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S8037 (16%) (s8037-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: S8037 (16%) (s8037-il)
Reynolds number: 100,000
Max Cl/Cd: 48.32 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8037-il-100000-n5.txt
Download as CSV file: xf-s8037-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.4565   0.08924   0.08397  -0.0595   1.0000   0.0266
 -12.000  -0.4936   0.07786   0.07251  -0.0667   1.0000   0.0262
 -11.750  -0.5242   0.07018   0.06475  -0.0714   1.0000   0.0258
 -11.500  -0.5514   0.06451   0.05896  -0.0738   1.0000   0.0255
 -11.250  -0.5804   0.05975   0.05404  -0.0745   1.0000   0.0254
 -11.000  -0.6059   0.05618   0.05033  -0.0732   1.0000   0.0254
 -10.750  -0.6310   0.05336   0.04738  -0.0702   1.0000   0.0254
 -10.500  -0.6555   0.05133   0.04523  -0.0656   1.0000   0.0253
 -10.250  -0.6821   0.05023   0.04409  -0.0593   0.9998   0.0253
 -10.000  -0.6774   0.04608   0.03948  -0.0604   0.9825   0.0257
  -9.750  -0.6704   0.04263   0.03554  -0.0602   0.9637   0.0264
  -9.500  -0.6562   0.03984   0.03231  -0.0604   0.9503   0.0275
  -9.250  -0.6312   0.03808   0.03044  -0.0616   0.9410   0.0286
  -9.000  -0.6058   0.03589   0.02795  -0.0627   0.9319   0.0296
  -8.750  -0.5795   0.03364   0.02536  -0.0635   0.9227   0.0306
  -8.500  -0.5491   0.03145   0.02274  -0.0647   0.9151   0.0320
  -8.250  -0.5205   0.03002   0.02128  -0.0657   0.9058   0.0333
  -8.000  -0.4896   0.02877   0.01989  -0.0670   0.8980   0.0355
  -7.750  -0.4612   0.02745   0.01831  -0.0674   0.8886   0.0379
  -7.500  -0.4325   0.02619   0.01706  -0.0682   0.8808   0.0397
  -7.250  -0.4093   0.02526   0.01604  -0.0678   0.8707   0.0422
  -7.000  -0.3829   0.02430   0.01497  -0.0679   0.8631   0.0457
  -6.750  -0.3636   0.02357   0.01421  -0.0667   0.8532   0.0496
  -6.500  -0.3407   0.02272   0.01324  -0.0660   0.8459   0.0542
  -6.250  -0.3232   0.02211   0.01259  -0.0643   0.8365   0.0607
  -6.000  -0.3020   0.02139   0.01184  -0.0633   0.8295   0.0706
  -5.750  -0.2854   0.02080   0.01127  -0.0615   0.8210   0.0836
  -5.500  -0.2659   0.02014   0.01068  -0.0602   0.8141   0.1044
  -5.250  -0.2487   0.01955   0.01022  -0.0585   0.8068   0.1353
  -5.000  -0.2324   0.01889   0.00978  -0.0566   0.7995   0.1818
  -4.750  -0.2166   0.01811   0.00935  -0.0547   0.7937   0.2559
  -4.500  -0.2064   0.01747   0.00913  -0.0517   0.7858   0.3429
  -4.250  -0.1911   0.01695   0.00897  -0.0492   0.7799   0.4369
  -4.000  -0.1745   0.01673   0.00898  -0.0467   0.7735   0.5080
  -3.750  -0.1553   0.01665   0.00899  -0.0447   0.7669   0.5602
  -3.500  -0.1321   0.01660   0.00891  -0.0433   0.7619   0.6026
  -3.250  -0.1122   0.01663   0.00895  -0.0414   0.7554   0.6354
  -3.000  -0.0892   0.01666   0.00896  -0.0400   0.7494   0.6639
  -2.750  -0.0636   0.01666   0.00888  -0.0391   0.7447   0.6908
  -2.500  -0.0404   0.01675   0.00898  -0.0378   0.7385   0.7142
  -2.250  -0.0165   0.01682   0.00900  -0.0366   0.7326   0.7383
  -2.000   0.0116   0.01684   0.00893  -0.0361   0.7281   0.7589
  -1.750   0.0369   0.01692   0.00898  -0.0354   0.7219   0.7753
  -1.500   0.0666   0.01699   0.00899  -0.0355   0.7162   0.7895
  -1.250   0.1001   0.01701   0.00891  -0.0364   0.7116   0.8022
  -1.000   0.1283   0.01709   0.00895  -0.0363   0.7056   0.8150
  -0.750   0.1557   0.01716   0.00895  -0.0362   0.6996   0.8283
  -0.500   0.1940   0.01721   0.00891  -0.0380   0.6949   0.8383
  -0.250   0.2253   0.01733   0.00899  -0.0387   0.6888   0.8498
   0.000   0.2545   0.01741   0.00904  -0.0390   0.6826   0.8624
   0.250   0.2966   0.01748   0.00902  -0.0416   0.6778   0.8700
   0.500   0.3266   0.01763   0.00915  -0.0422   0.6713   0.8812
   0.750   0.3645   0.01775   0.00923  -0.0442   0.6651   0.8892
   1.000   0.4008   0.01778   0.00917  -0.0458   0.6603   0.8986
   1.250   0.4363   0.01799   0.00940  -0.0475   0.6528   0.9067
   1.500   0.4713   0.01807   0.00943  -0.0490   0.6468   0.9156
   1.750   0.5096   0.01817   0.00949  -0.0511   0.6408   0.9227
   2.000   0.5416   0.01832   0.00966  -0.0522   0.6331   0.9321
   2.250   0.5803   0.01832   0.00959  -0.0543   0.6273   0.9395
   2.500   0.6121   0.01850   0.00983  -0.0555   0.6187   0.9490
   2.750   0.6462   0.01852   0.00979  -0.0568   0.6120   0.9587
   3.000   0.6813   0.01864   0.00995  -0.0587   0.6033   0.9670
   3.250   0.7175   0.01863   0.00992  -0.0605   0.5960   0.9753
   3.500   0.7510   0.01875   0.01008  -0.0621   0.5868   0.9845
   3.750   0.7898   0.01866   0.00994  -0.0645   0.5788   0.9915
   4.000   0.8265   0.01874   0.01009  -0.0669   0.5682   0.9991
   4.250   0.8460   0.01873   0.01005  -0.0656   0.5604   1.0000
   4.500   0.8583   0.01886   0.01022  -0.0629   0.5509   1.0000
   4.750   0.8736   0.01895   0.01030  -0.0607   0.5424   1.0000
   5.000   0.8881   0.01907   0.01043  -0.0584   0.5329   1.0000
   5.250   0.9018   0.01925   0.01062  -0.0559   0.5229   1.0000
   5.500   0.9194   0.01932   0.01066  -0.0540   0.5136   1.0000
   5.750   0.9314   0.01956   0.01095  -0.0512   0.5022   1.0000
   6.000   0.9456   0.01976   0.01116  -0.0488   0.4912   1.0000
   6.250   0.9613   0.01993   0.01129  -0.0466   0.4803   1.0000
   6.500   0.9746   0.02017   0.01156  -0.0440   0.4684   1.0000
   6.750   0.9868   0.02045   0.01185  -0.0412   0.4559   1.0000
   7.000   0.9995   0.02074   0.01213  -0.0386   0.4437   1.0000
   7.250   1.0120   0.02103   0.01240  -0.0359   0.4314   1.0000
   7.500   1.0233   0.02136   0.01271  -0.0330   0.4184   1.0000
   7.750   1.0321   0.02178   0.01313  -0.0298   0.4051   1.0000
   8.000   1.0401   0.02221   0.01356  -0.0265   0.3917   1.0000
   8.250   1.0455   0.02266   0.01399  -0.0227   0.3786   1.0000
   8.500   1.0504   0.02313   0.01444  -0.0189   0.3663   1.0000
   8.750   1.0551   0.02367   0.01493  -0.0152   0.3534   1.0000
   9.000   1.0595   0.02429   0.01552  -0.0117   0.3402   1.0000
   9.250   1.0639   0.02499   0.01622  -0.0085   0.3271   1.0000
   9.500   1.0683   0.02578   0.01700  -0.0054   0.3140   1.0000
   9.750   1.0732   0.02663   0.01783  -0.0026   0.3016   1.0000
  10.000   1.0783   0.02756   0.01872   0.0000   0.2898   1.0000
  10.250   1.0832   0.02856   0.01971   0.0024   0.2782   1.0000
  10.500   1.0887   0.02963   0.02080   0.0046   0.2670   1.0000
  10.750   1.0940   0.03076   0.02194   0.0066   0.2564   1.0000
  11.000   1.0991   0.03196   0.02311   0.0086   0.2465   1.0000
  11.250   1.1046   0.03322   0.02443   0.0103   0.2363   1.0000
  11.500   1.1099   0.03453   0.02574   0.0119   0.2273   1.0000
  11.750   1.1149   0.03592   0.02715   0.0135   0.2182   1.0000
  12.000   1.1197   0.03737   0.02866   0.0149   0.2094   1.0000
  12.250   1.1237   0.03890   0.03017   0.0162   0.2013   1.0000
  12.500   1.1285   0.04048   0.03183   0.0174   0.1930   1.0000
  12.750   1.1318   0.04213   0.03346   0.0186   0.1857   1.0000
  13.000   1.1359   0.04387   0.03531   0.0196   0.1778   1.0000
  13.250   1.1383   0.04568   0.03710   0.0206   0.1711   1.0000
  13.500   1.1421   0.04754   0.03908   0.0214   0.1641   1.0000
  13.750   1.1440   0.04952   0.04108   0.0222   0.1579   1.0000
  14.000   1.1471   0.05151   0.04316   0.0229   0.1517   1.0000
  14.250   1.1488   0.05366   0.04538   0.0234   0.1458   1.0000
  14.500   1.1508   0.05582   0.04754   0.0239   0.1406   1.0000
  14.750   1.1520   0.05820   0.05006   0.0242   0.1348   1.0000
  15.000   1.1529   0.06055   0.05243   0.0245   0.1301   1.0000
  15.250   1.1545   0.06298   0.05496   0.0247   0.1254   1.0000
  15.500   1.1545   0.06565   0.05775   0.0247   0.1207   1.0000
  15.750   1.1549   0.06823   0.06035   0.0247   0.1166   1.0000
  16.000   1.1552   0.07097   0.06320   0.0246   0.1126   1.0000
  16.250   1.1539   0.07399   0.06636   0.0243   0.1086   1.0000
  16.500   1.1529   0.07693   0.06936   0.0240   0.1050   1.0000
  16.750   1.1537   0.07965   0.07209   0.0237   0.1017   1.0000
  17.000   1.1500   0.08322   0.07586   0.0230   0.0985   1.0000
  17.250   1.1462   0.08679   0.07955   0.0222   0.0952   1.0000
  17.500   1.1449   0.08996   0.08278   0.0215   0.0923   1.0000
  17.750   1.1451   0.09293   0.08579   0.0209   0.0897   1.0000
  18.000   1.1368   0.09746   0.09053   0.0195   0.0872   1.0000
  18.250   1.1291   0.10192   0.09514   0.0180   0.0846   1.0000
  18.500   1.1244   0.10588   0.09919   0.0166   0.0822   1.0000
  18.750   1.1271   0.10852   0.10182   0.0159   0.0799   1.0000
  19.000   1.1176   0.11346   0.10692   0.0140   0.0780   1.0000
  19.250   1.0982   0.12039   0.11408   0.0108   0.0762   1.0000
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