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Determine pressure, temperature and Mach number downstream of the shock. Also calculate strength of shock.
written 6.3 years ago by | modified 2.1 years ago by |
A normal shock wave occurs in a duct in which air is flowing at a Mach number of 1.5.The static pressure and temperature upstream of the shock wave is 1.5 bar and $270^0C$.Determine pressure, temperature and Mach number downstream of the shock. Also calculate strength of shock.
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