Table 6 Flow conditions for NREL Phase VI rotor simulation
From: Review of vortex methods for rotor aerodynamics and wake dynamics
Parameter | Value |
|---|---|
Collective pitch angle, θc [deg.] | 4.815 |
Tip pitch angle, θtip [deg.] | 3 |
Rotating speed, Ω [rpm] | 72 |
Tip Mach number, Mtip [-] | 0.11 |
Wind speed, V∞ [m/s] | 5, 7, 10, 15, 20, 25 |
Yaw angle, β [deg.] | 0, 30 |