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Calculate the pressure, velocity and temperature just downstream of the shock wave. [ Take ratio of specific heat k = 1.4 and gas constant R = 287 J/kgk ]
written 6.3 years ago by
kedaryeole
• 150
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modified 2.1 years ago
by
sagarkolekar
★ 11k
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The pressure, velocity and temperature just upstream of a normal shock wave in air are 100 KPa (abs), 600 m/s and -200C respectively. Calculate the pressure, velocity and temperature just downstream of the shock wave. [ Take ratio of specific heat k = 1.4 and gas constant R = 287 J/kgk ]
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