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NASA SC(2)-0410 AIRFOIL (sc20410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0410 AIRFOIL (sc20410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.67 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20410-il-1000000-n5.txt
Download as CSV file: xf-sc20410-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0410 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.0016   0.13719   0.13502   0.0099   1.0000   0.0102
 -17.500  -1.1342   0.10461   0.10207  -0.0079   1.0000   0.0099
 -17.250  -1.1990   0.08701   0.08422  -0.0178   1.0000   0.0098
 -17.000  -1.2374   0.07476   0.07175  -0.0254   1.0000   0.0097
 -16.750  -1.2636   0.06551   0.06231  -0.0314   1.0000   0.0097
 -16.500  -1.2827   0.05843   0.05507  -0.0357   1.0000   0.0097
 -16.250  -1.2974   0.05286   0.04934  -0.0386   1.0000   0.0098
 -16.000  -1.3080   0.04832   0.04466  -0.0405   1.0000   0.0098
 -15.750  -1.3151   0.04451   0.04072  -0.0418   1.0000   0.0099
 -15.500  -1.3190   0.04125   0.03734  -0.0425   1.0000   0.0099
 -15.250  -1.3201   0.03846   0.03444  -0.0430   1.0000   0.0100
 -15.000  -1.3183   0.03605   0.03193  -0.0431   1.0000   0.0101
 -14.750  -1.3140   0.03397   0.02975  -0.0431   1.0000   0.0102
 -14.500  -1.3080   0.03212   0.02780  -0.0430   1.0000   0.0103
 -14.250  -1.3002   0.03048   0.02608  -0.0427   1.0000   0.0104
 -14.000  -1.2915   0.02899   0.02451  -0.0422   1.0000   0.0105
 -13.750  -1.2824   0.02763   0.02306  -0.0416   1.0000   0.0106
 -13.500  -1.2734   0.02635   0.02170  -0.0407   1.0000   0.0107
 -13.250  -1.2590   0.02514   0.02039  -0.0407   1.0000   0.0108
 -13.000  -1.2420   0.02401   0.01918  -0.0409   1.0000   0.0109
 -12.750  -1.2233   0.02298   0.01806  -0.0410   1.0000   0.0110
 -12.500  -1.2036   0.02206   0.01706  -0.0410   1.0000   0.0111
 -12.250  -1.1831   0.02121   0.01612  -0.0410   1.0000   0.0113
 -12.000  -1.1618   0.02042   0.01525  -0.0409   1.0000   0.0114
 -11.750  -1.1398   0.01966   0.01442  -0.0409   1.0000   0.0116
 -11.500  -1.1171   0.01896   0.01366  -0.0408   1.0000   0.0117
 -11.250  -1.0939   0.01830   0.01293  -0.0408   1.0000   0.0118
 -11.000  -1.0702   0.01769   0.01225  -0.0408   1.0000   0.0120
 -10.750  -1.0460   0.01711   0.01162  -0.0408   1.0000   0.0121
 -10.500  -1.0216   0.01657   0.01102  -0.0408   1.0000   0.0122
 -10.250  -0.9972   0.01588   0.01028  -0.0408   1.0000   0.0125
 -10.000  -0.9723   0.01529   0.00965  -0.0409   1.0000   0.0128
  -9.750  -0.9469   0.01478   0.00910  -0.0410   1.0000   0.0132
  -9.500  -0.9212   0.01432   0.00862  -0.0411   1.0000   0.0136
  -9.250  -0.8952   0.01389   0.00817  -0.0411   1.0000   0.0140
  -9.000  -0.8690   0.01349   0.00774  -0.0412   1.0000   0.0144
  -8.750  -0.8427   0.01310   0.00732  -0.0413   1.0000   0.0147
  -8.500  -0.8162   0.01274   0.00694  -0.0414   1.0000   0.0151
  -8.250  -0.7897   0.01239   0.00656  -0.0415   1.0000   0.0155
  -8.000  -0.7630   0.01201   0.00617  -0.0416   1.0000   0.0163
  -7.750  -0.7363   0.01168   0.00584  -0.0417   1.0000   0.0173
  -7.500  -0.7097   0.01138   0.00554  -0.0418   1.0000   0.0183
  -7.250  -0.6805   0.01108   0.00523  -0.0423   0.9997   0.0197
  -7.000  -0.6482   0.01077   0.00495  -0.0436   0.9988   0.0220
  -6.750  -0.6157   0.01049   0.00468  -0.0449   0.9978   0.0242
  -6.500  -0.5832   0.01022   0.00443  -0.0461   0.9968   0.0268
  -6.250  -0.5504   0.00999   0.00420  -0.0474   0.9957   0.0289
  -6.000  -0.5172   0.00973   0.00397  -0.0488   0.9947   0.0319
  -5.750  -0.4843   0.00952   0.00376  -0.0501   0.9934   0.0341
  -5.500  -0.4520   0.00929   0.00355  -0.0512   0.9915   0.0368
  -5.250  -0.4193   0.00907   0.00336  -0.0525   0.9896   0.0395
  -5.000  -0.3862   0.00889   0.00317  -0.0537   0.9878   0.0418
  -4.750  -0.3529   0.00867   0.00300  -0.0551   0.9862   0.0461
  -4.500  -0.3195   0.00848   0.00284  -0.0564   0.9846   0.0502
  -4.250  -0.2864   0.00826   0.00267  -0.0577   0.9823   0.0580
  -4.000  -0.2547   0.00808   0.00252  -0.0587   0.9781   0.0648
  -3.750  -0.2218   0.00789   0.00238  -0.0599   0.9747   0.0723
  -3.500  -0.1884   0.00769   0.00224  -0.0612   0.9718   0.0846
  -3.250  -0.1562   0.00747   0.00211  -0.0622   0.9667   0.1029
  -3.000  -0.1230   0.00719   0.00196  -0.0636   0.9599   0.1360
  -2.750  -0.0908   0.00692   0.00183  -0.0647   0.9500   0.1753
  -2.500  -0.0594   0.00665   0.00170  -0.0656   0.9361   0.2206
  -2.250  -0.0284   0.00633   0.00157  -0.0664   0.9197   0.2848
  -2.000   0.0029   0.00597   0.00144  -0.0674   0.9014   0.3652
  -1.750   0.0363   0.00541   0.00125  -0.0691   0.8806   0.4946
  -1.500   0.0673   0.00519   0.00124  -0.0699   0.8571   0.5830
  -1.250   0.0957   0.00525   0.00124  -0.0698   0.8268   0.6098
  -1.000   0.1244   0.00534   0.00127  -0.0699   0.7967   0.6300
  -0.750   0.1522   0.00554   0.00129  -0.0697   0.7465   0.6422
  -0.500   0.1801   0.00577   0.00134  -0.0696   0.6929   0.6516
  -0.250   0.2070   0.00623   0.00139  -0.0694   0.5874   0.6567
   0.000   0.2337   0.00681   0.00152  -0.0693   0.4606   0.6606
   0.250   0.2609   0.00735   0.00166  -0.0693   0.3526   0.6656
   0.500   0.2889   0.00772   0.00176  -0.0694   0.2821   0.6707
   0.750   0.3171   0.00802   0.00187  -0.0696   0.2262   0.6747
   1.000   0.3452   0.00833   0.00199  -0.0697   0.1750   0.6779
   1.500   0.4022   0.00877   0.00220  -0.0699   0.1178   0.6825
   1.750   0.4307   0.00897   0.00231  -0.0700   0.0977   0.6847
   2.000   0.4592   0.00917   0.00242  -0.0701   0.0814   0.6867
   2.500   0.5163   0.00951   0.00268  -0.0703   0.0619   0.6898
   2.750   0.5448   0.00968   0.00281  -0.0704   0.0552   0.6913
   3.000   0.5732   0.00984   0.00296  -0.0705   0.0504   0.6929
   3.250   0.6015   0.01002   0.00312  -0.0705   0.0455   0.6944
   3.500   0.6299   0.01019   0.00327  -0.0706   0.0421   0.6960
   3.750   0.6581   0.01039   0.00344  -0.0706   0.0386   0.6977
   4.000   0.6863   0.01056   0.00362  -0.0706   0.0367   0.6994
   4.250   0.7145   0.01075   0.00380  -0.0707   0.0343   0.7010
   4.500   0.7424   0.01098   0.00400  -0.0706   0.0317   0.7027
   4.750   0.7704   0.01116   0.00420  -0.0706   0.0301   0.7043
   5.000   0.7983   0.01138   0.00441  -0.0706   0.0277   0.7061
   5.250   0.8259   0.01161   0.00465  -0.0705   0.0255   0.7080
   5.500   0.8536   0.01183   0.00488  -0.0705   0.0233   0.7097
   5.750   0.8810   0.01211   0.00515  -0.0704   0.0211   0.7116
   6.000   0.9083   0.01237   0.00542  -0.0703   0.0193   0.7135
   6.250   0.9354   0.01268   0.00573  -0.0701   0.0176   0.7155
   6.500   0.9625   0.01298   0.00605  -0.0700   0.0168   0.7174
   6.750   0.9894   0.01328   0.00638  -0.0698   0.0161   0.7193
   7.000   1.0162   0.01361   0.00673  -0.0696   0.0155   0.7211
   7.250   1.0427   0.01397   0.00711  -0.0693   0.0149   0.7230
   7.500   1.0689   0.01437   0.00755  -0.0690   0.0143   0.7251
   7.750   1.0949   0.01479   0.00801  -0.0687   0.0139   0.7273
   8.000   1.1211   0.01516   0.00844  -0.0684   0.0137   0.7297
   8.250   1.1470   0.01557   0.00890  -0.0681   0.0134   0.7321
   8.500   1.1726   0.01599   0.00937  -0.0677   0.0132   0.7345
   8.750   1.1980   0.01644   0.00988  -0.0673   0.0130   0.7368
   9.250   1.2481   0.01739   0.01095  -0.0664   0.0125   0.7416
   9.500   1.2727   0.01790   0.01153  -0.0659   0.0123   0.7445
   9.750   1.2970   0.01843   0.01212  -0.0654   0.0121   0.7476
  10.000   1.3209   0.01898   0.01273  -0.0648   0.0119   0.7508
  10.250   1.3444   0.01959   0.01340  -0.0642   0.0116   0.7538
  10.500   1.3670   0.02030   0.01418  -0.0634   0.0114   0.7566
  10.750   1.3884   0.02113   0.01512  -0.0625   0.0111   0.7597
  11.000   1.4090   0.02203   0.01612  -0.0615   0.0110   0.7630
  11.250   1.4308   0.02272   0.01690  -0.0607   0.0109   0.7664
  11.500   1.4519   0.02345   0.01774  -0.0597   0.0108   0.7697
  11.750   1.4724   0.02422   0.01861  -0.0587   0.0107   0.7728
  12.000   1.4921   0.02504   0.01954  -0.0576   0.0106   0.7762
  12.250   1.5108   0.02591   0.02053  -0.0564   0.0105   0.7799
  12.500   1.5286   0.02684   0.02157  -0.0551   0.0104   0.7836
  13.000   1.5604   0.02889   0.02387  -0.0520   0.0103   0.7909
  13.250   1.5741   0.03000   0.02511  -0.0503   0.0102   0.7951
  13.500   1.5859   0.03120   0.02643  -0.0483   0.0101   0.7994
  13.750   1.5952   0.03246   0.02783  -0.0460   0.0100   0.8033
  14.000   1.5999   0.03375   0.02926  -0.0430   0.0099   0.8077
  14.250   1.5994   0.03520   0.03084  -0.0394   0.0099   0.8124
  14.750   1.5978   0.03877   0.03470  -0.0339   0.0097   0.8214
  15.000   1.5939   0.04107   0.03716  -0.0316   0.0097   0.8263
  15.250   1.5882   0.04377   0.04001  -0.0300   0.0096   0.8311
  15.500   1.5810   0.04691   0.04331  -0.0291   0.0096   0.8362
  15.750   1.5695   0.05092   0.04750  -0.0290   0.0095   0.8417
  16.000   1.5540   0.05603   0.05279  -0.0303   0.0095   0.8466
  16.250   1.5316   0.06304   0.06002  -0.0337   0.0095   0.8511
  16.500   1.4949   0.07446   0.07170  -0.0414   0.0095   0.8548
  16.750   1.3409   0.11385   0.11162  -0.0663   0.0098   0.8484
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