Subsonic Jet Noise from Nonaxisymmetric and Tabbed Nozzles

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Large-scale structure evolution and sound emission in high-speed jets: real-time visualization with simultaneous acoustic measurements (2005, methodology): “The convective velocity of the large-scale structures, uc, was measured as 266 m s−1 by Thurow et al. (2003). The theoretical convective Mach number, Mc, for the jet was 0.”
Active control of a Mach 0.9 jet for noise mitigation using plasma actuators (2007, background): “Tabs generate pairs of streamwise vortices in the jet [23] and provide a reduction in the far-field overall sound pressure level (OASPL) [29–31].”
The sources of jet noise: experimental evidence (2007, methodology): “Such a demonstration was carried out by Tam & Zaman (2000).”