Help with mass flow rate of turbine?

AI Thread Summary
The discussion focuses on calculating the mass flow rate of air through a turbine that expands air from 1300 kPa and 500°C to 100 kPa and 127°C. The user initially calculated a mass flow rate of 58.6 kg/s using the specific volume derived from the ideal gas law, but the expected answer is 46.9 kg/s. Participants suggest considering the conditions at the exhaust end, as the air expands after passing through the turbine, which may affect the specific volume and flow rate calculations. The user seeks clarification on their calculations and where they may have gone wrong. Accurate assessment of the exhaust conditions is crucial for determining the correct mass flow rate.
nate9519
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Homework Statement


An turbine expands air at 1300 kPa and 500oC to 100 kPa and 127oC. Air enters the turbine through a 0.2-m2 opening with an average velocity of 50 m/s, and exhausts through a 1-m2 opening. Determine (a) the mass flow rate of air through the turbine

Homework Equations


PV=RT
m dot = (1/v)(V)(A)

The Attempt at a Solution


[/B]
I use PV=RT to get specific volume. (.287 * 773)/1300 = .17065 m^3/kg
I then plug it into the formula for mass flow rate which is (1/.17065)(50)(.2) = 58.6 kg/s
the problem is that the answer is suppose to be 46.9 kg/s but I can see anything I've done wrong. can someone help??
 
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nate9519 said:

Homework Statement


An turbine expands air at 1300 kPa and 500oC to 100 kPa and 127oC. Air enters the turbine through a 0.2-m2 opening with an average velocity of 50 m/s, and exhausts through a 1-m2 opening. Determine (a) the mass flow rate of air through the turbine

Homework Equations


PV=RT
m dot = (1/v)(V)(A)

The Attempt at a Solution


[/B]
I use PV=RT to get specific volume. (.287 * 773)/1300 = .17065 m^3/kg
I then plug it into the formula for mass flow rate which is (1/.17065)(50)(.2) = 58.6 kg/s
the problem is that the answer is suppose to be 46.9 kg/s but I can see anything I've done wrong. can someone help??
Did you check what happens at the exhaust end? The air has expanded after going thru the turbine.
 
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