Numerical solution of the shock wave / turbulent boundary layer interaction problem
Abstract
The problem of shock wave / turbulent boundary layer interaction is considered. Numerical simulation is performed with numerical integration of the RANS equations and the two-equation turbulence model k-ω SST. The numerical results obtained with modified solver FlowER-Y are compared with experimental data. The special attention is paid to the uncertainties and the troubles attached to considered problem.
Downloads
Published
2017-01-31
Issue
Section
Aero- and hydrodynamics in energy machines
License
Copyright (c) 2017 С. В. Ершов, П. А. Поливанов, А. А. Сидоренко, А. И. Деревянко
This work is licensed under a Creative Commons Attribution-NoDerivatives 4.0 International License.
All authors agree with the following conditions:
- The authors reserve the right to claim authorship of their work and transfer to the journal the right of first publication of the work under the license agreement (the agreement).
- Authors have a right to conclude independently additional agreement on non-exclusive spreading the work in the form in which it was published by the jpurnal (for example, to place the work in institution repository or to publish as a part of a monograph), providing a link to the first publication of the work in this journal.
- Journal policy allows authors to place the manuscript in the Internet (for example, in the institution repository or on a personal web sites) both before its submission to the editorial board and during its editorial processing, as this ensures the productive scientific discussion and impact positively on the efficiency and dynamics of citation of published work (see The Effect of Open Access).
