Research Article
Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System
Table 12
Numerical calculation results of 3D internal flow field.
| | Flow rates (kg/s) | Total inlet pressure (Pa) | Total inlet temperature (K) | Total outlet pressure (Pa) | Total outlet temperature (K) | Outlet static pressure (Pa) |
| | 984.9 | 50,754 | 265.1 | 64,478 | 310 | 31,700 |
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