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S8035 for RC aerobatic 14% thick (s8035-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: S8035 for RC aerobatic 14% thick (s8035-il)
Reynolds number: 200,000
Max Cl/Cd: 52.04 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8035-il-200000.txt
Download as CSV file: xf-s8035-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8035 for RC aerobatic  14% thick               
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.9350   0.10677   0.10237  -0.0262   1.0000   0.0413
 -17.000  -0.9706   0.09640   0.09180  -0.0325   1.0000   0.0410
 -16.750  -1.0022   0.08741   0.08259  -0.0379   1.0000   0.0409
 -16.500  -1.0269   0.08016   0.07511  -0.0421   1.0000   0.0410
 -16.250  -1.0482   0.07393   0.06866  -0.0454   1.0000   0.0411
 -16.000  -1.0682   0.06842   0.06292  -0.0483   1.0000   0.0415
 -15.750  -1.0826   0.06366   0.05796  -0.0499   1.0000   0.0417
 -15.500  -1.0868   0.05994   0.05419  -0.0503   1.0000   0.0428
 -15.250  -1.0857   0.05733   0.05155  -0.0506   1.0000   0.0438
 -15.000  -1.0876   0.05452   0.04866  -0.0511   1.0000   0.0448
 -14.750  -1.0908   0.05166   0.04568  -0.0514   1.0000   0.0457
 -14.500  -1.0949   0.04883   0.04270  -0.0515   1.0000   0.0468
 -14.250  -1.0981   0.04620   0.03989  -0.0512   1.0000   0.0480
 -14.000  -1.1009   0.04380   0.03729  -0.0507   1.0000   0.0490
 -13.750  -1.1040   0.04166   0.03492  -0.0498   1.0000   0.0500
 -13.500  -1.0946   0.03935   0.03264  -0.0488   1.0000   0.0521
 -13.250  -1.0893   0.03775   0.03102  -0.0478   1.0000   0.0539
 -13.000  -1.0844   0.03617   0.02935  -0.0465   1.0000   0.0557
 -12.750  -1.0803   0.03464   0.02767  -0.0450   1.0000   0.0577
 -12.500  -1.0767   0.03317   0.02601  -0.0432   1.0000   0.0598
 -12.250  -1.0669   0.03153   0.02445  -0.0418   1.0000   0.0627
 -12.000  -1.0603   0.03041   0.02329  -0.0398   1.0000   0.0655
 -11.750  -1.0534   0.02934   0.02207  -0.0377   1.0000   0.0686
 -11.500  -1.0453   0.02798   0.02068  -0.0355   1.0000   0.0721
 -11.250  -1.0384   0.02703   0.01974  -0.0331   1.0000   0.0756
 -11.000  -1.0312   0.02627   0.01889  -0.0303   1.0000   0.0799
 -10.750  -1.0233   0.02524   0.01783  -0.0275   1.0000   0.0841
 -10.500  -1.0165   0.02450   0.01711  -0.0245   1.0000   0.0883
 -10.250  -1.0060   0.02388   0.01636  -0.0218   1.0000   0.0934
 -10.000  -0.9957   0.02292   0.01545  -0.0193   1.0000   0.0986
  -9.750  -0.9836   0.02233   0.01481  -0.0168   1.0000   0.1046
  -9.500  -0.9713   0.02153   0.01401  -0.0144   1.0000   0.1108
  -9.250  -0.9581   0.02096   0.01343  -0.0121   1.0000   0.1178
  -9.000  -0.9449   0.02025   0.01273  -0.0098   1.0000   0.1252
  -8.750  -0.9302   0.01976   0.01219  -0.0076   1.0000   0.1336
  -8.500  -0.9167   0.01910   0.01160  -0.0053   1.0000   0.1422
  -8.250  -0.9016   0.01858   0.01105  -0.0031   1.0000   0.1521
  -8.000  -0.8866   0.01810   0.01058  -0.0009   1.0000   0.1625
  -7.750  -0.8724   0.01754   0.01009   0.0014   1.0000   0.1729
  -7.500  -0.8574   0.01704   0.00961   0.0036   1.0000   0.1841
  -7.250  -0.8422   0.01662   0.00919   0.0058   1.0000   0.1962
  -7.000  -0.8272   0.01623   0.00882   0.0080   1.0000   0.2091
  -6.750  -0.8132   0.01581   0.00848   0.0104   1.0000   0.2221
  -6.500  -0.7993   0.01544   0.00817   0.0128   1.0000   0.2355
  -6.250  -0.7854   0.01511   0.00788   0.0151   1.0000   0.2496
  -6.000  -0.7714   0.01482   0.00764   0.0175   1.0000   0.2647
  -5.750  -0.7572   0.01457   0.00744   0.0197   1.0000   0.2802
  -5.500  -0.7428   0.01435   0.00727   0.0219   1.0000   0.2965
  -5.250  -0.7268   0.01416   0.00711   0.0237   0.9997   0.3140
  -5.000  -0.6844   0.01396   0.00701   0.0203   0.9936   0.3398
  -4.750  -0.6439   0.01374   0.00685   0.0174   0.9864   0.3659
  -4.500  -0.6034   0.01349   0.00671   0.0146   0.9795   0.3909
  -4.250  -0.5638   0.01324   0.00653   0.0120   0.9719   0.4157
  -4.000  -0.5265   0.01299   0.00636   0.0100   0.9637   0.4398
  -3.750  -0.4853   0.01274   0.00619   0.0073   0.9573   0.4647
  -3.500  -0.4493   0.01250   0.00603   0.0057   0.9484   0.4886
  -3.250  -0.4065   0.01222   0.00585   0.0028   0.9427   0.5137
  -3.000  -0.3696   0.01199   0.00568   0.0012   0.9340   0.5386
  -2.750  -0.3270   0.01170   0.00550  -0.0015   0.9277   0.5628
  -2.500  -0.2917   0.01149   0.00534  -0.0027   0.9175   0.5858
  -2.250  -0.2510   0.01123   0.00516  -0.0049   0.9101   0.6075
  -2.000  -0.2197   0.01107   0.00506  -0.0051   0.8973   0.6277
  -1.750  -0.1886   0.01093   0.00496  -0.0053   0.8843   0.6484
  -1.500  -0.1588   0.01083   0.00488  -0.0052   0.8709   0.6686
  -1.250  -0.1302   0.01074   0.00484  -0.0047   0.8563   0.6874
  -1.000  -0.1032   0.01067   0.00480  -0.0040   0.8407   0.7058
  -0.750  -0.0771   0.01063   0.00478  -0.0030   0.8246   0.7240
  -0.500  -0.0513   0.01060   0.00476  -0.0020   0.8083   0.7415
  -0.250  -0.0256   0.01058   0.00474  -0.0010   0.7920   0.7587
   0.000   0.0000   0.01058   0.00474   0.0000   0.7754   0.7754
   0.250   0.0256   0.01058   0.00474   0.0010   0.7587   0.7919
   0.500   0.0513   0.01060   0.00476   0.0020   0.7416   0.8083
   0.750   0.0770   0.01063   0.00478   0.0030   0.7240   0.8246
   1.000   0.1032   0.01067   0.00480   0.0040   0.7059   0.8408
   1.250   0.1302   0.01074   0.00484   0.0047   0.6873   0.8564
   1.500   0.1588   0.01083   0.00488   0.0052   0.6687   0.8709
   1.750   0.1886   0.01093   0.00496   0.0053   0.6484   0.8843
   2.000   0.2197   0.01107   0.00506   0.0051   0.6277   0.8973
   2.250   0.2510   0.01123   0.00516   0.0049   0.6076   0.9101
   2.500   0.2917   0.01149   0.00534   0.0027   0.5858   0.9175
   2.750   0.3271   0.01170   0.00550   0.0015   0.5629   0.9277
   3.000   0.3696   0.01199   0.00568  -0.0012   0.5385   0.9340
   3.250   0.4065   0.01222   0.00585  -0.0028   0.5138   0.9427
   3.500   0.4492   0.01249   0.00602  -0.0057   0.4887   0.9483
   3.750   0.4852   0.01274   0.00619  -0.0072   0.4647   0.9573
   4.000   0.5266   0.01299   0.00636  -0.0100   0.4401   0.9637
   4.250   0.5638   0.01324   0.00653  -0.0120   0.4158   0.9719
   4.500   0.6034   0.01349   0.00671  -0.0146   0.3910   0.9795
   4.750   0.6440   0.01374   0.00685  -0.0174   0.3659   0.9864
   5.000   0.6844   0.01396   0.00701  -0.0203   0.3396   0.9936
   5.250   0.7268   0.01416   0.00711  -0.0237   0.3142   0.9997
   5.500   0.7428   0.01434   0.00726  -0.0219   0.2965   1.0000
   5.750   0.7571   0.01456   0.00743  -0.0197   0.2803   1.0000
   6.000   0.7713   0.01482   0.00764  -0.0175   0.2647   1.0000
   6.250   0.7854   0.01511   0.00787  -0.0151   0.2496   1.0000
   6.500   0.7993   0.01544   0.00816  -0.0128   0.2356   1.0000
   6.750   0.8132   0.01581   0.00848  -0.0104   0.2222   1.0000
   7.000   0.8272   0.01623   0.00881  -0.0080   0.2090   1.0000
   7.250   0.8422   0.01661   0.00919  -0.0058   0.1962   1.0000
   7.500   0.8574   0.01704   0.00961  -0.0036   0.1841   1.0000
   7.750   0.8724   0.01753   0.01009  -0.0014   0.1730   1.0000
   8.000   0.8866   0.01809   0.01057   0.0009   0.1625   1.0000
   8.250   0.9016   0.01858   0.01105   0.0031   0.1521   1.0000
   8.500   0.9167   0.01910   0.01160   0.0053   0.1422   1.0000
   8.750   0.9302   0.01975   0.01218   0.0076   0.1336   1.0000
   9.000   0.9449   0.02025   0.01273   0.0098   0.1251   1.0000
   9.250   0.9581   0.02096   0.01342   0.0121   0.1178   1.0000
   9.500   0.9714   0.02154   0.01401   0.0144   0.1108   1.0000
   9.750   0.9836   0.02232   0.01480   0.0168   0.1046   1.0000
  10.000   0.9959   0.02292   0.01545   0.0192   0.0986   1.0000
  10.250   1.0062   0.02389   0.01637   0.0217   0.0934   1.0000
  10.500   1.0167   0.02451   0.01711   0.0244   0.0883   1.0000
  10.750   1.0236   0.02524   0.01782   0.0275   0.0841   1.0000
  11.000   1.0314   0.02628   0.01889   0.0302   0.0798   1.0000
  11.250   1.0387   0.02703   0.01974   0.0330   0.0757   1.0000
  11.500   1.0455   0.02798   0.02067   0.0355   0.0721   1.0000
  11.750   1.0539   0.02932   0.02205   0.0376   0.0687   1.0000
  12.000   1.0609   0.03040   0.02328   0.0398   0.0656   1.0000
  12.250   1.0675   0.03153   0.02445   0.0417   0.0627   1.0000
  12.500   1.0774   0.03319   0.02602   0.0431   0.0598   1.0000
  12.750   1.0814   0.03463   0.02766   0.0449   0.0578   1.0000
  13.000   1.0851   0.03616   0.02934   0.0465   0.0557   1.0000
  13.250   1.0895   0.03772   0.03098   0.0477   0.0537   1.0000
  13.500   1.0954   0.03933   0.03263   0.0488   0.0521   1.0000
  13.750   1.1047   0.04157   0.03483   0.0497   0.0500   1.0000
  14.000   1.1021   0.04380   0.03729   0.0506   0.0491   1.0000
  14.250   1.0991   0.04622   0.03992   0.0512   0.0480   1.0000
  14.500   1.0955   0.04878   0.04264   0.0514   0.0467   1.0000
  14.750   1.0921   0.05155   0.04556   0.0513   0.0456   1.0000
  15.000   1.0890   0.05440   0.04854   0.0510   0.0447   1.0000
  15.250   1.0872   0.05724   0.05145   0.0506   0.0437   1.0000
  15.500   1.0884   0.05986   0.05410   0.0502   0.0428   1.0000
  15.750   1.0844   0.06353   0.05783   0.0498   0.0417   1.0000
  16.000   1.0678   0.06854   0.06305   0.0479   0.0414   1.0000
  16.250   1.0487   0.07395   0.06869   0.0451   0.0411   1.0000
  16.500   1.0279   0.08019   0.07515   0.0419   0.0410   1.0000
  16.750   1.0037   0.08736   0.08253   0.0378   0.0409   1.0000
  17.000   0.9731   0.09616   0.09156   0.0323   0.0409   1.0000
  17.250   0.9330   0.10744   0.10305   0.0254   0.0412   1.0000
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