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

Table 7

Verification of the first layer grid height of the 3D internal flow field.

Grid density (million)	Height of first grid layer	Flow rates (kg/s)	Total inlet pressure (Pa)	Total outlet pressure (Pa)
0.95	5.00E−04	4.3	4902	5066
0.95	2.00E−05	4.3	5037	5221
0.95	1.00E−05	4.3	5152	5184
0.95	5.00E−06	4.3	5088	5209