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Airfoil Analysis (Lift coefficiet)

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Old   December 23, 2007, 01:07
Default Airfoil Analysis (Lift coefficiet)
  #1
Alex
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Hi, currently I am using CFD to analysis on an airfoil. And my question is about finding the spot for drag coefficient.

Here is what I did, I selected the forces under the report drop down menu. In there, I obtained drag coefficient by using the vector component. Once I have specified it, the forces as well as some other coefficients will be listed on the window. so here is my question; could someone please tell me which column and row indicates the drag coefficient.

Thank you so much.
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Old   December 23, 2007, 01:08
Default Re: Airfoil Analysis (Lift coefficiet)
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Alex
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sorry, the title should be written as drag coefficient
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Old   December 26, 2007, 10:19
Default Re: Airfoil Analysis (Lift coefficiet)
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ag
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You might get more response if you provide enough information to actually answer your question. For example, which tool are you using?
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