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Question
Select an appropriate set of variables that influence the drag force on an airfoil and write the final form in terms of dimensionless parameters.
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In this exercise, we are asked to derive an expression for the drag force acting on an airfoil. The variable parameters that will influence the drag force are listed below:
- - fluid density
- - velocity
- - fluid viscosity
- - length of chord
- - maximum thickness
- - nose radius
- - width
- - angle of attack
- - trailing edge angle
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