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Next, double click on Forces and click Print in the Force Reports menu. You should then obtain the following output in the command pane.
!ForceRep_Full.png|width=350!\
As one can see from the data above, the plate experiences a drag of approximately 0.008377 Newtons. Furthermore, the data states that the drag coefficient is approximately 0.01675. The drag coefficient is defined by the following equation.
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