Turboelectric Distributed Propulsion System Modelling

Doctoral thesis English OPEN
Liu, Chengyuan;
  • Publisher: Cranfield University
  • Subject: BLI | TeDP | Distortion | NASA N3-X Aircraft | Turbogenerator | Propulsor | thrust split ratio

The Blended-Wing-Body is a conceptual aircraft design with rear-mounted, over wing engines. Turboelectric distributed propulsion system with boundary layer ingestion has been considered for this aircraft. It uses electricity to transmit power from the core turbine to th... View more
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