How to Derive the Third Equation for Different Values of Gamma?

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SUMMARY

The discussion focuses on deriving the third equation for different values of gamma (\(\gamma\)) in the context of strong shock waves in gases, specifically with \(\gamma = 7/5\). The participant successfully calculates the density ratio \(\rho_2/\rho_1 = 6\) using the equations of state but seeks clarification on adapting the third equation, originally presented as \(\frac{1}{2} u + \frac{5}{2} \frac{P}{\rho} = constant\), which is valid only for \(\gamma = \frac{5}{3}\). The solution involves understanding the Rankine-Hugoniot conditions and how to modify the equation for different \(\gamma\) values.

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  • Knowledge of the equations of state for gases
  • Basic principles of thermodynamics related to compressible flow
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  • Study the derivation of the Rankine-Hugoniot conditions for various gas types
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Homework Statement



For the case of a strong shock propagating into a gas with \gamma=7/5 What is the ratio \rho2/\rho1

Homework Equations


\rho\ u=constant

P+ \rho\ u^2=constant

\frac{1}{2} u+ \frac{\gamma }{\gamma -1}\frac{\ P}{\rho} = constant

The Attempt at a Solution



I can use the 3 equations in this form to get \rho2/\rho1=6 but my problem is how do I arrive at the 3rd equation in the given form

we were given equation 3 in the form \frac{1}{2} u+ \frac{5}{2}\frac{\ P}{\rho} = constant but this is only valid for \gamma=\frac{5}{3}

I would like some advice on how to prove the adaption of equation 3 for different values of \gamma
 
Last edited:
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Hi oro,

Apologies but I don't quite understand what you're question is. If you wanted to solve the Rankine-Hugoniot condition for energy flow for something other than a monatomic gas, what's the problem with just plugging in a different value of \gamma into equation 3 in your list?
 

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