Deriving Efficiency of a Diesel Engine Formula

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SUMMARY

The discussion focuses on deriving the efficiency of a Diesel engine using the Diesel cycle, which includes adiabatic compression, isobaric expansion, adiabatic expansion, and isochoric cooling. Key equations include the efficiency formula e = 1 + QC/QH, the relationship γ (gamma) = cp/cv, and the work done during adiabatic processes. Participants emphasize the importance of calculating temperatures at various points using the ideal gas law and verifying energy conservation through the first law of thermodynamics. The discussion concludes that constructing a detailed table of states and energy changes is essential for accurately determining efficiency.

PREREQUISITES
  • Understanding of the Diesel cycle and its processes
  • Familiarity with thermodynamic principles, particularly the first law of thermodynamics
  • Knowledge of the ideal gas law and its applications
  • Proficiency in using equations related to adiabatic processes and efficiency calculations
NEXT STEPS
  • Study the derivation of the Diesel cycle efficiency formula in detail
  • Learn about the ideal gas law and its implications in thermodynamics
  • Explore the first law of thermodynamics and its application in energy systems
  • Investigate the significance of adiabatic processes in engine efficiency
USEFUL FOR

Mechanical engineers, thermodynamics students, and professionals involved in engine design and efficiency optimization will benefit from this discussion.

CallMeShady
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Homework Statement


The Diesel cycle is an idealized representation of the process that occurs in a Diesel combustion engine, as shown in the graph below. Starting at point a, the Diesel cycle consists of an adiabatic compression, an isobaric expansion, and adiabatic expansion and an isochoric cooling. Find the efficiency in terms of only the compression ratio, r = Va/Vb, γ (gamma), THot and TCold. Show all work!

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Homework Equations


e = 1 + QC/QH
γ (gamma) = cp/cv
dQ = dU + dW

For adiabatic expansion, TVγ-1 = constant, if the number of moles is constant PVγ = C where C is a constant.

Work for adiabatic process = W = (C/1-γ)(V21-γ - V11-γ)


The Attempt at a Solution


I am having problems starting up with this problem and writing it in terms of temperature. I know that temperature at Ta is equal to Tc which in turn is equal to TH from what I know. But, how do I begin after setting up the problem like this? I am sorry for not providing a "thorough" attempt at a solution; I am having problems at the initial steps which is why I can't do much. Any light on this problem would be appreciated.
 
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CallMeShady said:
I know that temperature at Ta is equal to Tc
How can that be? Surely Ta=Tcold.
 
An easy way to organize your thoughts would be to construct a Table as shown below and fill in the blanks. Start by figuring out the temperatures at each point using the ideal gas law. For example, ##T_a=\dfrac{p_a~rV}{nR}##. Then use ##T_a(rV)^{\gamma -1}=T_b(V)^{\gamma -1}## to find ##T_b## and so on for the remaining temperatures. Once you have all the temperatures, you can find the changes in internal energy using ##\Delta U=nC_V\Delta T##. Then you can fill in the rest of the entries.

The first law takes the form ##\Delta U = Q-W## where ##W## is the work done by the gas. To keep myself honest, I would calculate the work and the heat entering the gas independently and verify that the first law holds across each row. I would also verify that the sums of the entries in each column obey ##~~0=Q_{\text{Total}}-W_{\text{Total}}##.

Once you have completed the table, it's an easy matter to find the efficiency and answer any other question related to the cycle.

ΔU​
Q​
W​
a → b
b → c
c → d
d → a
Total
 

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