Dear @Jason.Jonkman ,
Thank you very much for your answer. I have another follow-up question about computing the induction factors (axial and tangential).
I am coupling FAST with a CFD solver so I disabled the wake model (set to None instead of SWIRL/WAKE) which means that Aerodynv14 will report a value of 0 for both AxInd and TanInd.
I have the 3 velocity components (VX/VY/VZ) from the `.wind` file from Aerodyn14 when using the option PRINT WIND. (from this post)
My approach to compute the axial induction at each blade node:
- Compute the wind speed normal to the rotor plane,
U, and computeAxInd = 1 - U/Uinf. - To compute the
TanInd:- Compute the relative speed from the Dynamic pressure output:
W = sqrt(2*DynPres/AirDens). - Compute the inflow angle:
PHI = Alpha + Pitch - Compute the Tangential relative speed:
VT = W * COS(PHI). - Compute
TanIndfrom the relation:VT = r*Omega (1 + tanInd).
- Compute the relative speed from the Dynamic pressure output:
I appreciate your feedback/corrections.
Best regards,
Y.Thiziri
