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January 26, 2018, 02:46 |
Airfoil AoA steped increment
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#1 |
New Member
Join Date: Jan 2018
Posts: 4
Rep Power: 8 |
Dear All,
I am fairly new to Fluent and UDF, therefore i would like to request some help on the following matter. I intend to perform a simulation on a 2D airfoil. The airfoil will remain stationary until the solution approaches convergence. After that it should update the angle of attack by 1 degree every, let's say t = c/U, where c is the chord length and U the freestream velocity. The range of angles of attack would be from -180 to 180 degrees. However it is ok for each simulation to go from 0 until the extreme angle. I have tried to create a '' for loop'' however it seems that something like that doesn't work. Also regarding the rotation function: can i simply use axis rotation equations? x'=x\cos \theta +y\sin \theta y'=-x\sin \theta +y\cos \theta .} These also didn't seem to work, but i'm guessing it's more of a coding issue. Thank you in advance for all the help on the matter. Best regards |
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