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Consider the flow of air through the venturi in an automobile carburetor. The volume flowrate through the venturi is .009 m^3/s. At the inlet to the venturi the cross sectional area is 5.0x10^-4 m^2, the pressure is 100 kPa, and the temperature is 35 degrees C. At the throat of the venturi the flow area is reduced to 1.7x10^-4 m^2. Assuming that the air can be considered incompressible: What is the air velocity at the inlet and throat of the venturi? What is the gage pressure at the throat of the venturi?

Consider the flow of air through the venturi in an automobile carburetor. The volume flowrate through the venturi is .009 m^3/s. At the inlet to the venturi the cross sectional area is 5.0x10^-4 m^2, the pressure is 100 kPa, and the temperature is 35 degrees C. At the throat of the venturi the flow area is reduced to 1.7x10^-4 m^2. Assuming that the air can be considered incompressible: What is the air velocity at the inlet and throat of the venturi? What is the gage pressure at the throat of the venturi?