Question: c++ coding When a Pitot tube is immersed in a supersonic stream, a curved shock wave is formed ahead of the Pitor tube mouth Since

c++ coding
When a Pitot tube is immersed in a supersonic stream, a curved shock wave is formed ahead of the Pitor tube mouth Since the radius of the curva vure of the shock is large, the shock may be assumed to be a normal shock. After the normal shock, the fluid stream decelerates isentropically to the total pressure Pool the entrance to the Pitot tube A pitot tube travelling in a supersonic wind-Tunnel gives values of 16 kPa and 70 Pa for the static pressure upstream of the shock and the pressure at the mouth of the tube respectively. Estimate the Mach number of the tunnel. If the stagnation temper- ature is 300C, calculate the static temperature and the total (stagnation) pressure upstream and downstream of the sube Curved shock front Pilot tube PX MX PoyStep by Step Solution
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