at a point in the test section of a supersonic windtunnel, the pressure and temperature are 0.54 x 10^5 N/m² a 238.1 K, Respicively. calculate the specific volume m^3 kg.
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Explanation:
From continuity equation,
....
From Bernoulli's equation,
.......
Solving eqns and we get
And
Rate of volume flow through the tube is
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