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S8036 (16%) (s8036-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: S8036 (16%) (s8036-il)
Reynolds number: 500,000
Max Cl/Cd: 87.28 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8036-il-500000.txt
Download as CSV file: xf-s8036-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.4599   0.11226   0.10981  -0.0464   1.0000   0.0162
 -15.250  -0.6145   0.10640   0.10372  -0.0450   1.0000   0.0154
 -15.000  -0.6910   0.08499   0.08201  -0.0583   1.0000   0.0149
 -14.750  -0.7407   0.07246   0.06919  -0.0660   1.0000   0.0143
 -14.500  -0.7701   0.06492   0.06145  -0.0701   1.0000   0.0143
 -14.250  -0.8042   0.05768   0.05393  -0.0731   1.0000   0.0141
 -14.000  -0.8454   0.05041   0.04624  -0.0746   1.0000   0.0138
 -13.750  -0.8479   0.04801   0.04379  -0.0745   1.0000   0.0140
 -13.500  -0.8639   0.04433   0.03988  -0.0738   1.0000   0.0139
 -13.250  -0.8736   0.04146   0.03684  -0.0727   1.0000   0.0140
 -13.000  -0.8796   0.03909   0.03432  -0.0711   1.0000   0.0141
 -12.750  -0.8878   0.03655   0.03156  -0.0689   1.0000   0.0139
 -12.500  -0.8858   0.03526   0.03022  -0.0670   1.0000   0.0143
 -12.250  -0.8891   0.03325   0.02802  -0.0644   1.0000   0.0141
 -12.000  -0.8885   0.03185   0.02652  -0.0618   1.0000   0.0143
 -11.750  -0.8875   0.03058   0.02514  -0.0588   1.0000   0.0145
 -11.500  -0.8863   0.02920   0.02363  -0.0556   1.0000   0.0145
 -11.250  -0.8851   0.02814   0.02248  -0.0521   1.0000   0.0147
 -11.000  -0.8849   0.02724   0.02150  -0.0482   1.0000   0.0148
 -10.750  -0.8882   0.02646   0.02064  -0.0434   1.0000   0.0150
 -10.500  -0.8692   0.02536   0.01942  -0.0429   0.9981   0.0153
 -10.250  -0.8368   0.02425   0.01817  -0.0450   0.9947   0.0157
 -10.000  -0.8069   0.02281   0.01663  -0.0465   0.9907   0.0161
  -9.750  -0.7766   0.02151   0.01530  -0.0482   0.9857   0.0164
  -9.500  -0.7494   0.02049   0.01427  -0.0490   0.9773   0.0168
  -9.250  -0.7239   0.01964   0.01338  -0.0493   0.9650   0.0175
  -9.000  -0.6969   0.01878   0.01247  -0.0497   0.9532   0.0182
  -8.750  -0.6609   0.01803   0.01162  -0.0519   0.9459   0.0191
  -8.500  -0.6261   0.01676   0.01036  -0.0543   0.9356   0.0203
  -8.250  -0.5796   0.01597   0.00952  -0.0589   0.9273   0.0219
  -8.000  -0.5352   0.01496   0.00845  -0.0632   0.9144   0.0242
  -7.750  -0.4965   0.01437   0.00775  -0.0659   0.8962   0.0268
  -7.500  -0.4724   0.01379   0.00710  -0.0656   0.8750   0.0302
  -7.250  -0.4530   0.01337   0.00661  -0.0642   0.8568   0.0344
  -7.000  -0.4342   0.01303   0.00621  -0.0625   0.8417   0.0399
  -6.500  -0.3973   0.01240   0.00553  -0.0590   0.8171   0.0559
  -6.250  -0.3780   0.01211   0.00523  -0.0574   0.8071   0.0673
  -6.000  -0.3597   0.01178   0.00493  -0.0557   0.7974   0.0826
  -5.500  -0.3219   0.01112   0.00440  -0.0524   0.7804   0.1303
  -5.250  -0.3040   0.01072   0.00414  -0.0506   0.7729   0.1676
  -5.000  -0.2876   0.01025   0.00388  -0.0485   0.7653   0.2200
  -4.750  -0.2712   0.00977   0.00361  -0.0465   0.7586   0.2845
  -4.500  -0.2563   0.00924   0.00339  -0.0441   0.7516   0.3589
  -4.250  -0.2402   0.00882   0.00321  -0.0419   0.7453   0.4290
  -4.000  -0.2220   0.00853   0.00310  -0.0399   0.7395   0.4873
  -3.750  -0.2018   0.00835   0.00304  -0.0382   0.7331   0.5310
  -3.500  -0.1795   0.00827   0.00301  -0.0370   0.7273   0.5652
  -3.250  -0.1557   0.00825   0.00299  -0.0360   0.7220   0.5900
  -3.000  -0.1315   0.00822   0.00297  -0.0351   0.7164   0.6082
  -2.750  -0.1065   0.00821   0.00293  -0.0344   0.7109   0.6227
  -2.500  -0.0806   0.00824   0.00291  -0.0339   0.7058   0.6358
  -2.250  -0.0559   0.00824   0.00290  -0.0331   0.7003   0.6493
  -2.000  -0.0307   0.00824   0.00289  -0.0324   0.6950   0.6618
  -1.750  -0.0040   0.00827   0.00287  -0.0320   0.6899   0.6721
  -1.500   0.0207   0.00828   0.00287  -0.0312   0.6845   0.6832
  -1.250   0.0462   0.00826   0.00288  -0.0306   0.6790   0.6945
  -1.000   0.0725   0.00829   0.00287  -0.0301   0.6740   0.7044
  -0.750   0.0984   0.00830   0.00288  -0.0297   0.6689   0.7130
  -0.500   0.1243   0.00829   0.00286  -0.0292   0.6633   0.7209
  -0.250   0.1511   0.00829   0.00285  -0.0288   0.6583   0.7282
   0.000   0.1774   0.00834   0.00285  -0.0285   0.6533   0.7355
   0.250   0.2038   0.00829   0.00285  -0.0281   0.6477   0.7420
   0.500   0.2300   0.00830   0.00284  -0.0277   0.6424   0.7493
   0.750   0.2570   0.00833   0.00284  -0.0275   0.6371   0.7563
   1.000   0.2824   0.00830   0.00286  -0.0269   0.6310   0.7638
   1.250   0.3080   0.00831   0.00284  -0.0263   0.6251   0.7718
   1.500   0.3347   0.00832   0.00287  -0.0260   0.6193   0.7792
   1.750   0.3595   0.00831   0.00288  -0.0254   0.6128   0.7876
   2.000   0.3858   0.00831   0.00289  -0.0250   0.6065   0.7952
   2.250   0.4106   0.00832   0.00292  -0.0243   0.5997   0.8044
   2.500   0.4359   0.00830   0.00293  -0.0237   0.5922   0.8132
   2.750   0.4603   0.00832   0.00295  -0.0229   0.5847   0.8237
   3.000   0.4852   0.00829   0.00299  -0.0222   0.5762   0.8339
   3.250   0.5100   0.00832   0.00303  -0.0216   0.5685   0.8456
   3.500   0.5344   0.00832   0.00308  -0.0208   0.5603   0.8589
   3.750   0.5608   0.00834   0.00315  -0.0204   0.5521   0.8728
   4.000   0.5888   0.00836   0.00323  -0.0205   0.5433   0.8880
   4.250   0.6205   0.00843   0.00334  -0.0213   0.5335   0.9036
   4.500   0.6573   0.00856   0.00348  -0.0233   0.5222   0.9178
   4.750   0.6966   0.00870   0.00364  -0.0259   0.5080   0.9297
   5.000   0.7387   0.00890   0.00382  -0.0291   0.4917   0.9372
   5.250   0.7770   0.00912   0.00401  -0.0315   0.4749   0.9454
   5.500   0.8138   0.00941   0.00424  -0.0336   0.4564   0.9520
   5.750   0.8453   0.00969   0.00449  -0.0346   0.4373   0.9611
   6.000   0.8745   0.01002   0.00475  -0.0351   0.4150   0.9714
   6.250   0.9083   0.01043   0.00506  -0.0367   0.3876   0.9777
   6.500   0.9391   0.01093   0.00541  -0.0379   0.3578   0.9852
   6.750   0.9729   0.01145   0.00578  -0.0397   0.3265   0.9909
   7.250   1.0411   0.01258   0.00660  -0.0439   0.2627   0.9998
   7.500   1.0457   0.01292   0.00686  -0.0397   0.2447   1.0000
   7.750   1.0493   0.01328   0.00715  -0.0353   0.2289   1.0000
   8.000   1.0507   0.01365   0.00744  -0.0303   0.2148   1.0000
   8.250   1.0512   0.01400   0.00774  -0.0252   0.2017   1.0000
   8.500   1.0551   0.01438   0.00807  -0.0209   0.1897   1.0000
   8.750   1.0600   0.01482   0.00847  -0.0168   0.1783   1.0000
   9.000   1.0654   0.01532   0.00892  -0.0130   0.1682   1.0000
   9.250   1.0727   0.01582   0.00939  -0.0097   0.1587   1.0000
   9.500   1.0809   0.01635   0.00991  -0.0067   0.1502   1.0000
   9.750   1.0874   0.01700   0.01052  -0.0035   0.1424   1.0000
  10.000   1.0974   0.01757   0.01111  -0.0010   0.1357   1.0000
  10.250   1.1045   0.01833   0.01183   0.0017   0.1290   1.0000
  10.500   1.1145   0.01901   0.01254   0.0039   0.1231   1.0000
  10.750   1.1236   0.01979   0.01332   0.0060   0.1178   1.0000
  11.000   1.1297   0.02080   0.01431   0.0084   0.1130   1.0000
  11.250   1.1423   0.02151   0.01508   0.0099   0.1092   1.0000
  11.500   1.1515   0.02246   0.01603   0.0116   0.1049   1.0000
  11.750   1.1563   0.02373   0.01729   0.0136   0.1010   1.0000
  12.000   1.1689   0.02456   0.01819   0.0148   0.0982   1.0000
  12.250   1.1796   0.02555   0.01923   0.0161   0.0951   1.0000
  12.500   1.1875   0.02676   0.02045   0.0174   0.0922   1.0000
  12.750   1.1903   0.02837   0.02206   0.0191   0.0889   1.0000
  13.000   1.2026   0.02935   0.02312   0.0200   0.0869   1.0000
  13.250   1.2134   0.03047   0.02430   0.0209   0.0844   1.0000
  13.500   1.2213   0.03181   0.02568   0.0219   0.0820   1.0000
  13.750   1.2256   0.03348   0.02735   0.0230   0.0795   1.0000
  14.000   1.2296   0.03519   0.02910   0.0240   0.0773   1.0000
  14.250   1.2399   0.03645   0.03045   0.0247   0.0756   1.0000
  14.500   1.2482   0.03790   0.03196   0.0253   0.0735   1.0000
  14.750   1.2549   0.03952   0.03363   0.0260   0.0715   1.0000
  15.000   1.2569   0.04158   0.03570   0.0267   0.0692   1.0000
  15.250   1.2592   0.04364   0.03781   0.0274   0.0673   1.0000
  15.500   1.2675   0.04525   0.03952   0.0277   0.0658   1.0000
  15.750   1.2740   0.04705   0.04139   0.0280   0.0640   1.0000
  16.000   1.2788   0.04906   0.04346   0.0282   0.0623   1.0000
  16.250   1.2802   0.05144   0.04585   0.0284   0.0604   1.0000
  16.500   1.2786   0.05406   0.04849   0.0288   0.0586   1.0000
  16.750   1.2850   0.05606   0.05062   0.0287   0.0574   1.0000
  17.000   1.2895   0.05829   0.05293   0.0286   0.0560   1.0000
  17.250   1.2938   0.06059   0.05530   0.0284   0.0543   1.0000
  17.500   1.2941   0.06334   0.05809   0.0280   0.0527   1.0000
  17.750   1.2921   0.06633   0.06111   0.0278   0.0516   1.0000
  18.000   1.2918   0.06920   0.06405   0.0274   0.0501   1.0000
  18.250   1.2935   0.07194   0.06689   0.0269   0.0490   1.0000
  18.500   1.2941   0.07485   0.06990   0.0263   0.0480   1.0000
  18.750   1.2942   0.07786   0.07300   0.0255   0.0469   1.0000
  19.000   1.2927   0.08113   0.07632   0.0247   0.0457   1.0000
  19.250   1.2877   0.08483   0.08005   0.0237   0.0446   1.0000
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