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S8038 (13%) (s8038-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S8038 (13%) (s8038-il)
Reynolds number: 200,000
Max Cl/Cd: 52.86 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8038-il-200000-n5.txt
Download as CSV file: xf-s8038-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8038 (13%)                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.6993   0.10382   0.09961  -0.0275   1.0000   0.0149
 -14.250  -0.7310   0.09216   0.08783  -0.0346   1.0000   0.0147
 -14.000  -0.7612   0.08186   0.07735  -0.0413   1.0000   0.0145
 -13.750  -0.7869   0.07349   0.06879  -0.0468   1.0000   0.0145
 -13.500  -0.8075   0.06685   0.06197  -0.0507   1.0000   0.0144
 -13.250  -0.8242   0.06143   0.05637  -0.0535   1.0000   0.0143
 -13.000  -0.8436   0.05615   0.05085  -0.0557   1.0000   0.0144
 -12.750  -0.8579   0.05194   0.04642  -0.0567   1.0000   0.0144
 -12.500  -0.8693   0.04837   0.04264  -0.0569   1.0000   0.0145
 -12.250  -0.8798   0.04517   0.03920  -0.0563   1.0000   0.0146
 -12.000  -0.8855   0.04259   0.03642  -0.0552   1.0000   0.0146
 -11.750  -0.8918   0.04012   0.03370  -0.0534   1.0000   0.0148
 -11.500  -0.8938   0.03816   0.03154  -0.0513   1.0000   0.0149
 -11.250  -0.8949   0.03637   0.02954  -0.0488   1.0000   0.0150
 -11.000  -0.8936   0.03469   0.02772  -0.0460   1.0000   0.0152
 -10.750  -0.8906   0.03328   0.02624  -0.0432   1.0000   0.0154
 -10.500  -0.8867   0.03201   0.02489  -0.0402   1.0000   0.0156
 -10.250  -0.8799   0.03099   0.02383  -0.0376   1.0000   0.0160
 -10.000  -0.8707   0.02996   0.02270  -0.0352   1.0000   0.0165
  -9.750  -0.8606   0.02887   0.02152  -0.0329   1.0000   0.0170
  -9.500  -0.8493   0.02780   0.02033  -0.0306   1.0000   0.0175
  -9.250  -0.8373   0.02674   0.01916  -0.0283   1.0000   0.0179
  -9.000  -0.8250   0.02568   0.01800  -0.0260   1.0000   0.0182
  -8.750  -0.8124   0.02471   0.01693  -0.0237   1.0000   0.0186
  -8.500  -0.8004   0.02373   0.01588  -0.0212   1.0000   0.0190
  -8.250  -0.7891   0.02279   0.01493  -0.0187   1.0000   0.0194
  -8.000  -0.7766   0.02200   0.01412  -0.0163   1.0000   0.0200
  -7.750  -0.7638   0.02127   0.01335  -0.0140   1.0000   0.0206
  -7.500  -0.7507   0.02060   0.01263  -0.0116   1.0000   0.0212
  -7.250  -0.7375   0.01997   0.01195  -0.0092   1.0000   0.0221
  -7.000  -0.7095   0.01925   0.01115  -0.0098   0.9968   0.0238
  -6.750  -0.6770   0.01850   0.01038  -0.0114   0.9917   0.0257
  -6.500  -0.6447   0.01781   0.00961  -0.0127   0.9857   0.0283
  -6.250  -0.6144   0.01705   0.00883  -0.0137   0.9787   0.0321
  -6.000  -0.5829   0.01636   0.00813  -0.0149   0.9718   0.0393
  -5.500  -0.5246   0.01498   0.00696  -0.0162   0.9550   0.0796
  -5.250  -0.4947   0.01433   0.00646  -0.0170   0.9465   0.1116
  -5.000  -0.4651   0.01369   0.00601  -0.0178   0.9375   0.1523
  -4.750  -0.4333   0.01289   0.00556  -0.0191   0.9298   0.2218
  -4.500  -0.4039   0.01222   0.00517  -0.0199   0.9195   0.2872
  -4.250  -0.3715   0.01164   0.00483  -0.0211   0.9104   0.3488
  -4.000  -0.3399   0.01114   0.00456  -0.0221   0.8998   0.4102
  -3.750  -0.3087   0.01078   0.00435  -0.0227   0.8879   0.4611
  -3.500  -0.2767   0.01052   0.00420  -0.0235   0.8761   0.5064
  -3.250  -0.2444   0.01036   0.00408  -0.0242   0.8639   0.5445
  -3.000  -0.2133   0.01026   0.00397  -0.0247   0.8509   0.5721
  -2.750  -0.1840   0.01020   0.00387  -0.0247   0.8372   0.5941
  -2.500  -0.1557   0.01015   0.00379  -0.0245   0.8237   0.6138
  -2.250  -0.1279   0.01013   0.00372  -0.0243   0.8104   0.6314
  -2.000  -0.1002   0.01012   0.00365  -0.0240   0.7974   0.6459
  -1.750  -0.0729   0.01012   0.00358  -0.0236   0.7845   0.6591
  -1.500  -0.0461   0.01013   0.00353  -0.0232   0.7718   0.6722
  -1.250  -0.0198   0.01013   0.00350  -0.0226   0.7591   0.6846
  -1.000   0.0066   0.01013   0.00347  -0.0220   0.7470   0.6959
  -0.750   0.0331   0.01015   0.00344  -0.0215   0.7353   0.7066
  -0.500   0.0595   0.01017   0.00341  -0.0210   0.7238   0.7175
  -0.250   0.0856   0.01018   0.00341  -0.0204   0.7117   0.7277
   0.000   0.1116   0.01020   0.00341  -0.0199   0.6998   0.7380
   0.250   0.1377   0.01023   0.00341  -0.0193   0.6878   0.7481
   0.500   0.1638   0.01026   0.00341  -0.0187   0.6754   0.7574
   0.750   0.1895   0.01029   0.00341  -0.0181   0.6624   0.7678
   1.000   0.2154   0.01032   0.00344  -0.0175   0.6495   0.7775
   1.250   0.2411   0.01035   0.00347  -0.0168   0.6365   0.7875
   1.500   0.2666   0.01039   0.00349  -0.0162   0.6224   0.7981
   1.750   0.2922   0.01043   0.00352  -0.0155   0.6063   0.8077
   2.000   0.3173   0.01049   0.00356  -0.0147   0.5891   0.8182
   2.250   0.3425   0.01055   0.00360  -0.0140   0.5719   0.8295
   2.500   0.3684   0.01062   0.00366  -0.0134   0.5544   0.8405
   2.750   0.3943   0.01070   0.00373  -0.0129   0.5365   0.8523
   3.000   0.4207   0.01080   0.00381  -0.0124   0.5171   0.8652
   3.250   0.4482   0.01092   0.00391  -0.0122   0.4963   0.8787
   3.500   0.4770   0.01109   0.00404  -0.0124   0.4731   0.8925
   3.750   0.5081   0.01128   0.00418  -0.0130   0.4463   0.9058
   4.000   0.5406   0.01154   0.00436  -0.0140   0.4154   0.9189
   4.500   0.6071   0.01224   0.00480  -0.0167   0.3445   0.9439
   5.000   0.6733   0.01312   0.00539  -0.0196   0.2737   0.9674
   5.250   0.7049   0.01360   0.00573  -0.0208   0.2425   0.9798
   5.500   0.7368   0.01407   0.00610  -0.0221   0.2158   0.9919
   5.750   0.7686   0.01454   0.00647  -0.0235   0.1940   1.0000
   6.000   0.7839   0.01491   0.00677  -0.0213   0.1791   1.0000
   6.250   0.7998   0.01530   0.00709  -0.0193   0.1655   1.0000
   6.500   0.8163   0.01571   0.00746  -0.0173   0.1538   1.0000
   6.750   0.8337   0.01610   0.00782  -0.0155   0.1436   1.0000
   7.000   0.8506   0.01652   0.00822  -0.0136   0.1355   1.0000
   7.250   0.8675   0.01695   0.00864  -0.0118   0.1274   1.0000
   7.500   0.8845   0.01739   0.00909  -0.0100   0.1205   1.0000
   7.750   0.9014   0.01784   0.00954  -0.0081   0.1140   1.0000
   8.000   0.9177   0.01834   0.01003  -0.0062   0.1088   1.0000
   8.250   0.9349   0.01880   0.01054  -0.0045   0.1036   1.0000
   8.500   0.9505   0.01934   0.01107  -0.0026   0.0989   1.0000
   8.750   0.9664   0.01987   0.01162  -0.0007   0.0948   1.0000
   9.000   0.9829   0.02036   0.01218   0.0011   0.0906   1.0000
   9.250   0.9975   0.02093   0.01275   0.0030   0.0868   1.0000
   9.500   1.0094   0.02157   0.01340   0.0054   0.0835   1.0000
   9.750   1.0237   0.02209   0.01402   0.0075   0.0804   1.0000
  10.000   1.0369   0.02267   0.01466   0.0096   0.0773   1.0000
  10.250   1.0483   0.02335   0.01535   0.0119   0.0745   1.0000
  10.500   1.0578   0.02420   0.01619   0.0142   0.0721   1.0000
  10.750   1.0715   0.02486   0.01699   0.0160   0.0698   1.0000
  11.000   1.0839   0.02562   0.01784   0.0178   0.0674   1.0000
  11.250   1.0953   0.02643   0.01873   0.0196   0.0651   1.0000
  11.500   1.1048   0.02738   0.01971   0.0214   0.0628   1.0000
  11.750   1.1119   0.02857   0.02091   0.0233   0.0608   1.0000
  12.000   1.1235   0.02951   0.02200   0.0247   0.0590   1.0000
  12.250   1.1334   0.03061   0.02323   0.0260   0.0570   1.0000
  12.500   1.1421   0.03180   0.02452   0.0274   0.0553   1.0000
  12.750   1.1498   0.03311   0.02591   0.0285   0.0537   1.0000
  13.000   1.1555   0.03461   0.02746   0.0296   0.0522   1.0000
  13.250   1.1594   0.03636   0.02924   0.0307   0.0508   1.0000
  13.500   1.1667   0.03792   0.03097   0.0315   0.0495   1.0000
  13.750   1.1726   0.03964   0.03283   0.0321   0.0480   1.0000
  14.000   1.1772   0.04152   0.03484   0.0326   0.0466   1.0000
  14.250   1.1807   0.04354   0.03699   0.0330   0.0454   1.0000
  14.500   1.1832   0.04574   0.03928   0.0331   0.0444   1.0000
  14.750   1.1841   0.04814   0.04177   0.0331   0.0435   1.0000
  15.000   1.1838   0.05077   0.04446   0.0330   0.0427   1.0000
  15.250   1.1825   0.05360   0.04738   0.0327   0.0418   1.0000
  15.500   1.1813   0.05654   0.05050   0.0322   0.0411   1.0000
  15.750   1.1785   0.05980   0.05394   0.0315   0.0403   1.0000
  16.000   1.1743   0.06333   0.05762   0.0304   0.0395   1.0000
  16.250   1.1692   0.06710   0.06155   0.0292   0.0389   1.0000
  16.500   1.1629   0.07120   0.06580   0.0275   0.0382   1.0000
  16.750   1.1553   0.07564   0.07037   0.0257   0.0376   1.0000
  17.000   1.1472   0.08030   0.07516   0.0235   0.0370   1.0000
  17.250   1.1375   0.08537   0.08036   0.0210   0.0365   1.0000
  17.500   1.1266   0.09082   0.08594   0.0182   0.0361   1.0000
  17.750   1.1144   0.09664   0.09189   0.0151   0.0358   1.0000
  18.000   1.1013   0.10276   0.09812   0.0118   0.0354   1.0000
  18.250   1.0892   0.10882   0.10428   0.0085   0.0349   1.0000
  18.750   1.0465   0.12532   0.12106  -0.0010   0.0344   1.0000
  19.000   0.9565   0.15040   0.14647  -0.0162   0.0344   1.0000
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