Research Article
Analysis on the Low Speed Performance of an Inward-Turning Multiduct Inlet for Turbine-Based Combined Cycle Engines
Figure 8
Effect of inflow speeds on the pressure distributions along the surface of the right T-duct in the plane under different rotational speeds of the turbine engine. (a) Ground test at inflow speed ; (b–d) wind tunnel test at inflow speeds of , 0.15, and 0.24, respectively.