# Title
RG 15A-1.8/11.0 airfoil
#
# Grid file
rg15a.grd
#
# Topology file
rg15a.top
#
# Plot file
plot_rg.v2d
#
 161      # no. of cells around airfoil (new point distribution)
 48       # no. of cells in wake
 48       # no. of cells in normal direction
 20.0     # distance to farfield
 0.005    # leading edge spacing in wall-normal direction
 0.010    # trailing edge spacing in x-(i-)direction
 0.010    # trailing edge spacing in wall-normal direction
 0.20     # spacing at wake exit in y-(j-)direction
 30       # Laplace grid: <0 - only Laplace / =0 - only elliptic / >0 - both
 70       # max. no. of grid smoothing iterations (if above >= 0)
 20       # max. no. of Gauss-Seidel iterations
 0.15     # spacing damping factor (0.-0.5)
 1.0      # decay of given spacing from boundary into field (1.0-10.0)
 0.15     # angle damping factor (0.-0.5)
 1.0      # decay of given angles from boundary into field (1.0-10.0)
 1.8      # overrelaxation factor (1.0-2.0)
 141      # no. of x-, y-coordinates; airfoil must be scaled to 0 <= x <= 1
 1.000000     0.000000
 0.988176     0.000422
 0.969996     0.000465
 0.951211     0.000167
 0.931896    -0.000380
 0.912132    -0.001145
 0.892004    -0.002109
 0.871562    -0.003260
 0.850848    -0.004571
 0.829917    -0.006021
 0.808802    -0.007598
 0.787517    -0.009284
 0.766088    -0.011057
 0.744544    -0.012902
 0.722903    -0.014804
 0.701187    -0.016743
 0.679444    -0.018695
 0.657744    -0.020633
 0.636149    -0.022531
 0.614700    -0.024355
 0.593394    -0.026064
 0.572190    -0.027630
 0.551031    -0.029046
 0.529859    -0.030311
 0.508626    -0.031442
 0.487320    -0.032463
 0.465959    -0.033391
 0.444573    -0.034233
 0.423193    -0.034994
 0.401848    -0.035667
 0.380551    -0.036246
 0.359319    -0.036729
 0.338190    -0.037119
 0.317219    -0.037409
 0.296465    -0.037591
 0.275994    -0.037659
 0.255901    -0.037610
 0.236311    -0.037442
 0.217367    -0.037149
 0.199216    -0.036731
 0.182004    -0.036193
 0.165862    -0.035548
 0.150878    -0.034807
 0.137096    -0.033988
 0.124501    -0.033106
 0.113045    -0.032178
 0.102646    -0.031217
 0.093209    -0.030230
 0.084634    -0.029222
 0.076825    -0.028200
 0.069694    -0.027165
 0.063160    -0.026122
 0.057151    -0.025071
 0.051604    -0.024011
 0.046464    -0.022940
 0.041688    -0.021860
 0.037239    -0.020768
 0.033094    -0.019653
 0.029233    -0.018502
 0.025631    -0.017309
 0.022266    -0.016071
 0.019099    -0.014798
 0.016096    -0.013502
 0.013233    -0.012196
 0.010509    -0.010874
 0.007994    -0.009481
 0.005753    -0.007958
 0.003832    -0.006260
 0.002251    -0.004362
 0.000999    -0.002301
 0.000000     0.000000
 0.000182     0.001283
 0.000435     0.002532
 0.001181     0.004995
 0.002271     0.007387
 0.003726     0.009704
 0.005522     0.011953
 0.007616     0.014143
 0.009950     0.016281
 0.012489     0.018377
 0.015243     0.020437
 0.018223     0.022475
 0.021442     0.024506
 0.024916     0.026545
 0.028667     0.028592
 0.032721     0.030645
 0.037104     0.032706
 0.041849     0.034775
 0.046998     0.036857
 0.052600     0.038958
 0.058705     0.041091
 0.065375     0.043262
 0.072679     0.045470
 0.080695     0.047709
 0.089508     0.049974
 0.099211     0.052257
 0.109896     0.054544
 0.121643     0.056820
 0.134514     0.059057
 0.148538     0.061227
 0.163706     0.063294
 0.179968     0.065217
 0.197231     0.066962
 0.215383     0.068497
 0.234296     0.069801
 0.253847     0.070864
 0.273915     0.071682
 0.294392     0.072255
 0.315196     0.072583
 0.336270     0.072674
 0.357561     0.072540
 0.379022     0.072190
 0.400617     0.071630
 0.422329     0.070870
 0.444145     0.069919
 0.466041     0.068791
 0.487995     0.067490
 0.509993     0.066020
 0.532033     0.064384
 0.554113     0.062586
 0.576236     0.060631
 0.598403     0.058528
 0.620610     0.056283
 0.642853     0.053904
 0.665124     0.051398
 0.687417     0.048769
 0.709732     0.046022
 0.732067     0.043164
 0.754407     0.040207
 0.776723     0.037155
 0.798998     0.034010
 0.821217     0.030777
 0.843335     0.027472
 0.865282     0.024103
 0.886985     0.020673
 0.908349     0.017199
 0.929233     0.013695
 0.949455     0.010132
 0.968928     0.006371
 0.987739     0.002393
 1.000000     0.000000
