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S1014 (s1014-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: S1014 (s1014-il)
Reynolds number: 50,000
Max Cl/Cd: 20.31 at α=9.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1014-il-50000-n5.txt
Download as CSV file: xf-s1014-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1014                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.6134   0.11152   0.10380  -0.0485   1.0000   0.0937
 -14.250  -0.6938   0.09148   0.08369  -0.0601   1.0000   0.0931
 -14.000  -0.7607   0.07916   0.07116  -0.0660   1.0000   0.0918
 -13.750  -0.7978   0.07250   0.06426  -0.0675   1.0000   0.0921
 -13.500  -0.8235   0.06767   0.05919  -0.0675   1.0000   0.0930
 -13.250  -0.8439   0.06371   0.05499  -0.0667   1.0000   0.0942
 -13.000  -0.8629   0.06028   0.05128  -0.0652   1.0000   0.0958
 -12.750  -0.8818   0.05735   0.04802  -0.0627   1.0000   0.0975
 -12.500  -0.8880   0.05542   0.04598  -0.0603   1.0000   0.0995
 -12.250  -0.8883   0.05435   0.04493  -0.0577   1.0000   0.1019
 -12.000  -0.8984   0.05330   0.04378  -0.0536   1.0000   0.1038
 -11.750  -0.9107   0.05219   0.04253  -0.0491   1.0000   0.1058
 -11.500  -0.9237   0.05103   0.04118  -0.0444   1.0000   0.1080
 -11.250  -0.9376   0.04985   0.03973  -0.0394   1.0000   0.1104
 -11.000  -0.9402   0.04871   0.03846  -0.0357   1.0000   0.1132
 -10.750  -0.9355   0.04780   0.03756  -0.0329   1.0000   0.1165
 -10.500  -0.9228   0.04644   0.03602  -0.0318   0.9972   0.1215
 -10.250  -0.9063   0.04496   0.03427  -0.0313   0.9939   0.1274
 -10.000  -0.8842   0.04386   0.03317  -0.0313   0.9914   0.1335
  -9.750  -0.8661   0.04266   0.03165  -0.0306   0.9889   0.1407
  -9.500  -0.8410   0.04170   0.03080  -0.0308   0.9871   0.1481
  -9.250  -0.8168   0.04073   0.02961  -0.0308   0.9852   0.1571
  -9.000  -0.7913   0.03994   0.02885  -0.0309   0.9837   0.1666
  -8.750  -0.7641   0.03919   0.02806  -0.0313   0.9823   0.1776
  -8.500  -0.7399   0.03850   0.02729  -0.0311   0.9805   0.1899
  -8.250  -0.7194   0.03784   0.02662  -0.0304   0.9783   0.2030
  -8.000  -0.6995   0.03718   0.02601  -0.0297   0.9761   0.2171
  -7.750  -0.6818   0.03652   0.02541  -0.0287   0.9740   0.2336
  -7.500  -0.6657   0.03587   0.02482  -0.0275   0.9721   0.2523
  -7.250  -0.6519   0.03520   0.02428  -0.0261   0.9704   0.2733
  -7.000  -0.6402   0.03451   0.02376  -0.0243   0.9687   0.2989
  -6.750  -0.6351   0.03385   0.02330  -0.0211   0.9663   0.3267
  -6.500  -0.6297   0.03319   0.02291  -0.0180   0.9636   0.3633
  -6.250  -0.6206   0.03269   0.02278  -0.0151   0.9613   0.4125
  -6.000  -0.5884   0.03327   0.02390  -0.0141   0.9605   0.4899
  -5.750  -0.5340   0.03557   0.02643  -0.0148   0.9604   0.5577
  -5.500  -0.5019   0.03706   0.02784  -0.0136   0.9591   0.5956
  -5.250  -0.4810   0.03795   0.02859  -0.0118   0.9571   0.6264
  -5.000  -0.4648   0.03862   0.02911  -0.0096   0.9549   0.6550
  -4.750  -0.4579   0.03922   0.02960  -0.0057   0.9525   0.6779
  -4.500  -0.4576   0.03960   0.02988  -0.0011   0.9496   0.7007
  -4.250  -0.4404   0.04034   0.03048   0.0012   0.9471   0.7200
  -4.000  -0.4229   0.04098   0.03100   0.0033   0.9449   0.7385
  -3.750  -0.3979   0.04167   0.03154   0.0042   0.9431   0.7554
  -3.500  -0.3645   0.04236   0.03210   0.0036   0.9415   0.7710
  -3.250  -0.3309   0.04292   0.03254   0.0029   0.9399   0.7857
  -3.000  -0.3098   0.04324   0.03276   0.0042   0.9375   0.7999
  -2.750  -0.2897   0.04346   0.03289   0.0055   0.9349   0.8139
  -2.500  -0.2557   0.04365   0.03299   0.0042   0.9328   0.8250
  -2.250  -0.2225   0.04371   0.03296   0.0027   0.9305   0.8344
  -2.000  -0.2040   0.04374   0.03291   0.0037   0.9276   0.8457
  -1.750  -0.1602   0.04373   0.03282   0.0001   0.9258   0.8521
  -1.500  -0.1523   0.04369   0.03273   0.0029   0.9219   0.8622
  -1.250  -0.1197   0.04360   0.03260   0.0013   0.9187   0.8680
  -1.000  -0.1057   0.04359   0.03254   0.0028   0.9145   0.8766
  -0.750  -0.0685   0.04353   0.03245   0.0002   0.9116   0.8813
  -0.500  -0.0387   0.04351   0.03241  -0.0012   0.9081   0.8869
  -0.250  -0.0347   0.04349   0.03238   0.0023   0.9021   0.8941
   0.000   0.0000   0.04344   0.03233   0.0000   0.8979   0.8979
   0.250   0.0346   0.04349   0.03238  -0.0023   0.8942   0.9021
   0.500   0.0388   0.04351   0.03241   0.0012   0.8869   0.9081
   0.750   0.0683   0.04352   0.03244  -0.0001   0.8813   0.9116
   1.000   0.1058   0.04358   0.03254  -0.0029   0.8766   0.9145
   1.250   0.1198   0.04359   0.03259  -0.0013   0.8680   0.9187
   1.500   0.1522   0.04368   0.03272  -0.0029   0.8622   0.9219
   1.750   0.1604   0.04372   0.03281  -0.0002   0.8521   0.9259
   2.000   0.2040   0.04373   0.03290  -0.0037   0.8457   0.9277
   2.250   0.2224   0.04371   0.03295  -0.0027   0.8345   0.9305
   2.500   0.2558   0.04364   0.03298  -0.0042   0.8251   0.9328
   2.750   0.2893   0.04345   0.03288  -0.0054   0.8140   0.9349
   3.000   0.3094   0.04323   0.03275  -0.0042   0.8000   0.9376
   3.250   0.3307   0.04291   0.03253  -0.0029   0.7858   0.9400
   3.500   0.3645   0.04235   0.03209  -0.0037   0.7711   0.9415
   3.750   0.3982   0.04165   0.03153  -0.0042   0.7554   0.9431
   4.000   0.4231   0.04097   0.03099  -0.0033   0.7387   0.9449
   4.250   0.4404   0.04033   0.03047  -0.0012   0.7201   0.9471
   4.500   0.4573   0.03961   0.02988   0.0011   0.7008   0.9496
   4.750   0.4583   0.03921   0.02959   0.0057   0.6781   0.9525
   5.250   0.4812   0.03793   0.02856   0.0118   0.6264   0.9571
   5.500   0.5020   0.03705   0.02782   0.0136   0.5957   0.9591
   5.750   0.5342   0.03555   0.02641   0.0147   0.5577   0.9604
   6.000   0.5884   0.03326   0.02388   0.0141   0.4899   0.9606
   6.250   0.6207   0.03268   0.02275   0.0151   0.4124   0.9614
   6.500   0.6298   0.03317   0.02289   0.0180   0.3632   0.9636
   6.750   0.6352   0.03384   0.02328   0.0211   0.3265   0.9663
   7.000   0.6402   0.03449   0.02374   0.0243   0.2986   0.9688
   7.250   0.6523   0.03518   0.02426   0.0260   0.2733   0.9705
   7.500   0.6659   0.03586   0.02481   0.0275   0.2519   0.9722
   7.750   0.6821   0.03651   0.02539   0.0287   0.2335   0.9740
   8.000   0.7000   0.03717   0.02600   0.0296   0.2170   0.9762
   8.250   0.7199   0.03783   0.02659   0.0303   0.2030   0.9784
   8.500   0.7404   0.03848   0.02727   0.0310   0.1899   0.9806
   8.750   0.7645   0.03917   0.02804   0.0312   0.1776   0.9823
   9.000   0.7920   0.03992   0.02883   0.0308   0.1666   0.9837
   9.250   0.8175   0.04072   0.02960   0.0306   0.1571   0.9853
   9.500   0.8412   0.04169   0.03078   0.0307   0.1480   0.9871
   9.750   0.8661   0.04265   0.03165   0.0306   0.1405   0.9890
  10.000   0.8845   0.04385   0.03316   0.0312   0.1335   0.9915
  10.250   0.9065   0.04493   0.03424   0.0312   0.1273   0.9940
  10.500   0.9234   0.04644   0.03602   0.0317   0.1214   0.9973
  10.750   0.9358   0.04779   0.03755   0.0329   0.1165   1.0000
  11.000   0.9399   0.04865   0.03840   0.0358   0.1131   1.0000
  11.250   0.9378   0.04984   0.03971   0.0394   0.1104   1.0000
  11.500   0.9238   0.05101   0.04116   0.0444   0.1079   1.0000
  11.750   0.9107   0.05216   0.04249   0.0491   0.1058   1.0000
  12.000   0.8984   0.05326   0.04375   0.0536   0.1038   1.0000
  12.250   0.8885   0.05431   0.04488   0.0577   0.1018   1.0000
  12.500   0.8887   0.05538   0.04593   0.0603   0.0994   1.0000
  12.750   0.8814   0.05735   0.04803   0.0627   0.0974   1.0000
  13.000   0.8634   0.06029   0.05129   0.0651   0.0958   1.0000
  13.250   0.8448   0.06371   0.05498   0.0666   0.0942   1.0000
  13.500   0.8241   0.06768   0.05920   0.0674   0.0928   1.0000
  13.750   0.7989   0.07251   0.06427   0.0673   0.0920   1.0000
  14.000   0.7622   0.07912   0.07111   0.0658   0.0917   1.0000
  14.250   0.6946   0.09155   0.08376   0.0599   0.0930   1.0000
  14.500   0.6141   0.11168   0.10397   0.0482   0.0936   1.0000
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