[mohammad]

Dear all,

I have submitteda a SCI paper for AOA determintaion, and I have used the results of Ansys CFX and Fluent for my validation ( with NREL Phase VI).

however, because of my CFD results are not very exact the reviewers have challenged my validation.

Now, I am looking for set of CFD results of NREL Phase VI at pitch angle of 5 degrees. I just need to use the pressure and velocity fields at two axial plane, one upstream and one downstream of the rotor blade.

I am hopfully looking for someone with high quality CFD data which can help me.

Definitely, I will acknowledge your contribution in my Paper and possibly add your name to the paper.

Regrads,
Mohammad