4Farthing P R, Chew J W, Owen J M. The use of de-swirl nozzles to reduce the pressure drop in a rotating cavity with radial inflow[R]. ASME 89-GT-184.
5Farthing P R, Owen J M. De-swirled radial intlow in a rotating cavity [J]. International Journal of Heat and Fluid Flow, 1991, 12( 1 ): 63-70.
6Firouzian M, Owen J M, Rogers R H. Flow and heat transfer in a rotating cavity with a radial inflow of fluid. Part 2: Velocity, pressure and heat transfer measurements [J]. International Journal of Heat and Fluid Flow, 1986 , 7 (1): 21-27.
8Negulescu, D. , Pfitzner M. : Secondary Air Systems in Aeroengines employing vortex reducers. ASME 2001 - GT - 0198, 2001.
9Peitsch, D. Stein, M., Hein, St. Niehuis, R., Reinm? ller, U. : Numerical Investigation of Vortex Reducer Flows in the High Pressure Compressor of Modem Aeroengines. ASME 2002 - GT - 30674, 2002.
10Andr~ Gtinther, Wieland Uffrecht, Erwin Kaiser, Stefan Oden- bach. Experimental analysis of varied vortex reducer configurations for the internalair system of jet engine gas turbines. ASME GT2008 - 50738.
