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ROTORCRAFT CONFIGURATION AND METHOD OF ROTORCRAFT DESIGN
ROTORCRAFT CONFIGURATION AND METHOD OF ROTORCRAFT DESIGN
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机译:旋翼桨叶配置和旋翼桨叶设计方法
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摘要
A rotorcraft is provided and includes a fuselage. The fuselage includes drag generating portions, a main rotor assembly and an auxiliary propulsor having an expected propulsion efficiency. The auxiliary propulsor is disposed to ingest boundary layer flows and in wake regions associated with the drag generating portions and is provided with a corresponding increase in the expected propulsion efficiency thereof.
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