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

AI Thread Summary
The discussion focuses on determining the final pressure and temperature of a gas undergoing adiabatic compression from an initial volume of 4.3L, pressure of 1.2 atm, and temperature of 310K to a final volume of 0.76L, using the ideal gas assumption with gamma equal to 1.4. Key equations for adiabatic processes are presented, including relationships for pressure and temperature based on volume changes. Participants emphasize the need to convert units to SI and clearly define known and unknown variables. The adiabatic condition implies that heat transfer is zero, leading to the use of specific formulas for pressure and temperature changes. The discussion highlights the importance of systematic problem-solving in thermodynamics.
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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})
 
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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}
 
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