What can you say about the lift force on the airfoil

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Reference no: EM13718798

1) At what position along the chord does the minimum pressure occur?

2) What is special about the point where C_p is a maximum?

3) Based upon the pressure coefficient plot, what can you say about the lift force on the airfoil?

4) What would be one major and obviously visible change to the velocity and pressure coefficient curves if you were to redo this problem with the airfoil at a non-zero angle of attack?

Reference no: EM13718798

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