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To find the Coefficients of Lift and Drag, click Results > Resports to bring up the Reports Window. In the Reports Window, select Forces and click Set Up.... This will bring up the Force Reports menu

Under the default parameters shown above, drag across the airfoil will be displayed. Click Print to print the drag coefficient to the command window. To print the lift coefficient, in the Force Reports window change the Direction Vector such that X > 1 and Y > 1

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