The influence of an oscillating wall on the position of oblique shocks in a 2D channel

In the paper we solve the problem of supersonic gas flow in a two-dimensional channel with the moving upper wall making oscillations according to the harmonic law. In order to obtain a numerical solution for gas dynamics equations we have implemented two difference schemes: the scheme with the space...

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Bibliographic Details
Published in:Journal of Physics: Conference Series Vol. 1214. P. 012005 (1-11)
Main Author: Perchatkina, E. V.
Other Authors: Minkov, Leonid L.
Format: Article
Language:English
Subjects:
Online Access:http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000660418
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039 9 |a 201907091823  |c 201907091635  |d VLOAD  |y 201907091603  |z Александр Эльверович Гилязов 
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100 1 |a Perchatkina, E. V.  |9 497212 
245 1 4 |a The influence of an oscillating wall on the position of oblique shocks in a 2D channel  |c E. V. Perchatkina, L. L. Minkov 
504 |a Библиогр.: 16 назв. 
520 3 |a In the paper we solve the problem of supersonic gas flow in a two-dimensional channel with the moving upper wall making oscillations according to the harmonic law. In order to obtain a numerical solution for gas dynamics equations we have implemented two difference schemes: the scheme with the space and time approximation of the first order and the scheme with the space approximation of the second order. The fluxes were computed using Van Leer's method. A special form of fluxes in the gas dynamics equations is given, which enables to calculate fluxes on cell faces of difference mesh using Van Leer's method. Depending on a type of the harmonic law and initial gas inflow conditions, the peculiarities of oblique-shock wave propagation in moving curvilinear domains have been investigated. It has been determined that under a particular oscillation frequency the presence of wall oscillation practically doesn't have an effect on the flow regime inside the domain. The convergence of the obtained solution is shown by calculations using difference grids with different numbers of cells. While comparing the numerical solution obtained due to our program with the one obtained with Ansys Fluent solver we found that the constructed code operates correctly. 
653 |a сверхзвуковое течение газа 
653 |a уравнения газовой динамики 
653 |a численное решение 
655 4 |a статьи в журналах  |9 879358 
700 1 |a Minkov, Leonid L.  |9 104783 
773 0 |t Journal of Physics: Conference Series  |d 2019  |g Vol. 1214. P. 012005 (1-11)  |x 1742-6588 
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