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Consider a circular cylinder in an ideal flow, with its axis perpendicular to the fiow. Let p be the angle measured between radi drawn to the leading edge (the stagnation point) and to any abitrary point on the cylinder. The pressure coefficient distribution along the cylindrical surface is given by Cp 1-4sin (m-p). Calculate the drag coefficient for the cylinder, based on projected frontal area of the cylinder. (Round the final answer to three decimal places.) The drag coefricient for the cylinder is

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