Consider a stationary, thin, flat plate with area of 2 m2 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 × 105 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 × 105 N/m2, and is constant over the face. Calculate the aerodynamic force in pounds on the plate. Note: The effect of shear stress is negligible for this case.
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