Research Article

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

Table 15

Fifteen rotor blades.

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

22.15106,857138,6781.2977890.561094
21.7106,744140,9811.3207390.788289
21.1106,944142,8481.3357270.829513
20.8106,946143,5331.3421070.753364
19.969106,8781442631.3497890.740856