Active control of high-speed and high-Reynolds-number jets using plasma actuators

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Machine Learning Control – Taming Nonlinear Dynamics and Turbulence (2016, background): “Examples include jets [235], mixing layers [206], wakes [263], car models [21], and the flow over a backward-facing step [271].”
High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “These waveforms seem to accomplish control based on thermal effects alone similar to arc filament-based plasma actuators (Samimy et al. 2007) and have demonstrated leading edge airfoil separation control authority up to Mach 0.85 (Roupassov et al. 2009).”
Active control of a Mach 0.9 jet for noise mitigation using plasma actuators (2007, background): “Figures 7b–7d show phase-averaged images of the jet forced with various azimuthal modes at StDF 0:33, which is around the jetpreferred Strouhal number [46,47].”
Coherent structure and sound production in the helical mode of a screeching axisymmetric jet (2014, background): “If these problems are adequately addressed, PIV can prove a robust tool for the study of supersonic jet flows, as evidenced by the work of Alkislar et al. (2003), Samimy et al. (2007) and others.”
Characterization of a High-Frequency Pulsed-Plasma Jet Actuator for Supersonic Flow Control (2010, methodology): “[14,15], who used a pulsed dc arc discharge to control the mixing of sub- and supersonic jets by perturbing the instability modes.”