What Are the Final Pressure and Temperature of an Adiabatic Gas Compression?

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Homework Help Overview

The problem involves an adiabatic gas compression where a mass of gas is initially at a volume of 4.3L, a pressure of 1.2 atm, and a temperature of 310K. The gas is compressed to a volume of 0.76L, and the goal is to determine the final pressure and temperature, assuming the gas behaves as an ideal gas with a specific heat ratio (gamma) of 1.4.

Discussion Character

  • Exploratory, Problem interpretation, Assumption checking

Approaches and Questions Raised

  • Participants discuss the initial setup of the problem, with one participant expressing uncertainty about how to begin. Others suggest organizing the known and unknown variables clearly. There is mention of using the relationships for adiabatic processes, including the equations for pressure and temperature ratios based on volume changes.

Discussion Status

The discussion is ongoing, with participants working through the initial steps of the problem. Some guidance has been provided regarding the organization of information and the application of relevant equations for adiabatic processes, but no consensus or complete solutions have emerged yet.

Contextual Notes

Participants are operating under the assumption that the gas behaves ideally and that the process is adiabatic, with the heat transfer (Q) being zero. There is a focus on ensuring all variables are clearly defined and converted to appropriate units.

terry2112
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Homework Statement



A mass of gas occupies a volume of 4.3L at a pressure of 1.2 atm and a temperature of 310K. It is compressed adiabatically to a volume of 0.76L.Determine (a)the final pressure and (b) the final temperature,assuming the gas to be an ideal gas for which gamma = 1.4.

Homework Equations



gamma = Cp/Cv
w = (1/gamma-1)(p1v1-p2v2)
w=-Cv(deltaT)



The Attempt at a Solution


I'm not really sure where to start but haf wote out everything and have converted all to basic SI units,explanation of solution of this question would be much appreciated.
 
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First start out by writing all of the given information in terms of those variables.
 
i did!
 
No you did not. As far as I can see, you didn't show any work.. you just stated the problem and showed some equations.

Let v_{i}=4.3L,p_{i}=1.2atm,T_{i}=310K etc. Now write the remaining given information in this format so that you can clearly see what are known and unknown variables(i.e. v_{f},T_{f})
 
Last edited:
V1 = 0.0043m^3,P1=121560Pa,T1=310K then goes through an adiabatic compression

to

V2=0.00076m^3,P2=?,T2=?

given gamma = 1.4
 
Since this is a adiabatic process, Q=0 so for some constant K, K=PV^{\gamma}
then, \frac{p_{2}}{p_{1}}=\left(\frac{v_{1}}{v_{2}}\right)^\gamma where subscript 2 means final state, subscript 1 means initial state.

and \frac{T_{2}}{T_{1}}=\left(\frac{v_{1}}{v_{2}}\right)^{\gamma-1}
 
Last edited:

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