Air flows supersonically toward the double wedge system in the figure The (x, y) coordinates of the tips are given Both wedges have 15 deg deflection angles The shock wave of the forward wedge strikes the tip of the aft wedge What is the free stream Mach number (i m 1 m Shocks (0, 0)...

However tricky the shock reflection m ...

Air flows supersonically toward the double-wedge system in the figure. The (x, y) coordinates of the tips

Question:

Air flows supersonically toward the double-wedge system in the figure. The (x, y) coordinates of the tips are given. Both wedges have 15° deflection angles. The shock wave of the forward wedge strikes the tip of the aft wedge. What is the free stream Mach number?