Velocity exiting Heat Exchanger

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SUMMARY

The discussion centers on calculating the exit velocity of cold air from a heat exchanger using conservation of mass principles. The inlet conditions are 400 K, 1.0 MPa pressure, and a velocity of 3 m/s, while the exit pressure is 300 kPa with the same area of 0.025 m². The user initially calculated the mass flow rate using the density of air at normal atmospheric pressure instead of 1.0 MPa, leading to an incorrect exit velocity of 4.2189 m/s. The correct approach requires using the density of air at the specified inlet pressure for accurate results.

PREREQUISITES
  • Understanding of conservation of mass principles in fluid dynamics
  • Knowledge of ideal gas laws and properties of gases
  • Familiarity with thermodynamic properties of air at varying pressures
  • Ability to perform calculations involving mass flow rates and velocities
NEXT STEPS
  • Learn how to calculate the density of air at different pressures using the ideal gas law
  • Study the application of Bernoulli's equation in fluid flow analysis
  • Explore the effects of temperature and pressure on gas properties
  • Investigate the use of computational fluid dynamics (CFD) for heat exchanger analysis
USEFUL FOR

Students in thermodynamics, mechanical engineers, and professionals involved in heat exchanger design and analysis will benefit from this discussion.

jdawg
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Homework Statement


Cold air enters a heat exchanger at 400 [K] and exits it at 1200 [K]. At the 0.025 [m2] inlet, the pressure is measured to be 1.0 [MPa] and the velocity is measured to be 3 [m/s]. The area of the exit is also 0.025 [m2] and the pressure here is measured to be 300 [kPa]. What is the velocity exiting the heat exchanger? Use conservation of mass principles.

Homework Equations

The Attempt at a Solution


So the mass flow rate going in equals the mass flow rate going out. m1=m2

I used this formula to calculate the mass flow rate:
m1=ρairA1v1
m=(1.225)(0.025)(3)=0.091875 kg/s

Since its an ideal gas, I substituted the mass flow rate equation into the ideal gas equation:

P2 =(m/(A2v2))RT2

I found R to be 0.287 kJ/(kg*K)

v2=[(0.091874 kg/s)(0.287 kJ/(kg*K))(1200K)]/[(300000 N/m2)(0.025 m2)]

I got v2= 4.2189 m/s as my velocity which is incorrect since my answer can only be 20,30,27,or 3.3333 m/s.

I can't see what I did wrong.
 

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jdawg said:

Homework Statement


Cold air enters a heat exchanger at 400 [K] and exits it at 1200 [K]. At the 0.025 [m2] inlet, the pressure is measured to be 1.0 [MPa] and the velocity is measured to be 3 [m/s]. The area of the exit is also 0.025 [m2] and the pressure here is measured to be 300 [kPa]. What is the velocity exiting the heat exchanger? Use conservation of mass principles.

Homework Equations

The Attempt at a Solution


So the mass flow rate going in equals the mass flow rate going out. m1=m2

I used this formula to calculate the mass flow rate:
m1=ρairA1v1
m=(1.225)(0.025)(3)=0.091875 kg/s

In your calculation of the inlet mass flow, you have apparently used the density of air at normal atmospheric pressure rather than a pressure of 1.0 MPa.
 
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Likes   Reactions: jdawg
Perfect, thanks!
 

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