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S8037 (16%) (s8037-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S8037 (16%) (s8037-il)
Reynolds number: 200,000
Max Cl/Cd: 68.95 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8037-il-200000-n5.txt
Download as CSV file: xf-s8037-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8037 (16%)                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.5893   0.07216   0.06795  -0.0680   1.0000   0.0145
 -13.000  -0.6284   0.06271   0.05825  -0.0741   1.0000   0.0145
 -12.750  -0.6538   0.05675   0.05208  -0.0768   1.0000   0.0143
 -12.500  -0.6748   0.05214   0.04728  -0.0779   1.0000   0.0143
 -12.250  -0.6957   0.04807   0.04300  -0.0777   1.0000   0.0143
 -12.000  -0.7120   0.04510   0.03982  -0.0764   1.0000   0.0147
 -11.750  -0.7262   0.04253   0.03706  -0.0741   1.0000   0.0148
 -11.500  -0.7383   0.04043   0.03478  -0.0710   1.0000   0.0149
 -11.250  -0.7543   0.03858   0.03269  -0.0667   1.0000   0.0153
 -11.000  -0.7529   0.03625   0.03003  -0.0651   0.9939   0.0155
 -10.750  -0.7390   0.03432   0.02796  -0.0651   0.9755   0.0160
 -10.500  -0.7195   0.03290   0.02644  -0.0655   0.9558   0.0164
 -10.250  -0.6929   0.03116   0.02452  -0.0671   0.9419   0.0169
 -10.000  -0.6619   0.02927   0.02238  -0.0694   0.9298   0.0174
  -9.750  -0.6289   0.02748   0.02034  -0.0717   0.9168   0.0181
  -9.500  -0.5945   0.02583   0.01839  -0.0741   0.9035   0.0188
  -9.250  -0.5625   0.02448   0.01694  -0.0760   0.8893   0.0195
  -9.000  -0.5343   0.02354   0.01590  -0.0770   0.8748   0.0204
  -8.750  -0.5085   0.02269   0.01490  -0.0773   0.8613   0.0214
  -8.500  -0.4861   0.02189   0.01389  -0.0767   0.8482   0.0226
  -8.250  -0.4677   0.02112   0.01307  -0.0755   0.8362   0.0234
  -8.000  -0.4490   0.02047   0.01234  -0.0742   0.8260   0.0242
  -7.750  -0.4312   0.01987   0.01165  -0.0726   0.8161   0.0254
  -7.500  -0.4129   0.01933   0.01097  -0.0710   0.8075   0.0267
  -7.250  -0.3957   0.01878   0.01037  -0.0693   0.7990   0.0283
  -7.000  -0.3770   0.01833   0.00985  -0.0678   0.7915   0.0300
  -6.250  -0.3214   0.01697   0.00827  -0.0629   0.7706   0.0382
  -6.000  -0.3021   0.01654   0.00781  -0.0614   0.7642   0.0434
  -5.750  -0.2824   0.01613   0.00738  -0.0599   0.7585   0.0508
  -5.500  -0.2628   0.01575   0.00700  -0.0584   0.7520   0.0616
  -5.250  -0.2428   0.01536   0.00663  -0.0570   0.7464   0.0771
  -4.750  -0.2031   0.01461   0.00603  -0.0542   0.7348   0.1253
  -4.500  -0.1841   0.01418   0.00573  -0.0527   0.7296   0.1645
  -4.250  -0.1672   0.01363   0.00545  -0.0508   0.7247   0.2266
  -4.000  -0.1534   0.01301   0.00521  -0.0484   0.7189   0.3124
  -3.750  -0.1385   0.01251   0.00503  -0.0460   0.7137   0.3954
  -3.500  -0.1207   0.01219   0.00491  -0.0439   0.7094   0.4628
  -3.250  -0.1017   0.01198   0.00487  -0.0420   0.7038   0.5144
  -3.000  -0.0804   0.01186   0.00482  -0.0405   0.6986   0.5557
  -2.750  -0.0572   0.01179   0.00475  -0.0394   0.6942   0.5888
  -2.500  -0.0347   0.01173   0.00473  -0.0381   0.6893   0.6179
  -2.250  -0.0115   0.01168   0.00471  -0.0370   0.6839   0.6422
  -2.000   0.0129   0.01164   0.00466  -0.0361   0.6792   0.6640
  -1.750   0.0372   0.01162   0.00463  -0.0351   0.6747   0.6864
  -1.500   0.0605   0.01160   0.00464  -0.0340   0.6691   0.7077
  -1.250   0.0855   0.01158   0.00461  -0.0332   0.6641   0.7250
  -0.750   0.1374   0.01156   0.00458  -0.0321   0.6540   0.7528
  -0.500   0.1636   0.01154   0.00456  -0.0317   0.6486   0.7654
  -0.250   0.1907   0.01154   0.00450  -0.0314   0.6441   0.7780
   0.000   0.2169   0.01155   0.00452  -0.0310   0.6383   0.7906
   0.250   0.2448   0.01155   0.00454  -0.0309   0.6327   0.8031
   0.500   0.2739   0.01156   0.00452  -0.0311   0.6279   0.8161
   0.750   0.3021   0.01159   0.00457  -0.0311   0.6221   0.8298
   1.000   0.3327   0.01162   0.00461  -0.0316   0.6160   0.8429
   1.250   0.3675   0.01167   0.00462  -0.0330   0.6110   0.8547
   1.500   0.4010   0.01174   0.00473  -0.0342   0.6040   0.8669
   1.750   0.4355   0.01181   0.00477  -0.0356   0.5975   0.8792
   2.000   0.4752   0.01191   0.00487  -0.0381   0.5906   0.8881
   2.250   0.5111   0.01201   0.00496  -0.0398   0.5832   0.8985
   2.500   0.5505   0.01212   0.00505  -0.0423   0.5763   0.9064
   2.750   0.5862   0.01223   0.00517  -0.0440   0.5679   0.9153
   3.000   0.6240   0.01236   0.00526  -0.0462   0.5603   0.9222
   3.250   0.6567   0.01250   0.00540  -0.0472   0.5513   0.9314
   3.500   0.6914   0.01265   0.00553  -0.0487   0.5429   0.9385
   3.750   0.7225   0.01280   0.00568  -0.0495   0.5337   0.9472
   4.000   0.7548   0.01296   0.00584  -0.0506   0.5246   0.9552
   4.250   0.7866   0.01312   0.00597  -0.0516   0.5149   0.9631
   4.500   0.8162   0.01329   0.00616  -0.0522   0.5041   0.9722
   4.750   0.8494   0.01346   0.00631  -0.0536   0.4928   0.9790
   5.000   0.8816   0.01364   0.00646  -0.0548   0.4806   0.9857
   5.250   0.9155   0.01383   0.00663  -0.0564   0.4677   0.9916
   5.500   0.9499   0.01401   0.00681  -0.0582   0.4536   0.9967
   5.750   0.9791   0.01420   0.00698  -0.0589   0.4394   1.0000
   6.000   0.9926   0.01441   0.00716  -0.0564   0.4272   1.0000
   6.250   1.0056   0.01465   0.00737  -0.0537   0.4144   1.0000
   6.500   1.0179   0.01492   0.00760  -0.0509   0.4012   1.0000
   6.750   1.0299   0.01521   0.00786  -0.0481   0.3877   1.0000
   7.000   1.0412   0.01553   0.00815  -0.0451   0.3735   1.0000
   7.250   1.0513   0.01589   0.00846  -0.0420   0.3592   1.0000
   7.500   1.0602   0.01627   0.00881  -0.0387   0.3449   1.0000
   7.750   1.0677   0.01669   0.00918  -0.0351   0.3306   1.0000
   8.000   1.0723   0.01711   0.00956  -0.0310   0.3174   1.0000
   8.250   1.0745   0.01754   0.00994  -0.0265   0.3052   1.0000
   8.500   1.0774   0.01803   0.01039  -0.0223   0.2928   1.0000
   8.750   1.0828   0.01855   0.01089  -0.0186   0.2807   1.0000
   9.000   1.0886   0.01912   0.01145  -0.0153   0.2696   1.0000
   9.250   1.0937   0.01979   0.01209  -0.0120   0.2590   1.0000
   9.500   1.1000   0.02049   0.01279  -0.0091   0.2483   1.0000
   9.750   1.1073   0.02123   0.01353  -0.0065   0.2384   1.0000
  10.000   1.1128   0.02211   0.01439  -0.0038   0.2288   1.0000
  10.250   1.1200   0.02299   0.01528  -0.0016   0.2190   1.0000
  10.500   1.1268   0.02395   0.01625   0.0006   0.2098   1.0000
  10.750   1.1321   0.02506   0.01734   0.0027   0.2009   1.0000
  11.000   1.1404   0.02607   0.01839   0.0044   0.1921   1.0000
  11.250   1.1457   0.02730   0.01961   0.0062   0.1839   1.0000
  11.500   1.1532   0.02847   0.02080   0.0078   0.1755   1.0000
  11.750   1.1591   0.02977   0.02213   0.0093   0.1684   1.0000
  12.000   1.1655   0.03109   0.02347   0.0107   0.1604   1.0000
  12.250   1.1711   0.03251   0.02491   0.0120   0.1541   1.0000
  12.500   1.1775   0.03392   0.02636   0.0132   0.1470   1.0000
  12.750   1.1816   0.03554   0.02799   0.0144   0.1413   1.0000
  13.000   1.1884   0.03699   0.02952   0.0154   0.1349   1.0000
  13.250   1.1912   0.03879   0.03133   0.0164   0.1295   1.0000
  13.500   1.1975   0.04037   0.03298   0.0172   0.1241   1.0000
  13.750   1.2015   0.04217   0.03482   0.0180   0.1188   1.0000
  14.000   1.2039   0.04416   0.03684   0.0188   0.1143   1.0000
  14.250   1.2095   0.04593   0.03869   0.0194   0.1094   1.0000
  14.500   1.2117   0.04807   0.04086   0.0200   0.1049   1.0000
  14.750   1.2140   0.05024   0.04310   0.0204   0.1011   1.0000
  15.000   1.2185   0.05225   0.04519   0.0208   0.0971   1.0000
  15.250   1.2197   0.05464   0.04764   0.0210   0.0934   1.0000
  15.500   1.2194   0.05725   0.05027   0.0212   0.0903   1.0000
  15.750   1.2233   0.05947   0.05261   0.0213   0.0867   1.0000
  16.000   1.2244   0.06204   0.05525   0.0213   0.0834   1.0000
  16.250   1.2226   0.06497   0.05822   0.0212   0.0806   1.0000
  16.500   1.2226   0.06775   0.06108   0.0210   0.0780   1.0000
  16.750   1.2242   0.07040   0.06384   0.0208   0.0753   1.0000
  17.000   1.2239   0.07334   0.06687   0.0204   0.0729   1.0000
  17.250   1.2209   0.07664   0.07022   0.0199   0.0705   1.0000
  17.500   1.2171   0.08008   0.07369   0.0193   0.0684   1.0000
  17.750   1.2178   0.08301   0.07676   0.0187   0.0664   1.0000
  18.000   1.2165   0.08625   0.08012   0.0180   0.0643   1.0000
  18.250   1.2134   0.08978   0.08374   0.0171   0.0623   1.0000
  18.500   1.2092   0.09348   0.08750   0.0161   0.0606   1.0000
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