Thermodynamics temperature question

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SUMMARY

The discussion centers on calculating thermodynamic properties of an ideal monatomic gas in an engine cycle involving two isobaric and two constant-volume processes. The user calculates the heat added to the gas as 2380.064 J using the equation Q=nCp(delta T) with Cp determined to be 20.81 J/(mol·K). For the heat removed, the user computes -1781.336 J, indicating a misunderstanding of the sign convention. The total work done by the engine is derived from the first law of thermodynamics, concluding that the work done equals the net heat transfer in a complete cycle, which is zero for a closed system.

PREREQUISITES
  • Understanding of the first law of thermodynamics
  • Familiarity with ideal gas laws and properties
  • Knowledge of molar specific heat capacities (Cp and Cv)
  • Ability to interpret pressure-volume graphs
NEXT STEPS
  • Study the derivation and application of the first law of thermodynamics in cyclic processes
  • Learn about the differences between isobaric and isochoric processes in thermodynamics
  • Explore the concept of internal energy change (ΔU) in thermodynamic cycles
  • Investigate the implications of heat transfer sign conventions in thermodynamic calculations
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Students studying thermodynamics, mechanical engineers, and anyone involved in the analysis of heat engines and energy transfer processes.

Meowzers
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Homework Statement



The pressure-volume graph shows an engine cycle with four processes: two isobaric, and two constant-volume. The engine uses 0.800 mol of an ideal monatomic gas as its working substance. For one engine cycle, calculate (a) the heat added to the gas, (b) the heat removed from the gas (stated as a positive number), and (c) the net work done by the engine.

http://www.slowbie.com/pressure-volume.gif


Homework Equations



Q=nCp(delta T), Cp=Cv+R
Q=heat, n=moles, Cp=molar specific heat, constant pressure, Cv=molar specific heat, constant volume, R=gas constant, T=temperature

The Attempt at a Solution



For part A, I used the molar specific heat-constant pressure equation to try to solve for the heat added to the gas.

Q=nCp(delta T), Cp=Cv+R
Cp=12.5+8.31
Cp=20.81
Then, I read the temperature difference from A to B.
Q=(.800)(20.81)(568K-425K)
Q=2380.064 J (Where am I making the error?)

For part B, is the amount of heat removed from the gas the same thing as part A but with temperature readings between C
and D?
With that, the equations would look like Q=(0.800)(20.81)(318-425)
Q=-1781.336 J

Thanks in advance!
 
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Meowzers said:

The Attempt at a Solution



For part A, I used the molar specific heat-constant pressure equation to try to solve for the heat added to the gas.

Q=nCp(delta T), Cp=Cv+R
Cp=12.5+8.31
Cp=20.81
Then, I read the temperature difference from A to B.
Q=(.800)(20.81)(568K-425K)
Q=2380.064 J (Where am I making the error?)

For part B, is the amount of heat removed from the gas the same thing as part A but with temperature readings between C
and D?
With that, the equations would look like Q=(0.800)(20.81)(318-425)
Q=-1781.336 J

Thanks in advance!

Heat is being added from D to A and from A to B. Heat is being removed from B to C and C to D. From D to A, Q+ = nC_v\Delta T and from A to B, Q+ = nC_p\Delta T. The total is Qh. Figure that out to get the total heat added. I think you can similarly determine the heat removed (Qc).

To find the work, use the first law: \Delta Q = Qh - Qc = \Delta U + W. What is \Delta U in a full cycle?

AM
 
Delta U is 0 in a full cycle since it returns to its initial state. So the work done is equal to the change in heat.

Thanks so much for your help! :)
 

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