Specific Internal Energy of a diatomic gas

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SUMMARY

The discussion focuses on calculating the specific internal energy of a diatomic gas, specifically hydrogen (H2), in the context of a J-shock propagating through neutral hydrogen gas. The internal energy per unit mass is defined by the equation U = ((γ) - 1)-1 * P/ρ, where γ for H2 is 7/5. The post-shock pressure P(1) is given as 5/6 * ρ(0) * v(0)2, and the density after the shock ρ(1) is 6 * ρ(0). The specific internal energy is derived as 3/2 * P(1)/ρ(1) = 9/32 * v(0)2.

PREREQUISITES
  • Understanding of thermodynamic principles, specifically internal energy calculations.
  • Familiarity with the properties of diatomic gases, particularly hydrogen (H2).
  • Knowledge of shock wave dynamics in gas physics.
  • Proficiency in using equations of state for gases, including the adiabatic constant (γ).
NEXT STEPS
  • Study the derivation of internal energy for diatomic gases in thermodynamics.
  • Learn about shock wave theory and its applications in astrophysics.
  • Explore the differences in degrees of freedom between monatomic and diatomic gases.
  • Investigate the implications of gas properties on shock wave behavior in various astrophysical contexts.
USEFUL FOR

This discussion is beneficial for physics students, astrophysicists, and researchers focusing on gas dynamics and thermodynamics, particularly those studying shock waves in astrophysical environments.

Carusun
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Hi all, I'm stuck on a question, and I'm hoping you guys can help... Anyway, here it is:

A J-shock in a Herbig-Haro object is propagating through neutral hydrogen gas at speed 100 kms-1. The gas has number density 107 m-3 and temperature 104 K.

(d) The internal energy per unit mass of a gas is,
U= ((gamma) - 1)^-1 * P/(rho). Use this to show that the specific internal energy of the post shock gas is, 3/2 * P(1)/(rho)(1)= 9/32 v(0)^2.

In this question;

(gamma) = the adiabatic constant, which, for H(2) is 7/5
P(1) = Post shock pressure = 5/6 (rho)(0) v(0)^2
(rho)(1) = 6(rho)(0)

which I believe is all that should be required, symbol-wise.

I can do this for a monatomic gas, but I'm having trouble getting the same result for a diatomic gas.
Have I made a mistake in assuming that the shock is propagating through a diatomic gas?
 
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Carusun said:
Hi all, I'm stuck on a question, and I'm hoping you guys can help... Anyway, here it is:

A J-shock in a Herbig-Haro object is propagating through neutral hydrogen gas at speed 100 kms-1. The gas has number density 107 m-3 and temperature 104 K.

(d) The internal energy per unit mass of a gas is,
U= ((gamma) - 1)^-1 * P/(rho). Use this to show that the specific internal energy of the post shock gas is, 3/2 * P(1)/(rho)(1)= 9/32 v(0)^2.

In this question;

(gamma) = the adiabatic constant, which, for H(2) is 7/5
P(1) = Post shock pressure = 5/6 (rho)(0) v(0)^2
(rho)(1) = 6(rho)(0)

which I believe is all that should be required, symbol-wise.

I can do this for a monatomic gas, but I'm having trouble getting the same result for a diatomic gas.
Have I made a mistake in assuming that the shock is propagating through a diatomic gas?
I am not sure I understand everything involved here, but I think the point may be that diatomic gas molecules have 5 degrees of freedom but that only three degrees of freedom (translation only) are involved in the propagation of a compression wave.

AM
 
That's great, thanks!

I had actually gone through this question the first time just assuming it was a monatomic gas, then kicking myself when I remembered H was diatomic.
Now, at least, I have a reason to do so, and am now kicking myself again...

Many thanks! :biggrin:
 

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