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Use UDF to change the attack angle of flow over 3D wing

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Old   May 3, 2013, 03:07
Default Use UDF to change the attack angle of flow over 3D wing
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nguyen van trieu
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Hi everyone,

I am a new with ANSYS FLUENT. I am doing simulation with the flow over 3Dwing (NACA0012). I want to change the attack angle by using UDF. Could anyone teach me how to use the UDF for this case?
thanks you!

Xavier
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Old   May 3, 2013, 03:34
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Are you studying the pitching motion of the wing or you simply want to study the flow at several angles of attack?
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Old   May 3, 2013, 05:55
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Hi,
if it just the angle of attack which you want to change, you can do it directly by changing the x and y component of velocity in the velocity inlent boundary condition.
If you want to learn to do it in udf you have to do the same by writing this component inside a small c program..
this is an example of how the inlet velocity is changed according to the y distance to get a profile

http://combust.hit.edu.cn:8080/fluen...udf/node61.htm
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Old   May 3, 2013, 14:42
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Sijal Ahmed Memon (turboenginner@gmail.com)
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You can also do it in workbench
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