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Mathematics, 08.09.2021 14:00 braydenmcd02

At a point in the test section of a supersonic wind tunnel, the air pressure and temperature are 0.45 x 10^5 N/m 2 and 233.5 K, respectively. Calculate the specific volume in m^3/kg.​

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At a point in the test section of a supersonic wind tunnel, the air pressure and temperature are 0.4...
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