Consider a (15^{circ}) half-angle wedge at zero angle of attack in a Mach 3 flow of air.
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Consider a \(15^{\circ}\) half-angle wedge at zero angle of attack in a Mach 3 flow of air. Calculate the drag coefficient. Assume that the pressure exerted over the base of the wedge, the base pressure, is equal to the free-stream pressure.
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