... at MTU Aero Engines as a high-lift profile with a Reynolds number typical for low-pressure turbines in jet engines. At design conditions, the flow on the stator 2 suction side features a pronounced separation bubble. To study the behavior of the stator 2 boundary layer and the interaction mechanisms...

... and Turbulence Quantities ,” Exp. Fluids 0723-4864 , 6 , pp. 400 – 408 . Shapiro , A. H. , 1953 , “ The Dynamics and Thermodynamics of Compressible Fluid Flow ,” Wiley , New York, Chap. 6, Vol. I , pp. 159 – 186 . 15 11 2005 02 06 2006 exhaust systems jet engines...

... with pressure ratios in the 2:1 range. While such arrangements were satisfactory for commercial use where weight was not a major consideration, they were not suitable for jet engines. The centrifugal compressor for the Whittle engine, the first British jet engine, was developed by trial and error with numerous...