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Forum: Main CFD Forum

March 21, 2013, 08:04

Replies: 5

Angle of attack not changed

Views: 1,229

Posted By flotus1

Just like I thought... The straight...

Just like I thought...

The straight boundaries (symmetry I guess) at the top and bottom of your domain guide the flow towards an AoA of 0°. No matter what you specify at the inlet.

Forum: Main CFD Forum

March 21, 2013, 06:14

Replies: 5

Angle of attack not changed

Views: 1,229

Posted By flotus1

What does your computational domain look like?...

What does your computational domain look like? What other boundary conditions do you have besides the velocity inlet?
A sketch or even a screenshot might be helpful.

And which soler are you using?

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