Engineering, 24.03.2021 19:50 LoneWolves
A circular cylinder of 1 m radius is moving in the direction of the negative x-axis with a velocity of 5 m/s. The circulation around the cylinder is 10p m2 /s. Plot the polar pressure coefficient distribution about cylinder as if it were an airfoil (negative cp up, curve for upper and lower surface) and determine the 2D lift coefficient.
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A circular cylinder of 1 m radius is moving in the direction of the negative x-axis with a velocity...
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