Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System

Table 20

Twenty-four rotor blades.

Flow rates (kg/s)	Total inlet pressure (Pa)	Total outlet pressure (Pa)	Boost ratio
35.22	42,526	43,114	1.013827
31.16	37,507	58,901	1.370400
29.70	37,503	60,837	1.422190
27.00	37,568	62,219	1.456170