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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:等离子执行器,用于减少垂直起飞和着陆飞机的机翼,纳科斯和/或机身上的行李
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摘要
An aircraft includes a surface over which an airflow passes. A plasma actuator (1) 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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