Experimental and Numerical Investigation of the Mixing Ratio for Various Vane Swirlers of the Combustion Chamber of a Gas Turbine Engine.

Autor:	Nguen, T. D., Aleksandrov, Yu. B., Sulaiman, A. I., Mingazov, B. G.
Zdroj:	Russian Aeronautics; Dec2020, Vol. 63 Issue 4, p669-676, 8p
Abstrakt:	The paper investigates the swirling flow behind the GTE combustion chamber swirler with blades installed under different angles. The mixing ratio in the flow is experimentally analyzed and compared with the estimated values obtained by a numerical approach and using various models of turbulent viscosity. [ABSTRACT FROM AUTHOR]
Databáze:	Complementary Index
Externí odkaz:	Zobrazit plný text záznamu Full text from SpringerLink