| Autor: |
Vankova, O. S., Zakharova, Yu. V., Fedorova, N. N., Goldfeld, M. A. |
| Zdroj: |
AIP Conference Proceedings; 2018, Vol. 2036 Issue 1, p040018-1-040018-8, 8p |
| Abstrakt: |
The paper presents results of joint calculation and experimental research of a supersonic flow in the channel of the combustor with variable input conditions. Experimental studies are carried out in the hot-shot aerodynamic facility IT-302M with Mach number at the entrance to the combustor M = 4. Numerical simulations are performed using the ANSYS CFD (Fluent) software. The numerical technique to put the transient conditions at the inlet is developed. Based on the results of calculations, the effect of the unsteady input conditions on the flow structure in the channel under investigation is estimated. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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