Moving expansion waves: Difference between revisions
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==== Moving Expansion Waves ==== | |||
The expansion wave propagation into the driver section in a shock tube can be described using characteristic lines. | |||
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The expansion is propagating into stagnant fluid in region four (the driver section), which means that the flow properties ahead of the expansion wave are constant. | |||
<math display="block"> | |||
J^+_a=J^+_b | J^+_a=J^+_b | ||
</math> | |||
<math>J^+</math> invariants constant along <math>C^+</math> characteristics | |||
<math display="block"> | |||
J^+_a=J^+_c=J^+_e | J^+_a=J^+_c=J^+_e | ||
</math> | |||
<math display="block"> | |||
J^+_b=J^+_d=J^+_f | J^+_b=J^+_d=J^+_f | ||
</math> | |||
Since <math>J^+_a=J^+_b</math> this also implies <math>J^+_e=J^+_f</math>. In fact, since the flow properties ahead of the expansion are constant, all <math>C^+</math> lines will have the same <math>J^+</math> value. | |||
<math>J^-</math> invariants constant along <math>C^-</math> characteristics | |||
<math display="block"> | |||
J^-_c=J^-_d | J^-_c=J^-_d | ||
</math> | |||
<math display="block"> | |||
J^-_e=J^-_f | J^-_e=J^-_f | ||
</math> | |||
<math display="block"> | |||
\left. | \left. | ||
\begin{aligned} | \begin{aligned} | ||
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\right\}\Rightarrow u_e=u_f \Rightarrow a_e=a_f | \right\}\Rightarrow u_e=u_f \Rightarrow a_e=a_f | ||
</math> | |||
Due to the fact the <math>J^+</math> is constant in the entire expansion region, <math>u</math> and <math>a</math> will be constant along each <math>C^-</math> line. | |||
The constant <math>J^+</math> value can be used to obtain relations for the variation of flow properties through the expansion region. Evaluation of the <math>J^+</math> invariant at any position within the expansion region should give the same value as in region 4. | |||
<math display="block"> | |||
u+\frac{2a}{\gamma-1}=u_4+\frac{2a_4}{\gamma-1}=0+\frac{2a_4}{\gamma-1} | u+\frac{2a}{\gamma-1}=u_4+\frac{2a_4}{\gamma-1}=0+\frac{2a_4}{\gamma-1} | ||
</math> | |||
and thus | |||
<math display="block"> | |||
\frac{a}{a_4}=1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right) | \frac{a}{a_4}=1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right) | ||
</math> | |||
Eqn. \ref{eq:expansion:a} and <math>a=\sqrt{\gamma RT}</math> gives | |||
<math display="block"> | |||
\frac{T}{T_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^2 | \frac{T}{T_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^2 | ||
</math> | |||
Using isentropic relations, we can get pressure ratio and density ratio | |||
<math display="block"> | |||
\frac{p}{p_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^{2\gamma/(\gamma-1)} | \frac{p}{p_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^{2\gamma/(\gamma-1)} | ||
</math> | |||
<math display="block"> | |||
\frac{\rho}{\rho_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^{2/(\gamma-1)} | \frac{\rho}{\rho_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^{2/(\gamma-1)} | ||
</math> | |||
Revision as of 08:15, 23 March 2026
Moving Expansion Waves
The expansion wave propagation into the driver section in a shock tube can be described using characteristic lines.
The expansion is propagating into stagnant fluid in region four (the driver section), which means that the flow properties ahead of the expansion wave are constant.
invariants constant along characteristics
Since this also implies . In fact, since the flow properties ahead of the expansion are constant, all lines will have the same value.
invariants constant along characteristics
Due to the fact the is constant in the entire expansion region, and will be constant along each line.
The constant value can be used to obtain relations for the variation of flow properties through the expansion region. Evaluation of the invariant at any position within the expansion region should give the same value as in region 4.
and thus
Eqn. \ref{eq:expansion:a} and gives
Using isentropic relations, we can get pressure ratio and density ratio