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===6<sup>th</sup> Try=== ====Euler Equation==== From, for example, [[PGE/Euler#in_terms_of_velocity:_2|here]] we can write the, <div align="center"> <span id="ConservingMomentum:Eulerian"><font color="#770000">'''Eulerian Representation'''</font></span><br /> of the Euler Equation, {{Template:Math/EQ_Euler02}} </div> In steady-state, we should set <math>\partial\vec{v}/\partial t = 0</math>. There are various ways of expressing the nonlinear term on the LHS; from [[PGE/Euler#in_terms_of_the_vorticity:|here]], for example, we find, <div align="center"> <math> (\vec{v}\cdot\nabla)\vec{v} = \frac{1}{2}\nabla(\vec{v}\cdot\vec{v}) - \vec{v}\times(\nabla\times\vec{v}) = \frac{1}{2}\nabla(v^2) + \vec{\zeta}\times \vec{v} , </math> </div> where, <div align="center"> <math> \vec\zeta \equiv \nabla\times\vec{v} </math> </div> is commonly referred to as the [https://en.wikipedia.org/wiki/Vorticity vorticity]. ====Axisymmetric Configurations==== From, for example, [[AxisymmetricConfigurations/PGE#CYLconvectiveOperator|here]], we appreciate that, quite generally, for axisymmetric systems when written in cylindrical coordinates, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math> (\vec{v} \cdot \nabla )\vec{v} </math> </td> <td align="center"> = </td> <td align="left"> <math> \hat{e}_\varpi \biggl[ v_\varpi \frac{\partial v_\varpi}{\partial\varpi} + v_z \frac{\partial v_\varpi}{\partial z} - \frac{v_\varphi v_\varphi}{\varpi} \biggr] + \hat{e}_\varphi \biggl[ v_\varpi \frac{\partial v_\varphi}{\partial \varpi} + v_z \frac{\partial v_\varphi}{\partial z} + \frac{v_\varphi v_\varpi}{\varpi} \biggr] + \hat{e}_z \biggl[ v_\varpi \frac{\partial v_z}{\partial\varpi} + v_z \frac{\partial v_z}{\partial z} \biggr] \, . </math> </td> </tr> </table> We seek steady-state configurations for which <math>v_\varpi =0</math> and <math>v_z = 0</math>, in which case this expression simplifies considerably to, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math> (\vec{v} \cdot \nabla )\vec{v} </math> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> \hat{e}_\varpi \biggl[ - \frac{v_\varphi v_\varphi}{\varpi} \biggr] </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> \hat{e}_\varpi \biggl[ - \frac{j^2}{\varpi^3} \biggr] \, , </math> </td> </tr> </table> where, in this last expression we have replaced <math>v_\varphi</math> with the specific angular momentum, <math>j \equiv \varpi v_\varphi = (\varpi^2 \dot\varphi)</math>, which is a [[AxisymmetricConfigurations/PGE#Conservation_of_Specific_Angular_Momentum_(CYL.)|conserved quantity in dynamically evolving systems]]. NOTE: Up to this point in our discussion, <math>j</math> can be a function of both coordinates, that is, <math>j = j(\varpi, z)</math>. As has been highlighted [[AxisymmetricConfigurations/PGE#RelevantCylindricalComponents|here]] for example — for the axisymmetric configurations under consideration — the <math>\hat{e}_\varpi</math> and <math>\hat{e}_z</math> components of the Euler equation become, respectively,</span> <table border="1" align="center" cellpadding="10"><tr><td align="center"> <table border="0" cellpadding="5" align="center"> <tr> <td align="right"><math>{\hat{e}}_\varpi</math>: </td> <td align="right"> <math> - \frac{j^2}{\varpi^3} </math> </td> <td align="center"> = </td> <td align="left"> <math> - \biggl[ \frac{1}{\rho}\frac{\partial P}{\partial\varpi} + \frac{\partial \Phi}{\partial\varpi}\biggr] </math> </td> </tr> <tr> <td align="right"><math>{\hat{e}}_z</math>: </td> <td align="right"> <math> 0 </math> </td> <td align="center"> = </td> <td align="left"> <math> - \biggl[ \frac{1}{\rho}\frac{\partial P}{\partial z} + \frac{\partial \Phi}{\partial z} \biggr] </math> </td> </tr> </table> </td></tr></table> ====Strategy==== <font color="red">STEP 1:</font> For the problem being tackled here, we start by recognizing that when considering hydrostatic balance in the <math>\hat{e}_z</math> direction, we have analytically known expressions for both <math>\rho(\varpi, z)</math> and <math>\partial\Phi/\partial z</math>. This means, therefore, that we can construct an analytical expression for the vertical component of the pressure gradient, specifically, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math> \frac{\partial P}{\partial z} </math> </td> <td align="center"> = </td> <td align="left"> <math> - \rho \cdot \frac{\partial \Phi}{\partial z} \, . </math> </td> </tr> <tr> <td align="right"><math>\Rightarrow ~~~ \frac{1}{(\pi G\rho_c^2 a_\ell^2)} \cdot \frac{\partial P}{\partial \zeta}</math></td> <td align="center"><math>=</math></td> <td align="left"> <math> \frac{\rho}{\rho_c} \cdot \frac{\partial}{\partial \zeta} \biggl\{ \frac{\Phi_\mathrm{grav}}{(-\pi G\rho_c a_\ell^2)} \biggr\} </math> </td> </tr> </table> <font color="red">STEP 2:</font> Because we want the meridional-plane, constant-pressure contours to align with the meridional-plane, constant density contours, we can determine the radial component of the pressure gradient by forcing the slope of the tangent vector to match the tangent vector of the density contour. <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>\frac{\partial P}{\partial \zeta} </math> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> - \frac{1}{m}\biggl[\frac{\partial P}{\partial \chi}\biggr] = -\frac{\chi(1-e^2)}{\zeta} \biggl[\frac{\partial P}{\partial \chi}\biggr] </math> </td> </tr> <tr> <td align="right"> <math>\Rightarrow ~~~ \frac{1}{(\pi G\rho_c^2 a_\ell^2)} \cdot \frac{\partial P}{\partial \chi} </math> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> -\frac{\zeta}{\chi(1-e^2)} \biggl[\frac{1}{(\pi G\rho_c^2 a_\ell^2)} \cdot \frac{\partial P}{\partial \zeta}\biggr] </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> -\frac{\zeta}{\chi(1-e^2)} \biggl\{ \frac{\rho}{\rho_c} \cdot \frac{\partial}{\partial \zeta} \biggl[ \frac{\Phi_\mathrm{grav}}{(-\pi G\rho_c a_\ell^2)} \biggr] \biggr\} \, . </math> </td> </tr> </table> <font color="red">STEP 3:</font> Via the radial component of the hydrostatic balance expression, we can determine analytically the distribution of specific angular momentum. <table border="0" align="center" cellpadding="8"> <tr> <td align="right"> <math> \frac{j^2}{\varpi^3} </math> </td> <td align="center"> = </td> <td align="left"> <math> \biggl[ \frac{1}{\rho}\frac{\partial P}{\partial\varpi} + \frac{\partial \Phi}{\partial\varpi}\biggr] </math> </td> </tr> <tr> <td align="right"> <math>\Rightarrow ~~~ \frac{j^2 }{(\pi G \rho_c a_\ell^4)} \cdot \frac{1}{\chi^3} </math> </td> <td align="center"><math>=</math></td> <td align="left"> <math> \biggl(\frac{\rho}{\rho_c}\biggr)^{-1} \biggl[\frac{1}{(\pi G \rho_c^2 a_\ell^2)} \biggr]\frac{\partial P}{\partial \chi} - \frac{\partial}{\partial \chi} \biggl\{ \frac{\Phi_\mathrm{grav}}{(-\pi G \rho_c a_\ell^2)} \biggr\} </math> </td> </tr> </table> <font color="red">STEP 4:</font> From knowledge of both components of <math>\nabla P</math>, see if the expression for the pressure can be ascertained. ====Implication==== Hence, <table border="0" align="center" cellpadding="8"> <tr> <td align="right"> <math> \frac{j^2 }{(\pi G \rho_c a_\ell^4)} \cdot \frac{1}{\chi^3} </math> </td> <td align="center"><math>=</math></td> <td align="left"> <math> -\frac{\zeta}{\chi(1-e^2)} \cdot \frac{\partial}{\partial \zeta} \biggl[ \frac{\Phi_\mathrm{grav}}{(-\pi G\rho_c a_\ell^2)} \biggr] - \frac{\partial}{\partial \chi} \biggl\{ \frac{\Phi_\mathrm{grav}}{(-\pi G \rho_c a_\ell^2)} \biggr\} \, . </math> </td> </tr> </table> Now, given that, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>\frac{ \Phi_\mathrm{grav}(\varpi,z)}{(-\pi G\rho_c a_\ell^2)} </math> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> \frac{1}{2} I_\mathrm{BT} - A_\ell \chi^2 - A_s \zeta^2 + \frac{1}{2}\biggl[(A_{s s} a_\ell^2) \zeta^4 + 2(A_{\ell s}a_\ell^2 )\chi^2 \zeta^2 + (A_{\ell \ell} a_\ell^2) \chi^4 \biggr] \, , </math> </td> </tr> </table> we see that the pair of partial derivative expressions are: <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>\frac{\partial}{\partial \zeta} \biggl[ \frac{\Phi_\mathrm{grav}}{(-\pi G\rho_c a_\ell^2)} \biggr] </math> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> 2\biggl[(A_{s s} a_\ell^2) \zeta^3 + (A_{\ell s}a_\ell^2 )\chi^2 \zeta - A_s \zeta \biggr] \, ; </math> </td> <tr> <td align="right"> <math>\frac{\partial}{\partial \chi} \biggl[ \frac{\Phi_\mathrm{grav}}{(-\pi G\rho_c a_\ell^2)} \biggr] </math> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> 2\biggl[ (A_{\ell \ell} a_\ell^2) \chi^3 + (A_{\ell s}a_\ell^2 )\chi \zeta^2 - A_\ell \chi\biggr] \, . </math> </td> </tr> </table> As a result we find, <table border="0" align="center" cellpadding="8"> <tr> <td align="right"> <math> \frac{j^2 (1-e^2)}{(\pi G \rho_c a_\ell^4)} \cdot \frac{1}{\chi^2} </math> </td> <td align="center"><math>=</math></td> <td align="left"> <math> -2\zeta \biggl[(A_{s s} a_\ell^2) \zeta^3 + (A_{\ell s}a_\ell^2 )\chi^2 \zeta - A_s \zeta \biggr] - 2\chi(1-e^2) \biggl[ (A_{\ell \ell} a_\ell^2) \chi^3 + (A_{\ell s}a_\ell^2 )\chi \zeta^2 - A_\ell \chi\biggr] </math> </td> </tr> <tr> <td align="right"> <math> \Rightarrow ~~~ \frac{j^2 (1-e^2)}{(2\pi G \rho_c a_\ell^4)} \cdot \frac{1}{\chi^2} </math> </td> <td align="center"><math>=</math></td> <td align="left"> <math> \biggl[-(A_{s s} a_\ell^2) \zeta^4 - (A_{\ell s}a_\ell^2 )\chi^2 \zeta^2 + A_s \zeta^2 \biggr] + (1-e^2) \biggl[ -(A_{\ell \ell} a_\ell^2) \chi^4 - (A_{\ell s}a_\ell^2 )\chi^2 \zeta^2 + A_\ell \chi^2\biggr] </math> </td> </tr> </table> Next, regarding <font color="red">STEP 4</font>, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"><math>\frac{1}{(\pi G\rho_c^2 a_\ell^2)} \cdot \frac{\partial P}{\partial \zeta}</math></td> <td align="center"><math>=</math></td> <td align="left"> <math> \frac{\rho}{\rho_c} \cdot \frac{\partial}{\partial \zeta} \biggl\{ \frac{\Phi_\mathrm{grav}}{(-\pi G\rho_c a_\ell^2)} \biggr\} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"><math>=</math></td> <td align="left"> <math> 2\biggl[1 - \chi^2 - \zeta^2(1-e^2)^{-1} \biggr] \biggl[(A_{s s} a_\ell^2) \zeta^3 + (A_{\ell s}a_\ell^2 )\chi^2 \zeta - A_s \zeta \biggr] </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"><math>=</math></td> <td align="left"> <math> 2\biggl[(A_{s s} a_\ell^2) \zeta^3 + (A_{\ell s}a_\ell^2 )\chi^2 \zeta - A_s \zeta \biggr] - 2\biggl[(A_{s s} a_\ell^2) \chi^2 \zeta^3 + (A_{\ell s}a_\ell^2 )\chi^4 \zeta - A_s \chi^2\zeta \biggr] - 2\biggl[(A_{s s} a_\ell^2) \zeta^5(1-e^2)^{-1} + (A_{\ell s}a_\ell^2 )\chi^2 \zeta^3(1-e^2)^{-1} - A_s \zeta^3(1-e^2)^{-1} \biggr] </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"><math>=</math></td> <td align="left"> <math> 2 \biggl\{ (A_{s s} a_\ell^2) \zeta^3 + (A_{\ell s}a_\ell^2 )\chi^2 \zeta - A_s \zeta -(A_{s s} a_\ell^2) \chi^2 \zeta^3 - (A_{\ell s}a_\ell^2 )\chi^4 \zeta + A_s \chi^2\zeta -(A_{s s} a_\ell^2) \zeta^5(1-e^2)^{-1} - (A_{\ell s}a_\ell^2 )\chi^2 \zeta^3(1-e^2)^{-1} + A_s \zeta^3(1-e^2)^{-1} \biggr\} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"><math>=</math></td> <td align="left"> <math> 2 \biggl\{ \biggl[ (A_{\ell s}a_\ell^2 )\chi^2 - A_s - (A_{\ell s}a_\ell^2 )\chi^4 + A_s \chi^2\biggr]\zeta + \biggl[ (A_{s s} a_\ell^2) -(A_{s s} a_\ell^2) \chi^2 - (A_{\ell s}a_\ell^2 )\chi^2 (1-e^2)^{-1} + A_s (1-e^2)^{-1}\biggr] \zeta^3 + \biggl[-(A_{s s} a_\ell^2) (1-e^2)^{-1} \biggr]\zeta^5 \biggr\} </math> </td> </tr> <tr> <td align="right"><math>\Rightarrow ~~~ \frac{12 P}{(2\pi G\rho_c^2 a_\ell^2)} </math></td> <td align="center"><math>\sim</math></td> <td align="left"> <math> 6\biggl[ (A_{\ell s}a_\ell^2 )\chi^2 - A_s - (A_{\ell s}a_\ell^2 )\chi^4 + A_s \chi^2\biggr]\zeta^2 + 3\biggl[ (A_{s s} a_\ell^2) -(A_{s s} a_\ell^2) \chi^2 - (A_{\ell s}a_\ell^2 )\chi^2 (1-e^2)^{-1} + A_s (1-e^2)^{-1}\biggr] \zeta^4 + 2\biggl[-(A_{s s} a_\ell^2) (1-e^2)^{-1} \biggr]\zeta^6 </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"><math>=</math></td> <td align="left"> <math> 6(A_{\ell s}a_\ell^2 )\zeta^2\chi^2 - 6A_s\zeta^2 - 6(A_{\ell s}a_\ell^2 )\zeta^2\chi^4 + 6A_s \zeta^2 \chi^2 + 3(A_{s s} a_\ell^2)\zeta^4 -3(A_{s s} a_\ell^2) \zeta^4\chi^2 - 3(A_{\ell s}a_\ell^2 )\zeta^4\chi^2 (1-e^2)^{-1} + 3A_s \zeta^4(1-e^2)^{-1} - 2(A_{s s} a_\ell^2) \zeta^6(1-e^2)^{-1} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"><math>=</math></td> <td align="left"> <math> + \biggl[ 3(A_{s s} a_\ell^2)\zeta^4 + 3A_s \zeta^4(1-e^2)^{-1} - 6A_s\zeta^2 - 2(A_{s s} a_\ell^2) \zeta^6(1-e^2)^{-1}\biggr] + \biggl[ 6(A_{\ell s}a_\ell^2 )\zeta^2 + 6A_s \zeta^2 - 3(A_{s s} a_\ell^2) \zeta^4 - 3(A_{\ell s}a_\ell^2 )\zeta^4 (1-e^2)^{-1}\biggr]\chi^2 + \biggl[ - 6(A_{\ell s}a_\ell^2 )\zeta^2 \biggr] \chi^4 \, ; </math> </td> </tr> </table> and, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>\frac{1}{(\pi G\rho_c^2 a_\ell^2)} \cdot \frac{\partial P}{\partial \chi} </math> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> -\frac{\zeta}{\chi(1-e^2)} \biggl\{ \frac{\rho}{\rho_c} \cdot \frac{\partial}{\partial \zeta} \biggl\{ \frac{\Phi_\mathrm{grav}}{(-\pi G\rho_c a_\ell^2)} \biggr\} \biggr\} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> -\frac{\zeta}{\chi(1-e^2)} \biggl\{ 2\biggl[(A_{s s} a_\ell^2) \zeta^3 + (A_{\ell s}a_\ell^2 )\chi^2 \zeta - A_s \zeta \biggr] - 2\biggl[(A_{s s} a_\ell^2) \chi^2 \zeta^3 + (A_{\ell s}a_\ell^2 )\chi^4 \zeta - A_s \chi^2\zeta \biggr] - 2\biggl[(A_{s s} a_\ell^2) \zeta^5(1-e^2)^{-1} + (A_{\ell s}a_\ell^2 )\chi^2 \zeta^3(1-e^2)^{-1} - A_s \zeta^3(1-e^2)^{-1} \biggr] \biggr\} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> -\frac{1}{(1-e^2)} \biggl\{ 2\biggl[(A_{s s} a_\ell^2) \chi^{-1}\zeta^4 + (A_{\ell s}a_\ell^2 )\chi \zeta^2 - A_s \chi^{-1}\zeta^2 \biggr] - 2\biggl[(A_{s s} a_\ell^2) \chi \zeta^4 + (A_{\ell s}a_\ell^2 )\chi^3 \zeta^2 - A_s \chi\zeta^2 \biggr] - 2\biggl[(A_{s s} a_\ell^2) \chi^{-1}\zeta^6(1-e^2)^{-1} + (A_{\ell s}a_\ell^2 )\chi \zeta^4(1-e^2)^{-1} - A_s \chi^{-1}\zeta^4(1-e^2)^{-1} \biggr] \biggr\} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> \frac{2}{(1-e^2)} \biggl\{ -(A_{s s} a_\ell^2) \chi^{-1}\zeta^4 - (A_{\ell s}a_\ell^2 )\chi \zeta^2 + A_s \chi^{-1}\zeta^2 + (A_{s s} a_\ell^2) \chi \zeta^4 + (A_{\ell s}a_\ell^2 )\chi^3 \zeta^2 - A_s \chi\zeta^2 + (A_{s s} a_\ell^2) \chi^{-1}\zeta^6(1-e^2)^{-1} + (A_{\ell s}a_\ell^2 )\chi \zeta^4(1-e^2)^{-1} - A_s \chi^{-1}\zeta^4(1-e^2)^{-1} \biggr\} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>=</math> </td> <td align="left"> <math> \frac{2}{(1-e^2)} \biggl\{ \biggl[A_s \zeta^2 -(A_{s s} a_\ell^2) \zeta^4 - A_s \zeta^4(1-e^2)^{-1} + (A_{s s} a_\ell^2) \zeta^6(1-e^2)^{-1} \biggr]\chi^{-1} + \biggl[ - (A_{\ell s}a_\ell^2 )\zeta^2 - A_s \zeta^2 +(A_{s s} a_\ell^2) \zeta^4 + (A_{\ell s}a_\ell^2 )\zeta^4(1-e^2)^{-1} \biggr]\chi + \biggl[(A_{\ell s}a_\ell^2 )\zeta^2 \biggr]\chi^3 \biggr\} </math> </td> </tr> <tr> <td align="right"> <math> \Rightarrow ~~~ \frac{(1-e^2)P}{(2\pi G\rho_c^2 a_\ell^2)} </math> </td> <td align="center"> <math>\sim</math> </td> <td align="left"> <math> \biggl[A_s \zeta^2 -(A_{s s} a_\ell^2) \zeta^4 - A_s \zeta^4(1-e^2)^{-1} + (A_{s s} a_\ell^2) \zeta^6(1-e^2)^{-1} \biggr]\ln(\chi) + \frac{1}{2}\biggl[- (A_{\ell s}a_\ell^2 )\zeta^2- A_s \zeta^2+(A_{s s} a_\ell^2) \zeta^4+ (A_{\ell s}a_\ell^2 )\zeta^4(1-e^2)^{-1}\biggr]\chi^2 + \frac{1}{4}\biggl[(A_{\ell s}a_\ell^2 )\zeta^2 \biggr]\chi^4 \, . </math> </td> </tr> </table>
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