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

Table 11

Iteration data of 3D outflow field.

Flow rates(kg/s)	Total inlet pressure (Pa)	Total outlet pressure (Pa)	Outlet static pressure (Pa)
810	33,662	49,038	28,698
874	34,072	52,558	29,957
940	34,406	56,697	30,435
984	34,619	59,868	29,904
1002	34,710	61,293	29,501
1023	34,822	63,009	29,093
1134	35,782	71,615	29,095