Engineering
Engineering, 14.09.2019 00:30, milkshakegrande101

An airfoil is flying at 300 m/s at sea level. at a point on the airfoil surface, the pressure is 0.87 atm. assuming isentropic flow, calculate the velocity at that point.

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An airfoil is flying at 300 m/s at sea level. at a point on the airfoil surface, the pressure is 0.8...

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