(Solved): 1. Supersonic Wedge: Consider the 2D wedge shown in the figure. The wedge has a nose angle of \( 1 ...

1. Supersonic Wedge: Consider the 2D wedge shown in the figure. The wedge has a nose angle of \( 10^{\circ} \) and is inclined \( 8^{\circ} \) relative to a flow at Mach 2.0, which has a stagnation pressure of 2 bar. (a) Draw the wedge with the appropriate waves at the nose. (b) Determine the Mach number, static pressure, and static temperature above the wedge. (c) Determine the Mach number, static pressure, static temperature, and stagnation pressure below the wedge. (d) At approximately what inclination angle would a detached bow shock form in front of the wedge?