Learning Forum

[marco.peviani]

Hi everyone, I have a NACA 4410 profile which I have done an analysis at different AoA (parameterizing the AoA) to find the CL and the CD. Now I want another run but with a 2410 with flaps, matching the lift from the first analysis to get the flap angle to have the same LIft.

For example I have the 4410 at 5° of AoA and I find that the CL is 0.93, now with the same CL I want to find the Flap angle (of 2410).

How can I do ?
Thanks in advance

[Federico]

Hello Marco, 

you can set up a parametric simulation with the AoA as your parameter using Workbench. Set a range values expected for the AoA and run through these points until you approach the desired value. 

Working with Parameters and Design Points (ansys.com)

[marco.peviani]

Thanks for the reply, but my problem is related to the matching of the CL without going to trial and error also because for this project I have to do various simulations and it would take a lot. Would it be possible to have AoA as output variable matching the CL?