Consider a stationary, thin, fiat plate with area of 2m2 for each face oriented perpendicular to a flow. The pressure exerted on the front face of the plate (facing into the flow) is 1.0715 x I OS N/m2, and is constant over the face. The pressure exerted on the back face of the plate (facing away from the flow) is 1.01 x 10SN/m2, and is constant over the face. Calculate the aerodynamic force in pounds on the plate.

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