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S1016 (s1016-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S1016 (s1016-il)
Reynolds number: 500,000
Max Cl/Cd: 41.77 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1016-il-500000-n5.txt
Download as CSV file: xf-s1016-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1016                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1231   0.08385   0.07886  -0.0565   0.8716   0.0235
 -19.500  -1.1331   0.07882   0.07372  -0.0590   0.8699   0.0239
 -19.250  -1.1412   0.07420   0.06897  -0.0611   0.8681   0.0244
 -19.000  -1.1462   0.07017   0.06481  -0.0628   0.8664   0.0249
 -18.750  -1.1512   0.06625   0.06077  -0.0644   0.8647   0.0253
 -18.500  -1.1541   0.06273   0.05713  -0.0656   0.8630   0.0259
 -18.250  -1.1585   0.05917   0.05347  -0.0666   0.8614   0.0265
 -17.750  -1.1607   0.05315   0.04727  -0.0680   0.8586   0.0279
 -17.500  -1.1589   0.05060   0.04464  -0.0683   0.8573   0.0286
 -17.250  -1.1551   0.04834   0.04228  -0.0685   0.8560   0.0295
 -17.000  -1.1505   0.04623   0.04009  -0.0686   0.8547   0.0304
 -16.750  -1.1477   0.04402   0.03782  -0.0684   0.8534   0.0312
 -16.500  -1.1430   0.04208   0.03581  -0.0682   0.8521   0.0321
 -16.250  -1.1367   0.04035   0.03401  -0.0678   0.8508   0.0332
 -16.000  -1.1290   0.03880   0.03238  -0.0673   0.8496   0.0343
 -15.750  -1.1199   0.03740   0.03090  -0.0668   0.8484   0.0353
 -15.500  -1.1132   0.03586   0.02931  -0.0661   0.8471   0.0367
 -15.250  -1.1044   0.03455   0.02795  -0.0653   0.8458   0.0381
 -15.000  -1.0942   0.03337   0.02670  -0.0645   0.8445   0.0394
 -14.750  -1.0830   0.03230   0.02555  -0.0638   0.8434   0.0407
 -14.500  -1.0728   0.03117   0.02438  -0.0629   0.8424   0.0421
 -14.250  -1.0615   0.03013   0.02331  -0.0620   0.8416   0.0437
 -14.000  -1.0489   0.02920   0.02233  -0.0611   0.8408   0.0455
 -13.750  -1.0349   0.02837   0.02145  -0.0603   0.8400   0.0470
 -13.500  -1.0230   0.02744   0.02051  -0.0593   0.8391   0.0491
 -13.250  -1.0093   0.02663   0.01967  -0.0584   0.8382   0.0511
 -13.000  -0.9945   0.02591   0.01891  -0.0575   0.8373   0.0532
 -12.750  -0.9796   0.02521   0.01816  -0.0566   0.8364   0.0550
 -12.500  -0.9655   0.02446   0.01742  -0.0555   0.8355   0.0575
 -12.250  -0.9497   0.02383   0.01676  -0.0546   0.8347   0.0600
 -12.000  -0.9330   0.02326   0.01615  -0.0537   0.8338   0.0625
 -11.750  -0.9182   0.02259   0.01548  -0.0526   0.8330   0.0655
 -11.500  -0.9015   0.02203   0.01490  -0.0517   0.8322   0.0687
 -11.250  -0.8836   0.02154   0.01438  -0.0509   0.8314   0.0717
 -11.000  -0.8675   0.02096   0.01381  -0.0498   0.8306   0.0754
 -10.750  -0.8501   0.02046   0.01330  -0.0489   0.8299   0.0792
 -10.500  -0.8318   0.02002   0.01283  -0.0480   0.8292   0.0826
 -10.250  -0.8145   0.01952   0.01234  -0.0470   0.8284   0.0867
 -10.000  -0.7960   0.01910   0.01190  -0.0461   0.8276   0.0909
  -9.750  -0.7775   0.01869   0.01148  -0.0451   0.8266   0.0950
  -9.500  -0.7594   0.01826   0.01106  -0.0441   0.8258   0.1001
  -9.250  -0.7396   0.01790   0.01069  -0.0434   0.8253   0.1048
  -9.000  -0.7208   0.01749   0.01031  -0.0425   0.8247   0.1099
  -8.750  -0.7013   0.01712   0.00995  -0.0416   0.8240   0.1158
  -8.500  -0.6815   0.01677   0.00961  -0.0408   0.8234   0.1209
  -8.250  -0.6623   0.01640   0.00927  -0.0398   0.8227   0.1275
  -7.750  -0.6225   0.01573   0.00865  -0.0381   0.8212   0.1410
  -7.250  -0.5826   0.01510   0.00808  -0.0363   0.8196   0.1563
  -7.000  -0.5622   0.01481   0.00781  -0.0354   0.8187   0.1649
  -6.750  -0.5428   0.01448   0.00753  -0.0344   0.8176   0.1754
  -6.500  -0.5233   0.01417   0.00727  -0.0334   0.8167   0.1863
  -6.250  -0.5032   0.01390   0.00703  -0.0324   0.8159   0.1971
  -6.000  -0.4837   0.01360   0.00678  -0.0313   0.8151   0.2101
  -5.750  -0.4650   0.01328   0.00654  -0.0301   0.8143   0.2248
  -5.500  -0.4462   0.01298   0.00630  -0.0289   0.8135   0.2393
  -5.250  -0.4281   0.01267   0.00605  -0.0275   0.8124   0.2562
  -5.000  -0.4104   0.01235   0.00581  -0.0260   0.8114   0.2745
  -4.750  -0.3936   0.01204   0.00558  -0.0244   0.8106   0.2948
  -4.500  -0.3787   0.01174   0.00537  -0.0223   0.8096   0.3176
  -4.250  -0.3655   0.01148   0.00521  -0.0199   0.8085   0.3406
  -4.000  -0.3539   0.01125   0.00510  -0.0171   0.8072   0.3660
  -3.750  -0.3422   0.01101   0.00499  -0.0143   0.8057   0.3940
  -3.500  -0.3285   0.01072   0.00486  -0.0119   0.8039   0.4265
  -3.250  -0.3137   0.01044   0.00473  -0.0097   0.8022   0.4606
  -3.000  -0.2994   0.01010   0.00457  -0.0074   0.8003   0.5013
  -2.750  -0.2837   0.00976   0.00442  -0.0052   0.7986   0.5444
  -2.500  -0.2674   0.00940   0.00428  -0.0032   0.7970   0.5921
  -2.250  -0.2486   0.00910   0.00422  -0.0014   0.7955   0.6421
  -2.000  -0.2246   0.00904   0.00438  -0.0005   0.7941   0.6847
  -1.750  -0.1967   0.00913   0.00453  -0.0002   0.7926   0.7119
  -1.500  -0.1692   0.00920   0.00461  -0.0001   0.7903   0.7278
  -1.250  -0.1421   0.00926   0.00469   0.0000   0.7867   0.7382
  -1.000  -0.1142   0.00925   0.00467   0.0001   0.7829   0.7459
  -0.750  -0.0855   0.00921   0.00460   0.0001   0.7794   0.7523
  -0.500  -0.0573   0.00910   0.00442   0.0001   0.7764   0.7587
  -0.250  -0.0279   0.00915   0.00449  -0.0001   0.7728   0.7625
   0.000   0.0000   0.00920   0.00457   0.0000   0.7672   0.7672
   0.250   0.0279   0.00914   0.00449   0.0001   0.7624   0.7728
   0.500   0.0573   0.00910   0.00442  -0.0001   0.7587   0.7764
   0.750   0.0855   0.00921   0.00460  -0.0001   0.7524   0.7794
   1.000   0.1142   0.00925   0.00467  -0.0001   0.7458   0.7829
   1.250   0.1421   0.00926   0.00469   0.0000   0.7382   0.7867
   1.500   0.1692   0.00920   0.00461   0.0001   0.7279   0.7903
   1.750   0.1967   0.00913   0.00453   0.0002   0.7120   0.7926
   2.000   0.2246   0.00904   0.00437   0.0005   0.6843   0.7941
   2.250   0.2484   0.00911   0.00422   0.0015   0.6411   0.7955
   2.500   0.2673   0.00941   0.00428   0.0032   0.5913   0.7970
   2.750   0.2838   0.00976   0.00442   0.0052   0.5446   0.7986
   3.000   0.2997   0.01009   0.00457   0.0073   0.5026   0.8003
   3.250   0.3142   0.01043   0.00473   0.0096   0.4620   0.8022
   3.500   0.3285   0.01072   0.00486   0.0119   0.4266   0.8039
   3.750   0.3424   0.01100   0.00499   0.0143   0.3944   0.8057
   4.000   0.3542   0.01125   0.00510   0.0171   0.3667   0.8072
   4.250   0.3658   0.01148   0.00521   0.0198   0.3410   0.8085
   4.500   0.3791   0.01173   0.00537   0.0223   0.3182   0.8097
   4.750   0.3938   0.01204   0.00558   0.0243   0.2950   0.8106
   5.000   0.4106   0.01235   0.00581   0.0260   0.2747   0.8114
   5.250   0.4280   0.01267   0.00605   0.0275   0.2554   0.8124
   5.500   0.4463   0.01298   0.00630   0.0289   0.2394   0.8135
   5.750   0.4650   0.01329   0.00654   0.0301   0.2241   0.8143
   6.000   0.4839   0.01359   0.00678   0.0313   0.2100   0.8151
   6.250   0.5033   0.01390   0.00703   0.0324   0.1969   0.8159
   6.500   0.5233   0.01418   0.00727   0.0334   0.1854   0.8167
   6.750   0.5430   0.01448   0.00753   0.0344   0.1754   0.8176
   7.000   0.5623   0.01481   0.00781   0.0354   0.1646   0.8187
   7.250   0.5829   0.01509   0.00807   0.0363   0.1565   0.8197
   7.750   0.6228   0.01573   0.00865   0.0381   0.1408   0.8212
   8.000   0.6420   0.01609   0.00896   0.0390   0.1334   0.8220
   8.250   0.6626   0.01639   0.00927   0.0398   0.1273   0.8227
   8.500   0.6819   0.01676   0.00960   0.0407   0.1210   0.8234
   8.750   0.7017   0.01711   0.00994   0.0415   0.1155   0.8240
   9.000   0.7211   0.01748   0.01030   0.0424   0.1098   0.8247
   9.250   0.7400   0.01789   0.01069   0.0433   0.1047   0.8253
   9.500   0.7598   0.01825   0.01105   0.0441   0.1000   0.8259
   9.750   0.7777   0.01869   0.01147   0.0451   0.0947   0.8266
  10.000   0.7964   0.01909   0.01189   0.0460   0.0907   0.8275
  10.250   0.8149   0.01951   0.01233   0.0469   0.0865   0.8284
  10.500   0.8322   0.02001   0.01282   0.0479   0.0823   0.8292
  10.750   0.8507   0.02045   0.01328   0.0488   0.0790   0.8299
  11.000   0.8680   0.02095   0.01380   0.0498   0.0753   0.8306
  11.250   0.8842   0.02153   0.01436   0.0508   0.0716   0.8314
  11.500   0.9021   0.02202   0.01489   0.0516   0.0686   0.8322
  11.750   0.9187   0.02259   0.01547   0.0526   0.0653   0.8330
  12.000   0.9336   0.02325   0.01613   0.0537   0.0624   0.8339
  12.250   0.9504   0.02382   0.01674   0.0545   0.0601   0.8347
  12.500   0.9662   0.02445   0.01740   0.0554   0.0575   0.8355
  12.750   0.9805   0.02519   0.01814   0.0565   0.0550   0.8364
  13.000   0.9953   0.02588   0.01888   0.0574   0.0531   0.8373
  13.250   1.0101   0.02660   0.01965   0.0583   0.0511   0.8382
  13.500   1.0238   0.02741   0.02048   0.0592   0.0491   0.8391
  13.750   1.0357   0.02835   0.02143   0.0602   0.0472   0.8400
  14.000   1.0498   0.02917   0.02230   0.0610   0.0454   0.8408
  14.250   1.0625   0.03009   0.02327   0.0619   0.0439   0.8417
  14.500   1.0737   0.03114   0.02435   0.0628   0.0421   0.8425
  14.750   1.0838   0.03228   0.02552   0.0637   0.0407   0.8435
  15.000   1.0953   0.03332   0.02665   0.0644   0.0393   0.8446
  15.250   1.1056   0.03449   0.02788   0.0652   0.0380   0.8459
  15.500   1.1144   0.03580   0.02925   0.0659   0.0366   0.8471
  15.750   1.1216   0.03731   0.03081   0.0667   0.0355   0.8484
  16.000   1.1305   0.03871   0.03229   0.0672   0.0342   0.8497
  16.250   1.1381   0.04027   0.03393   0.0677   0.0332   0.8509
  16.500   1.1443   0.04200   0.03573   0.0681   0.0321   0.8522
  16.750   1.1494   0.04391   0.03769   0.0683   0.0311   0.8535
  17.000   1.1521   0.04611   0.03995   0.0685   0.0303   0.8548
  17.250   1.1568   0.04821   0.04215   0.0684   0.0295   0.8561
  17.500   1.1605   0.05048   0.04451   0.0683   0.0285   0.8574
  17.750   1.1626   0.05299   0.04711   0.0679   0.0280   0.8587
  18.000   1.1626   0.05583   0.05003   0.0674   0.0270   0.8601
  18.250   1.1604   0.05900   0.05330   0.0666   0.0264   0.8616
  18.500   1.1568   0.06248   0.05688   0.0655   0.0260   0.8632
  18.750   1.1536   0.06601   0.06053   0.0643   0.0254   0.8649
  19.000   1.1495   0.06981   0.06446   0.0628   0.0249   0.8667
  19.250   1.1434   0.07400   0.06876   0.0611   0.0244   0.8684
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