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Compressible Orszag-Tang Vortex

The Orszag-Tang vortex is an initial value problem in a square periodic domain (length L). It has been investigated by [66] and [64] amongst others . It demonstrates that turbulent scales can result from a coherent initial condition with only two spatial frequencies.

The initial conditions we used were:

where C fixes the initial background mach speed and p is the instantaneous pressure for the equivalent incompressible flow. A summary of the simulation parameters is given in table 8.2, and figure 8.3 shows the mesh used for this case.


  
Figure 8.3: Mesh used for the compressible Orszag-Tang vortex simulations on a structured mesh.
\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Eps/8x8.quadmesh.eps,width=4.00in}
}\end{figure}


 
Table 8.2: Simulation parameters for the compressible Orszag-Tang Vortex.
Parameter Value
Dimension 2d
Sv 100
Sr 100
A (Alfven Number) 1.
Mach 0.5
N 19
KQuad 64
Method Discontinuous Galerkin

In figure 8.4 we show iso-contours of the conserved variables at t=1. We see that using an expansion order of nineteen shows very smooth and symmetric fields.


\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 ...cew/Thesis/Figures1/Eps/tang.comp.m0.5.energy_t1.eps,width=3.00in}
}\end{figure}

\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 .../tcew/Thesis/Figures1/Eps/tang.comp.m0.5.ymom_t1.eps,width=3.00in}
}\end{figure}

  
Figure 8.4: Compressible Orszag-Tang Vortex (t=1, instantaneous fields, Mach=0.5). Top left: density, Top right: energy, Middle left: x-component of momentum, Middle right: y-component of momentum, Bottom left: x component of magnetic field, Bottom right: y component of magnetic field.
\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 .../tcew/Thesis/Figures1/Eps/tang.comp.m0.5.ymag_t1.eps,width=3.00in}
}\end{figure}


\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 ...cew/Thesis/Figures1/Eps/tang.comp.m0.5.divmom_t1.eps,width=3.00in}
}\end{figure}

\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 ...cew/Thesis/Figures1/Eps/tang.comp.m0.5.divmag_t1.eps,width=3.00in}
}\end{figure}

 
Figure 8.5: Compressible Orszag-Tang Vortex (t=1, instantaneous fields, Mach=0.5). Top left: curl of momentum, Top right: divergence of momentum, Middle left: curl of magnetic field, Middle right: divergence of magnetic field, Bottom left: momentum streamlines, Bottom right: magnetic field streamlines.
\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 ...Thesis/Figures1/Eps/tang.comp.m0.5.magstreams_t1.eps,width=3.00in}
}\end{figure}

We now consider the effect of expansion order and using an unstructured grid on accuracy. Vorticity is a good indicator of noise in the solution of unsteady simulations. Low resolution will show up as non-smoothness in vorticity since it is the derivative of the computed fields. In figure 8.7 we compare the vorticity at time t=1 for a 132 triangle mesh (shown in figure 8.6) run with N=4 and N=6. The top figures show how the vorticity varies across the lower-left to top-right diagonal. The vorticity in this direction should be symmetric about the mid-point. We see that at N=4 the profile is noisy, the peeks are not well resolved and the symmetry is not very well represented. At N=6 the symmetry is better but the profile is still quite noisy. In the next figure 8.8 we see at N=10 that the symmetry is very good but the slopes are still a little rough. Finally, at N=16 we see that the symmetry is perfect and the profile is very smooth. We also see that the smoothness of the iso-contours improve with each increase in expansion order.


  
Figure 8.6: Compressible Orszag-Tang vortex triangle mesh with K=132.
\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Eps/tang.comp.tri.mesh.eps,width=4.50in}
}\end{figure}


\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 ...igures1/Eps/tang.comp.vort.extr.n7.eps,height=1.80in,width=3.00in}
}\end{figure}

  
Figure 8.7: Compressible Orszag-Tang Vortex (t=1, instantaneous fields, Mach=0.2, K=132). Top Left: Curl of momentum along the diagonal(N=4), Botton Left: Iso-contours of curl of momentum(N=4), Top Right: Curl of momentum along the diagonal(N=6), Bottom Right: Iso-contours of curl of momentum(N=6)
\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 ...nch7/tcew/Thesis/Figures1/Eps/tang.comp.vort.n7.eps,width=3.00in}
}.\end{figure}


\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 ...gures1/Eps/tang.comp.vort.extr.n17.eps,height=1.80in,width=3.00in}
}\end{figure}

  
Figure 8.8: Compressible Orszag-Tang Vortex (t=1, instantaneous fields, Mach=0.2, K=132). Top Left: Curl of momentum along the diagonal(N=10), Botton Left: Iso-contours of curl of momentum(N=10), Top Right: Curl of momentum along the diagonal(N=16), Bottom Right: Iso-contours of curl of momentum(N=16)
\begin{figure}
\centerline{
\psfig {file=/crunch/crunch7/tcew/Thesis/Figures1/Ep...
 ...nch7/tcew/Thesis/Figures1/Eps/tang.comp.vort.n17.eps,width=3.00in}
}\end{figure}


next up previous contents
Next: Flow Past a Cylinder Up: Compressible Viscous Magnetohydrodynamics Simulations Previous: Three-Dimensional Magnetohydrostatic Example
T. Warburton
10/24/1998