Analysis on the Low Speed Performance of an Inward-Turning Multiduct Inlet for Turbine-Based Combined Cycle Engines

Figure 6

Total pressure distributions on the exit plane of the right T-duct at with (a) 0 degree of angle of attack and (b) 8 degree of angle of attack. Mach number distributions on the exit plane of the right T-duct with (c) 0 degree of angle of attack and (d) 8 degrees of angle of attack.