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NASA SC(2)-0010 AIRFOIL (sc20010-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0010 AIRFOIL (sc20010-il)
Reynolds number: 500,000
Max Cl/Cd: 56.59 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20010-il-500000-n5.txt
Download as CSV file: xf-sc20010-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0010 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0992   0.09342   0.09043   0.0022   1.0000   0.0127
 -15.500  -1.1528   0.07625   0.07292  -0.0093   1.0000   0.0126
 -15.250  -1.1800   0.06622   0.06265  -0.0164   1.0000   0.0125
 -15.000  -1.2009   0.05879   0.05502  -0.0211   1.0000   0.0125
 -14.750  -1.2170   0.05308   0.04912  -0.0240   1.0000   0.0126
 -14.500  -1.2291   0.04849   0.04436  -0.0255   1.0000   0.0126
 -14.250  -1.2374   0.04473   0.04043  -0.0262   1.0000   0.0127
 -14.000  -1.2422   0.04165   0.03721  -0.0262   1.0000   0.0128
 -13.750  -1.2444   0.03908   0.03450  -0.0256   1.0000   0.0129
 -13.500  -1.2442   0.03692   0.03220  -0.0246   1.0000   0.0130
 -13.250  -1.2424   0.03504   0.03019  -0.0231   1.0000   0.0132
 -13.000  -1.2393   0.03339   0.02841  -0.0213   1.0000   0.0133
 -12.750  -1.2350   0.03193   0.02681  -0.0190   1.0000   0.0134
 -12.500  -1.2278   0.03060   0.02535  -0.0169   1.0000   0.0135
 -12.250  -1.2164   0.02932   0.02394  -0.0154   1.0000   0.0137
 -12.000  -1.2031   0.02809   0.02258  -0.0140   1.0000   0.0138
 -11.750  -1.1881   0.02693   0.02129  -0.0127   1.0000   0.0140
 -11.500  -1.1718   0.02583   0.02006  -0.0116   1.0000   0.0142
 -11.250  -1.1543   0.02478   0.01888  -0.0105   1.0000   0.0144
 -11.000  -1.1358   0.02380   0.01777  -0.0096   1.0000   0.0147
 -10.750  -1.1164   0.02287   0.01673  -0.0087   1.0000   0.0149
 -10.500  -1.0962   0.02199   0.01574  -0.0079   1.0000   0.0151
 -10.250  -1.0752   0.02118   0.01482  -0.0071   1.0000   0.0153
 -10.000  -1.0538   0.02041   0.01394  -0.0064   1.0000   0.0155
  -9.750  -1.0331   0.01949   0.01297  -0.0056   1.0000   0.0159
  -9.500  -1.0108   0.01879   0.01222  -0.0051   1.0000   0.0164
  -9.250  -0.9876   0.01818   0.01156  -0.0046   1.0000   0.0168
  -9.000  -0.9640   0.01761   0.01094  -0.0041   1.0000   0.0174
  -8.750  -0.9402   0.01704   0.01031  -0.0036   1.0000   0.0179
  -8.500  -0.9162   0.01648   0.00969  -0.0031   1.0000   0.0184
  -8.250  -0.8919   0.01596   0.00910  -0.0027   1.0000   0.0189
  -8.000  -0.8677   0.01540   0.00850  -0.0023   1.0000   0.0195
  -7.750  -0.8432   0.01490   0.00799  -0.0019   1.0000   0.0204
  -7.500  -0.8182   0.01446   0.00753  -0.0015   1.0000   0.0214
  -7.250  -0.7930   0.01405   0.00708  -0.0012   1.0000   0.0226
  -7.000  -0.7679   0.01364   0.00665  -0.0008   1.0000   0.0239
  -6.750  -0.7426   0.01326   0.00628  -0.0005   1.0000   0.0258
  -6.500  -0.7171   0.01294   0.00593  -0.0002   1.0000   0.0281
  -6.250  -0.6919   0.01259   0.00562   0.0002   1.0000   0.0309
  -6.000  -0.6649   0.01232   0.00533   0.0002   0.9978   0.0338
  -5.750  -0.6328   0.01198   0.00503  -0.0009   0.9880   0.0373
  -5.500  -0.6006   0.01173   0.00475  -0.0020   0.9769   0.0404
  -5.250  -0.5690   0.01143   0.00447  -0.0030   0.9641   0.0439
  -5.000  -0.5385   0.01120   0.00422  -0.0036   0.9492   0.0474
  -4.750  -0.5101   0.01098   0.00398  -0.0037   0.9325   0.0511
  -4.500  -0.4836   0.01076   0.00376  -0.0034   0.9156   0.0559
  -4.250  -0.4575   0.01059   0.00355  -0.0030   0.9003   0.0609
  -4.000  -0.4315   0.01038   0.00334  -0.0026   0.8863   0.0674
  -3.750  -0.4050   0.01020   0.00314  -0.0022   0.8737   0.0741
  -3.500  -0.3782   0.01002   0.00296  -0.0020   0.8624   0.0836
  -3.250  -0.3514   0.00980   0.00278  -0.0018   0.8526   0.0988
  -3.000  -0.3244   0.00958   0.00261  -0.0017   0.8434   0.1193
  -2.750  -0.2974   0.00933   0.00245  -0.0016   0.8356   0.1483
  -2.500  -0.2705   0.00902   0.00230  -0.0015   0.8278   0.1900
  -2.250  -0.2437   0.00871   0.00215  -0.0015   0.8206   0.2435
  -2.000  -0.2173   0.00826   0.00199  -0.0014   0.8131   0.3205
  -1.750  -0.1915   0.00773   0.00182  -0.0013   0.8066   0.4235
  -1.500  -0.1656   0.00718   0.00168  -0.0011   0.8011   0.5318
  -1.250  -0.1395   0.00685   0.00170  -0.0008   0.7952   0.6308
  -1.000  -0.1118   0.00681   0.00171  -0.0006   0.7881   0.6679
  -0.750  -0.0839   0.00676   0.00172  -0.0005   0.7776   0.6954
  -0.500  -0.0562   0.00674   0.00173  -0.0002   0.7672   0.7199
  -0.250  -0.0280   0.00673   0.00173  -0.0002   0.7589   0.7333
   0.000   0.0000   0.00672   0.00174   0.0000   0.7471   0.7471
   0.250   0.0280   0.00673   0.00173   0.0002   0.7334   0.7590
   0.500   0.0561   0.00674   0.00173   0.0002   0.7197   0.7674
   0.750   0.0839   0.00676   0.00172   0.0005   0.6958   0.7776
   1.000   0.1117   0.00681   0.00171   0.0006   0.6679   0.7881
   1.250   0.1394   0.00685   0.00170   0.0008   0.6304   0.7952
   1.500   0.1656   0.00718   0.00168   0.0011   0.5317   0.8011
   1.750   0.1914   0.00774   0.00182   0.0013   0.4226   0.8066
   2.000   0.2173   0.00826   0.00199   0.0014   0.3211   0.8130
   2.250   0.2437   0.00871   0.00215   0.0015   0.2435   0.8206
   2.500   0.2705   0.00902   0.00230   0.0015   0.1900   0.8278
   2.750   0.2974   0.00933   0.00245   0.0016   0.1482   0.8356
   3.000   0.3244   0.00958   0.00261   0.0017   0.1192   0.8434
   3.250   0.3514   0.00980   0.00278   0.0018   0.0988   0.8526
   3.500   0.3782   0.01002   0.00296   0.0020   0.0836   0.8624
   3.750   0.4050   0.01020   0.00314   0.0022   0.0741   0.8737
   4.000   0.4315   0.01038   0.00334   0.0026   0.0674   0.8864
   4.250   0.4575   0.01059   0.00355   0.0030   0.0609   0.9003
   4.500   0.4836   0.01076   0.00376   0.0034   0.0559   0.9157
   4.750   0.5101   0.01098   0.00398   0.0037   0.0511   0.9325
   5.000   0.5385   0.01120   0.00422   0.0036   0.0475   0.9493
   5.250   0.5690   0.01143   0.00447   0.0030   0.0439   0.9641
   5.500   0.6006   0.01173   0.00475   0.0020   0.0404   0.9769
   5.750   0.6329   0.01198   0.00503   0.0009   0.0372   0.9881
   6.000   0.6649   0.01232   0.00533  -0.0002   0.0338   0.9979
   6.250   0.6919   0.01259   0.00562  -0.0002   0.0309   1.0000
   6.500   0.7171   0.01294   0.00593   0.0002   0.0281   1.0000
   6.750   0.7426   0.01326   0.00628   0.0005   0.0258   1.0000
   7.000   0.7679   0.01364   0.00665   0.0008   0.0239   1.0000
   7.250   0.7930   0.01405   0.00708   0.0012   0.0226   1.0000
   7.500   0.8182   0.01446   0.00753   0.0015   0.0214   1.0000
   7.750   0.8432   0.01490   0.00799   0.0019   0.0204   1.0000
   8.000   0.8678   0.01540   0.00850   0.0023   0.0195   1.0000
   8.250   0.8919   0.01596   0.00910   0.0027   0.0189   1.0000
   8.500   0.9163   0.01648   0.00969   0.0031   0.0184   1.0000
   8.750   0.9402   0.01704   0.01031   0.0036   0.0179   1.0000
   9.000   0.9640   0.01761   0.01093   0.0041   0.0174   1.0000
   9.250   0.9876   0.01818   0.01156   0.0045   0.0168   1.0000
   9.500   1.0108   0.01879   0.01222   0.0050   0.0164   1.0000
   9.750   1.0331   0.01949   0.01297   0.0056   0.0159   1.0000
  10.000   1.0538   0.02041   0.01395   0.0064   0.0155   1.0000
  10.250   1.0753   0.02118   0.01481   0.0071   0.0153   1.0000
  10.500   1.0963   0.02199   0.01574   0.0079   0.0151   1.0000
  10.750   1.1165   0.02286   0.01672   0.0087   0.0149   1.0000
  11.000   1.1359   0.02379   0.01777   0.0096   0.0147   1.0000
  11.250   1.1544   0.02478   0.01888   0.0105   0.0144   1.0000
  11.500   1.1719   0.02583   0.02006   0.0116   0.0142   1.0000
  11.750   1.1883   0.02693   0.02129   0.0127   0.0140   1.0000
  12.000   1.2033   0.02809   0.02258   0.0140   0.0138   1.0000
  12.250   1.2166   0.02932   0.02394   0.0153   0.0137   1.0000
  12.500   1.2281   0.03060   0.02535   0.0169   0.0135   1.0000
  12.750   1.2353   0.03193   0.02681   0.0190   0.0134   1.0000
  13.000   1.2398   0.03338   0.02840   0.0212   0.0133   1.0000
  13.250   1.2430   0.03504   0.03019   0.0230   0.0132   1.0000
  13.500   1.2449   0.03690   0.03218   0.0245   0.0130   1.0000
  13.750   1.2453   0.03905   0.03446   0.0255   0.0129   1.0000
  14.000   1.2433   0.04161   0.03716   0.0261   0.0128   1.0000
  14.250   1.2384   0.04470   0.04041   0.0261   0.0127   1.0000
  14.500   1.2302   0.04846   0.04433   0.0254   0.0126   1.0000
  14.750   1.2178   0.05309   0.04913   0.0238   0.0126   1.0000
  15.000   1.2015   0.05885   0.05508   0.0209   0.0125   1.0000
  15.250   1.1811   0.06623   0.06266   0.0162   0.0125   1.0000
  15.500   1.1537   0.07634   0.07302   0.0090   0.0125   1.0000
  15.750   1.1013   0.09328   0.09028  -0.0023   0.0127   1.0000
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