Editing
Appendix/Ramblings/HybridSchemeOld
(section)
Jump to navigation
Jump to search
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
===An Element of the Hybrid Scheme=== This last equation displays one subtle, but valuable, element of the hybrid scheme developed by [http://adsabs.harvard.edu/abs/2010CQGra..27q5002C Call, Tohline, & Lehner (2010)]. The velocity component, <math>~v_\phi</math>, that appears in the formulation of the relevant conserved quantity — the inertial-frame angular momentum density — is drawn from the velocity vector, <math>~\vec{v}</math>, which is different from the transport velocity vector, <math>~\vec{u}</math>, that defines the Eulerian frame from which the dynamical evolution of the system is being viewed. This equation is usually written, instead, in a form such that the angular momentum density is expressed in terms of the azimuthal component of the transport velocity; see, for example, equation (7) in [http://adsabs.harvard.edu/abs/1978ApJ...224..497N Norman & Wilson (1978)] and equation (12) in [http://adsabs.harvard.edu/abs/1997ApJ...490..311N New & Tohline (1997)]. In this more familiar formulation, the momentum density and the transport velocity both directly refer to the same frame of reference. But, as a consequence, the source term is more complicated. The more familiar formulation — including its modified source term — can be derived from our "hybrid" formulation by recognizing that, <div align="center"> <table border="0" cellpadding="3"> <tr> <td align="right"> <math> ~v_\phi </math> </td> <td align="center"> <math>~=~</math> </td> <td align="left"> <math> ~u_\phi + \varpi\Omega_0 \, . </math> </td> </tr> </table> </div> So we can write, <div align="center"> <table border="0" cellpadding="3"> <tr> <td align="right"> <math> \frac{\partial [\rho \varpi (u_\phi + \varpi\Omega_0 ) ]}{\partial t} + \nabla\cdot \{[\rho \varpi ( u_\phi + \varpi\Omega_0)] \vec{u} \} </math> </td> <td align="center"> <math>~=~</math> </td> <td align="left"> <math> ~S_{\phi i} \, , </math> </td> </tr> </table> </div> where, as shorthand, we have used, <div align="center"> <table border="0" cellpadding="3"> <tr> <td align="right"> <math> ~S_{\phi i} </math> </td> <td align="center"> <math>~\equiv~</math> </td> <td align="left"> <math> - \frac{\partial P}{\partial\phi} - \rho \frac{\partial \Phi}{\partial\phi} \, . </math> </td> </tr> </table> </div> This implies, <div align="center"> <table border="0" cellpadding="3"> <tr> <td align="right"> <math> \frac{\partial (\rho \varpi u_\phi )}{\partial t} + \nabla\cdot [ (\rho \varpi u_\phi) \vec{u} ] </math> </td> <td align="center"> <math>~=~</math> </td> <td align="left"> <math> S_{\phi i} - \frac{\partial [\rho \varpi (\varpi\Omega_0 ) ]}{\partial t} - \nabla\cdot \{[\rho \varpi (\varpi\Omega_0)] \vec{u} \} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>~=~</math> </td> <td align="left"> <math> S_{\phi i} - \varpi^2\Omega_0 \biggl\{ \frac{\partial \rho}{\partial t} + \nabla\cdot (\rho \vec{u} ) \biggr\} - \rho \vec{u}\cdot \nabla(\varpi^2 \Omega_0) </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>~=~</math> </td> <td align="left"> <math> S_{\phi i} - 2\rho \varpi u_\varpi \Omega_0 \, . </math> </td> </tr> </table> </div> As we see, all terms involving the velocity now explicitly refer to <math>~\vec{u}</math> and, hence, to the velocity as measured in the rotating reference frame. But the source now includes a Coriolis term. This corresponds the scalar equation and representation referred to as "Case B (<math>~\eta=3'</math>)" in [http://adsabs.harvard.edu/abs/2010CQGra..27q5002C CTL (2010)]. <div align="center"> <table border="1" cellpadding="5" width="100%"> <tr> <td align="center" colspan="2"> From Tables 6.1 & 6.2 of [http://adsabs.harvard.edu/abs/2010CQGra..27q5002C Call, Tohline, & Lehner (2010)] <br> '''Case B''' <math>~(\eta = 3')</math> <br> as before: <math>~(\rho h)_\mathrm{CTL} \rightarrow \rho</math> ; <math>~(R)_\mathrm{CTL} \rightarrow \varpi</math> ; <math>~(R u^\phi)_\mathrm{CTL} \rightarrow \varpi\dot\phi = v_\phi</math> <br>additional replacements: <math>~(\bar\omega u^{t'})_\mathrm{CTL} \rightarrow \Omega_0</math> ; <math>~u^R \rightarrow v_\varpi = u_\varpi</math> </td> </tr> <tr> <td align="center"> <math>~\psi_{(3')}</math> </td> <td align="center"> <math>~S_{(3')}</math> </td> </tr> <tr> <td align="center"> <math>~\rho \varpi (v_\phi - \varpi\Omega_0) = \rho \varpi u_\phi </math> </td> <td align="center"> <math>~ - \frac{\partial P}{\partial\phi} - \rho \frac{\partial \Phi}{\partial\phi} - 2\rho\varpi u_\varpi \Omega_0</math> </td> </tr> </table> </div>
Summary:
Please note that all contributions to JETohlineWiki may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see
JETohlineWiki:Copyrights
for details).
Do not submit copyrighted work without permission!
Cancel
Editing help
(opens in new window)
Navigation menu
Personal tools
Not logged in
Talk
Contributions
Log in
Namespaces
Page
Discussion
English
Views
Read
Edit
View history
More
Search
Navigation
Main page
Tiled Menu
Table of Contents
Old (VisTrails) Cover
Appendices
Variables & Parameters
Key Equations
Special Functions
Permissions
Formats
References
lsuPhys
Ramblings
Uploaded Images
Originals
Recent changes
Random page
Help about MediaWiki
Tools
What links here
Related changes
Special pages
Page information