A description of the transport scheme used for the Clawpack results can be found here (claw_results.tex, claw_results.pdf).
3.000000 5.65839e-01 5.75607e-01 1.500000 4.04397e-01 4.81569e-01 0.750000 2.06064e-01 2.93164e-01 0.375000 6.94662e-02 1.07191e-01 0.187500 1.93500e-02 3.09628e-02 0.093750 5.72179e-03 8.81991e-03
3.000000 5.30073e-01 5.64210e-01 1.500000 2.77313e-01 3.24941e-01 0.750000 9.83552e-02 1.37264e-01 0.375000 2.47144e-02 4.40165e-02 0.187500 8.03807e-03 1.28511e-02 0.093750 3.58440e-03 4.14425e-03
Convergence rates for Gaussian hills
CLAW & 1.0 & 1.7 & 1.8 & 1.8 & 1.7
Note : We use N=320 for the minimal resolution in the shape preserving case, and N=480 in the unfiltered case.
3.000000 5.51596e-01 6.53696e-01 1.500000 4.78092e-01 5.42753e-01 0.750000 3.39679e-01 4.81308e-01 0.375000 1.55890e-01 2.38079e-01 0.187500 5.12136e-02 7.88296e-02 0.093750 1.56016e-02 2.60692e-02
3.000000 5.31379e-01 6.56001e-01 1.500000 3.89954e-01 4.75146e-01 0.750000 1.90717e-01 2.50207e-01 0.375000 5.01513e-02 8.24015e-02 0.187500 1.25366e-02 2.31665e-02 0.093750 4.85587e-03 6.93453e-03
CLAW & un & 1.0 & 0.1875^$\circ$ \\ CLAW & sp & 1.0 & 0.28125^\circ$ \\
Note : The N-effective we use in the unfiltered case is N=480, and in the shape preserving case is N=320.
0.10 69.08 0.15 155.64 0.20 135.93 0.25 132.98 0.30 118.31 0.35 106.99 0.40 94.87 0.45 77.20 0.50 57.69 0.55 40.12 0.60 14.24 0.65 1.76 0.70 0.00 0.75 0.00 0.80 0.00 0.85 0.00 0.90 0.00 0.95 0.00 1.00 0.00
0.10 63.72 0.15 173.44 0.20 143.94 0.25 138.31 0.30 126.64 0.35 119.49 0.40 106.43 0.45 94.95 0.50 73.88 0.55 63.46 0.60 45.10 0.65 26.17 0.70 12.94 0.75 0.00 0.80 0.00 0.85 0.00 0.90 0.00 0.95 0.00 1.00 0.00
0.10 79.46 0.15 115.79 0.20 110.92 0.25 108.87 0.30 106.87 0.35 105.50 0.40 101.53 0.45 100.62 0.50 94.76 0.55 89.70 0.60 84.71 0.65 78.14 0.70 68.98 0.75 57.87 0.80 38.84 0.85 10.16 0.90 0.00 0.95 0.00 1.00 0.00
0.10 62.77 0.15 126.66 0.20 117.73 0.25 114.21 0.30 111.26 0.35 109.00 0.40 104.79 0.45 102.59 0.50 101.40 0.55 93.65 0.60 88.36 0.65 84.24 0.70 75.25 0.75 64.41 0.80 50.00 0.85 30.03 0.90 7.98 0.95 0.00 1.00 0.00
0.10 89.61 0.15 101.40 0.20 100.77 0.25 100.15 0.30 100.01 0.35 100.11 0.40 100.25 0.45 100.21 0.50 99.83 0.55 99.58 0.60 99.33 0.65 98.34 0.70 98.50 0.75 98.60 0.80 97.67 0.85 96.40 0.90 90.33 0.95 68.18 1.00 0.00lf-CLAW-dx0.1875-un-CFL0.95.dat
0.10 77.30 0.15 102.15 0.20 100.58 0.25 100.14 0.30 99.75 0.35 99.39 0.40 99.47 0.45 99.42 0.50 99.34 0.55 99.19 0.60 99.44 0.65 99.39 0.70 99.50 0.75 99.54 0.80 99.66 0.85 100.18 0.90 99.36 0.95 97.78 1.00 0.00
Filament results
CLAW & 1.5$^\circ$ & 0.95 & 5.22$ \times 10^{-1}$ & 7.70$ \times 10^{-1}$ & 1.60$ \times 10^{-1}$ & -3.20$ \times 10^{-1}$ & 4.84$ \times 10^{-1}$ & 6.98$ \times 10^{-1}$ & -1.71$ \times 10^{-1}$ & -2.02$ \times 10^{-3}$ \\ % CLAW & 0.75$^\circ$ & 0.95 & 4.45$ \times 10^{-1}$ & 9.25$ \times 10^{-1}$ & 2.46$ \times 10^{-1}$ & -3.59$ \times 10^{-1}$ & 3.61$ \times 10^{-1}$ & 7.99$ \times 10^{-1}$ & 8.79$ \times 10^{-3}$ & -4.46$ \times 10^{-3}$ \\ % CLAW & 0.1875$^\circ$ & 0.95 & 2.73$ \times 10^{-1}$ & 9.86$ \times 10^{-1}$ & 3.48$ \times 10^{-1}$ & -3.65$ \times 10^{-1}$ & -- & -- & -- & -- \\ % CLAW & 0.28125$^\circ$ & 0.95 & -- & -- & -- & -- & 2.34$ \times 10^{-1}$ & 8.40$ \times 10^{-1}$ & 1.12$ \times 10^{-2}$ & -7.79$ \times 10^{-3}$ \\
Contour data for the rough distribution (slotted cylinder) can be found here.
CLAW & 1.5$^\circ$ & 1.0 & 6.87$\times 10^{-3}$ & 2.89$\times 10^{-4}$ & 7.60$\times 10^{-3}$ & 6.15$\times 10^{-3}$ & 2.78$\times 10^{-6}$ & 3.59$\times 10^{-5}$\\ % CLAW & 0.75$^\circ$ & 1.0 & 3.22$\times 10^{-3}$ & 5.28$\times 10^{-4}$ & 4.89$\times 10^{-4}$ & 2.31$\times 10^{-3}$ & 5.52$\times 10^{-6}$ & 3.53$\times 10^{-5}$\\ % CLAW & 0.1875$^ \circ$ & 1.0 & 4.58$\times 10^ {-4}$ & 2.73$\times 10^ {-4}$ & 4.74$\times 10^ {-4}$ & -- & -- & -- \\ % CLAW & 0.28125$^\circ$ & 1.0 & -- & -- & -- & 3.40$\times 10^ {-4}$ & 1.27$\times 10^ {-4}$ & 1.92$\times 10^ {-5}$\\
Mixing data for scatter plots, along with plots of mixing diagnostic can be found here
CLAW & 1.5$^\circ$ & 0.95 & 3.98$ \times 10^{-1}$ & 5.13$ \times 10^{-1}$ & -1.65$ \times 10^{-2}$ & -2.15$ \times 10^{-1}$ & 3.76$ \times 10^{-1}$ & 4.94$ \times 10^{-1}$ & -5.32$ \times 10^{-1}$ & -4.39$ \times 10^{-4}$ \\ % CLAW & 0.75$^\circ$ & 0.95 & 2.44$ \times 10^{-1}$ & 3.17$ \times 10^{-1}$ & -5.29$ \times 10^{-2}$ & -1.91$ \times 10^{-1}$ & 1.80$ \times 10^{-1}$ & 2.75$ \times 10^{-1}$ & -2.85$ \times 10^{-3}$ & -8.50$ \times 10^{-4}$ \\ % CLAW & 0.1875$^\circ$ & 0.95 & 3.03$ \times 10^{-2}$ & 4.49$ \times 10^{-2}$ & 2.82$ \times 10^{-3}$ & -4.05$ \times 10^{-2}$ & -- & -- & -- & -- \\ % CLAW & 0.28125$^\circ$ & 0.95 & -- & -- & -- & -- & 2.65$ \times 10^{-2}$ & 5.93$ \times 10^{-2}$ & -6.00$ \times 10^{-2}$ & -1.06$ \times 10^{-3}$ \\
Contour data for the cosine bells (divergent winds) can be found here.