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

Table 6

Verification of grid density of 3D outflow field.

Grid density (million)	Height of first grid layer
1.0	5.00E−05	0.304928	0.015642	19.497
2.0	5.00E−05	0.312245	0.014854	21.021
3.3	5.00E−05	0.314682	0.014437	21.797
4.3	5.00E−05	0.314945	0.014237	21.917