[danuco]

Hi all,
I am currently doing my final degree project to finish my studies in aeroespace engineering. I have to study several wings in ANSYS-FLUENT aerodynamically and to verify the obtained results with experimental results.
I am having a lot of problems because in my simulations, the stall appears before that it has to be. For example, the stall appears to 12º angle of attack in the experimental data and it appears to 8º angle of attack in my simulation.
any advice about what can be happening??
It is urgent, I have to submit my project in less than a month!

Sorry for my English