Question: Problem 1 : Consider the figure below. The velocity profiles at the upstream end ( surface 1 ) and at the downstream end ( surface

Problem 1:
Consider the figure below. The velocity profiles at the upstream end (surface 1) and at the downstream end (surface 2) of the rectangular control volume have been measured. The flow is incompressible, twodimensional, and steady. The vertical dimension H is 0.025c. The pressure is P over the entire surface of the control volume. What is the drag coefficient for the airfoil?
Problem 1 : Consider the figure below. The

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