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Question
The lift on an airfoil depends on the aircraft speed , the speed of sound , the fluid density, the airfoil chord length , the airfoil thickness , and the angle of attack . Find an expression for .
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In this exercise, we are asked to derive an expression for the lift produced by an airfoil. The given variable parameters are listed below:
- - lift force
- - velocity
- - speed of sound
- - fluid density
- - airfoil chord length
- - airfoil thickness
- - angle of attack
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