I will provide 2D airfoil mesh file, using ansys fluent run the 2D airfoil at different AOA i.e. 0, 2,4,6,8,10,12,14,16 upto stall.
Two set of Cl vs. AOA curve for 40 Deg and 50 Deg.
I can do this task and will match with the real case. Accuracy guaranteed.
I am an assistant professor and have worked on many airfoils in Ansys fluent. Not an easy task if you really need a good result.
Let me know if I can do this task.
Thank you
I am Raghul from Tamilnadu and i completed Aeronautical engineering, and i completed cfd course in Niharika institute,Bangalore.
Relevant Skills and Experience
I did ICEM CFD Course in vangalore