Research Article
Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System
Table 8
Grid density verification of 3D internal flow field.
| | Grid density (million) | Height of first grid layer | Flow rates (kg/s) | Total inlet pressure (Pa) | Total outlet pressure (Pa) |
| | 0.70 | 1.00E−05 | 4.2 | 4928 | 5078 | | 0.95 | 1.00E−05 | 4.3 | 5152 | 5184 | | 1.20 | 1.00E−05 | 4.3 | 5069 | 5200 |
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