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Next: Appendix C: The homogeneous Up: Alkhalifah: TI traveltimes in Previous: Appendix A: Expansion in

Appendix B: Expansion in $\theta $ and $\eta $

For an expansion in $\theta $ and $\eta $, simultaneously, I use the following trial solution:

\begin{displaymath}
\tau(x,z) \approx \tau_{0}(x,z) +\tau_{\eta}(x,z) \eta+\tau...
...ta}(x,z) \eta \sin\theta+ \tau_{\theta_2}(x,z) \sin^{2}\theta,
\end{displaymath} (30)

in terms of the coefficients $\tau_{i}$, where the $i$ corresponds to $\eta,\theta,\eta_2,\eta \theta$, and $\theta_2$. Inserting the trial solution, equation B-1, into equation A-1 yields again a long formula, but by setting both $\sin\theta=0$ and $\eta=0$, I obtain the zeroth-order term given by
\begin{displaymath}
v^2(x,y,z) \left(\frac{\partial \tau_{0}}{\partial x}\right)...
...,z) \left(\frac{\partial \tau_{0}}{\partial z}\right)^2 = 1\;,
\end{displaymath} (31)

which is simply the eikonal formula for elliptical anisotropy. By equating the coefficients of the powers of the independent parameter $\sin\theta$ and $\eta $, in succession starting with first powers of the two parameters, we end up first with the coefficients of first-power in $\sin\theta$ and zeroth power in $\eta $, simplified by using equation B-2, and given by
\begin{displaymath}
v^2 \frac{\partial \tau_{0}}{\partial x} \frac{\partial \ta...
...l \tau_{0}}{\partial x} \frac{\partial \tau_{0}}{\partial
z},
\end{displaymath} (32)

which is a first-order linear partial differential equation in $\tau_{\theta}$. The coefficients of zero-power in $\sin\theta$ and the first-power in $\eta $ is given by
\begin{displaymath}
v^2
\frac{\partial \tau_{0}}{\partial x} \frac{\partial \ta...
...2
\left(\frac{\partial \tau_{0}}{\partial z}\right)^2\right),
\end{displaymath} (33)

The coefficients of the square terms in $\sin\theta$, with some manipulation, results in the following relation
$\displaystyle 2 v^2 \frac{\partial \tau _{0}}{\partial x}
\frac{\partial \tau ...
...al
x}\right)^2-v^2 \left(\frac{\partial \tau _{\theta}}{\partial
x}\right)^2-$      
$\displaystyle 2 \left(v^{2}-v_t^{2}\right)
\frac{\partial \tau _{\theta}}{\par...
...ac{\partial \tau _{0}}{\partial x} \frac{\partial
\tau _{\theta}}{\partial z}-$      
$\displaystyle v_t^2 \left(\frac{\partial \tau _{0}}{\partial
x}\right)^2-v_t^2...
...ft(v^{2}-v_t^{2}\right)
\left(\frac{\partial \tau _{0}}{\partial
z}\right)^2,$     (34)

which is again a first-order linear partial differential equation in $\tau_{\theta_2}$ with an obviously more complicated source function given by the right hand side. The coefficients of the square terms in $\eta $, with also some manipulation, results in the following relation
$\displaystyle 2 v^2 \frac{\partial \tau _{0}}{\partial x} \frac{\partial \tau
...
...artial \tau _{0}}{\partial
x} \frac{\partial \tau _{\eta}}{\partial z}\right)-$      
$\displaystyle v^2
\left(\frac{\partial \tau _{\eta}}{\partial x}\right)^2- 4 v...
...}}{\partial
x}-v_t^2 \left(\frac{\partial \tau _{\eta}}{\partial
z}\right)^2,$     (35)

which is again a first-order linear partial differential equation in $\tau_{\eta_2}$ with a again complicated source function.

Finally, the coefficients of the first-power terms in both $\sin\theta$ and $\eta $ results also in a first-order linear partial differential equation in $\tau_{\eta \theta}$ given by

    $\displaystyle 2 v^2 \frac{\partial
\tau _{0}}{\partial x} \frac{\partial \tau ...
...rtial \tau _{0}}{\partial z} \frac{\partial \tau
_{\eta \theta}}{\partial z} =$  
    $\displaystyle 4 v_t^2 v^2 \frac{\partial \tau _{0}}{\partial x} \frac{\partial ...
...tau _{\theta}}{\partial z}-\frac{\partial \tau
_{0}}{\partial x}\right)\right)$  
    $\displaystyle -2 v^2 \frac{\partial \tau _{0}}{\partial
x} \frac{\partial \tau...
...rtial \tau _{\theta}}{\partial
x}+\frac{\partial \tau _{0}}{\partial z}\right)$  
    $\displaystyle +2 v_t^2
\frac{\partial \tau _{\eta}}{\partial x} \frac{\partial...
...tial
\tau _{\theta}}{\partial z}-\frac{\partial \tau _{0}}{\partial x}\right).$ (36)

Though the equation seems complicated, many of the variables of the source function (right hand side) can be evaluated during the evaluation of equations B-3 and B-4 in a fashion that will not add much to the cost.

Using Shanks transforms (Bender and Orszag, 1978) we can isolate and remove the most transient behavior of the expansion B-1 in $\eta $ (the $\theta $ expansion did not improve with such a treatment) by first defining the following parameters:

$\displaystyle A_0$ $\textstyle =$ $\displaystyle \tau_{0}+ \tau_{\theta} \sin\theta+ \tau_{\theta_2} \sin^{2}\theta$  
$\displaystyle A_1$ $\textstyle =$ $\displaystyle A_{0} + \left(\tau_{\eta}+ \tau_{\eta \theta} \sin\theta \right) \eta$  
$\displaystyle A_2$ $\textstyle =$ $\displaystyle A_{1} + \tau_{\eta_2} \eta^2$ (37)

The first sequence of Shanks transforms uses $A_0$, $A_1$, and $A_2$, and thus, is given by
$\displaystyle \tau(x,z) \approx \frac{A_0 A_2-A_1^2}{A_0-2 A_1+A_2} = \tau_{0}(x,z)+ \tau_{\theta}(x,z) \sin\theta+ \tau_{\theta_2}(x,z) \sin^{2}\theta$      
$\displaystyle +\frac{\eta \left(\tau_{\eta}(x,z)+ \tau_{\eta \theta}(x,z) \sin\...
...tau_{\eta}(x,z)+ \tau_{\eta \theta}(x,z) \sin\theta -\eta \tau _{\eta_2}(x,z)}.$     (38)


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Next: Appendix C: The homogeneous Up: Alkhalifah: TI traveltimes in Previous: Appendix A: Expansion in

2013-04-02