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

Table 17

Twenty-four rotor blades.

Flow rates(kg/s)	Total inlet pressure (Pa)	Total outlet pressure (Pa)	Boost ratio	Fan efficiency
22.05	106,101	137160	1.292730	0.818845
21.71	105927	138204	1.304710	0.823746
21.14	105879	140320	1.325286	0.841195
20.89	105850	141294	1.334849	0.845656
20.50	105,852	143210	1.352924	0.828095
20.27	105910	144224	1.361752	0.766227
19.71	105980	145096	1.369095	0.787453