Abstract
Current paper is devoted to study new plasma actuator type—plasma synthetic jet actuator, based on the magnetohydrodynamic flow acceleration. Gas is accelerated inside the planar channel by the pulsed arc with current ∼ 300 A, moving in the external magnetic field of 1.2 T. The channel is opened at both sides. The asymmetric jet, formed at one of the channel ends is studied by means of shadow imaging and particle image velocimetry. The total thrust of the system is estimated by integrating velocity field and by direct measurement of the recoil force.
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