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S8036 (16%) (s8036-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: S8036 (16%) (s8036-il)
Reynolds number: 100,000
Max Cl/Cd: 47.95 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8036-il-100000-n5.txt
Download as CSV file: xf-s8036-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.5026   0.11066   0.10503  -0.0470   1.0000   0.0267
 -13.500  -0.5236   0.10113   0.09550  -0.0516   1.0000   0.0263
 -13.250  -0.5715   0.08653   0.08078  -0.0604   1.0000   0.0259
 -13.000  -0.6079   0.07698   0.07107  -0.0663   1.0000   0.0255
 -12.750  -0.6370   0.07012   0.06404  -0.0697   1.0000   0.0253
 -12.500  -0.6639   0.06446   0.05818  -0.0716   1.0000   0.0252
 -12.250  -0.6851   0.06006   0.05358  -0.0721   1.0000   0.0250
 -12.000  -0.7061   0.05612   0.04943  -0.0716   1.0000   0.0251
 -11.750  -0.7234   0.05283   0.04594  -0.0701   1.0000   0.0252
 -11.500  -0.7389   0.04999   0.04287  -0.0678   1.0000   0.0254
 -11.250  -0.7521   0.04753   0.04019  -0.0648   1.0000   0.0256
 -11.000  -0.7619   0.04543   0.03789  -0.0614   1.0000   0.0257
 -10.750  -0.7717   0.04346   0.03570  -0.0573   1.0000   0.0261
 -10.500  -0.7795   0.04173   0.03375  -0.0529   1.0000   0.0264
 -10.250  -0.7852   0.04021   0.03201  -0.0485   1.0000   0.0267
 -10.000  -0.7865   0.03904   0.03082  -0.0447   1.0000   0.0272
  -9.750  -0.7875   0.03803   0.02978  -0.0408   1.0000   0.0276
  -9.500  -0.7890   0.03719   0.02890  -0.0369   0.9996   0.0283
  -9.250  -0.7587   0.03538   0.02686  -0.0389   0.9922   0.0302
  -9.000  -0.7283   0.03357   0.02483  -0.0406   0.9845   0.0318
  -8.750  -0.7000   0.03211   0.02333  -0.0419   0.9748   0.0333
  -8.500  -0.6720   0.03063   0.02172  -0.0428   0.9648   0.0353
  -8.250  -0.6438   0.02926   0.02025  -0.0437   0.9552   0.0374
  -8.000  -0.6141   0.02810   0.01905  -0.0451   0.9468   0.0411
  -7.750  -0.5881   0.02694   0.01784  -0.0455   0.9365   0.0445
  -7.500  -0.5572   0.02585   0.01663  -0.0468   0.9292   0.0498
  -7.250  -0.5305   0.02481   0.01563  -0.0474   0.9196   0.0557
  -7.000  -0.5018   0.02381   0.01460  -0.0483   0.9114   0.0637
  -6.750  -0.4749   0.02286   0.01365  -0.0488   0.9021   0.0740
  -6.500  -0.4488   0.02200   0.01278  -0.0490   0.8930   0.0877
  -6.250  -0.4230   0.02113   0.01197  -0.0492   0.8842   0.1059
  -6.000  -0.3996   0.02038   0.01129  -0.0489   0.8746   0.1313
  -5.750  -0.3759   0.01953   0.01061  -0.0486   0.8661   0.1672
  -5.500  -0.3582   0.01876   0.01006  -0.0473   0.8561   0.2168
  -5.250  -0.3396   0.01787   0.00952  -0.0460   0.8480   0.2916
  -5.000  -0.3273   0.01720   0.00923  -0.0434   0.8381   0.3733
  -4.750  -0.3079   0.01670   0.00907  -0.0417   0.8307   0.4569
  -4.500  -0.2891   0.01657   0.00910  -0.0396   0.8220   0.5154
  -4.250  -0.2655   0.01652   0.00906  -0.0384   0.8148   0.5607
  -4.000  -0.2426   0.01655   0.00904  -0.0370   0.8075   0.5936
  -3.750  -0.2194   0.01661   0.00905  -0.0357   0.7998   0.6199
  -3.500  -0.1919   0.01664   0.00897  -0.0352   0.7943   0.6440
  -3.250  -0.1721   0.01673   0.00901  -0.0333   0.7860   0.6635
  -3.000  -0.1469   0.01679   0.00898  -0.0324   0.7797   0.6829
  -2.750  -0.1215   0.01688   0.00901  -0.0314   0.7736   0.7008
  -2.500  -0.0975   0.01698   0.00907  -0.0303   0.7665   0.7158
  -2.250  -0.0675   0.01702   0.00903  -0.0303   0.7611   0.7278
  -2.000  -0.0437   0.01705   0.00899  -0.0294   0.7548   0.7391
  -1.750  -0.0190   0.01708   0.00896  -0.0286   0.7482   0.7494
  -1.500   0.0108   0.01706   0.00885  -0.0288   0.7431   0.7582
  -1.250   0.0340   0.01710   0.00884  -0.0278   0.7367   0.7677
  -1.000   0.0603   0.01713   0.00882  -0.0274   0.7305   0.7760
  -0.750   0.0893   0.01712   0.00873  -0.0275   0.7256   0.7851
  -0.500   0.1141   0.01718   0.00877  -0.0269   0.7190   0.7934
  -0.250   0.1399   0.01722   0.00877  -0.0264   0.7128   0.8023
   0.000   0.1709   0.01721   0.00870  -0.0269   0.7079   0.8102
   0.250   0.1958   0.01730   0.00879  -0.0264   0.7011   0.8186
   0.500   0.2227   0.01733   0.00880  -0.0262   0.6948   0.8271
   0.750   0.2571   0.01735   0.00876  -0.0273   0.6900   0.8343
   1.000   0.2794   0.01746   0.00890  -0.0264   0.6826   0.8439
   1.250   0.3121   0.01753   0.00896  -0.0273   0.6765   0.8512
   1.500   0.3422   0.01755   0.00894  -0.0277   0.6712   0.8605
   1.750   0.3724   0.01771   0.00916  -0.0283   0.6634   0.8679
   2.000   0.4027   0.01773   0.00916  -0.0288   0.6575   0.8775
   2.250   0.4377   0.01788   0.00934  -0.0303   0.6503   0.8841
   2.500   0.4660   0.01795   0.00942  -0.0304   0.6429   0.8944
   2.750   0.5055   0.01802   0.00949  -0.0327   0.6360   0.8999
   3.000   0.5344   0.01814   0.00966  -0.0330   0.6271   0.9097
   3.250   0.5730   0.01817   0.00968  -0.0351   0.6196   0.9157
   3.500   0.6055   0.01829   0.00987  -0.0362   0.6097   0.9241
   3.750   0.6409   0.01834   0.00993  -0.0378   0.6004   0.9314
   4.000   0.6765   0.01837   0.00996  -0.0394   0.5898   0.9386
   4.250   0.7083   0.01846   0.01012  -0.0404   0.5776   0.9474
   4.500   0.7409   0.01851   0.01018  -0.0414   0.5656   0.9569
   4.750   0.7760   0.01852   0.01020  -0.0430   0.5528   0.9650
   5.000   0.8080   0.01859   0.01030  -0.0441   0.5390   0.9749
   5.250   0.8404   0.01870   0.01045  -0.0454   0.5238   0.9849
   5.500   0.8751   0.01879   0.01058  -0.0472   0.5072   0.9939
   5.750   0.9046   0.01887   0.01067  -0.0480   0.4899   1.0000
   6.000   0.9111   0.01900   0.01078  -0.0442   0.4748   1.0000
   6.250   0.9184   0.01917   0.01092  -0.0406   0.4588   1.0000
   6.500   0.9261   0.01938   0.01107  -0.0369   0.4413   1.0000
   6.750   0.9332   0.01965   0.01128  -0.0333   0.4222   1.0000
   7.000   0.9399   0.01998   0.01155  -0.0295   0.4020   1.0000
   7.250   0.9458   0.02036   0.01186  -0.0257   0.3815   1.0000
   7.500   0.9503   0.02082   0.01220  -0.0216   0.3609   1.0000
   7.750   0.9535   0.02133   0.01260  -0.0174   0.3410   1.0000
   8.000   0.9538   0.02186   0.01304  -0.0127   0.3219   1.0000
   8.250   0.9544   0.02245   0.01355  -0.0083   0.3039   1.0000
   8.500   0.9557   0.02313   0.01415  -0.0042   0.2866   1.0000
   8.750   0.9576   0.02389   0.01484  -0.0004   0.2699   1.0000
   9.000   0.9608   0.02472   0.01560   0.0030   0.2548   1.0000
   9.250   0.9643   0.02563   0.01645   0.0061   0.2404   1.0000
   9.500   0.9684   0.02660   0.01736   0.0089   0.2276   1.0000
  10.000   0.9786   0.02870   0.01941   0.0137   0.2042   1.0000
  10.250   0.9848   0.02980   0.02050   0.0157   0.1943   1.0000
  10.500   0.9897   0.03103   0.02167   0.0177   0.1855   1.0000
  10.750   0.9979   0.03215   0.02284   0.0193   0.1765   1.0000
  11.000   1.0036   0.03344   0.02407   0.0211   0.1697   1.0000
  11.250   1.0125   0.03461   0.02533   0.0224   0.1620   1.0000
  11.500   1.0185   0.03598   0.02664   0.0239   0.1558   1.0000
  11.750   1.0279   0.03720   0.02794   0.0251   0.1495   1.0000
  12.000   1.0354   0.03855   0.02932   0.0263   0.1440   1.0000
  12.250   1.0433   0.03993   0.03069   0.0274   0.1391   1.0000
  12.500   1.0519   0.04129   0.03215   0.0284   0.1338   1.0000
  12.750   1.0590   0.04276   0.03364   0.0294   0.1292   1.0000
  13.000   1.0676   0.04418   0.03506   0.0303   0.1253   1.0000
  13.250   1.0756   0.04570   0.03671   0.0311   0.1209   1.0000
  13.500   1.0824   0.04728   0.03836   0.0319   0.1171   1.0000
  13.750   1.0901   0.04881   0.03986   0.0327   0.1138   1.0000
  14.000   1.0969   0.05054   0.04175   0.0333   0.1103   1.0000
  14.250   1.1026   0.05235   0.04368   0.0339   0.1068   1.0000
  14.500   1.1077   0.05420   0.04558   0.0343   0.1037   1.0000
  14.750   1.1152   0.05585   0.04722   0.0349   0.1010   1.0000
  15.000   1.1184   0.05807   0.04962   0.0352   0.0982   1.0000
  15.250   1.1215   0.06032   0.05203   0.0354   0.0954   1.0000
  15.500   1.1245   0.06257   0.05438   0.0356   0.0929   1.0000
  15.750   1.1281   0.06474   0.05659   0.0357   0.0906   1.0000
  16.000   1.1345   0.06670   0.05856   0.0359   0.0885   1.0000
  16.250   1.1303   0.06999   0.06210   0.0356   0.0863   1.0000
  16.500   1.1269   0.07324   0.06556   0.0351   0.0842   1.0000
  16.750   1.1247   0.07641   0.06886   0.0346   0.0822   1.0000
  17.000   1.1243   0.07935   0.07189   0.0340   0.0804   1.0000
  17.250   1.1275   0.08181   0.07437   0.0337   0.0787   1.0000
  17.500   1.1245   0.08523   0.07790   0.0329   0.0772   1.0000
  17.750   1.1094   0.09060   0.08354   0.0311   0.0759   1.0000
  18.000   1.0906   0.09673   0.08992   0.0286   0.0746   1.0000
  18.250   1.0694   0.10350   0.09692   0.0257   0.0734   1.0000
  18.500   1.0415   0.11178   0.10541   0.0216   0.0724   1.0000
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