Numerical simulations of shock-wave interaction with a boundary layer in the plane supersonic flows with jet injection
- Authors: Beketaeva A.O.1, Moisseyeva Y.S.1, Naimanova A.Z.1
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Affiliations:
- Institute of Mathematics and Mathematical Modeling
- Issue: Vol 23, No 2 (2016)
- Pages: 173-183
- Section: Article
- URL: https://journals.rcsi.science/1531-8699/article/view/216348
- DOI: https://doi.org/10.1134/S0869864316020037
- ID: 216348
Cite item
Abstract
A supersonic air flow in a plane channel with a transverse turbulent jet of hydrogen injected through a slot on the bottom wall is simulated. The algorithm for solving the Favre-averaged Navier-Stokes equations for the flow of a perfect multispecies gas on the basis of the WENO scheme is proposed. The main attention is paid to the interaction of the shock-wave structure with the boundary layers on the upper and lower duct walls under the conditions of an internal turbulent flow. Namely, a detailed study of the structure of the flow is done, and separation and mixing depending on the jet slot width are investigated. It is found that in addition to well-known shock-wave structures produced by the interaction of the free stream with the transverse jet and the bow shock interaction with the boundary layers near the walls, an additional system of shock waves and the flow separation arise on the bottom wall downstream at some distance from the jet. The comparison with the experimental data is performed.
About the authors
A. O. Beketaeva
Institute of Mathematics and Mathematical Modeling
Author for correspondence.
Email: azimaras@mail.ru
Kazakhstan, Almaty
Ye. S. Moisseyeva
Institute of Mathematics and Mathematical Modeling
Email: azimaras@mail.ru
Kazakhstan, Almaty
A. Zh. Naimanova
Institute of Mathematics and Mathematical Modeling
Email: azimaras@mail.ru
Kazakhstan, Almaty