Research Article
Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System
Table 2
Initial parameters list of BWB-350 and power system.
| | Design parameters | Design values |
| | Fuselage length (m) | 44.6 | | Spread length (m) | 68.2 | | Reference total area (m2) | 560 | | Average aerodynamic chord length (m) | 10.2 | | Engine section length (m) | 5.88 | | Inlet location from leading edge (m) | 35.6 | | Inlet area (m2) | 18.53 | | Tail nozzle outlet area (m2) | 14.68 |
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