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

Table 18

Fifteen rotor blades.

Flow rates (kg/s)	Total inlet pressure (Pa)	Total outlet pressure (Pa)	Boost ratio
52.00	41,149	43,356	1.053634
44.00	41,549	44,456	1.069966
37.70	41,087	50,874	1.238202
31.00	37,955	57,337	1.390657