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We need to set the parameters so drag across the airfoil (keep in mind, which is at an angle) will be displayed. In the Force Reports window change the Direction Vector such that X > .9945 and Y > .1045. 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 > -.1045 and Y > .9945. Again, press Print.

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