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Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft
Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft
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机译:等离子致动器,用于减少垂直起降飞机的机翼,机舱和/或机身上的阻力
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摘要
An aircraft includes a surface over which an airflow passes. A plasma actuator is configured to generate a plasma above the surface, the plasma coupling a directed momentum into the air surrounding the surface to reduce separation of the airflow from the surface. A method of reducing separation of an airflow from a surface of an aircraft includes generating a plasma in air surrounding the surface at a position where the airflow would separate from the surface in the absence of the plasma.
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