An airflow with velocity, temperature and pressure of 850 m/s, 25oC and 50 kPa absolute, respectively, is

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An airflow with velocity, temperature and pressure of 850 m/s, 25oC and 50 kPa absolute, respectively, is turned with an oblique shock emanating from the wall, which makes an abrupt 20o corner. For a weak shock, determine
(a) the downstream Mach number and
(b) the pressure (p).
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