(Solved): Required Information The scramjet engine in the first Image is supersonic throughout. The second I ...

Required Information The scramjet engine in the first Image is supersonic throughout. The second Image shows its sketch. Test the following design. The flow enters at \( M a=7 \) and air propertles for \( 10,000 \mathrm{~m} \) altitude. Inlet area is \( 1.2 \mathrm{~m}^{2} \), the minimum area is \( 0.15 \mathrm{~m}^{2} \). and the exit area is \( 0.85 \mathrm{~m}^{2} \). Determine the exlt Mach number, the exit velocity, and the exit pressure. The Mach number at the exit is The exit velocity is \( \mathrm{m} / \mathrm{s} \). The exit pressure is Pa.