Research Article
Numerical Investigation of an Unsteady Blade Surface Blowing Method to Reduce Rotor Blade-Vortex Interaction Noise
Table 3
Comparisons of the thrust coefficient and SPL for the baseline case and the steady/unsteady blowing cases.
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Notes: The decrease in SPLs at the microphones compared with the baseline case is shown in bold. | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||