Research Article

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

Table 16

Eighteen rotor blades.

Flow rates(kg/s)Total inlet pressure (Pa)Total outlet pressure (Pa)Boost ratioFan efficiency

22.42107,451137,9741.2840640.867326
22.09107,639139,9671.3003420.878934
21.71107,697142,0301.3187890.843172
21.47107,791143,0261.3268830.822364
21.09107,847143,5191.3307650.755491
20.36108,062145,4961.3371580.682653
19.72108,185146,1251.3507120.646103