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=Spherically Symmetric Configurations (Part I)=
=Spherically Symmetric Configurations (Part II)=
[[Image:LSU_Structure_still.gif|74px|left]]
[[Image:LSU_Structure_still.gif|74px|left]]
Equilibrium, spherically symmetric '''structures''' are obtained by searching for time-independent solutions to the above set of simplified governing equations.  The steady-state flow field that must be adopted to satisfy both a spherically symmetric geometry and the time-independent constraint is, <math>\vec{v} = \hat{e}_r v_r = 0</math>. After setting the radial velocity, <math>v_r</math>, and all time-derivatives to zero, we see that the <math>1^\mathrm{st}</math> (continuity) and <math>3^\mathrm{rd}</math> (first law of thermodynamics) equations are trivially satisfied while the <math>2^\mathrm{nd}</math> (Euler) and <math>4^\mathrm{th}</math> give, respectively,
Equilibrium, spherically symmetric '''structures''' are obtained by searching for time-independent solutions to the above set of simplified governing equations.  The steady-state flow field that must be adopted to satisfy both a spherically symmetric geometry and the time-independent constraint is, <math>\vec{v} = \hat{e}_r v_r = 0</math>. After setting the radial velocity, <math>v_r</math>, and all time-derivatives to zero, we see that the <math>1^\mathrm{st}</math> (continuity) and <math>3^\mathrm{rd}</math> (first law of thermodynamics) equations are trivially satisfied while the <math>2^\mathrm{nd}</math> (Euler) and <math>4^\mathrm{th}</math> give, respectively,

Revision as of 20:49, 1 February 2010

Whitworth's (1981) Isothermal Free-Energy Surface
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Spherically Symmetric Configurations (Part II)

LSU Structure still.gif

Equilibrium, spherically symmetric structures are obtained by searching for time-independent solutions to the above set of simplified governing equations. The steady-state flow field that must be adopted to satisfy both a spherically symmetric geometry and the time-independent constraint is, <math>\vec{v} = \hat{e}_r v_r = 0</math>. After setting the radial velocity, <math>v_r</math>, and all time-derivatives to zero, we see that the <math>1^\mathrm{st}</math> (continuity) and <math>3^\mathrm{rd}</math> (first law of thermodynamics) equations are trivially satisfied while the <math>2^\mathrm{nd}</math> (Euler) and <math>4^\mathrm{th}</math> give, respectively,

Hydrostatic Balance

<math>\frac{1}{\rho}\frac{dP}{dr} =- \frac{d\Phi}{dr} </math> ,

and,

Poisson Equation

<math>\frac{1}{r^2} \biggl[\frac{d }{dr} \biggl( r^2 \frac{d \Phi}{dr} \biggr) \biggr] = 4\pi G \rho </math> .


(We recognize the first of these expressions as being the statement of hydrostatic balance appropriate for spherically symmetric configurations.)

We need one supplemental relation to close this set of equations because there are two equations, but three unknown functions — <math>~P</math>(r), <math>~\rho</math>(r), and <math>~\Phi</math>(r). As has been outlined in our discussion of supplemental relations for time-independent problems, in the context of this H_Book we will close this set of equations by specifying a structural, barotropic relationship between <math>~P</math> and <math>~\rho</math>. (See below.)

Solution Strategies

When attempting to solve the identified pair of simplified governing differential equations, it will be useful to note that, in a spherically symmetric configuration (where <math>~\rho</math> is not a function of <math>\theta</math> or <math>\varphi</math>), the differential mass <math>dm_r</math> that is enclosed within a spherical shell of thickness <math>dr</math> is,

<math>dm_r = \rho dr \oint dS = r^2 \rho dr \int_0^\pi \sin\theta d\theta \int_0^{2\pi} d\varphi = 4\pi r^2 \rho dr</math> ,

where we have pulled from the Wikipedia discussion of integration and differentiation in spherical coordinates to define the spherical surface element <math>dS</math>. Integrating from the center of the spherical configuration (<math>r=0</math>) out to some finite radius <math>r</math> that is still inside the configuration gives the mass enclosed within that radius, <math>M_r</math>; specifically,

<math>M_r \equiv \int_0^r dm_r = \int_0^r 4\pi r^2 \rho dr</math> .

We can also state that,

LSU Key.png

<math>~\frac{dM_r}{dr} = 4\pi r^2 \rho</math>

This differential relation is often identified as a statement of mass conservation that replaces the equation of continuity for spherically symmetric, static equilibrium structures.

Technique #1

Integrating the Poisson equation once, from the center of the configuration (<math>r=0</math>) out to some finite radius <math>r</math> that is still inside the configuration, gives,

<math> \int_0^r d\biggl( r^2 \frac{d \Phi}{dr} \biggr) = \int_0^r 4\pi G r^2 \rho dr </math>

<math> \Rightarrow ~~~~~ r^2 \frac{d \Phi}{dr} \biggr|_0^r = GM_r </math> .

Now, as long as <math>d\Phi/dr</math> increases less steeply than <math>r^{-2}</math> as we move toward the center of the configuration — indeed, we will find that <math>d\Phi/dr</math> usually goes smoothly to zero at the center — the term on the left-hand-side of this last expression will go to zero at <math>r=0</math>. Hence, this first integration of the Poisson equation gives,

<math> \frac{d \Phi}{dr} = \frac{G M_r}{r^2} </math> .

Substituting this expression into the hydrostatic balance equation gives,

LSU Key.png

<math>~\frac{dP}{dr} = - \frac{GM_r \rho}{r^2}</math>

that is, a single governing integro-differential equation which depends only on the two unknown functions, <math>~P</math> and <math>~\rho</math> .


Technique #2

As long as we are examining only barotropic structures, we can replace <math>dP/\rho</math> by d<math>~H</math> in the hydrostatic balance relation to obtain,

<math>\frac{dH}{dr} =- \frac{d\Phi}{dr} </math> .

If we multiply this expression through by <math>r^2</math> then differentiate it with respect to <math>r</math>, we obtain,

<math>\frac{d}{dr}\biggl( r^2 \frac{dH}{dr} \biggr) =- \frac{d}{dr} \biggl( r^2 \frac{d\Phi}{dr} \biggr)</math> ,

which can be used to replace the left-hand-side of the Poisson equation and give,

<math>\frac{1}{r^2} \frac{d}{dr}\biggl( r^2 \frac{dH}{dr} \biggr) =- 4\pi G \rho</math> ,

that is, a single second-order governing differential equation which depends only on the two unknown functions, <math>~H</math> and <math>~\rho</math>.

Whitworth's (1981) Isothermal Free-Energy Surface

© 2014 - 2021 by Joel E. Tohline
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