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S8038 (13%) (s8038-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S8038 (13%) (s8038-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.82 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s8038-il-1000000.txt
Download as CSV file: xf-s8038-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.7770   0.12500   0.12291  -0.0141   1.0000   0.0092
 -16.500  -0.7898   0.11718   0.11501  -0.0182   1.0000   0.0092
 -16.250  -0.8124   0.10771   0.10544  -0.0234   1.0000   0.0091
 -16.000  -0.8717   0.09130   0.08880  -0.0327   1.0000   0.0089
 -15.750  -0.8901   0.08341   0.08080  -0.0376   1.0000   0.0090
 -15.500  -0.9227   0.07378   0.07098  -0.0432   1.0000   0.0088
 -15.250  -0.9405   0.06700   0.06406  -0.0474   1.0000   0.0089
 -15.000  -0.9517   0.06185   0.05877  -0.0504   1.0000   0.0089
 -14.750  -0.9686   0.05630   0.05307  -0.0530   1.0000   0.0089
 -14.500  -0.9766   0.05226   0.04890  -0.0549   1.0000   0.0090
 -14.250  -0.9919   0.04761   0.04408  -0.0563   1.0000   0.0089
 -14.000  -1.0007   0.04402   0.04035  -0.0570   1.0000   0.0090
 -13.750  -1.0045   0.04125   0.03744  -0.0572   1.0000   0.0090
 -13.500  -1.0056   0.03898   0.03505  -0.0570   1.0000   0.0091
 -13.250  -1.0076   0.03671   0.03267  -0.0564   1.0000   0.0091
 -13.000  -1.0073   0.03502   0.03085  -0.0555   1.0000   0.0091
 -12.750  -1.0241   0.03124   0.02682  -0.0531   1.0000   0.0093
 -12.500  -1.0252   0.02935   0.02481  -0.0510   1.0000   0.0094
 -12.250  -1.0294   0.02724   0.02257  -0.0481   1.0000   0.0095
 -12.000  -1.0269   0.02604   0.02129  -0.0454   1.0000   0.0096
 -11.750  -1.0254   0.02496   0.02016  -0.0421   1.0000   0.0098
 -11.500  -1.0248   0.02403   0.01916  -0.0381   1.0000   0.0098
 -11.250  -1.0221   0.02335   0.01844  -0.0342   1.0000   0.0100
 -11.000  -1.0148   0.02239   0.01739  -0.0312   1.0000   0.0100
 -10.750  -1.0036   0.02172   0.01668  -0.0287   1.0000   0.0103
 -10.500  -0.9926   0.02097   0.01587  -0.0262   1.0000   0.0104
 -10.250  -0.9809   0.02025   0.01509  -0.0236   1.0000   0.0106
 -10.000  -0.9674   0.01965   0.01445  -0.0213   1.0000   0.0109
  -9.750  -0.9547   0.01896   0.01370  -0.0188   1.0000   0.0111
  -9.500  -0.9410   0.01836   0.01305  -0.0165   1.0000   0.0113
  -9.250  -0.9258   0.01791   0.01254  -0.0143   1.0000   0.0116
  -9.000  -0.9122   0.01732   0.01190  -0.0119   1.0000   0.0117
  -8.750  -0.8832   0.01664   0.01116  -0.0126   0.9987   0.0118
  -8.500  -0.8535   0.01556   0.01000  -0.0138   0.9965   0.0121
  -8.250  -0.8222   0.01465   0.00904  -0.0152   0.9945   0.0126
  -8.000  -0.7911   0.01398   0.00833  -0.0163   0.9923   0.0130
  -7.750  -0.7600   0.01342   0.00775  -0.0173   0.9892   0.0133
  -7.500  -0.7269   0.01293   0.00723  -0.0186   0.9865   0.0138
  -7.250  -0.6927   0.01246   0.00672  -0.0202   0.9844   0.0143
  -7.000  -0.6619   0.01202   0.00626  -0.0210   0.9805   0.0148
  -6.750  -0.6317   0.01155   0.00576  -0.0216   0.9754   0.0155
  -6.500  -0.5984   0.01104   0.00523  -0.0230   0.9719   0.0165
  -6.250  -0.5713   0.01066   0.00483  -0.0228   0.9637   0.0175
  -6.000  -0.5379   0.01029   0.00445  -0.0240   0.9588   0.0187
  -5.750  -0.5060   0.00988   0.00405  -0.0249   0.9506   0.0215
  -5.500  -0.4664   0.00931   0.00358  -0.0277   0.9451   0.0395
  -5.250  -0.4282   0.00874   0.00319  -0.0302   0.9353   0.0735
  -5.000  -0.3900   0.00824   0.00285  -0.0328   0.9215   0.1125
  -4.750  -0.3577   0.00786   0.00258  -0.0339   0.9020   0.1493
  -4.500  -0.3311   0.00757   0.00236  -0.0337   0.8807   0.1881
  -4.250  -0.3076   0.00728   0.00217  -0.0329   0.8596   0.2290
  -4.000  -0.2844   0.00705   0.00201  -0.0319   0.8400   0.2690
  -3.750  -0.2617   0.00681   0.00186  -0.0309   0.8218   0.3136
  -3.500  -0.2391   0.00655   0.00172  -0.0298   0.8050   0.3627
  -3.250  -0.2159   0.00633   0.00160  -0.0288   0.7900   0.4084
  -3.000  -0.1931   0.00609   0.00150  -0.0278   0.7757   0.4619
  -2.750  -0.1695   0.00590   0.00143  -0.0269   0.7623   0.5102
  -2.500  -0.1446   0.00581   0.00139  -0.0262   0.7497   0.5423
  -2.250  -0.1191   0.00577   0.00135  -0.0255   0.7377   0.5659
  -2.000  -0.0931   0.00575   0.00133  -0.0250   0.7257   0.5854
  -1.750  -0.0666   0.00573   0.00130  -0.0246   0.7141   0.5999
  -1.500  -0.0400   0.00574   0.00128  -0.0242   0.7022   0.6123
  -1.250  -0.0134   0.00577   0.00126  -0.0238   0.6901   0.6237
  -1.000   0.0130   0.00577   0.00125  -0.0233   0.6781   0.6362
  -0.750   0.0397   0.00577   0.00125  -0.0230   0.6669   0.6467
  -0.500   0.0668   0.00580   0.00124  -0.0227   0.6560   0.6555
   0.000   0.1202   0.00585   0.00123  -0.0220   0.6315   0.6728
   0.250   0.1466   0.00587   0.00124  -0.0215   0.6170   0.6819
   0.500   0.1732   0.00590   0.00125  -0.0212   0.6029   0.6909
   0.750   0.1998   0.00594   0.00127  -0.0208   0.5891   0.6995
   1.000   0.2264   0.00599   0.00128  -0.0204   0.5757   0.7072
   1.250   0.2529   0.00603   0.00131  -0.0200   0.5617   0.7160
   1.500   0.2793   0.00608   0.00134  -0.0196   0.5477   0.7248
   1.750   0.3057   0.00615   0.00138  -0.0192   0.5331   0.7341
   2.000   0.3318   0.00620   0.00142  -0.0188   0.5169   0.7426
   2.250   0.3580   0.00628   0.00146  -0.0184   0.4987   0.7520
   2.500   0.3832   0.00638   0.00153  -0.0177   0.4758   0.7618
   2.750   0.4086   0.00649   0.00159  -0.0172   0.4555   0.7721
   3.250   0.4586   0.00674   0.00175  -0.0159   0.4085   0.7946
   3.500   0.4832   0.00689   0.00186  -0.0152   0.3831   0.8064
   3.750   0.5075   0.00705   0.00197  -0.0145   0.3581   0.8191
   4.000   0.5313   0.00723   0.00209  -0.0136   0.3315   0.8332
   4.250   0.5545   0.00744   0.00224  -0.0127   0.3024   0.8488
   4.500   0.5771   0.00767   0.00240  -0.0116   0.2721   0.8668
   4.750   0.6002   0.00787   0.00257  -0.0107   0.2460   0.8878
   5.000   0.6249   0.00807   0.00276  -0.0100   0.2221   0.9130
   5.250   0.6576   0.00838   0.00301  -0.0112   0.1968   0.9392
   5.500   0.6998   0.00873   0.00328  -0.0146   0.1738   0.9551
   6.000   0.7785   0.00945   0.00383  -0.0201   0.1379   0.9745
   6.250   0.8099   0.00976   0.00408  -0.0210   0.1262   0.9856
   6.500   0.8437   0.01006   0.00434  -0.0225   0.1161   0.9923
   6.750   0.8791   0.01037   0.00460  -0.0244   0.1055   0.9962
   7.000   0.9152   0.01071   0.00488  -0.0265   0.0958   0.9991
   7.250   0.9414   0.01097   0.00512  -0.0264   0.0901   1.0000
   7.500   0.9594   0.01128   0.00539  -0.0245   0.0842   1.0000
   7.750   0.9797   0.01147   0.00561  -0.0231   0.0818   1.0000
   8.000   0.9992   0.01173   0.00586  -0.0215   0.0783   1.0000
   8.250   1.0176   0.01207   0.00617  -0.0197   0.0737   1.0000
   8.500   1.0374   0.01233   0.00645  -0.0182   0.0713   1.0000
   8.750   1.0577   0.01256   0.00671  -0.0168   0.0694   1.0000
   9.000   1.0771   0.01284   0.00700  -0.0153   0.0668   1.0000
   9.250   1.0954   0.01318   0.00733  -0.0136   0.0639   1.0000
   9.500   1.1122   0.01361   0.00777  -0.0116   0.0608   1.0000
   9.750   1.1326   0.01383   0.00802  -0.0103   0.0597   1.0000
  10.000   1.1521   0.01409   0.00832  -0.0089   0.0578   1.0000
  10.250   1.1702   0.01441   0.00864  -0.0072   0.0554   1.0000
  10.500   1.1864   0.01483   0.00905  -0.0053   0.0527   1.0000
  10.750   1.2025   0.01524   0.00949  -0.0033   0.0504   1.0000
  11.000   1.2206   0.01549   0.00977  -0.0017   0.0487   1.0000
  11.250   1.2350   0.01583   0.01013   0.0006   0.0467   1.0000
  11.500   1.2476   0.01625   0.01055   0.0032   0.0444   1.0000
  11.750   1.2581   0.01682   0.01114   0.0059   0.0419   1.0000
  12.000   1.2751   0.01712   0.01148   0.0076   0.0405   1.0000
  12.250   1.2892   0.01759   0.01198   0.0096   0.0389   1.0000
  12.500   1.3021   0.01814   0.01253   0.0117   0.0368   1.0000
  12.750   1.3113   0.01891   0.01332   0.0141   0.0347   1.0000
  13.000   1.3256   0.01944   0.01391   0.0158   0.0338   1.0000
  13.250   1.3394   0.02001   0.01453   0.0174   0.0327   1.0000
  13.500   1.3512   0.02073   0.01530   0.0191   0.0317   1.0000
  13.750   1.3620   0.02156   0.01614   0.0208   0.0303   1.0000
  14.000   1.3698   0.02262   0.01723   0.0226   0.0288   1.0000
  14.250   1.3790   0.02365   0.01832   0.0241   0.0278   1.0000
  14.500   1.3905   0.02457   0.01931   0.0252   0.0273   1.0000
  14.750   1.4011   0.02560   0.02041   0.0262   0.0265   1.0000
  15.000   1.4099   0.02683   0.02171   0.0273   0.0259   1.0000
  15.250   1.4176   0.02821   0.02314   0.0281   0.0251   1.0000
  15.500   1.4237   0.02979   0.02476   0.0289   0.0243   1.0000
  15.750   1.4259   0.03179   0.02682   0.0296   0.0233   1.0000
  16.000   1.4276   0.03393   0.02904   0.0301   0.0227   1.0000
  16.250   1.4354   0.03556   0.03076   0.0303   0.0224   1.0000
  16.500   1.4406   0.03750   0.03278   0.0304   0.0220   1.0000
  16.750   1.4454   0.03950   0.03487   0.0305   0.0215   1.0000
  17.000   1.4463   0.04200   0.03747   0.0303   0.0213   1.0000
  17.250   1.4486   0.04441   0.03994   0.0300   0.0206   1.0000
  17.500   1.4463   0.04738   0.04300   0.0296   0.0202   1.0000
  17.750   1.4442   0.05045   0.04614   0.0289   0.0196   1.0000
  18.000   1.4376   0.05417   0.04995   0.0279   0.0194   1.0000
  18.250   1.4287   0.05831   0.05419   0.0266   0.0190   1.0000
  18.500   1.4165   0.06304   0.05902   0.0249   0.0184   1.0000
  18.750   1.4059   0.06768   0.06377   0.0232   0.0181   1.0000
  19.000   1.3991   0.07187   0.06807   0.0215   0.0179   1.0000
  19.250   1.3924   0.07613   0.07243   0.0199   0.0175   1.0000
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