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S8036 (16%) (s8036-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S8036 (16%) (s8036-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.6 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8036-il-1000000.txt
Download as CSV file: xf-s8036-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.7908   0.11841   0.11595  -0.0380   1.0000   0.0087
 -18.000  -0.8336   0.10563   0.10294  -0.0449   1.0000   0.0085
 -17.750  -0.8703   0.09475   0.09187  -0.0508   1.0000   0.0086
 -17.500  -0.8891   0.08746   0.08444  -0.0548   1.0000   0.0085
 -17.250  -0.8796   0.08501   0.08196  -0.0562   1.0000   0.0083
 -17.000  -0.9160   0.07538   0.07212  -0.0613   1.0000   0.0084
 -16.750  -0.9234   0.07062   0.06725  -0.0637   1.0000   0.0083
 -16.500  -0.9306   0.06610   0.06264  -0.0660   1.0000   0.0083
 -16.250  -0.9503   0.06019   0.05657  -0.0685   1.0000   0.0084
 -16.000  -0.9525   0.05683   0.05313  -0.0698   1.0000   0.0083
 -15.750  -0.9723   0.05161   0.04774  -0.0712   1.0000   0.0084
 -15.500  -0.9809   0.04801   0.04402  -0.0718   1.0000   0.0084
 -15.250  -0.9897   0.04457   0.04046  -0.0721   1.0000   0.0085
 -15.000  -0.9965   0.04153   0.03734  -0.0720   1.0000   0.0086
 -14.750  -0.9987   0.03906   0.03475  -0.0716   1.0000   0.0086
 -14.500  -0.9989   0.03690   0.03252  -0.0710   1.0000   0.0086
 -14.250  -1.0000   0.03477   0.03031  -0.0701   1.0000   0.0087
 -14.000  -0.9964   0.03315   0.02863  -0.0691   1.0000   0.0088
 -13.750  -0.9949   0.03145   0.02687  -0.0679   1.0000   0.0089
 -13.500  -0.9908   0.03005   0.02540  -0.0665   1.0000   0.0090
 -13.250  -0.9886   0.02857   0.02386  -0.0647   1.0000   0.0092
 -13.000  -0.9867   0.02716   0.02237  -0.0626   1.0000   0.0092
 -12.750  -0.9836   0.02595   0.02109  -0.0603   1.0000   0.0092
 -12.500  -0.9773   0.02509   0.02017  -0.0581   1.0000   0.0096
 -12.250  -0.9759   0.02400   0.01901  -0.0551   1.0000   0.0094
 -12.000  -0.9731   0.02315   0.01810  -0.0519   1.0000   0.0096
 -11.750  -0.9704   0.02243   0.01732  -0.0484   1.0000   0.0098
 -11.500  -0.9630   0.02152   0.01634  -0.0459   0.9994   0.0098
 -11.250  -0.9344   0.02060   0.01536  -0.0474   0.9972   0.0100
 -11.000  -0.9037   0.01980   0.01450  -0.0491   0.9947   0.0102
 -10.750  -0.8751   0.01903   0.01367  -0.0502   0.9915   0.0104
 -10.500  -0.8470   0.01822   0.01280  -0.0512   0.9869   0.0105
 -10.250  -0.8295   0.01712   0.01163  -0.0503   0.9776   0.0109
  -9.750  -0.7804   0.01571   0.01014  -0.0502   0.9493   0.0114
  -9.500  -0.7358   0.01494   0.00933  -0.0544   0.9410   0.0119
  -9.250  -0.6798   0.01419   0.00853  -0.0610   0.9333   0.0126
  -9.000  -0.6231   0.01343   0.00768  -0.0678   0.9176   0.0132
  -8.750  -0.5878   0.01286   0.00698  -0.0699   0.8868   0.0141
  -8.500  -0.5699   0.01263   0.00662  -0.0681   0.8588   0.0149
  -8.250  -0.5534   0.01244   0.00632  -0.0659   0.8375   0.0155
  -8.000  -0.5375   0.01214   0.00592  -0.0636   0.8207   0.0167
  -7.750  -0.5194   0.01191   0.00563  -0.0618   0.8067   0.0181
  -7.250  -0.4814   0.01142   0.00504  -0.0584   0.7837   0.0229
  -7.000  -0.4618   0.01119   0.00477  -0.0568   0.7741   0.0266
  -6.750  -0.4418   0.01093   0.00451  -0.0553   0.7648   0.0312
  -6.500  -0.4212   0.01070   0.00427  -0.0539   0.7568   0.0364
  -6.250  -0.4001   0.01046   0.00404  -0.0526   0.7489   0.0433
  -6.000  -0.3793   0.01025   0.00382  -0.0513   0.7415   0.0523
  -5.750  -0.3575   0.01000   0.00362  -0.0501   0.7348   0.0630
  -5.500  -0.3358   0.00978   0.00343  -0.0489   0.7283   0.0757
  -5.250  -0.3141   0.00956   0.00324  -0.0478   0.7224   0.0915
  -5.000  -0.2926   0.00928   0.00306  -0.0466   0.7165   0.1138
  -4.750  -0.2718   0.00900   0.00287  -0.0452   0.7105   0.1425
  -4.500  -0.2520   0.00866   0.00268  -0.0437   0.7049   0.1836
  -4.250  -0.2322   0.00828   0.00250  -0.0422   0.6996   0.2323
  -4.000  -0.2143   0.00784   0.00230  -0.0404   0.6943   0.2996
  -3.750  -0.1955   0.00746   0.00213  -0.0386   0.6890   0.3646
  -3.500  -0.1755   0.00710   0.00199  -0.0371   0.6842   0.4268
  -3.250  -0.1542   0.00684   0.00189  -0.0358   0.6788   0.4774
  -3.000  -0.1325   0.00667   0.00182  -0.0345   0.6737   0.5209
  -2.750  -0.1085   0.00655   0.00179  -0.0336   0.6691   0.5532
  -2.500  -0.0832   0.00648   0.00176  -0.0330   0.6639   0.5752
  -2.250  -0.0577   0.00646   0.00173  -0.0324   0.6586   0.5904
  -2.000  -0.0319   0.00645   0.00171  -0.0319   0.6535   0.6035
  -1.750  -0.0055   0.00641   0.00169  -0.0315   0.6486   0.6166
  -1.500   0.0206   0.00641   0.00167  -0.0311   0.6434   0.6290
  -1.250   0.0464   0.00642   0.00166  -0.0306   0.6381   0.6387
  -0.750   0.0994   0.00638   0.00165  -0.0298   0.6284   0.6586
  -0.500   0.1254   0.00640   0.00164  -0.0294   0.6233   0.6684
  -0.250   0.1519   0.00640   0.00165  -0.0290   0.6183   0.6767
   0.000   0.1789   0.00640   0.00164  -0.0288   0.6129   0.6837
   0.250   0.2047   0.00641   0.00164  -0.0283   0.6072   0.6910
   0.500   0.2315   0.00643   0.00165  -0.0280   0.6016   0.6976
   0.750   0.2581   0.00642   0.00165  -0.0277   0.5956   0.7038
   1.000   0.2839   0.00644   0.00167  -0.0272   0.5896   0.7104
   1.250   0.3108   0.00646   0.00168  -0.0270   0.5839   0.7169
   1.500   0.3369   0.00646   0.00170  -0.0266   0.5773   0.7235
   1.750   0.3622   0.00650   0.00172  -0.0260   0.5703   0.7313
   2.000   0.3885   0.00651   0.00174  -0.0257   0.5626   0.7385
   2.250   0.4132   0.00655   0.00178  -0.0250   0.5546   0.7462
   2.500   0.4397   0.00657   0.00180  -0.0247   0.5469   0.7539
   2.750   0.4643   0.00660   0.00185  -0.0240   0.5394   0.7620
   3.000   0.4903   0.00662   0.00189  -0.0236   0.5316   0.7706
   3.250   0.5144   0.00666   0.00194  -0.0228   0.5227   0.7799
   3.500   0.5397   0.00669   0.00199  -0.0222   0.5141   0.7899
   3.750   0.5632   0.00674   0.00205  -0.0213   0.5047   0.8011
   4.000   0.5869   0.00679   0.00212  -0.0205   0.4923   0.8130
   4.250   0.6101   0.00685   0.00219  -0.0195   0.4794   0.8264
   4.750   0.6539   0.00702   0.00238  -0.0170   0.4495   0.8594
   5.000   0.6766   0.00711   0.00250  -0.0160   0.4343   0.8800
   5.250   0.7035   0.00723   0.00266  -0.0159   0.4166   0.9048
   5.500   0.7415   0.00751   0.00291  -0.0184   0.3926   0.9272
   5.750   0.7888   0.00792   0.00321  -0.0231   0.3625   0.9389
   6.000   0.8344   0.00838   0.00354  -0.0275   0.3309   0.9467
   6.250   0.8716   0.00884   0.00388  -0.0299   0.3028   0.9553
   6.500   0.8997   0.00931   0.00423  -0.0304   0.2767   0.9670
   6.750   0.9243   0.00978   0.00458  -0.0301   0.2514   0.9788
   7.000   0.9522   0.01024   0.00493  -0.0305   0.2300   0.9856
   7.250   0.9845   0.01069   0.00528  -0.0320   0.2090   0.9899
   7.500   1.0151   0.01116   0.00565  -0.0331   0.1904   0.9939
   7.750   1.0493   0.01162   0.00601  -0.0351   0.1717   0.9965
   8.000   1.0834   0.01204   0.00635  -0.0371   0.1577   0.9990
   8.250   1.1063   0.01237   0.00664  -0.0366   0.1474   1.0000
   8.500   1.1081   0.01263   0.00688  -0.0316   0.1397   1.0000
   8.750   1.1130   0.01287   0.00710  -0.0272   0.1336   1.0000
   9.000   1.1184   0.01320   0.00740  -0.0230   0.1261   1.0000
   9.250   1.1277   0.01350   0.00769  -0.0197   0.1204   1.0000
   9.500   1.1353   0.01391   0.00807  -0.0162   0.1139   1.0000
   9.750   1.1471   0.01423   0.00841  -0.0135   0.1098   1.0000
  10.000   1.1567   0.01467   0.00883  -0.0106   0.1045   1.0000
  10.250   1.1669   0.01514   0.00929  -0.0079   0.0997   1.0000
  10.500   1.1789   0.01558   0.00975  -0.0055   0.0962   1.0000
  10.750   1.1892   0.01613   0.01029  -0.0031   0.0924   1.0000
  11.000   1.1989   0.01675   0.01092  -0.0006   0.0885   1.0000
  11.250   1.2123   0.01726   0.01147   0.0012   0.0864   1.0000
  11.500   1.2237   0.01790   0.01211   0.0032   0.0835   1.0000
  11.750   1.2334   0.01867   0.01288   0.0052   0.0803   1.0000
  12.000   1.2432   0.01948   0.01372   0.0071   0.0775   1.0000
  12.250   1.2565   0.02015   0.01444   0.0085   0.0758   1.0000
  12.500   1.2683   0.02095   0.01526   0.0099   0.0739   1.0000
  12.750   1.2785   0.02187   0.01620   0.0114   0.0716   1.0000
  13.000   1.2869   0.02295   0.01730   0.0130   0.0692   1.0000
  13.250   1.2976   0.02394   0.01833   0.0142   0.0670   1.0000
  13.500   1.3099   0.02484   0.01927   0.0152   0.0653   1.0000
  13.750   1.3202   0.02591   0.02037   0.0163   0.0636   1.0000
  14.000   1.3287   0.02713   0.02161   0.0175   0.0615   1.0000
  14.250   1.3344   0.02860   0.02311   0.0187   0.0594   1.0000
  14.500   1.3453   0.02970   0.02426   0.0195   0.0577   1.0000
  14.750   1.3558   0.03086   0.02547   0.0203   0.0561   1.0000
  15.000   1.3636   0.03226   0.02689   0.0212   0.0542   1.0000
  15.250   1.3693   0.03386   0.02851   0.0220   0.0523   1.0000
  15.500   1.3749   0.03551   0.03020   0.0228   0.0503   1.0000
  15.750   1.3841   0.03688   0.03163   0.0234   0.0488   1.0000
  16.000   1.3902   0.03855   0.03336   0.0240   0.0477   1.0000
  16.250   1.3952   0.04036   0.03518   0.0245   0.0457   1.0000
  16.500   1.3966   0.04256   0.03741   0.0251   0.0440   1.0000
  16.750   1.4024   0.04438   0.03929   0.0254   0.0429   1.0000
  17.000   1.4080   0.04625   0.04123   0.0257   0.0419   1.0000
  17.250   1.4122   0.04831   0.04334   0.0259   0.0405   1.0000
  17.500   1.4127   0.05078   0.04583   0.0260   0.0387   1.0000
  17.750   1.4122   0.05341   0.04851   0.0261   0.0378   1.0000
  18.000   1.4144   0.05579   0.05097   0.0261   0.0370   1.0000
  18.250   1.4182   0.05805   0.05329   0.0260   0.0359   1.0000
  18.500   1.4187   0.06071   0.05602   0.0258   0.0349   1.0000
  18.750   1.4178   0.06358   0.05894   0.0255   0.0342   1.0000
  19.000   1.4150   0.06669   0.06211   0.0250   0.0333   1.0000
  19.250   1.4074   0.07048   0.06595   0.0244   0.0321   1.0000
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