Air flowing at M = 2.5 encounters an oblique shock, what is the Mach number downstream and the deflection in flow direct
Posted: Mon May 02, 2022 3:18 pm
Air flowing at M = 2.5 encounters an oblique shock, what is the
Mach number downstream and the deflection in flow direction if the
shock is at 40° to the flow?
Mach number downstream and the deflection in flow direction if the
shock is at 40° to the flow?