电邮这篇文章 The interaction of shock waves with a boundary layer on a sharp plate and a blunted plate
- 作者: Bashkin V.A.1,2, Egorov I.V.1,2, Palchekovskaya N.V.1,2
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隶属关系:
- Central Aerohydrodynamic Institute
- Moscow Institute of Physics and Technology (State University)
- 期: 卷 54, 编号 3 (2016)
- 页面: 356-369
- 栏目: Heat and Mass Transfer and Physical Gasdynamics
- URL: https://journals.rcsi.science/0018-151X/article/view/156791
- DOI: https://doi.org/10.1134/S0018151X16020012
- ID: 156791
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详细
The interaction of shock waves with a turbulent boundary layer on a sharp plate and a blunted plate is numerically investigated. The shock waves in the flow are generated by wedges installed on the flat plate. The flow is simulated by the dynamic equations of a viscous perfect gas. The effect of the blunting radius of the plate’s leading edge and the wedge angle on the flow field and the local aerodynamic coefficients is shown. The calculated results are in agreement with the experimental data.
作者简介
V. Bashkin
Central Aerohydrodynamic Institute; Moscow Institute of Physics and Technology (State University)
Email: nathalie.palchekovskaya@gmail.com
俄罗斯联邦, Zhukovsky, Moscow oblast, 140180; Dolgoprudnyi, Moscow oblast, 141700
I. Egorov
Central Aerohydrodynamic Institute; Moscow Institute of Physics and Technology (State University)
Email: nathalie.palchekovskaya@gmail.com
俄罗斯联邦, Zhukovsky, Moscow oblast, 140180; Dolgoprudnyi, Moscow oblast, 141700
N. Palchekovskaya
Central Aerohydrodynamic Institute; Moscow Institute of Physics and Technology (State University)
编辑信件的主要联系方式.
Email: nathalie.palchekovskaya@gmail.com
俄罗斯联邦, Zhukovsky, Moscow oblast, 140180; Dolgoprudnyi, Moscow oblast, 141700
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