Airfoil Analysis (Lift coefficiet)
 

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.

Re: Airfoil Analysis (Lift coefficiet)
 

sorry, the title should be written as drag coefficient

Re: Airfoil Analysis (Lift coefficiet)
 

You might get more response if you provide enough information to actually answer your question. For example, which tool are you using?