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===Riemann-Derived Expressions=== <table border="0" cellpadding="10" align="right" width="30%"><tr><td align="center"> <table border="1" align="center" cellpadding="8"> <tr><td align="center"> ''Inertial Frame'' (green with subscript "0") <br />and ''Body Frame'' (black and unsubscripted). </td> </tr> <tr> <td align="center">[[File:InertialAxes05.png|400px|Inertial and Body Frames]]</td> </tr> <tr><td align="center"> For our chosen [[ThreeDimensionalConfigurations/RiemannTypeI#Case_I|Example Type I Ellipsoid]], we have, <math>~\Omega_2 = 0.3639</math> and <math>~\Omega_3 = 0.6633</math>, in which case, <math>~\Omega_0 = 0.7566</math> and <math>~\delta = 0.5018 ~\mathrm{rad} = 28.75^\circ</math>. </td> </tr> </table> </td></tr></table> The purple (ellipsoidal) configuration is spinning with frequency, <math>~\Omega_0</math> about the <math>~z_0</math>-axis of the "inertial frame," as illustrated; that is, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>~\boldsymbol\Omega</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~\boldsymbol{\hat{k}_0}\Omega_0 \, .</math> </td> </tr> </table> Also as illustrated, the "body frame," which is attached to and aligned with the principal axes of the purple ellipsoid, is tilted at an angle, <math>~\delta</math>, with respect to the inertial frame. Hence, as viewed from the ''body'' frame, we have, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>~\boldsymbol\Omega</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~\biggl[ \boldsymbol{\hat\jmath }\sin\delta + \boldsymbol{\hat{k} }\cos\delta \biggr]\Omega_0 \, .</math> </td> </tr> </table> Now, adhering to the notation used by [[Appendix/References#EFE|[<font color="red">EFE</font>] ]] — see, for example, the first paragraph of §51 (p. 156) — we should write, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>~\boldsymbol\Omega</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~\boldsymbol{\hat\jmath }\Omega_2 + \boldsymbol{\hat{k} }\Omega_3 ~~~~~\Rightarrow ~~~ \Omega_2 = \Omega_0\sin\delta </math> and, <math>~\Omega_3 = \Omega_0\cos\delta \, .</math> </td> </tr> </table> This means that, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>~\Omega_0</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~ \biggl[\Omega_2^2 + \Omega_3^2 \biggr]^{1 / 2} </math> and, <math>~\delta = \tan^{-1}\biggl[ \frac{\Omega_2}{\Omega_3} \biggr] \, .</math> </td> </tr> </table> As we have summarized in an [[ThreeDimensionalConfigurations/RiemannTypeI#EFEvelocities|accompanying discussion]] of Riemann Type 1 ellipsoids, [[Appendix/References#EFE|[<font color="red">EFE</font>] ]] provides an expression for the velocity vector of each fluid element, given its instantaneous ''body''-coordinate position (x, y, z) = (x<sub>1</sub>, x<sub>2</sub>, x<sub>3</sub>) — see his Eq. (154), Chapter 7, §51 (p. 156). As viewed from the rotating frame of reference, the three component expressions are, <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>~\dot{x} = u_1 = \boldsymbol{\hat\imath} \cdot \boldsymbol{u}</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~\biggl(\frac{a}{b}\biggr)^2 \gamma \Omega_3 y - \biggl(\frac{a}{c}\biggr)^2 \beta \Omega_2 z</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~- \biggl[ \frac{a^2}{a^2 + b^2} \biggr] \zeta_3 y + \biggl[ \frac{a^2}{a^2 + c^2} \biggr] \zeta_2 z \, ,</math> </td> </tr> <tr> <td align="right"> <math>~\dot{y} = u_2 = \boldsymbol{\hat\jmath} \cdot \boldsymbol{u}</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~- \gamma \Omega_3 x</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~+\biggl[ \frac{b^2}{a^2 + b^2} \biggr] \zeta_3 x \, ,</math> </td> </tr> <tr> <td align="right"> <math>~\dot{z} = u_3 = \boldsymbol{\hat{k}} \cdot \boldsymbol{u}</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~+ \beta \Omega_2 x</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~- \biggl[ \frac{c^2}{a^2 + c^2} \biggr] \zeta_2 x \, ,</math> </td> </tr> </table> <span id="betagamma">where,</span> <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>~\beta</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~ - \biggl[ \frac{c^2}{a^2 + c^2} \biggr] \frac{\zeta_2}{\Omega_2} </math> </td> <td align="center"> and, </td> <td align="right"> <math>~\gamma</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~ - \biggl[ \frac{b^2}{a^2 + b^2} \biggr] \frac{\zeta_3}{\Omega_3} \, . </math> </td> </tr> </table> <table border="1" cellpadding="8" width="90%" align="center"> <tr><td align="left" colspan="2"> <div align="center">'''Rotating-Frame Vorticity'''</div> </td> </tr> <tr> <td align="center"> <table border="0" cellpadding="5" align="center"> <tr> <td align="right"> <math>~\boldsymbol{\zeta} \equiv \boldsymbol{\nabla \times}\bold{u}</math> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~ \boldsymbol{\hat\imath} \biggl[ \frac{\partial \dot{z} }{\partial y} - \frac{\partial \dot{y}}{\partial z} \biggr] + \boldsymbol{\hat\jmath} \biggl[ \frac{\partial \dot{x}}{\partial z} - \frac{\partial \dot{z}}{\partial x} \biggr] + \bold{\hat{k}} \biggl[ \frac{\partial \dot{y}}{\partial x} - \frac{\partial \dot{x}}{\partial y} \biggr] </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~ \boldsymbol{\hat\jmath} \biggl\{ \biggl[ \frac{a^2}{a^2 + c^2} \biggr] \zeta_2 + \biggl[ \frac{c^2}{a^2 + c^2} \biggr] \zeta_2 \biggr\} + \bold{\hat{k}} \biggl\{ \biggl[ \frac{b^2}{a^2 + b^2} \biggr] \zeta_3 + \biggl[ \frac{a^2}{a^2 + b^2} \biggr] \zeta_3 \biggr\} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"> <math>~=</math> </td> <td align="left"> <math>~ \boldsymbol{\hat\jmath} ~\zeta_2 + \bold{\hat{k}} ~\zeta_3 \, . </math> </td> </tr> </table> For our chosen [[ThreeDimensionalConfigurations/RiemannTypeI#Case_I|Example Type I Ellipsoid]], we have, <math>~\zeta_2 = -2.2794</math> and <math>~\Omega_3 = -1.9637</math>, in which case, <math>~\zeta_\mathrm{rot} = (\zeta_2^2 + \zeta_3^2)^{1 / 2} = 2.2794</math> and <math>~\xi \equiv \tan^{-1}[\zeta_2/\zeta_3] = 4.0013 ~\mathrm{rad} = 229.26^\circ</math>. </td> <td align="center"> [[File:VorticityAxis04.png|350px|center|Vorticity Axis]] </td> </tr> </table>
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