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METHOD OF CONTROLLING FLIGHT OF AIR MOVABLE PLATFORM AND PLASMA ACTUATOR FOR AFFECTING BOUNDARY LAYER FLOW ON SURFACE OF OBJECT
METHOD OF CONTROLLING FLIGHT OF AIR MOVABLE PLATFORM AND PLASMA ACTUATOR FOR AFFECTING BOUNDARY LAYER FLOW ON SURFACE OF OBJECT
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机译:影响物体表面边界层流动的可移动平台和等离子作动器的飞行控制方法
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摘要
PPROBLEM TO BE SOLVED: To provide a system and a method for a plasma actuator for controlling the direction and/or the attitude thereof adapted to the use of an air movable platform such as an aircraft. PSOLUTION: The system comprises at least one plasma actuator having first and second electrodes mounted on the surface of the aircraft. The first and second electrodes are parallel to a boundary layer flow path on the surface. A third electrode is mounted between the first and second electrodes while being laterally displaced from the first and second electrodes. When a high AC voltage signal is applied between the first and third electrodes, a fluid flow is induced between the electrodes excited to assist the delay of the peeling of a boundary layer. When the AC voltage signal is applied between the second and third electrodes, an induced fluid flow is caused to form a reverse effect for peeling the boundary layer from the surface. A plurality of actuators can be selectively disposed at various positions of the aircraft, and selectively so excited as to provide a directional control and/or an attitude control. PCOPYRIGHT: (C)2009,JPO&INPIT
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