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NASA SC(2)-1010 AIRFOIL (sc21010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-1010 AIRFOIL (sc21010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.9 at α=-2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc21010-il-1000000-n5.txt
Download as CSV file: xf-sc21010-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-1010 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.9985   0.07933   0.07668  -0.0531   0.9999   0.0111
 -18.500  -1.0471   0.06653   0.06367  -0.0609   0.9999   0.0110
 -18.250  -1.0777   0.05730   0.05426  -0.0671   0.9999   0.0109
 -18.000  -1.0969   0.05037   0.04719  -0.0720   0.9999   0.0110
 -17.750  -1.1096   0.04486   0.04154  -0.0759   0.9999   0.0110
 -17.500  -1.1165   0.04057   0.03713  -0.0787   0.9999   0.0111
 -17.250  -1.1221   0.03702   0.03347  -0.0805   0.9999   0.0112
 -17.000  -1.1302   0.03412   0.03048  -0.0808   0.9999   0.0112
 -16.750  -1.1483   0.03191   0.02819  -0.0781   0.9999   0.0113
 -16.500  -1.1436   0.02963   0.02581  -0.0794   0.9992   0.0114
 -16.250  -1.1201   0.02741   0.02345  -0.0839   0.9975   0.0115
 -16.000  -1.0933   0.02551   0.02142  -0.0883   0.9961   0.0117
 -15.750  -1.0643   0.02394   0.01972  -0.0922   0.9950   0.0118
 -15.500  -1.0345   0.02265   0.01831  -0.0954   0.9941   0.0119
 -15.250  -1.0063   0.02158   0.01714  -0.0976   0.9928   0.0121
 -15.000  -0.9777   0.02063   0.01608  -0.0997   0.9913   0.0122
 -14.750  -0.9487   0.01937   0.01472  -0.1022   0.9900   0.0125
 -14.500  -0.9187   0.01842   0.01369  -0.1043   0.9889   0.0128
 -14.250  -0.8881   0.01764   0.01285  -0.1063   0.9880   0.0131
 -14.000  -0.8570   0.01695   0.01210  -0.1082   0.9871   0.0134
 -13.750  -0.8254   0.01631   0.01141  -0.1101   0.9864   0.0137
 -13.500  -0.7934   0.01572   0.01075  -0.1120   0.9857   0.0140
 -13.250  -0.7611   0.01515   0.01013  -0.1138   0.9850   0.0143
 -13.000  -0.7289   0.01464   0.00955  -0.1156   0.9844   0.0147
 -12.750  -0.6967   0.01416   0.00902  -0.1173   0.9837   0.0150
 -12.500  -0.6655   0.01372   0.00852  -0.1187   0.9825   0.0153
 -12.250  -0.6350   0.01313   0.00789  -0.1200   0.9805   0.0159
 -12.000  -0.6039   0.01268   0.00742  -0.1214   0.9785   0.0165
 -11.750  -0.5723   0.01229   0.00700  -0.1227   0.9767   0.0171
 -11.500  -0.5406   0.01192   0.00660  -0.1241   0.9750   0.0177
 -11.250  -0.5085   0.01157   0.00622  -0.1255   0.9735   0.0183
 -11.000  -0.4763   0.01126   0.00586  -0.1268   0.9721   0.0188
 -10.750  -0.4441   0.01088   0.00547  -0.1283   0.9706   0.0199
 -10.500  -0.4142   0.01059   0.00517  -0.1291   0.9677   0.0210
 -10.250  -0.3838   0.01033   0.00490  -0.1300   0.9649   0.0222
 -10.000  -0.3529   0.01010   0.00464  -0.1309   0.9625   0.0231
  -9.750  -0.3214   0.00980   0.00434  -0.1320   0.9603   0.0247
  -9.500  -0.2901   0.00956   0.00410  -0.1330   0.9582   0.0262
  -9.250  -0.2596   0.00936   0.00388  -0.1338   0.9556   0.0275
  -9.000  -0.2293   0.00914   0.00366  -0.1346   0.9523   0.0292
  -8.750  -0.1988   0.00893   0.00345  -0.1354   0.9490   0.0312
  -8.500  -0.1683   0.00876   0.00327  -0.1361   0.9459   0.0332
  -8.250  -0.1375   0.00857   0.00307  -0.1369   0.9430   0.0358
  -8.000  -0.1071   0.00838   0.00290  -0.1376   0.9396   0.0386
  -7.750  -0.0768   0.00823   0.00274  -0.1383   0.9358   0.0412
  -7.500  -0.0461   0.00805   0.00258  -0.1390   0.9322   0.0466
  -7.250  -0.0154   0.00787   0.00243  -0.1398   0.9291   0.0543
  -7.000   0.0153   0.00771   0.00231  -0.1405   0.9259   0.0637
  -6.750   0.0460   0.00755   0.00219  -0.1413   0.9221   0.0740
  -6.500   0.0768   0.00738   0.00208  -0.1420   0.9181   0.0895
  -6.250   0.1075   0.00722   0.00198  -0.1427   0.9143   0.1058
  -6.000   0.1383   0.00708   0.00188  -0.1435   0.9107   0.1239
  -5.750   0.1695   0.00690   0.00180  -0.1443   0.9069   0.1499
  -5.500   0.2010   0.00669   0.00171  -0.1453   0.9033   0.1869
  -5.250   0.2328   0.00646   0.00163  -0.1463   0.9001   0.2353
  -5.000   0.2646   0.00625   0.00157  -0.1474   0.8970   0.2864
  -4.750   0.2964   0.00603   0.00153  -0.1484   0.8930   0.3400
  -4.500   0.3275   0.00588   0.00151  -0.1492   0.8876   0.3876
  -4.250   0.3576   0.00581   0.00150  -0.1497   0.8815   0.4129
  -4.000   0.3877   0.00573   0.00149  -0.1501   0.8718   0.4439
  -3.750   0.4169   0.00571   0.00148  -0.1502   0.8583   0.4638
  -3.500   0.4455   0.00574   0.00146  -0.1502   0.8389   0.4802
  -3.250   0.4744   0.00576   0.00147  -0.1503   0.8198   0.4979
  -3.000   0.5032   0.00581   0.00148  -0.1504   0.7985   0.5164
  -2.750   0.5313   0.00591   0.00152  -0.1503   0.7668   0.5350
  -2.500   0.5571   0.00626   0.00159  -0.1497   0.6935   0.5490
  -2.250   0.5789   0.00720   0.00186  -0.1485   0.5361   0.5575
  -2.000   0.6019   0.00811   0.00217  -0.1478   0.3905   0.5673
  -1.750   0.6276   0.00866   0.00238  -0.1475   0.3031   0.5761
  -1.500   0.6535   0.00916   0.00259  -0.1472   0.2293   0.5855
  -1.250   0.6801   0.00956   0.00278  -0.1470   0.1723   0.5949
  -1.000   0.7070   0.00991   0.00297  -0.1468   0.1302   0.6055
  -0.750   0.7343   0.01019   0.00316  -0.1467   0.1010   0.6164
  -0.500   0.7617   0.01045   0.00334  -0.1465   0.0811   0.6265
  -0.250   0.7892   0.01067   0.00352  -0.1464   0.0676   0.6366
   0.000   0.8166   0.01091   0.00371  -0.1462   0.0543   0.6469
   0.250   0.8439   0.01114   0.00391  -0.1460   0.0463   0.6573
   0.500   0.8713   0.01135   0.00412  -0.1458   0.0413   0.6666
   0.750   0.8986   0.01157   0.00432  -0.1456   0.0377   0.6741
   1.000   0.9258   0.01178   0.00454  -0.1453   0.0349   0.6811
   1.250   0.9527   0.01203   0.00477  -0.1450   0.0318   0.6878
   1.500   0.9798   0.01223   0.00499  -0.1448   0.0303   0.6937
   1.750   1.0066   0.01246   0.00523  -0.1444   0.0285   0.7000
   2.000   1.0331   0.01274   0.00549  -0.1440   0.0265   0.7058
   2.250   1.0598   0.01297   0.00576  -0.1437   0.0254   0.7116
   2.500   1.0862   0.01322   0.00602  -0.1433   0.0241   0.7180
   2.750   1.1124   0.01350   0.00631  -0.1428   0.0226   0.7236
   3.000   1.1382   0.01380   0.00662  -0.1423   0.0212   0.7294
   3.250   1.1643   0.01407   0.00692  -0.1418   0.0203   0.7347
   3.500   1.1900   0.01437   0.00724  -0.1413   0.0193   0.7394
   3.750   1.2154   0.01469   0.00757  -0.1407   0.0184   0.7442
   4.000   1.2403   0.01508   0.00797  -0.1400   0.0174   0.7493
   4.250   1.2656   0.01540   0.00833  -0.1394   0.0170   0.7546
   4.500   1.2905   0.01574   0.00872  -0.1387   0.0164   0.7601
   4.750   1.3151   0.01610   0.00912  -0.1380   0.0158   0.7666
   5.000   1.3394   0.01649   0.00953  -0.1372   0.0153   0.7722
   5.250   1.3634   0.01690   0.00997  -0.1363   0.0148   0.7777
   5.500   1.3868   0.01737   0.01047  -0.1354   0.0142   0.7828
   5.750   1.4100   0.01785   0.01099  -0.1344   0.0138   0.7871
   6.000   1.4333   0.01827   0.01147  -0.1335   0.0136   0.7910
   6.250   1.4563   0.01872   0.01198  -0.1324   0.0133   0.7954
   6.500   1.4788   0.01920   0.01251  -0.1313   0.0130   0.7999
   6.750   1.5009   0.01969   0.01306  -0.1302   0.0127   0.8045
   7.000   1.5226   0.02020   0.01363  -0.1290   0.0124   0.8096
   7.250   1.5439   0.02074   0.01422  -0.1277   0.0122   0.8148
   7.500   1.5647   0.02130   0.01482  -0.1264   0.0119   0.8192
   7.750   1.5848   0.02190   0.01548  -0.1249   0.0117   0.8236
   8.000   1.6039   0.02256   0.01621  -0.1233   0.0114   0.8283
   8.250   1.6216   0.02335   0.01706  -0.1214   0.0112   0.8327
   8.500   1.6378   0.02418   0.01798  -0.1193   0.0110   0.8366
   8.750   1.6546   0.02485   0.01874  -0.1173   0.0109   0.8410
   9.000   1.6704   0.02556   0.01953  -0.1152   0.0108   0.8456
   9.250   1.6848   0.02630   0.02037  -0.1128   0.0107   0.8501
   9.500   1.6973   0.02708   0.02125  -0.1101   0.0106   0.8554
   9.750   1.7074   0.02791   0.02217  -0.1070   0.0105   0.8609
  10.000   1.7183   0.02878   0.02314  -0.1042   0.0103   0.8655
  10.250   1.7292   0.02967   0.02414  -0.1015   0.0102   0.8701
  10.500   1.7391   0.03067   0.02523  -0.0987   0.0101   0.8747
  10.750   1.7484   0.03172   0.02639  -0.0960   0.0099   0.8795
  11.000   1.7571   0.03282   0.02759  -0.0933   0.0098   0.8852
  11.500   1.7709   0.03535   0.03035  -0.0878   0.0096   0.8998
  11.750   1.7766   0.03669   0.03184  -0.0851   0.0095   0.9142
  12.000   1.7787   0.03811   0.03341  -0.0819   0.0094   1.0001
  12.250   1.7825   0.03980   0.03520  -0.0795   0.0093   1.0001
  12.500   1.7852   0.04165   0.03715  -0.0771   0.0093   1.0001
  12.750   1.7867   0.04366   0.03927  -0.0748   0.0092   1.0001
  13.000   1.7864   0.04591   0.04164  -0.0726   0.0091   1.0001
  13.250   1.7849   0.04836   0.04420  -0.0707   0.0090   1.0001
  13.500   1.7809   0.05120   0.04716  -0.0689   0.0090   1.0001
  13.750   1.7749   0.05438   0.05047  -0.0674   0.0089   1.0001
  14.000   1.7666   0.05798   0.05420  -0.0663   0.0088   1.0001
  14.250   1.7554   0.06220   0.05856  -0.0657   0.0088   1.0001
  14.500   1.7418   0.06708   0.06360  -0.0658   0.0087   1.0001
  14.750   1.7250   0.07286   0.06953  -0.0669   0.0087   1.0001
  15.000   1.7055   0.07962   0.07648  -0.0691   0.0087   1.0001
  15.250   1.6814   0.08792   0.08497  -0.0729   0.0087   1.0001
  15.500   1.6508   0.09828   0.09553  -0.0787   0.0087   1.0001
  15.750   1.6113   0.11133   0.10883  -0.0866   0.0087   1.0001
  16.000   1.5524   0.12951   0.12730  -0.0980   0.0088   1.0001
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