Research Article

Numerical Investigation of an Unsteady Blade Surface Blowing Method to Reduce Rotor Blade-Vortex Interaction Noise

Table 1

Coordinates of microphone locations (normalized by the rotor chord length) [20, 21, 33].

Microphone

1-63.430.00.0
2-31.7170.00.0
3-27.46715.8580.0
6-27.4670.015.858
7-23.78715.85813.733
8-27.4670.0-15.858
9-23.78715.858-13.733