International Journal of Aerospace Engineering / 2016 / Article / Fig 9

Research Article

Effects of Freestream Turbulence on Cavity Tone and Sound Source

Figure 9

Predicted coherence of velocity, , at fundamental frequency in spanwise direction ( = 0.5 and = 0) for cavity flow ( = 0.5) with original and wider computational domains of = 1.0 and 2.0.