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

Table 19

Eighteen rotor blades.

Flow rates (kg/s)	Total inlet pressure (Pa)	Total outlet pressure (Pa)	Boost ratio
56.60	43,577	45,558	1.045460
46.00	43,138	49,001	1.135913
38.10	40,036	52,164	1.302927
32.30	37,246	58,086	1.359523
29.00	37,327	61,208	1.439778
26.70	37,359	62,893	1.493477