Difference between revisions of "User:Tohline/SSC/Stability/InstabilityOnsetOverview"
Line 23: | Line 23: | ||
<table border="1" align="center" cellpadding="8" width="1050px"> | <table border="1" align="center" cellpadding="8" width="1050px"> | ||
<tr> | <tr> | ||
<td align="center" colspan=" | <td align="center" colspan="5"> | ||
<b>Figure 1:</b> Equilibrium | <b>Figure 1:</b> Equilibrium Sequences of Pressure-Truncated Isothermal Spheres<br />(viewed from three different astrophysical perspectives) | ||
</td> | </td> | ||
</tr> | </tr> | ||
<tr> | <tr> | ||
<td align="center" width=" | <td align="center"><font color="black" size="+2">●</font></td><td align="center"><math>~\xi_e</math></td> | ||
<td align="center" width=" | <td align="center" width="300px">External Pressure vs. Volume<br /><font size="-1">(Fixed Mass)</font></td> | ||
<td align="center" width=" | <td align="center" width="300px">Mass vs. Radius<br /><font size="-1">(Fixed External Pressure)</font></td> | ||
<td align="center" width="300px">Mass vs. Central Density<br /><font size="-1">(Fixed External Pressure)</font></td> | |||
</tr> | </tr> | ||
<tr> | <tr> | ||
<td align="center" colspan="3"> | <td align="center" colspan="1"><font color="yellow" size="+2">●</font></td> <td align="right" colspan="1">4.05</td> | ||
[[File:IsothermalTruncCombined3.png| | <td align="center" colspan="3" rowspan="7"> | ||
[[File:IsothermalTruncCombined3.png|900px|center|Pressure-Truncated Isothermal Equilibrium Sequence]] | |||
</td> | </td> | ||
</tr> | |||
<tr> | |||
<td align="center" colspan="1"><font color="darkgreen" size="+2">●</font></td> <td align="right" colspan="1">6.45</td> | |||
</tr> | |||
<tr> | |||
<td align="center" colspan="1"><font color="purple" size="+2">●</font></td> <td align="right" colspan="1">9.00</td> | |||
</tr> | |||
<tr> | |||
<td align="center" colspan="1"><font color="darkgreen" size="+2">●</font></td> <td align="right" colspan="1">67.00</td> | |||
</tr> | |||
<tr> | |||
<td align="center" colspan="1"><font color="purple" size="+2">●</font></td> <td align="right" colspan="1">98.50</td> | |||
</tr> | |||
<tr> | |||
<td align="center" colspan="1"><font color="darkgreen" size="+2">●</font></td> <td align="right" colspan="1">735.00</td> | |||
</tr> | |||
<tr> | |||
<td align="center" colspan="1"><font color="purple" size="+2">●</font></td> <td align="right" colspan="1">1060.00</td> | |||
</tr> | </tr> | ||
</table> | </table> | ||
</div> | </div> | ||
This equation — in the following, slightly rewritten form — can be found among our selected set of [[User:Tohline/Appendix/Equation_templates#Stability:__Radial_Pulsation|''key equations'' associated with the study of radial pulsation]], and will henceforth be referred to as the, | This equation — in the following, slightly rewritten form — can be found among our selected set of [[User:Tohline/Appendix/Equation_templates#Stability:__Radial_Pulsation|''key equations'' associated with the study of radial pulsation]], and will henceforth be referred to as the, |
Revision as of 16:56, 20 March 2017
Overview: Marginally Unstable Pressure-Truncated Configurations
Additional details may be found here.
| Tiled Menu | Tables of Content | Banner Video | Tohline Home Page | |
Isothermal
Once a central density, <math>~\rho_c</math>, and constituent fluid sound speed, <math>~c_s</math>, have been specified, the internal structure of an equilibrium, isothermal sphere can be completely described in terms of the function, <math>~\psi(\xi) \equiv \ln(\rho_c/\rho)</math>, which is a solution of the,
Isothermal Lane-Emden Equation
|
subject to the boundary conditions, <math>~ \psi = 0</math> and <math>~d\psi/d\xi = 0</math> at <math>~\xi = 0</math>. In isolation, the isothermal sphere extends to infinity. But configurations of finite extent can be constructed by truncating the function, <math>~\psi</math>, at some radius, <math>~0 < \xi_e < \infty</math> — such that the surface density is finite and set by the value of <math>~\psi_e \equiv \psi(\xi_e)</math> — and embedding the configuration in a hot, tenuous medium that exerts an "external" pressure, <math>~P_e = c_s^2 \rho_c e^{-\psi_e}</math>, uniformly across the surface of the — now, truncated — sphere. The internal structure of such a "pressure-truncated" isothermal sphere is completely describable in terms of the same function, <math>~\psi(\xi)</math>, that describes the structure of the isolated isothermal sphere, except that beyond <math>~\xi_e</math> the function becomes irrelevant.
A sequence of equilibrium, pressure-truncated isothermal spheres is readily defined by varying the value of <math>~\xi_e</math>. Figure 1 displays the behavior of such an equilibrium sequence, as viewed from three different astrophysical perspectives (in all cases, <math>~c_s</math> is held fixed while <math>~\xi_e</math> is varied monotonically along the sequence): Left panel — A pressure-volume diagram, which shows how the truncated configuration's equilibrium volume varies with the externally applied pressure, if the configuration's mass is held fixed. Center panel — A mass-radius diagram, which shows how the truncated configuration's mass varies with the equilibrium radius, if the external pressure is held fixed. Right panel — A diagram that shows how the configuration's mass varies with central density, if the external pressure is held fixed.
Figure 1: Equilibrium Sequences of Pressure-Truncated Isothermal Spheres |
||||
● | <math>~\xi_e</math> | External Pressure vs. Volume (Fixed Mass) |
Mass vs. Radius (Fixed External Pressure) |
Mass vs. Central Density (Fixed External Pressure) |
● | 4.05 | |||
● | 6.45 | |||
● | 9.00 | |||
● | 67.00 | |||
● | 98.50 | |||
● | 735.00 | |||
● | 1060.00 |
This equation — in the following, slightly rewritten form — can be found among our selected set of key equations associated with the study of radial pulsation, and will henceforth be referred to as the,
Isothermal LAWE
<math>~0 = \frac{d^2x}{d\xi^2} + \biggl[4 - \xi \biggl( \frac{d\psi}{d\xi} \biggr) \biggr] \frac{1}{\xi} \cdot \frac{dx}{d\xi} + \biggl[ \biggl( \frac{\sigma_c^2}{6\gamma_\mathrm{g}}\biggr)\xi^2 - \alpha \xi \biggl( \frac{d\psi}{d\xi} \biggr) \biggr] \frac{x}{\xi^2} </math> |
|
where: <math>~\sigma_c^2 \equiv \frac{3\omega^2}{2\pi G\rho_c}</math> and, <math>~\alpha \equiv \biggl(3 - \frac{4}{\gamma_\mathrm{g}}\biggr)</math> |
Yabushita (1974, 1975) showed that the following eigenvector specification provides a
Precise Solution to the Isothermal LAWE | ||
<math>~\sigma_c^2 = 0</math> |
and |
<math>~x = 1 - \biggl( \frac{1}{\xi e^{-\psi}}\biggr) \frac{d\psi}{d\xi} \, ,</math> |
if the adiabatic exponent is assigned the value, <math>~\gamma_g = 1</math>, in which case the parameter, <math>~\alpha = -1</math>. When viewed in concert with the surface boundary condition,
<math>~\frac{d\ln x}{d\ln\xi}</math> |
<math>~=</math> |
<math>~- 3 \, ,</math> |
the relevant configuration is precisely defined by the surface condition, xxx, which is identical to the configuration at the turning point.
Polytropic
Given a value of the polytropic index, <math>~n</math>, the internal structure of a detailed force-balance model is provided via the function, <math>~\theta(\xi)</math>, which is a solution of the,
Polytropic Lane-Emden Equation
|
subject to the boundary conditions, <math>~\Theta_H = 1</math> and <math>~d\Theta_H/d\xi = 0</math> at <math>~\xi = 0</math>.
To identify pure radial oscillation modes, we seek solutions to the,
Polytropic LAWE
<math>~0 = \frac{d^2x}{d\xi^2} + \biggl[ 4 - (n+1) Q \biggr] \frac{1}{\xi} \cdot \frac{dx}{d\xi} + (n+1) \biggl[ \biggl( \frac{\sigma_c^2}{6\gamma_g } \biggr) \frac{\xi^2}{\theta} - \alpha Q\biggr] \frac{x}{\xi^2} </math> |
|
where: <math>~Q(\xi) \equiv - \frac{d\ln\theta}{d\ln\xi} \, ,</math> <math>~\sigma_c^2 \equiv \frac{3\omega^2}{2\pi G\rho_c} \, ,</math> and, <math>~\alpha \equiv \biggl(3 - \frac{4}{\gamma_\mathrm{g}}\biggr)</math> |
We have discovered that, for any value of the polytropic index in the range, <math>~3 \le n < \infty</math>, the following eigenvector specification provides a
|
if the adiabatic exponent is assigned the value, <math>~\gamma_g = (n+1)/n</math>, in which case the parameter, <math>~\alpha = (3-n)/(n+1)</math>.
References
© 2014 - 2021 by Joel E. Tohline |