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S1012 (s1012-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: S1012 (s1012-il)
Reynolds number: 500,000
Max Cl/Cd: 53.5 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1012-il-500000.txt
Download as CSV file: xf-s1012-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1012                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.9917   0.11846   0.11553  -0.0108   1.0000   0.0197
 -18.000  -1.0230   0.10720   0.10409  -0.0180   1.0000   0.0196
 -17.750  -1.0500   0.09740   0.09412  -0.0242   1.0000   0.0196
 -17.500  -1.0740   0.08840   0.08494  -0.0300   1.0000   0.0196
 -17.250  -1.0990   0.07974   0.07609  -0.0354   1.0000   0.0197
 -17.000  -1.1188   0.07241   0.06859  -0.0398   1.0000   0.0197
 -16.750  -1.1383   0.06563   0.06163  -0.0435   1.0000   0.0198
 -16.500  -1.1521   0.06018   0.05603  -0.0462   1.0000   0.0200
 -16.250  -1.1642   0.05534   0.05106  -0.0481   1.0000   0.0202
 -16.000  -1.1721   0.05143   0.04703  -0.0493   1.0000   0.0205
 -15.750  -1.1765   0.04822   0.04374  -0.0500   1.0000   0.0208
 -15.500  -1.1780   0.04553   0.04097  -0.0502   1.0000   0.0211
 -15.250  -1.1791   0.04302   0.03836  -0.0501   1.0000   0.0214
 -15.000  -1.1780   0.04087   0.03612  -0.0497   1.0000   0.0219
 -14.750  -1.1777   0.03870   0.03382  -0.0490   1.0000   0.0223
 -14.500  -1.1745   0.03687   0.03188  -0.0482   1.0000   0.0228
 -14.250  -1.1708   0.03514   0.03002  -0.0471   1.0000   0.0232
 -14.000  -1.1655   0.03359   0.02834  -0.0460   1.0000   0.0236
 -13.750  -1.1582   0.03226   0.02686  -0.0447   1.0000   0.0240
 -13.500  -1.1591   0.03003   0.02453  -0.0428   1.0000   0.0247
 -13.250  -1.1530   0.02862   0.02308  -0.0413   1.0000   0.0255
 -13.000  -1.1432   0.02756   0.02196  -0.0399   1.0000   0.0260
 -12.750  -1.1323   0.02658   0.02093  -0.0385   1.0000   0.0268
 -12.500  -1.1198   0.02574   0.02002  -0.0371   1.0000   0.0277
 -12.250  -1.1067   0.02490   0.01908  -0.0357   1.0000   0.0286
 -12.000  -1.0924   0.02416   0.01822  -0.0344   1.0000   0.0292
 -11.750  -1.0849   0.02273   0.01674  -0.0323   1.0000   0.0304
 -11.500  -1.0717   0.02192   0.01592  -0.0307   1.0000   0.0315
 -11.250  -1.0562   0.02129   0.01526  -0.0294   1.0000   0.0327
 -11.000  -1.0397   0.02071   0.01462  -0.0281   1.0000   0.0342
 -10.750  -1.0215   0.02028   0.01411  -0.0269   1.0000   0.0354
 -10.500  -1.0116   0.01932   0.01314  -0.0247   1.0000   0.0373
 -10.250  -0.9811   0.01870   0.01252  -0.0262   0.9844   0.0396
 -10.000  -0.9488   0.01817   0.01192  -0.0278   0.9743   0.0420
  -9.750  -0.9214   0.01736   0.01104  -0.0286   0.9643   0.0446
  -9.500  -0.8967   0.01686   0.01052  -0.0286   0.9550   0.0472
  -9.250  -0.8749   0.01656   0.01016  -0.0278   0.9462   0.0498
  -9.000  -0.8543   0.01622   0.00972  -0.0267   0.9394   0.0521
  -8.750  -0.8367   0.01564   0.00916  -0.0252   0.9328   0.0553
  -8.500  -0.8156   0.01536   0.00882  -0.0242   0.9278   0.0582
  -8.250  -0.7928   0.01514   0.00853  -0.0234   0.9235   0.0608
  -8.000  -0.7735   0.01460   0.00799  -0.0221   0.9188   0.0648
  -7.750  -0.7511   0.01432   0.00770  -0.0213   0.9151   0.0686
  -7.500  -0.7274   0.01415   0.00745  -0.0206   0.9121   0.0719
  -7.250  -0.7065   0.01368   0.00701  -0.0196   0.9091   0.0769
  -7.000  -0.6824   0.01342   0.00675  -0.0192   0.9063   0.0817
  -6.750  -0.6585   0.01316   0.00644  -0.0186   0.9036   0.0862
  -6.500  -0.6358   0.01281   0.00613  -0.0179   0.9010   0.0926
  -6.250  -0.6107   0.01265   0.00592  -0.0174   0.8988   0.0978
  -6.000  -0.5886   0.01229   0.00562  -0.0165   0.8964   0.1060
  -5.750  -0.5639   0.01209   0.00539  -0.0161   0.8942   0.1136
  -5.500  -0.5394   0.01181   0.00517  -0.0156   0.8921   0.1236
  -5.250  -0.5149   0.01154   0.00496  -0.0152   0.8900   0.1344
  -5.000  -0.4902   0.01130   0.00477  -0.0148   0.8880   0.1475
  -4.750  -0.4657   0.01105   0.00458  -0.0143   0.8861   0.1634
  -4.500  -0.4413   0.01080   0.00441  -0.0138   0.8841   0.1827
  -4.250  -0.4175   0.01052   0.00424  -0.0132   0.8822   0.2077
  -4.000  -0.3941   0.01022   0.00409  -0.0126   0.8805   0.2421
  -3.750  -0.3711   0.00989   0.00395  -0.0119   0.8789   0.2877
  -3.500  -0.3490   0.00944   0.00379  -0.0112   0.8768   0.3509
  -3.250  -0.3291   0.00889   0.00361  -0.0100   0.8744   0.4366
  -3.000  -0.3113   0.00824   0.00343  -0.0084   0.8721   0.5426
  -2.750  -0.2943   0.00770   0.00347  -0.0062   0.8697   0.6689
  -2.500  -0.2690   0.00776   0.00366  -0.0054   0.8679   0.7240
  -2.250  -0.2419   0.00786   0.00376  -0.0050   0.8662   0.7456
  -2.000  -0.2148   0.00800   0.00389  -0.0046   0.8645   0.7611
  -1.750  -0.1873   0.00813   0.00401  -0.0044   0.8625   0.7728
  -1.500  -0.1598   0.00825   0.00412  -0.0042   0.8600   0.7833
  -1.250  -0.1321   0.00832   0.00422  -0.0040   0.8568   0.7904
  -1.000  -0.1053   0.00836   0.00422  -0.0034   0.8524   0.7983
  -0.750  -0.0793   0.00834   0.00418  -0.0024   0.8456   0.8046
  -0.500  -0.0535   0.00822   0.00404  -0.0013   0.8356   0.8106
  -0.250  -0.0272   0.00819   0.00395  -0.0006   0.8279   0.8167
   0.000   0.0000   0.00816   0.00396   0.0000   0.8217   0.8217
   0.250   0.0272   0.00819   0.00396   0.0006   0.8168   0.8279
   0.500   0.0535   0.00822   0.00404   0.0013   0.8106   0.8356
   0.750   0.0793   0.00833   0.00418   0.0024   0.8045   0.8456
   1.000   0.1054   0.00836   0.00422   0.0034   0.7984   0.8524
   1.250   0.1321   0.00833   0.00422   0.0040   0.7905   0.8568
   1.500   0.1598   0.00825   0.00412   0.0042   0.7833   0.8600
   1.750   0.1872   0.00813   0.00401   0.0044   0.7728   0.8625
   2.000   0.2147   0.00800   0.00388   0.0046   0.7609   0.8645
   2.250   0.2419   0.00786   0.00376   0.0050   0.7457   0.8662
   2.500   0.2690   0.00776   0.00366   0.0054   0.7240   0.8679
   2.750   0.2944   0.00770   0.00347   0.0062   0.6701   0.8697
   3.000   0.3113   0.00824   0.00343   0.0084   0.5431   0.8721
   3.250   0.3290   0.00889   0.00361   0.0100   0.4363   0.8744
   3.500   0.3490   0.00944   0.00379   0.0112   0.3502   0.8768
   3.750   0.3711   0.00988   0.00395   0.0119   0.2878   0.8789
   4.000   0.3941   0.01022   0.00409   0.0126   0.2423   0.8805
   4.250   0.4175   0.01052   0.00424   0.0132   0.2078   0.8822
   4.500   0.4413   0.01080   0.00441   0.0138   0.1827   0.8841
   4.750   0.4657   0.01105   0.00458   0.0143   0.1633   0.8861
   5.000   0.4902   0.01130   0.00477   0.0148   0.1474   0.8880
   5.250   0.5149   0.01154   0.00496   0.0152   0.1344   0.8900
   5.500   0.5394   0.01181   0.00517   0.0156   0.1235   0.8921
   5.750   0.5639   0.01209   0.00539   0.0161   0.1136   0.8942
   6.000   0.5885   0.01229   0.00562   0.0165   0.1059   0.8964
   6.250   0.6108   0.01265   0.00592   0.0174   0.0978   0.8988
   6.500   0.6358   0.01281   0.00613   0.0179   0.0926   0.9010
   6.750   0.6586   0.01315   0.00644   0.0186   0.0863   0.9036
   7.000   0.6823   0.01343   0.00675   0.0192   0.0817   0.9063
   7.250   0.7065   0.01368   0.00700   0.0197   0.0768   0.9091
   7.500   0.7275   0.01414   0.00745   0.0206   0.0719   0.9121
   7.750   0.7511   0.01432   0.00770   0.0213   0.0686   0.9151
   8.000   0.7735   0.01460   0.00799   0.0222   0.0649   0.9188
   8.250   0.7926   0.01515   0.00854   0.0234   0.0609   0.9235
   8.500   0.8157   0.01536   0.00883   0.0241   0.0582   0.9278
   8.750   0.8367   0.01564   0.00916   0.0252   0.0554   0.9328
   9.000   0.8544   0.01621   0.00972   0.0267   0.0521   0.9393
   9.250   0.8753   0.01655   0.01014   0.0278   0.0497   0.9461
   9.500   0.8970   0.01685   0.01051   0.0286   0.0472   0.9549
   9.750   0.9217   0.01735   0.01103   0.0286   0.0445   0.9643
  10.000   0.9490   0.01817   0.01191   0.0278   0.0420   0.9743
  10.250   0.9813   0.01871   0.01252   0.0262   0.0396   0.9844
  10.500   1.0117   0.01932   0.01315   0.0247   0.0374   1.0000
  10.750   1.0214   0.02031   0.01414   0.0269   0.0354   1.0000
  11.000   1.0398   0.02072   0.01463   0.0281   0.0342   1.0000
  11.250   1.0563   0.02130   0.01527   0.0293   0.0328   1.0000
  11.500   1.0719   0.02193   0.01593   0.0307   0.0316   1.0000
  11.750   1.0852   0.02272   0.01674   0.0322   0.0305   1.0000
  12.000   1.0925   0.02418   0.01823   0.0344   0.0293   1.0000
  12.250   1.1071   0.02490   0.01908   0.0357   0.0285   1.0000
  12.500   1.1203   0.02571   0.01999   0.0371   0.0276   1.0000
  12.750   1.1322   0.02664   0.02099   0.0385   0.0269   1.0000
  13.000   1.1440   0.02752   0.02192   0.0398   0.0260   1.0000
  13.250   1.1533   0.02863   0.02308   0.0412   0.0254   1.0000
  13.500   1.1592   0.03006   0.02456   0.0428   0.0247   1.0000
  13.750   1.1592   0.03220   0.02680   0.0446   0.0240   1.0000
  14.000   1.1663   0.03357   0.02831   0.0459   0.0237   1.0000
  14.250   1.1712   0.03518   0.03006   0.0470   0.0233   1.0000
  14.500   1.1754   0.03684   0.03185   0.0481   0.0227   1.0000
  14.750   1.1781   0.03872   0.03384   0.0489   0.0223   1.0000
  15.000   1.1799   0.04073   0.03596   0.0496   0.0218   1.0000
  15.250   1.1796   0.04304   0.03838   0.0500   0.0215   1.0000
  15.500   1.1804   0.04532   0.04073   0.0501   0.0210   1.0000
  15.750   1.1785   0.04804   0.04354   0.0499   0.0207   1.0000
  16.000   1.1740   0.05128   0.04687   0.0493   0.0204   1.0000
  16.250   1.1650   0.05531   0.05103   0.0480   0.0202   1.0000
  16.500   1.1531   0.06011   0.05595   0.0461   0.0199   1.0000
  16.750   1.1383   0.06573   0.06174   0.0434   0.0198   1.0000
  17.000   1.1193   0.07244   0.06862   0.0397   0.0197   1.0000
  17.250   1.0978   0.08009   0.07645   0.0350   0.0196   1.0000
  17.500   1.0764   0.08817   0.08471   0.0299   0.0196   1.0000
  17.750   1.0516   0.09720   0.09391   0.0242   0.0196   1.0000
  18.000   1.0200   0.10799   0.10489   0.0173   0.0196   1.0000
  18.250   0.9916   0.11867   0.11574   0.0106   0.0197   1.0000
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