Email this article The interaction of shock waves with a boundary layer on a sharp plate and a blunted plate
- Authors: Bashkin V.A.1,2, Egorov I.V.1,2, Palchekovskaya N.V.1,2
-
Affiliations:
- Central Aerohydrodynamic Institute
- Moscow Institute of Physics and Technology (State University)
- Issue: Vol 54, No 3 (2016)
- Pages: 356-369
- Section: 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
Cite item
Open Access
Access granted
Subscription Access
Abstract
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.
About the authors
V. A. Bashkin
Central Aerohydrodynamic Institute; Moscow Institute of Physics and Technology (State University)
Email: nathalie.palchekovskaya@gmail.com
Russian Federation, Zhukovsky, Moscow oblast, 140180; Dolgoprudnyi, Moscow oblast, 141700
I. V. Egorov
Central Aerohydrodynamic Institute; Moscow Institute of Physics and Technology (State University)
Email: nathalie.palchekovskaya@gmail.com
Russian Federation, Zhukovsky, Moscow oblast, 140180; Dolgoprudnyi, Moscow oblast, 141700
N. V. Palchekovskaya
Central Aerohydrodynamic Institute; Moscow Institute of Physics and Technology (State University)
Author for correspondence.
Email: nathalie.palchekovskaya@gmail.com
Russian Federation, Zhukovsky, Moscow oblast, 140180; Dolgoprudnyi, Moscow oblast, 141700
Supplementary files
