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S8038 (13%) (s8038-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S8038 (13%) (s8038-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.62 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8038-il-1000000-n5.txt
Download as CSV file: xf-s8038-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8038 (13%)                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.8777   0.13402   0.13166  -0.0094   1.0000   0.0061
 -18.250  -0.9119   0.12256   0.12006  -0.0153   1.0000   0.0060
 -18.000  -0.9387   0.11304   0.11043  -0.0202   1.0000   0.0061
 -17.750  -0.9678   0.10336   0.10061  -0.0253   1.0000   0.0061
 -17.500  -0.9929   0.09472   0.09185  -0.0298   1.0000   0.0061
 -17.250  -1.0231   0.08537   0.08235  -0.0348   1.0000   0.0060
 -17.000  -1.0418   0.07826   0.07512  -0.0386   1.0000   0.0061
 -16.750  -1.0613   0.07119   0.06791  -0.0424   1.0000   0.0061
 -16.500  -1.0784   0.06483   0.06141  -0.0458   1.0000   0.0061
 -16.250  -1.0918   0.05933   0.05578  -0.0486   1.0000   0.0060
 -16.000  -1.1014   0.05468   0.05102  -0.0508   1.0000   0.0061
 -15.750  -1.1076   0.05072   0.04695  -0.0524   1.0000   0.0062
 -15.500  -1.1184   0.04642   0.04252  -0.0539   1.0000   0.0061
 -15.250  -1.1212   0.04329   0.03927  -0.0548   1.0000   0.0063
 -15.000  -1.1222   0.04050   0.03638  -0.0553   1.0000   0.0063
 -14.750  -1.1259   0.03760   0.03337  -0.0555   1.0000   0.0063
 -14.500  -1.1240   0.03539   0.03107  -0.0554   1.0000   0.0064
 -14.250  -1.1242   0.03313   0.02870  -0.0550   1.0000   0.0064
 -14.000  -1.1212   0.03128   0.02677  -0.0543   1.0000   0.0065
 -13.750  -1.1176   0.02962   0.02501  -0.0533   1.0000   0.0066
 -13.500  -1.1143   0.02805   0.02335  -0.0521   1.0000   0.0066
 -13.250  -1.1092   0.02676   0.02198  -0.0505   1.0000   0.0066
 -13.000  -1.1032   0.02564   0.02078  -0.0488   1.0000   0.0067
 -12.750  -1.0962   0.02469   0.01976  -0.0468   1.0000   0.0067
 -12.500  -1.0920   0.02370   0.01869  -0.0442   1.0000   0.0068
 -12.250  -1.0941   0.02257   0.01747  -0.0403   1.0000   0.0069
 -12.000  -1.0934   0.02181   0.01665  -0.0363   1.0000   0.0069
 -11.750  -1.0926   0.02102   0.01580  -0.0320   1.0000   0.0071
 -11.500  -1.0837   0.02027   0.01499  -0.0292   1.0000   0.0072
 -11.250  -1.0710   0.01970   0.01439  -0.0269   1.0000   0.0073
 -11.000  -1.0592   0.01905   0.01369  -0.0244   1.0000   0.0074
 -10.750  -1.0442   0.01860   0.01319  -0.0223   1.0000   0.0076
 -10.500  -1.0307   0.01801   0.01256  -0.0200   1.0000   0.0077
 -10.250  -1.0036   0.01742   0.01193  -0.0205   0.9989   0.0079
 -10.000  -0.9744   0.01682   0.01128  -0.0214   0.9973   0.0080
  -9.750  -0.9449   0.01624   0.01065  -0.0223   0.9955   0.0082
  -9.500  -0.9147   0.01568   0.01004  -0.0233   0.9939   0.0084
  -9.250  -0.8879   0.01518   0.00950  -0.0235   0.9915   0.0086
  -9.000  -0.8603   0.01467   0.00895  -0.0238   0.9885   0.0087
  -8.750  -0.8310   0.01419   0.00843  -0.0245   0.9855   0.0089
  -8.500  -0.8013   0.01377   0.00798  -0.0252   0.9826   0.0091
  -8.250  -0.7788   0.01333   0.00751  -0.0243   0.9755   0.0092
  -8.000  -0.7539   0.01279   0.00693  -0.0239   0.9682   0.0096
  -7.750  -0.7266   0.01235   0.00647  -0.0240   0.9609   0.0100
  -7.500  -0.6947   0.01195   0.00606  -0.0251   0.9543   0.0104
  -7.250  -0.6581   0.01155   0.00563  -0.0272   0.9476   0.0108
  -7.000  -0.6140   0.01115   0.00521  -0.0309   0.9414   0.0113
  -6.750  -0.5686   0.01078   0.00480  -0.0349   0.9302   0.0117
  -6.500  -0.5278   0.01044   0.00438  -0.0379   0.9104   0.0124
  -6.250  -0.4975   0.01021   0.00406  -0.0385   0.8833   0.0135
  -6.000  -0.4725   0.01005   0.00381  -0.0379   0.8588   0.0146
  -5.750  -0.4488   0.00990   0.00358  -0.0370   0.8369   0.0165
  -5.500  -0.4258   0.00971   0.00335  -0.0360   0.8180   0.0222
  -5.250  -0.4025   0.00950   0.00313  -0.0350   0.8015   0.0313
  -5.000  -0.3793   0.00928   0.00292  -0.0341   0.7860   0.0440
  -4.500  -0.3322   0.00884   0.00253  -0.0324   0.7580   0.0777
  -4.250  -0.3086   0.00860   0.00235  -0.0316   0.7449   0.1022
  -4.000  -0.2848   0.00838   0.00218  -0.0308   0.7323   0.1265
  -3.750  -0.2611   0.00815   0.00202  -0.0299   0.7196   0.1570
  -3.500  -0.2377   0.00790   0.00187  -0.0291   0.7073   0.1933
  -3.250  -0.2134   0.00767   0.00174  -0.0284   0.6962   0.2280
  -3.000  -0.1899   0.00739   0.00161  -0.0276   0.6856   0.2761
  -2.750  -0.1667   0.00710   0.00148  -0.0267   0.6752   0.3304
  -2.500  -0.1422   0.00688   0.00138  -0.0260   0.6648   0.3723
  -2.250  -0.1174   0.00670   0.00130  -0.0254   0.6553   0.4106
  -1.750  -0.0669   0.00643   0.00118  -0.0243   0.6346   0.4780
  -1.500  -0.0411   0.00636   0.00114  -0.0238   0.6230   0.5028
  -1.250  -0.0152   0.00632   0.00111  -0.0233   0.6106   0.5253
  -0.750   0.0370   0.00625   0.00109  -0.0224   0.5862   0.5700
  -0.500   0.0639   0.00625   0.00108  -0.0221   0.5751   0.5822
  -0.250   0.0907   0.00628   0.00108  -0.0218   0.5634   0.5938
   0.000   0.1171   0.00631   0.00109  -0.0214   0.5482   0.6056
   0.250   0.1434   0.00636   0.00110  -0.0210   0.5294   0.6166
   0.500   0.1696   0.00642   0.00112  -0.0206   0.5102   0.6276
   0.750   0.1958   0.00650   0.00115  -0.0201   0.4910   0.6368
   1.250   0.2484   0.00666   0.00122  -0.0194   0.4543   0.6535
   1.500   0.2745   0.00674   0.00126  -0.0189   0.4355   0.6625
   1.750   0.3007   0.00685   0.00131  -0.0186   0.4160   0.6713
   2.000   0.3263   0.00697   0.00138  -0.0181   0.3938   0.6790
   2.250   0.3519   0.00713   0.00146  -0.0176   0.3689   0.6872
   2.500   0.3764   0.00732   0.00155  -0.0169   0.3366   0.6956
   2.750   0.4013   0.00752   0.00166  -0.0163   0.3090   0.7044
   3.000   0.4261   0.00769   0.00177  -0.0157   0.2845   0.7137
   3.250   0.4506   0.00791   0.00189  -0.0151   0.2573   0.7221
   3.500   0.4755   0.00809   0.00202  -0.0145   0.2358   0.7309
   3.750   0.5003   0.00827   0.00215  -0.0139   0.2163   0.7393
   4.000   0.5250   0.00847   0.00229  -0.0133   0.1981   0.7487
   4.250   0.5495   0.00865   0.00244  -0.0126   0.1812   0.7579
   4.500   0.5740   0.00885   0.00259  -0.0120   0.1645   0.7681
   4.750   0.5984   0.00903   0.00275  -0.0113   0.1515   0.7790
   5.000   0.6228   0.00919   0.00291  -0.0106   0.1409   0.7904
   5.250   0.6473   0.00933   0.00307  -0.0100   0.1321   0.8030
   5.500   0.6713   0.00950   0.00324  -0.0092   0.1233   0.8171
   5.750   0.6952   0.00964   0.00342  -0.0084   0.1157   0.8329
   6.000   0.7184   0.00980   0.00360  -0.0075   0.1072   0.8511
   6.250   0.7415   0.00995   0.00380  -0.0066   0.1004   0.8727
   6.500   0.7656   0.01007   0.00400  -0.0058   0.0950   0.9002
   6.750   0.7980   0.01027   0.00426  -0.0069   0.0891   0.9325
   7.000   0.8434   0.01060   0.00459  -0.0110   0.0819   0.9531
   7.250   0.8882   0.01098   0.00493  -0.0151   0.0738   0.9653
   7.500   0.9249   0.01126   0.00521  -0.0172   0.0702   0.9793
   7.750   0.9534   0.01153   0.00548  -0.0176   0.0673   0.9906
   8.250   1.0148   0.01216   0.00609  -0.0194   0.0605   0.9999
   8.500   1.0361   0.01239   0.00633  -0.0182   0.0589   1.0000
   8.750   1.0561   0.01264   0.00660  -0.0168   0.0569   1.0000
   9.000   1.0754   0.01292   0.00689  -0.0152   0.0546   1.0000
   9.250   1.0944   0.01323   0.00719  -0.0136   0.0521   1.0000
   9.500   1.1137   0.01352   0.00750  -0.0121   0.0504   1.0000
   9.750   1.1333   0.01379   0.00779  -0.0107   0.0491   1.0000
  10.000   1.1521   0.01408   0.00811  -0.0091   0.0471   1.0000
  10.250   1.1698   0.01444   0.00846  -0.0074   0.0446   1.0000
  10.500   1.1869   0.01481   0.00883  -0.0056   0.0423   1.0000
  10.750   1.2048   0.01513   0.00918  -0.0039   0.0408   1.0000
  11.000   1.2208   0.01549   0.00955  -0.0019   0.0384   1.0000
  11.250   1.2339   0.01589   0.00996   0.0006   0.0363   1.0000
  11.500   1.2466   0.01631   0.01039   0.0031   0.0344   1.0000
  11.750   1.2610   0.01670   0.01081   0.0052   0.0332   1.0000
  12.000   1.2745   0.01716   0.01129   0.0074   0.0310   1.0000
  12.250   1.2879   0.01766   0.01182   0.0095   0.0298   1.0000
  12.500   1.3003   0.01824   0.01241   0.0116   0.0279   1.0000
  12.750   1.3140   0.01877   0.01298   0.0135   0.0270   1.0000
  13.000   1.3268   0.01937   0.01363   0.0154   0.0259   1.0000
  13.250   1.3386   0.02006   0.01434   0.0172   0.0246   1.0000
  13.500   1.3499   0.02081   0.01513   0.0190   0.0238   1.0000
  13.750   1.3603   0.02165   0.01601   0.0207   0.0226   1.0000
  14.000   1.3719   0.02247   0.01689   0.0222   0.0220   1.0000
  14.250   1.3825   0.02339   0.01785   0.0235   0.0211   1.0000
  14.500   1.3924   0.02441   0.01893   0.0248   0.0204   1.0000
  14.750   1.4006   0.02561   0.02017   0.0261   0.0194   1.0000
  15.000   1.4089   0.02688   0.02150   0.0271   0.0188   1.0000
  15.250   1.4158   0.02831   0.02299   0.0280   0.0182   1.0000
  15.500   1.4244   0.02967   0.02443   0.0287   0.0178   1.0000
  15.750   1.4317   0.03121   0.02604   0.0293   0.0172   1.0000
  16.000   1.4380   0.03289   0.02778   0.0298   0.0167   1.0000
  16.250   1.4428   0.03476   0.02972   0.0301   0.0161   1.0000
  16.500   1.4461   0.03685   0.03188   0.0303   0.0155   1.0000
  16.750   1.4470   0.03924   0.03433   0.0304   0.0147   1.0000
  17.000   1.4489   0.04161   0.03680   0.0303   0.0147   1.0000
  17.250   1.4491   0.04423   0.03950   0.0300   0.0140   1.0000
  17.500   1.4480   0.04706   0.04242   0.0296   0.0137   1.0000
  17.750   1.4456   0.05014   0.04558   0.0289   0.0129   1.0000
  18.000   1.4422   0.05346   0.04901   0.0280   0.0129   1.0000
  18.250   1.4359   0.05721   0.05284   0.0269   0.0124   1.0000
  18.500   1.4255   0.06163   0.05735   0.0254   0.0117   1.0000
  18.750   1.4151   0.06621   0.06203   0.0238   0.0113   1.0000
  19.000   1.4035   0.07106   0.06699   0.0218   0.0108   1.0000
  19.250   1.3876   0.07666   0.07270   0.0195   0.0101   1.0000
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