Effects of Inlet Conditions on Performance of Two Dimensional Diffusers
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Experimental apparatus methods
Energy redistributions in diffusing
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adverse pressure gradient boundary layer thickness centerbody centerline Cochran and Kline CpRi CURVE 13 DATA SYMMETRIC INLET diffuser flows diffuser throat Dimensionless diverging wall downstream dynamic pressure Effect of inlet energy redistributions exit plane fixed stall flow patterns flow regime fluctuations fluid fully developed stall fusers geometry head loss inches incompressible flow increase inlet boundary layer inlet flow inlet kinetic energy inlet profiles inlet velocity profiles isentropic kinetic energy efflux L/Wj L/Wl L/Wx large transitory stall line a-a measured mixing Moore and Kline NACA Number obtained one-dimensional inlet kinetic parallel wall PERFORMANCE DATA SYMMETRIC pressure recovery secondary flows separation patterns shift shown in Fig splitter stall inception Stanford University static pressure Steady 29 symmetric inlet conditions TASME tested thin inlet boundary tion Total divergence angle turbulence intensity two-dimensional stall uncertainty undisturbed flow undisturbed inlet upstream values of 29 Waitman wall shear