Assume that, at a point on the wing of the Concorde supersonic transport, the air temperature is -10°C and the pressure is I. 7 X 104 N/m2. Calculate the density at this point. 2.8 At a point in the test section of a supersonic wind , the air pressure and temperature are 0.5 x 105 N/m2 and 240 K, respectively. Calculate the specific volume.
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