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S8036 (16%) (s8036-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S8036 (16%) (s8036-il)
Reynolds number: 200,000
Max Cl/Cd: 61.75 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8036-il-200000-n5.txt
Download as CSV file: xf-s8036-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8036 (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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.6857   0.08242   0.07779  -0.0607   1.0000   0.0143
 -14.500  -0.7205   0.07283   0.06794  -0.0664   1.0000   0.0141
 -14.250  -0.7435   0.06627   0.06117  -0.0697   1.0000   0.0141
 -14.000  -0.7637   0.06071   0.05539  -0.0719   1.0000   0.0140
 -13.750  -0.7769   0.05654   0.05105  -0.0730   1.0000   0.0142
 -13.500  -0.7881   0.05286   0.04718  -0.0735   1.0000   0.0142
 -13.250  -0.7984   0.04950   0.04365  -0.0734   1.0000   0.0144
 -13.000  -0.8062   0.04656   0.04054  -0.0728   1.0000   0.0145
 -12.750  -0.8112   0.04404   0.03785  -0.0718   1.0000   0.0146
 -12.500  -0.8152   0.04186   0.03550  -0.0705   1.0000   0.0150
 -12.250  -0.8166   0.03981   0.03331  -0.0689   1.0000   0.0149
 -12.000  -0.8185   0.03792   0.03123  -0.0669   1.0000   0.0153
 -11.750  -0.8191   0.03625   0.02934  -0.0646   1.0000   0.0157
 -11.500  -0.8176   0.03467   0.02763  -0.0622   1.0000   0.0159
 -11.250  -0.8154   0.03347   0.02642  -0.0597   1.0000   0.0162
 -11.000  -0.8131   0.03243   0.02533  -0.0569   1.0000   0.0165
 -10.750  -0.8117   0.03147   0.02433  -0.0537   1.0000   0.0168
 -10.500  -0.8112   0.03059   0.02340  -0.0501   1.0000   0.0172
 -10.000  -0.7794   0.02829   0.02089  -0.0485   0.9937   0.0182
  -9.750  -0.7533   0.02699   0.01945  -0.0494   0.9857   0.0187
  -9.250  -0.7118   0.02477   0.01713  -0.0491   0.9573   0.0200
  -9.000  -0.6849   0.02376   0.01605  -0.0499   0.9463   0.0209
  -8.750  -0.6570   0.02272   0.01490  -0.0507   0.9348   0.0222
  -8.500  -0.6253   0.02171   0.01385  -0.0525   0.9248   0.0239
  -8.250  -0.5891   0.02079   0.01284  -0.0550   0.9155   0.0261
  -8.000  -0.5560   0.01988   0.01188  -0.0569   0.9033   0.0288
  -7.750  -0.5227   0.01905   0.01095  -0.0587   0.8909   0.0319
  -7.500  -0.4903   0.01833   0.01016  -0.0602   0.8786   0.0360
  -7.250  -0.4616   0.01769   0.00946  -0.0610   0.8655   0.0415
  -7.000  -0.4368   0.01716   0.00889  -0.0608   0.8520   0.0481
  -6.750  -0.4138   0.01668   0.00837  -0.0603   0.8397   0.0567
  -6.500  -0.3913   0.01624   0.00789  -0.0595   0.8288   0.0672
  -6.250  -0.3725   0.01581   0.00748  -0.0580   0.8177   0.0797
  -6.000  -0.3529   0.01540   0.00708  -0.0567   0.8082   0.0962
  -5.500  -0.3155   0.01459   0.00637  -0.0536   0.7903   0.1438
  -5.000  -0.2813   0.01366   0.00571  -0.0499   0.7747   0.2240
  -4.750  -0.2670   0.01313   0.00541  -0.0475   0.7666   0.2830
  -4.500  -0.2526   0.01260   0.00514  -0.0451   0.7600   0.3537
  -4.250  -0.2385   0.01217   0.00498  -0.0425   0.7528   0.4219
  -4.000  -0.2211   0.01189   0.00489  -0.0403   0.7461   0.4797
  -3.750  -0.2005   0.01175   0.00483  -0.0387   0.7404   0.5240
  -3.500  -0.1792   0.01167   0.00481  -0.0372   0.7338   0.5573
  -3.250  -0.1560   0.01164   0.00477  -0.0361   0.7279   0.5838
  -3.000  -0.1320   0.01164   0.00472  -0.0351   0.7228   0.6060
  -2.750  -0.1087   0.01163   0.00471  -0.0340   0.7166   0.6248
  -2.500  -0.0843   0.01163   0.00467  -0.0331   0.7110   0.6410
  -2.250  -0.0591   0.01165   0.00465  -0.0323   0.7062   0.6575
  -2.000  -0.0354   0.01165   0.00467  -0.0313   0.7003   0.6729
  -1.750  -0.0106   0.01167   0.00464  -0.0305   0.6950   0.6857
  -1.500   0.0158   0.01168   0.00459  -0.0301   0.6903   0.6961
  -1.250   0.0409   0.01168   0.00458  -0.0295   0.6846   0.7049
  -1.000   0.0664   0.01168   0.00455  -0.0289   0.6790   0.7133
  -0.750   0.0930   0.01168   0.00450  -0.0285   0.6742   0.7210
  -0.500   0.1190   0.01169   0.00450  -0.0281   0.6687   0.7285
  -0.250   0.1438   0.01170   0.00448  -0.0274   0.6629   0.7367
   0.000   0.1708   0.01170   0.00447  -0.0271   0.6576   0.7438
   0.250   0.1962   0.01172   0.00446  -0.0266   0.6524   0.7523
   0.500   0.2220   0.01172   0.00449  -0.0261   0.6462   0.7592
   0.750   0.2482   0.01174   0.00448  -0.0257   0.6409   0.7671
   1.000   0.2744   0.01176   0.00449  -0.0253   0.6355   0.7744
   1.250   0.2998   0.01177   0.00455  -0.0248   0.6291   0.7822
   1.500   0.3259   0.01179   0.00454  -0.0243   0.6235   0.7905
   1.750   0.3522   0.01182   0.00460  -0.0240   0.6173   0.7985
   2.000   0.3770   0.01184   0.00463  -0.0233   0.6103   0.8077
   2.250   0.4050   0.01186   0.00465  -0.0233   0.6043   0.8163
   2.500   0.4296   0.01189   0.00474  -0.0226   0.5964   0.8262
   2.750   0.4576   0.01192   0.00478  -0.0225   0.5894   0.8360
   3.000   0.4844   0.01196   0.00488  -0.0223   0.5811   0.8464
   3.250   0.5124   0.01201   0.00492  -0.0223   0.5728   0.8578
   3.500   0.5430   0.01208   0.00505  -0.0229   0.5625   0.8684
   3.750   0.5738   0.01216   0.00513  -0.0235   0.5521   0.8797
   4.000   0.6067   0.01226   0.00525  -0.0246   0.5402   0.8908
   4.250   0.6417   0.01239   0.00541  -0.0262   0.5276   0.9009
   4.500   0.6754   0.01253   0.00558  -0.0275   0.5152   0.9119
   4.750   0.7124   0.01271   0.00575  -0.0296   0.5013   0.9199
   5.000   0.7459   0.01290   0.00593  -0.0309   0.4858   0.9297
   5.250   0.7815   0.01312   0.00614  -0.0327   0.4678   0.9375
   5.500   0.8129   0.01338   0.00635  -0.0337   0.4468   0.9471
   5.750   0.8405   0.01371   0.00660  -0.0340   0.4241   0.9584
   6.000   0.8682   0.01406   0.00689  -0.0343   0.3986   0.9696
   6.250   0.8941   0.01451   0.00723  -0.0344   0.3725   0.9818
   6.500   0.9229   0.01503   0.00762  -0.0353   0.3439   0.9914
   6.750   0.9538   0.01560   0.00806  -0.0368   0.3145   0.9990
   7.250   0.9657   0.01644   0.00872  -0.0292   0.2781   1.0000
   7.500   0.9687   0.01687   0.00908  -0.0248   0.2621   1.0000
   7.750   0.9687   0.01730   0.00943  -0.0198   0.2472   1.0000
   8.000   0.9711   0.01775   0.00983  -0.0154   0.2331   1.0000
   8.250   0.9747   0.01826   0.01029  -0.0114   0.2195   1.0000
   8.500   0.9797   0.01882   0.01080  -0.0077   0.2071   1.0000
   8.750   0.9852   0.01943   0.01138  -0.0043   0.1962   1.0000
   9.000   0.9906   0.02011   0.01202  -0.0011   0.1858   1.0000
   9.250   0.9984   0.02078   0.01268   0.0016   0.1758   1.0000
   9.500   1.0050   0.02156   0.01344   0.0044   0.1670   1.0000
   9.750   1.0126   0.02236   0.01424   0.0068   0.1588   1.0000
  10.000   1.0204   0.02322   0.01510   0.0090   0.1519   1.0000
  10.250   1.0287   0.02411   0.01600   0.0111   0.1450   1.0000
  10.500   1.0359   0.02512   0.01701   0.0131   0.1390   1.0000
  10.750   1.0452   0.02606   0.01799   0.0148   0.1329   1.0000
  11.000   1.0516   0.02723   0.01914   0.0165   0.1277   1.0000
  11.250   1.0614   0.02825   0.02021   0.0180   0.1228   1.0000
  11.500   1.0697   0.02939   0.02138   0.0194   0.1179   1.0000
  11.750   1.0756   0.03074   0.02273   0.0208   0.1138   1.0000
  12.000   1.0856   0.03185   0.02392   0.0220   0.1100   1.0000
  12.250   1.0942   0.03309   0.02521   0.0231   0.1059   1.0000
  12.500   1.1004   0.03454   0.02666   0.0242   0.1024   1.0000
  12.750   1.1076   0.03595   0.02812   0.0252   0.0991   1.0000
  13.000   1.1165   0.03726   0.02952   0.0261   0.0960   1.0000
  13.250   1.1236   0.03874   0.03105   0.0270   0.0928   1.0000
  13.500   1.1288   0.04040   0.03273   0.0278   0.0903   1.0000
  13.750   1.1346   0.04206   0.03443   0.0286   0.0879   1.0000
  14.000   1.1428   0.04355   0.03603   0.0292   0.0853   1.0000
  14.250   1.1495   0.04521   0.03777   0.0298   0.0829   1.0000
  14.500   1.1543   0.04707   0.03968   0.0303   0.0805   1.0000
  14.750   1.1579   0.04908   0.04171   0.0307   0.0786   1.0000
  15.000   1.1632   0.05097   0.04368   0.0311   0.0766   1.0000
  15.250   1.1694   0.05283   0.04566   0.0314   0.0745   1.0000
  15.500   1.1744   0.05485   0.04777   0.0316   0.0725   1.0000
  15.750   1.1778   0.05708   0.05008   0.0317   0.0706   1.0000
  16.000   1.1794   0.05951   0.05254   0.0317   0.0689   1.0000
  16.250   1.1818   0.06190   0.05498   0.0317   0.0672   1.0000
  16.500   1.1857   0.06422   0.05743   0.0316   0.0656   1.0000
  16.750   1.1887   0.06666   0.05999   0.0314   0.0640   1.0000
  17.000   1.1904   0.06931   0.06274   0.0310   0.0624   1.0000
  17.250   1.1908   0.07215   0.06566   0.0305   0.0610   1.0000
  17.500   1.1903   0.07513   0.06868   0.0299   0.0596   1.0000
  17.750   1.1903   0.07805   0.07166   0.0294   0.0584   1.0000
  18.000   1.1901   0.08114   0.07492   0.0287   0.0571   1.0000
  18.250   1.1888   0.08443   0.07835   0.0278   0.0557   1.0000
  18.500   1.1871   0.08781   0.08184   0.0268   0.0545   1.0000
  18.750   1.1846   0.09134   0.08547   0.0257   0.0534   1.0000
  19.000   1.1818   0.09495   0.08916   0.0245   0.0524   1.0000
  19.250   1.1787   0.09861   0.09288   0.0231   0.0514   1.0000
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