suppose air is flowing throught the nozzle(adsbygoogle = window.adsbygoogle || []).push({});

with the inlet conditions

static pressure = .2 MPa

static temperature = 350 K

velocty of air at the inlet = 150 m/s

speed of sound for ideal gas is given by c = sqrt (k * R * T)

suppose if i want to calculate the speed of sound at the inlet do i have to consider the static temperature or the stagnation temperature?

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# Nozzle flow

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