Abstract: Abstract. This paper describes the experimental characterization of a no-moving-parts, plasma-switched, two-stage, fluidic vortex valve capable of throttling Mach-0.85 air-flow at 5 bar. In the first stage, a sparkjet is ...

Abstract: Fluidic oscillators show promise for use in aerodynamic flow control applications, with many studies reporting oscillation frequencies in the 1–10 kHz range. Spyropoulos, “A Sonic Oscillator,” introduced a “sonic” oscillator ...