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How to set AOA for an Airfoil in CFX?

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Old   September 18, 2013, 02:19
Unhappy How to set AOA for an Airfoil in CFX?
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I am using CFX 13, and I want to do analysis of a half delta wing which is at an AOA of 5 deg. At inlet I am giving Total pressure values, and in the flow direction I am giving the unit vector components along X and Z directions. My question is are the settings correct and Does the direction components in flow direction tab take unit vector values or Actual velocity components. Or is der any other method for doing so.

Thank you

Last edited by fender26; September 19, 2013 at 04:22.
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angle of attack, aoa, wing

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