1999
DOI: 10.1007/bf02698746
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Turbulence suppression in subsonic jets by high-frequency acoustic excitation

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Cited by 8 publications
(2 citation statements)
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“…Conversely, a high-frequency acoustic input, at a frequency equal to Strouhal numbers from 1.5 to 5, causes vortex reduction in the jet mixing layer, resulting in attenuation of turbulent intermixing [18]. This behaviour was noted for a wide range of Reynolds number, from 10 2 to 10 6 .…”
Section: Introductionmentioning
confidence: 79%
“…Conversely, a high-frequency acoustic input, at a frequency equal to Strouhal numbers from 1.5 to 5, causes vortex reduction in the jet mixing layer, resulting in attenuation of turbulent intermixing [18]. This behaviour was noted for a wide range of Reynolds number, from 10 2 to 10 6 .…”
Section: Introductionmentioning
confidence: 79%
“…During the 1960s and 70s researchers in the Russian Central Aerodynamical Institute (TSAGI) proposed and demonstrated a method of controlling turbulence in submerged jets by the application of an acoustic wave [47,48]. This process was subsequently investigated in more detail by many other researchers [12][13][14][15][16][17][18]49,20,22,23,50,51]; the underlying mechanism can be considered as a manifestation of stochastic resonance [52].…”
Section: Control Of Noise-driven Pendulum Oscillations By a Harmonic mentioning
confidence: 99%