Aerodynamic Improvement of a Compact Centrifugal Compressor.

Autor: Boldyrev, Yu. Ya., Aleshin, M. V., Davydov, I. S., Sundukov, M. Yu.
Zdroj: Russian Engineering Research; Jun2019, Vol. 39 Issue 6, p463-468, 6p
Abstrakt: For the example of the JetCat P-200RX turbojet engine, optimization of the diffuser and straightening unit of a compact centrifugal compressor is considered, on the basis of a mathematical model of viscous turbulent air flow. The goal of optimization is to increase the isentropic (adiabatic) efficiency of the compressor. [ABSTRACT FROM AUTHOR]
Databáze: Complementary Index