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Engineering, 14.09.2019 04:30 jaylanmahone223

At a point on the airfoil in subsonic wind tunnel, the air pressure and temperature are 0.4 atm and 5°c, respectively. assuming the flow is isentropic. if the ambient air pressure is 1 atm, calculate the ambient air temperature and density.

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At a point on the airfoil in subsonic wind tunnel, the air pressure and temperature are 0.4 atm and...
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