Request for NREL Phase VI data for method validation
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.
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