Research Article
Modelling and Design Optimization of a Novel Wide-Body Transport Aircraft to Improve the Structural Integrity
Table 6
Top-level design requirements.
| | Requirement | Notations | Value | Units |
| | Maximum cruise velocity | | 850 | km/hr | | Cruise altitude | ρa | 12.2 | km | | Range | R | 6500 | km | | Diversion range | Rr | 400 | km | | Seating capacity | n | 275 | — | | Trapped fuel | — | 6% | — | | Engine | — | GEnx-1B54/P2 | — | | Thrust of each engine | T | 255 | kN | | Specific fuel consumptions | SFC | 0.37 | hr−1 | | Fuselage configuration | — | Wide-body/twin aisle | — | | Maximum take-off and landing field lengths | TLO | <1600 | m |
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Note that: List the equipment required to conduct passenger missions and emergency evacuation as per FAR and airworthiness standards.
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