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

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SUMMARY

The discussion focuses on calculating the final pressure and temperature of an adiabatic gas compression involving a gas with an initial volume of 4.3L, pressure of 1.2 atm, and temperature of 310K, compressed to a final volume of 0.76L. The specific heat ratio (gamma) is given as 1.4. The equations utilized include the relationships for adiabatic processes, specifically K=PV^gamma and the ratios for pressure and temperature changes. The final pressure and temperature can be determined using the formulas p2/p1 = (v1/v2)^gamma and T2/T1 = (v1/v2)^(gamma-1).

PREREQUISITES
  • Understanding of ideal gas laws and properties
  • Knowledge of adiabatic processes in thermodynamics
  • Familiarity with the specific heat ratio (gamma)
  • Ability to convert units to SI standards
NEXT STEPS
  • Calculate final pressure using the formula p2 = p1 * (v1/v2)^gamma
  • Determine final temperature using the formula T2 = T1 * (v1/v2)^(gamma-1)
  • Explore the implications of adiabatic processes in real-world applications
  • Review the derivation of the adiabatic process equations for deeper understanding
USEFUL FOR

Students studying thermodynamics, engineers working with gas compression systems, and anyone interested in the principles of adiabatic processes in physics.

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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