of the boundary layer separation on a finite-width wedge

S. M. Bosnyakova, A. A. Babulinb, V. V. Vlasenkoa, M. F. Engulatovaa, S. V. Matyasha, S. V. Mikhaylova

a Zhukovsky Central Hydrodynamic Institute (TsAGI, Zhukovsky)
b JSC Sukhoi New Civil Technologies (Moscow)

Abstract: The work is devoted to validation of modern differential models of turbulence on an example of calculation of flow in separation zone arising in supersonic flow around a compression wedge. Experimental data for the 25$^\circ$ wedge, obtained in the ITAM SB RAS by A. A. Zheltovodov, are used. These data are compared with the results of 3D and 2D calculations with the use of several differential models of turbulence. Modification of SST model, allowing to improve the quality of separation zone description, is proposed. 3D structure of the separation on the wedge is analyzed.

Keywords: supersonic flow, boundary layer separation, compression wedge, turbulence model, validation.

Received: 16.03.2015


 English version:
Mathematical Models and Computer Simulations, 2016, 8:3, 238–248

Bibliographic databases:


© Steklov Math. Inst. of RAS, 2025