The manuscript presents selected designs of DBD palm actuators used to control the flow of the boundary layer on the surface of the wing. Presented is the principle of DBD plasma actuator operation and the process of the formation of the "ion wind". The manuscript presents the results of tests carried out on the sash model with the profile SD 7003 with a DBD plasma actuator with two mesh electrodes, for which tests were carried out and tunnel images were recorded.
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