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S8037 (16%) (s8037-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S8037 (16%) (s8037-il)
Reynolds number: 500,000
Max Cl/Cd: 85.29 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8037-il-500000-n5.txt
Download as CSV file: xf-s8037-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8037 (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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.7438   0.08803   0.08474  -0.0567   1.0000   0.0081
 -16.000  -0.7773   0.07777   0.07426  -0.0627   1.0000   0.0081
 -15.750  -0.7986   0.07025   0.06658  -0.0671   1.0000   0.0081
 -15.500  -0.8282   0.06208   0.05817  -0.0716   1.0000   0.0080
 -15.250  -0.8383   0.05734   0.05333  -0.0742   1.0000   0.0081
 -15.000  -0.8427   0.05370   0.04962  -0.0759   1.0000   0.0082
 -14.750  -0.8563   0.04917   0.04494  -0.0776   1.0000   0.0082
 -14.500  -0.8655   0.04547   0.04109  -0.0786   1.0000   0.0082
 -14.250  -0.8688   0.04269   0.03822  -0.0790   1.0000   0.0083
 -14.000  -0.8718   0.04014   0.03558  -0.0789   1.0000   0.0084
 -13.750  -0.8733   0.03792   0.03327  -0.0785   1.0000   0.0085
 -13.500  -0.8776   0.03559   0.03081  -0.0775   1.0000   0.0085
 -13.250  -0.8780   0.03379   0.02892  -0.0762   1.0000   0.0085
 -13.000  -0.8767   0.03230   0.02735  -0.0747   1.0000   0.0088
 -12.750  -0.8778   0.03072   0.02567  -0.0725   1.0000   0.0088
 -12.500  -0.8767   0.02948   0.02434  -0.0702   1.0000   0.0089
 -12.000  -0.8451   0.02672   0.02135  -0.0704   0.9887   0.0094
 -11.750  -0.8327   0.02545   0.01996  -0.0694   0.9608   0.0095
 -11.500  -0.7936   0.02398   0.01832  -0.0736   0.9431   0.0098
 -11.000  -0.6931   0.02105   0.01506  -0.0865   0.9081   0.0105
 -10.750  -0.6586   0.02020   0.01403  -0.0892   0.8769   0.0109
 -10.500  -0.6419   0.01964   0.01331  -0.0878   0.8509   0.0112
 -10.250  -0.6289   0.01912   0.01265  -0.0856   0.8320   0.0114
 -10.000  -0.6158   0.01864   0.01204  -0.0833   0.8169   0.0118
  -9.750  -0.6019   0.01820   0.01148  -0.0810   0.8039   0.0122
  -9.500  -0.5865   0.01784   0.01098  -0.0789   0.7930   0.0126
  -9.250  -0.5747   0.01731   0.01038  -0.0762   0.7830   0.0130
  -9.000  -0.5618   0.01686   0.00985  -0.0736   0.7748   0.0133
  -8.750  -0.5459   0.01647   0.00940  -0.0716   0.7665   0.0137
  -8.500  -0.5285   0.01608   0.00894  -0.0698   0.7593   0.0143
  -8.250  -0.5101   0.01571   0.00850  -0.0682   0.7521   0.0147
  -8.000  -0.4915   0.01535   0.00806  -0.0665   0.7458   0.0151
  -7.750  -0.4722   0.01499   0.00763  -0.0650   0.7398   0.0158
  -7.500  -0.4533   0.01459   0.00719  -0.0634   0.7337   0.0164
  -7.250  -0.4331   0.01428   0.00682  -0.0621   0.7280   0.0173
  -7.000  -0.4117   0.01400   0.00649  -0.0609   0.7227   0.0182
  -6.750  -0.3906   0.01370   0.00614  -0.0596   0.7172   0.0191
  -6.500  -0.3698   0.01339   0.00579  -0.0583   0.7119   0.0203
  -6.250  -0.3479   0.01312   0.00548  -0.0572   0.7071   0.0217
  -6.000  -0.3257   0.01286   0.00518  -0.0561   0.7019   0.0234
  -5.750  -0.3036   0.01261   0.00491  -0.0550   0.6969   0.0262
  -5.500  -0.2814   0.01236   0.00464  -0.0539   0.6924   0.0302
  -5.250  -0.2588   0.01210   0.00439  -0.0529   0.6877   0.0366
  -5.000  -0.2362   0.01185   0.00417  -0.0519   0.6829   0.0457
  -4.750  -0.2138   0.01160   0.00395  -0.0509   0.6785   0.0585
  -4.250  -0.1682   0.01112   0.00357  -0.0490   0.6695   0.0905
  -4.000  -0.1453   0.01089   0.00339  -0.0480   0.6649   0.1119
  -3.750  -0.1231   0.01064   0.00321  -0.0470   0.6607   0.1400
  -3.500  -0.1015   0.01030   0.00304  -0.0458   0.6565   0.1810
  -3.250  -0.0825   0.00983   0.00285  -0.0443   0.6517   0.2524
  -2.750  -0.0452   0.00898   0.00253  -0.0408   0.6428   0.4066
  -2.500  -0.0237   0.00872   0.00245  -0.0396   0.6381   0.4576
  -2.250  -0.0015   0.00854   0.00238  -0.0384   0.6330   0.5001
  -2.000   0.0213   0.00842   0.00233  -0.0373   0.6282   0.5356
  -1.750   0.0446   0.00831   0.00230  -0.0362   0.6235   0.5691
  -1.500   0.0684   0.00823   0.00228  -0.0353   0.6184   0.5961
  -1.250   0.0930   0.00819   0.00225  -0.0345   0.6132   0.6151
  -1.000   0.1175   0.00815   0.00223  -0.0338   0.6086   0.6360
  -0.750   0.1418   0.00809   0.00223  -0.0329   0.6032   0.6578
  -0.500   0.1665   0.00807   0.00221  -0.0322   0.5979   0.6745
  -0.250   0.1917   0.00807   0.00220  -0.0316   0.5931   0.6880
   0.000   0.2172   0.00804   0.00221  -0.0310   0.5877   0.7006
   0.250   0.2425   0.00804   0.00221  -0.0304   0.5820   0.7126
   0.750   0.2932   0.00804   0.00222  -0.0293   0.5701   0.7353
   1.000   0.3181   0.00806   0.00223  -0.0286   0.5637   0.7466
   1.500   0.3684   0.00807   0.00229  -0.0274   0.5509   0.7722
   1.750   0.3931   0.00810   0.00232  -0.0267   0.5447   0.7860
   2.000   0.4185   0.00810   0.00237  -0.0261   0.5373   0.7996
   2.250   0.4429   0.00814   0.00241  -0.0254   0.5299   0.8143
   2.500   0.4690   0.00815   0.00247  -0.0250   0.5222   0.8297
   2.750   0.4948   0.00821   0.00254  -0.0246   0.5141   0.8467
   3.000   0.5240   0.00824   0.00262  -0.0249   0.5057   0.8643
   3.250   0.5566   0.00833   0.00274  -0.0260   0.4970   0.8822
   3.500   0.5957   0.00845   0.00288  -0.0286   0.4869   0.8982
   3.750   0.6393   0.00862   0.00304  -0.0322   0.4757   0.9107
   4.000   0.6845   0.00883   0.00321  -0.0362   0.4629   0.9192
   4.250   0.7251   0.00905   0.00339  -0.0392   0.4494   0.9282
   4.500   0.7638   0.00928   0.00360  -0.0417   0.4359   0.9348
   4.750   0.7957   0.00952   0.00380  -0.0428   0.4220   0.9437
   5.000   0.8279   0.00977   0.00402  -0.0439   0.4084   0.9502
   5.500   0.8795   0.01034   0.00448  -0.0436   0.3791   0.9691
   5.750   0.9066   0.01063   0.00473  -0.0437   0.3653   0.9763
   6.250   0.9622   0.01133   0.00529  -0.0445   0.3313   0.9873
   6.500   0.9907   0.01174   0.00562  -0.0452   0.3112   0.9917
   7.000   1.0507   0.01255   0.00627  -0.0474   0.2754   0.9981
   7.250   1.0768   0.01294   0.00660  -0.0476   0.2604   1.0000
   7.500   1.0874   0.01325   0.00688  -0.0445   0.2493   1.0000
   7.750   1.0970   0.01356   0.00717  -0.0412   0.2400   1.0000
   8.250   1.1065   0.01419   0.00775  -0.0327   0.2216   1.0000
   8.500   1.1123   0.01457   0.00810  -0.0288   0.2126   1.0000
   8.750   1.1202   0.01497   0.00849  -0.0254   0.2038   1.0000
   9.000   1.1283   0.01541   0.00892  -0.0222   0.1955   1.0000
   9.250   1.1353   0.01595   0.00943  -0.0189   0.1862   1.0000
   9.500   1.1449   0.01646   0.00994  -0.0162   0.1780   1.0000
   9.750   1.1524   0.01711   0.01056  -0.0134   0.1694   1.0000
  10.000   1.1621   0.01773   0.01119  -0.0110   0.1618   1.0000
  10.250   1.1702   0.01848   0.01192  -0.0086   0.1538   1.0000
  10.500   1.1798   0.01922   0.01267  -0.0065   0.1468   1.0000
  10.750   1.1884   0.02008   0.01352  -0.0044   0.1400   1.0000
  11.000   1.1983   0.02091   0.01437  -0.0026   0.1340   1.0000
  11.250   1.2063   0.02192   0.01538  -0.0008   0.1279   1.0000
  11.500   1.2165   0.02283   0.01632   0.0008   0.1221   1.0000
  11.750   1.2240   0.02397   0.01744   0.0024   0.1161   1.0000
  12.000   1.2338   0.02499   0.01850   0.0038   0.1112   1.0000
  12.250   1.2420   0.02616   0.01969   0.0052   0.1060   1.0000
  12.500   1.2497   0.02740   0.02095   0.0065   0.1016   1.0000
  12.750   1.2586   0.02859   0.02218   0.0076   0.0974   1.0000
  13.000   1.2652   0.02998   0.02358   0.0089   0.0928   1.0000
  13.250   1.2723   0.03136   0.02500   0.0100   0.0886   1.0000
  13.500   1.2792   0.03280   0.02646   0.0110   0.0844   1.0000
  13.750   1.2839   0.03443   0.02812   0.0121   0.0806   1.0000
  14.000   1.2903   0.03598   0.02971   0.0129   0.0778   1.0000
  14.250   1.2969   0.03754   0.03132   0.0138   0.0748   1.0000
  14.500   1.3005   0.03940   0.03321   0.0146   0.0712   1.0000
  14.750   1.3040   0.04133   0.03518   0.0153   0.0685   1.0000
  15.000   1.3103   0.04305   0.03696   0.0158   0.0662   1.0000
  15.250   1.3146   0.04498   0.03895   0.0164   0.0635   1.0000
  15.500   1.3169   0.04717   0.04119   0.0168   0.0610   1.0000
  15.750   1.3185   0.04948   0.04354   0.0172   0.0586   1.0000
  16.000   1.3231   0.05153   0.04566   0.0175   0.0564   1.0000
  16.250   1.3254   0.05384   0.04803   0.0177   0.0541   1.0000
  16.500   1.3255   0.05645   0.05069   0.0178   0.0520   1.0000
  16.750   1.3250   0.05917   0.05346   0.0178   0.0500   1.0000
  17.000   1.3276   0.06160   0.05596   0.0178   0.0481   1.0000
  17.250   1.3277   0.06435   0.05878   0.0176   0.0464   1.0000
  17.500   1.3247   0.06752   0.06200   0.0173   0.0442   1.0000
  17.750   1.3220   0.07070   0.06524   0.0170   0.0424   1.0000
  18.000   1.3219   0.07362   0.06824   0.0166   0.0414   1.0000
  18.250   1.3199   0.07681   0.07151   0.0160   0.0395   1.0000
  18.500   1.3156   0.08034   0.07510   0.0154   0.0379   1.0000
  18.750   1.3097   0.08414   0.07896   0.0145   0.0366   1.0000
  19.000   1.3051   0.08783   0.08274   0.0137   0.0357   1.0000
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