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机译:Over-wing integration of ultra-high bypass ratio engines: A coupled wing redesign and engine position study
Chalmers University of Technology, Hoersalsvaegen 7A, SE-41296, Gothenburg, Sweden;
GKN Aerospace Sweden AB, Flygmotorvaegen I, SE-46138, Trollhaettan, Sweden;
Over-wing nacelle; Propulsion integration; Ultra-high bypass ratio; Computational fluid dynamics; Aerodynamics; Wing design;