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Effect of the wall properties on the shock wave / laminar boundary layer interaction
Author(s) -
A. I. Kutepova,
П. А. Поливанов,
A. A. Sidorenko
Publication year - 2019
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1369/1/012037
Subject(s) - laminar flow , wedge (geometry) , boundary layer , mechanics , materials science , shock wave , heat transfer , oblique shock , flow (mathematics) , optics , physics
The CFD calculations have been performed based on RANS approach with the Menter transition model [1]. The boundary layer developing on a flat plate was considered. To generate the incident shock wave, a wedge was installed over the plate. The wall was represented by one cm thick solid flat plate made from aluminum and polyacetal. Flow parameters were M ∞ =1.41, P 0 =0.7 bar, T 0 =293K. As a result of solving the conjugate heat transfer problem, the SWBLI flow was studied. The temperature and pressure distributions on the wall for different surface materials were obtained. It was found that the streamwise heat fluxes inside the wall can lead to a change of the separation zone length.

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