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S8036 (16%) (s8036-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: S8036 (16%) (s8036-il)
Reynolds number: 200,000
Max Cl/Cd: 70.23 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8036-il-200000.txt
Download as CSV file: xf-s8036-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.3870   0.09112   0.08765  -0.0550   1.0000   0.0444
 -12.000  -0.7316   0.05892   0.05398  -0.0714   1.0000   0.0314
 -11.750  -0.7387   0.05560   0.05059  -0.0698   1.0000   0.0312
 -11.500  -0.7474   0.05271   0.04764  -0.0676   1.0000   0.0309
 -11.250  -0.7641   0.05024   0.04504  -0.0639   1.0000   0.0307
 -11.000  -0.7806   0.04823   0.04291  -0.0592   1.0000   0.0305
 -10.750  -0.8005   0.04641   0.04097  -0.0533   1.0000   0.0304
 -10.500  -0.8158   0.04443   0.03883  -0.0479   1.0000   0.0302
 -10.250  -0.8307   0.04270   0.03696  -0.0422   1.0000   0.0301
 -10.000  -0.8497   0.04139   0.03550  -0.0356   1.0000   0.0301
  -9.750  -0.8490   0.03918   0.03303  -0.0330   0.9972   0.0300
  -9.500  -0.8231   0.03600   0.02938  -0.0348   0.9906   0.0304
  -9.250  -0.7954   0.03365   0.02643  -0.0363   0.9837   0.0314
  -9.000  -0.7635   0.03113   0.02386  -0.0382   0.9775   0.0324
  -8.750  -0.7265   0.02930   0.02193  -0.0408   0.9730   0.0334
  -8.500  -0.6935   0.02761   0.02009  -0.0423   0.9655   0.0346
  -8.250  -0.6548   0.02600   0.01826  -0.0447   0.9610   0.0361
  -8.000  -0.6211   0.02433   0.01660  -0.0463   0.9542   0.0381
  -7.750  -0.5840   0.02314   0.01540  -0.0486   0.9490   0.0411
  -7.500  -0.5490   0.02186   0.01414  -0.0506   0.9435   0.0454
  -7.250  -0.5157   0.02068   0.01292  -0.0521   0.9363   0.0507
  -7.000  -0.4771   0.01946   0.01173  -0.0548   0.9320   0.0587
  -6.750  -0.4489   0.01844   0.01077  -0.0555   0.9224   0.0689
  -6.500  -0.4142   0.01736   0.00977  -0.0575   0.9161   0.0850
  -6.250  -0.3898   0.01647   0.00897  -0.0574   0.9050   0.1060
  -6.000  -0.3631   0.01550   0.00817  -0.0577   0.8964   0.1411
  -5.750  -0.3460   0.01466   0.00758  -0.0562   0.8849   0.1916
  -5.500  -0.3344   0.01379   0.00710  -0.0536   0.8737   0.2706
  -5.250  -0.3220   0.01295   0.00670  -0.0509   0.8645   0.3749
  -5.000  -0.3133   0.01253   0.00662  -0.0471   0.8535   0.4575
  -4.750  -0.2932   0.01232   0.00659  -0.0453   0.8461   0.5263
  -4.500  -0.2767   0.01234   0.00668  -0.0427   0.8364   0.5685
  -4.250  -0.2520   0.01240   0.00670  -0.0416   0.8298   0.6022
  -4.000  -0.2330   0.01251   0.00679  -0.0395   0.8211   0.6268
  -3.750  -0.2087   0.01260   0.00678  -0.0384   0.8143   0.6481
  -3.500  -0.1856   0.01271   0.00685  -0.0371   0.8073   0.6658
  -3.250  -0.1625   0.01281   0.00691  -0.0358   0.8001   0.6824
  -3.000  -0.1341   0.01291   0.00695  -0.0354   0.7947   0.6979
  -2.750  -0.1115   0.01302   0.00708  -0.0340   0.7873   0.7116
  -2.500  -0.0857   0.01310   0.00711  -0.0332   0.7810   0.7248
  -2.250  -0.0583   0.01321   0.00714  -0.0327   0.7761   0.7389
  -2.000  -0.0387   0.01332   0.00726  -0.0308   0.7687   0.7528
  -1.750  -0.0094   0.01339   0.00731  -0.0307   0.7629   0.7634
  -1.500   0.0173   0.01343   0.00728  -0.0302   0.7579   0.7740
  -1.250   0.0405   0.01349   0.00736  -0.0291   0.7508   0.7832
  -1.000   0.0670   0.01348   0.00728  -0.0287   0.7451   0.7920
  -0.750   0.0958   0.01353   0.00728  -0.0287   0.7400   0.8001
  -0.500   0.1170   0.01353   0.00729  -0.0274   0.7330   0.8089
  -0.250   0.1466   0.01354   0.00727  -0.0275   0.7275   0.8165
   0.000   0.1716   0.01356   0.00723  -0.0269   0.7221   0.8256
   0.250   0.1978   0.01361   0.00732  -0.0264   0.7153   0.8331
   0.500   0.2232   0.01358   0.00724  -0.0258   0.7098   0.8426
   0.750   0.2543   0.01365   0.00731  -0.0264   0.7043   0.8496
   1.000   0.2751   0.01366   0.00733  -0.0249   0.6973   0.8598
   1.250   0.3102   0.01368   0.00733  -0.0262   0.6919   0.8662
   1.500   0.3330   0.01372   0.00737  -0.0252   0.6855   0.8767
   1.750   0.3673   0.01378   0.00746  -0.0264   0.6784   0.8831
   2.000   0.4004   0.01379   0.00740  -0.0273   0.6730   0.8921
   2.250   0.4322   0.01390   0.00758  -0.0282   0.6648   0.8992
   2.500   0.4689   0.01394   0.00758  -0.0298   0.6580   0.9067
   2.750   0.5030   0.01403   0.00769  -0.0311   0.6504   0.9141
   3.000   0.5442   0.01408   0.00773  -0.0337   0.6420   0.9191
   3.250   0.5754   0.01412   0.00777  -0.0343   0.6337   0.9284
   3.500   0.6203   0.01413   0.00775  -0.0377   0.6239   0.9314
   3.750   0.6602   0.01420   0.00785  -0.0402   0.6134   0.9361
   4.000   0.6951   0.01419   0.00777  -0.0415   0.6048   0.9442
   4.250   0.7354   0.01426   0.00790  -0.0441   0.5931   0.9485
   4.500   0.7707   0.01430   0.00795  -0.0457   0.5825   0.9563
   4.750   0.8109   0.01430   0.00791  -0.0483   0.5716   0.9619
   5.000   0.8435   0.01435   0.00802  -0.0494   0.5580   0.9713
   5.250   0.8838   0.01435   0.00804  -0.0522   0.5428   0.9770
   5.500   0.9206   0.01438   0.00808  -0.0543   0.5267   0.9849
   5.750   0.9603   0.01438   0.00807  -0.0571   0.5079   0.9920
   6.000   1.0008   0.01439   0.00805  -0.0601   0.4873   0.9986
   6.250   1.0134   0.01443   0.00807  -0.0577   0.4692   1.0000
   6.500   1.0174   0.01452   0.00812  -0.0535   0.4519   1.0000
   6.750   1.0215   0.01467   0.00823  -0.0492   0.4332   1.0000
   7.000   1.0255   0.01490   0.00838  -0.0449   0.4125   1.0000
   7.250   1.0289   0.01523   0.00859  -0.0404   0.3902   1.0000
   7.500   1.0322   0.01561   0.00888  -0.0359   0.3663   1.0000
   7.750   1.0329   0.01611   0.00923  -0.0310   0.3431   1.0000
   8.000   1.0341   0.01662   0.00964  -0.0263   0.3195   1.0000
   8.250   1.0310   0.01716   0.01006  -0.0207   0.2990   1.0000
   8.500   1.0268   0.01774   0.01052  -0.0150   0.2804   1.0000
   8.750   1.0248   0.01842   0.01107  -0.0100   0.2628   1.0000
   9.000   1.0252   0.01914   0.01171  -0.0057   0.2460   1.0000
   9.250   1.0264   0.01996   0.01243  -0.0017   0.2309   1.0000
   9.500   1.0294   0.02080   0.01321   0.0018   0.2171   1.0000
   9.750   1.0345   0.02166   0.01404   0.0048   0.2047   1.0000
  10.000   1.0397   0.02260   0.01494   0.0075   0.1939   1.0000
  10.250   1.0437   0.02369   0.01592   0.0103   0.1846   1.0000
  10.500   1.0520   0.02461   0.01689   0.0124   0.1752   1.0000
  10.750   1.0588   0.02571   0.01793   0.0145   0.1675   1.0000
  11.000   1.0676   0.02670   0.01895   0.0163   0.1601   1.0000
  11.250   1.0759   0.02785   0.02003   0.0181   0.1536   1.0000
  11.500   1.0855   0.02887   0.02112   0.0196   0.1473   1.0000
  11.750   1.0951   0.03001   0.02218   0.0211   0.1418   1.0000
  12.000   1.1056   0.03108   0.02334   0.0225   0.1367   1.0000
  12.250   1.1148   0.03221   0.02451   0.0238   0.1317   1.0000
  12.500   1.1284   0.03330   0.02547   0.0249   0.1268   1.0000
  12.750   1.1364   0.03452   0.02686   0.0262   0.1230   1.0000
  13.000   1.1463   0.03570   0.02810   0.0272   0.1191   1.0000
  13.250   1.1571   0.03688   0.02926   0.0283   0.1154   1.0000
  13.500   1.1697   0.03808   0.03049   0.0292   0.1118   1.0000
  13.750   1.1771   0.03947   0.03202   0.0303   0.1085   1.0000
  14.000   1.1852   0.04082   0.03343   0.0312   0.1052   1.0000
  14.250   1.1983   0.04199   0.03455   0.0320   0.1020   1.0000
  14.500   1.2084   0.04345   0.03610   0.0328   0.0991   1.0000
  14.750   1.2126   0.04516   0.03797   0.0337   0.0965   1.0000
  15.000   1.2192   0.04675   0.03964   0.0344   0.0937   1.0000
  15.250   1.2282   0.04817   0.04105   0.0350   0.0911   1.0000
  15.500   1.2428   0.04955   0.04243   0.0357   0.0882   1.0000
  15.750   1.2423   0.05175   0.04485   0.0364   0.0864   1.0000
  16.000   1.2437   0.05392   0.04717   0.0369   0.0843   1.0000
  16.250   1.2472   0.05590   0.04923   0.0373   0.0821   1.0000
  16.500   1.2553   0.05750   0.05083   0.0376   0.0799   1.0000
  16.750   1.2688   0.05912   0.05244   0.0383   0.0776   1.0000
  17.000   1.2618   0.06215   0.05571   0.0384   0.0764   1.0000
  17.250   1.2565   0.06522   0.05899   0.0384   0.0750   1.0000
  17.500   1.2506   0.06843   0.06238   0.0381   0.0735   1.0000
  17.750   1.2477   0.07142   0.06549   0.0378   0.0721   1.0000
  18.000   1.2485   0.07400   0.06814   0.0375   0.0706   1.0000
  18.250   1.2562   0.07589   0.07002   0.0375   0.0691   1.0000
  18.500   1.2567   0.07892   0.07313   0.0375   0.0676   1.0000
  18.750   1.2384   0.08397   0.07843   0.0360   0.0670   1.0000
  19.000   1.2181   0.08963   0.08433   0.0341   0.0664   1.0000
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