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S8055 (12%) (s8055-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S8055 (12%) (s8055-il)
Reynolds number: 1,000,000
Max Cl/Cd: 88.73 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8055-il-1000000-n5.txt
Download as CSV file: xf-s8055-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8055 (12%)                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.8491   0.05218   0.04967  -0.0616   1.0000   0.0041
 -13.500  -0.8794   0.04364   0.04091  -0.0681   1.0000   0.0041
 -13.250  -0.9009   0.03842   0.03548  -0.0703   1.0000   0.0041
 -13.000  -0.9097   0.03539   0.03232  -0.0705   1.0000   0.0041
 -12.750  -0.9147   0.03307   0.02988  -0.0697   1.0000   0.0041
 -12.500  -0.8997   0.03046   0.02705  -0.0728   0.9486   0.0042
 -12.250  -0.9069   0.02850   0.02478  -0.0700   0.9145   0.0041
 -12.000  -0.9110   0.02713   0.02321  -0.0664   0.8978   0.0042
 -11.750  -0.9076   0.02600   0.02192  -0.0635   0.8867   0.0042
 -11.500  -0.8992   0.02477   0.02053  -0.0614   0.8787   0.0042
 -11.250  -0.8866   0.02373   0.01935  -0.0598   0.8719   0.0043
 -11.000  -0.8719   0.02280   0.01829  -0.0583   0.8665   0.0044
 -10.750  -0.8564   0.02176   0.01711  -0.0570   0.8615   0.0044
 -10.500  -0.8404   0.02069   0.01588  -0.0557   0.8565   0.0044
 -10.250  -0.8219   0.01987   0.01493  -0.0546   0.8522   0.0045
 -10.000  -0.8017   0.01912   0.01408  -0.0537   0.8486   0.0046
  -9.750  -0.7817   0.01829   0.01314  -0.0528   0.8448   0.0047
  -9.500  -0.7609   0.01753   0.01226  -0.0519   0.8411   0.0047
  -9.250  -0.7392   0.01686   0.01148  -0.0512   0.8377   0.0049
  -9.000  -0.7169   0.01622   0.01074  -0.0505   0.8347   0.0050
  -8.750  -0.6938   0.01561   0.01005  -0.0499   0.8317   0.0051
  -8.500  -0.6701   0.01508   0.00944  -0.0493   0.8287   0.0053
  -8.250  -0.6466   0.01452   0.00880  -0.0488   0.8256   0.0053
  -8.000  -0.6222   0.01407   0.00827  -0.0483   0.8227   0.0055
  -7.750  -0.5977   0.01363   0.00775  -0.0478   0.8200   0.0055
  -7.500  -0.5727   0.01318   0.00725  -0.0474   0.8175   0.0056
  -7.250  -0.5477   0.01273   0.00676  -0.0471   0.8148   0.0057
  -7.000  -0.5232   0.01220   0.00616  -0.0466   0.8118   0.0058
  -6.750  -0.4980   0.01177   0.00568  -0.0462   0.8089   0.0061
  -6.500  -0.4723   0.01143   0.00530  -0.0459   0.8060   0.0063
  -6.250  -0.4463   0.01111   0.00493  -0.0456   0.8032   0.0065
  -6.000  -0.4198   0.01081   0.00461  -0.0454   0.8005   0.0067
  -5.750  -0.3932   0.01052   0.00430  -0.0452   0.7976   0.0070
  -5.500  -0.3665   0.01027   0.00401  -0.0450   0.7947   0.0073
  -5.250  -0.3396   0.01004   0.00376  -0.0448   0.7918   0.0076
  -5.000  -0.3129   0.00979   0.00346  -0.0446   0.7889   0.0082
  -4.750  -0.2859   0.00955   0.00321  -0.0444   0.7861   0.0091
  -4.500  -0.2586   0.00934   0.00300  -0.0443   0.7829   0.0099
  -4.250  -0.2314   0.00912   0.00278  -0.0442   0.7792   0.0117
  -4.000  -0.2043   0.00893   0.00258  -0.0440   0.7756   0.0151
  -3.750  -0.1773   0.00871   0.00238  -0.0439   0.7723   0.0236
  -3.500  -0.1500   0.00849   0.00222  -0.0438   0.7691   0.0345
  -3.250  -0.1226   0.00829   0.00207  -0.0437   0.7655   0.0472
  -3.000  -0.0957   0.00804   0.00192  -0.0436   0.7617   0.0709
  -2.750  -0.0692   0.00777   0.00177  -0.0434   0.7577   0.1058
  -2.500  -0.0427   0.00746   0.00164  -0.0433   0.7530   0.1539
  -2.250  -0.0163   0.00716   0.00151  -0.0431   0.7471   0.2054
  -2.000   0.0101   0.00689   0.00140  -0.0429   0.7415   0.2595
  -1.750   0.0369   0.00663   0.00131  -0.0428   0.7355   0.3118
  -1.500   0.0634   0.00638   0.00123  -0.0426   0.7284   0.3686
  -1.250   0.0900   0.00614   0.00115  -0.0425   0.7192   0.4243
  -1.000   0.1163   0.00592   0.00107  -0.0422   0.7077   0.4838
  -0.750   0.1424   0.00571   0.00101  -0.0419   0.6947   0.5454
  -0.500   0.1682   0.00554   0.00097  -0.0415   0.6795   0.6066
  -0.250   0.1943   0.00545   0.00097  -0.0411   0.6612   0.6563
   0.000   0.2207   0.00544   0.00098  -0.0408   0.6414   0.6908
   0.250   0.2475   0.00548   0.00100  -0.0405   0.6226   0.7135
   0.500   0.2741   0.00556   0.00104  -0.0402   0.5999   0.7315
   0.750   0.3003   0.00569   0.00109  -0.0399   0.5722   0.7481
   1.000   0.3267   0.00583   0.00115  -0.0396   0.5450   0.7599
   1.250   0.3533   0.00597   0.00121  -0.0394   0.5206   0.7709
   1.500   0.3799   0.00610   0.00128  -0.0391   0.4982   0.7824
   1.750   0.4063   0.00624   0.00136  -0.0388   0.4748   0.7916
   2.000   0.4324   0.00643   0.00145  -0.0386   0.4485   0.8006
   2.250   0.4582   0.00661   0.00155  -0.0382   0.4213   0.8103
   2.500   0.4842   0.00678   0.00165  -0.0379   0.3976   0.8189
   2.750   0.5098   0.00698   0.00176  -0.0375   0.3729   0.8281
   3.000   0.5351   0.00718   0.00189  -0.0371   0.3462   0.8377
   3.500   0.5855   0.00758   0.00216  -0.0362   0.2997   0.8564
   4.000   0.6347   0.00809   0.00247  -0.0352   0.2491   0.8709
   4.250   0.6599   0.00830   0.00262  -0.0348   0.2312   0.8785
   4.500   0.6847   0.00848   0.00278  -0.0343   0.2163   0.8868
   4.750   0.7096   0.00868   0.00293  -0.0338   0.2030   0.8960
   5.000   0.7338   0.00887   0.00311  -0.0332   0.1893   0.9070
   5.250   0.7581   0.00905   0.00328  -0.0325   0.1774   0.9196
   5.500   0.7828   0.00923   0.00346  -0.0320   0.1664   0.9349
   5.750   0.8104   0.00947   0.00368  -0.0321   0.1541   0.9522
   6.000   0.8429   0.00974   0.00391  -0.0334   0.1427   0.9676
   6.250   0.8758   0.01004   0.00415  -0.0349   0.1315   0.9812
   6.500   0.9077   0.01032   0.00439  -0.0361   0.1216   0.9922
   6.750   0.9396   0.01059   0.00463  -0.0373   0.1139   0.9997
   7.000   0.9612   0.01086   0.00487  -0.0363   0.1060   1.0000
   7.250   0.9833   0.01110   0.00509  -0.0353   0.0996   1.0000
   7.500   1.0045   0.01141   0.00535  -0.0343   0.0913   1.0000
   7.750   1.0258   0.01172   0.00563  -0.0333   0.0833   1.0000
   8.000   1.0473   0.01202   0.00591  -0.0323   0.0771   1.0000
   8.250   1.0682   0.01236   0.00622  -0.0313   0.0712   1.0000
   8.500   1.0896   0.01266   0.00652  -0.0303   0.0667   1.0000
   8.750   1.1104   0.01299   0.00685  -0.0293   0.0622   1.0000
   9.000   1.1304   0.01336   0.00719  -0.0281   0.0574   1.0000
   9.250   1.1505   0.01370   0.00754  -0.0270   0.0533   1.0000
   9.500   1.1680   0.01412   0.00793  -0.0255   0.0482   1.0000
   9.750   1.1855   0.01446   0.00829  -0.0238   0.0454   1.0000
  10.000   1.2014   0.01489   0.00871  -0.0220   0.0420   1.0000
  10.250   1.2178   0.01530   0.00913  -0.0203   0.0396   1.0000
  10.500   1.2347   0.01571   0.00956  -0.0188   0.0376   1.0000
  10.750   1.2504   0.01620   0.01006  -0.0172   0.0350   1.0000
  11.000   1.2660   0.01672   0.01059  -0.0156   0.0327   1.0000
  11.250   1.2825   0.01719   0.01109  -0.0142   0.0315   1.0000
  11.500   1.2985   0.01771   0.01164  -0.0128   0.0302   1.0000
  11.750   1.3136   0.01828   0.01224  -0.0113   0.0289   1.0000
  12.000   1.3281   0.01891   0.01290  -0.0098   0.0276   1.0000
  12.250   1.3428   0.01954   0.01357  -0.0084   0.0264   1.0000
  12.500   1.3577   0.02017   0.01424  -0.0071   0.0253   1.0000
  12.750   1.3716   0.02087   0.01498  -0.0058   0.0240   1.0000
  13.000   1.3846   0.02165   0.01578  -0.0044   0.0227   1.0000
  13.250   1.3969   0.02249   0.01665  -0.0031   0.0214   1.0000
  13.500   1.4102   0.02328   0.01750  -0.0018   0.0209   1.0000
  13.750   1.4221   0.02417   0.01843  -0.0006   0.0193   1.0000
  14.000   1.4329   0.02517   0.01947   0.0007   0.0181   1.0000
  14.250   1.4432   0.02622   0.02056   0.0020   0.0170   1.0000
  14.500   1.4536   0.02728   0.02168   0.0031   0.0159   1.0000
  14.750   1.4606   0.02863   0.02305   0.0044   0.0139   1.0000
  15.000   1.4690   0.02991   0.02439   0.0056   0.0127   1.0000
  15.250   1.4730   0.03159   0.02609   0.0068   0.0103   1.0000
  15.500   1.4760   0.03339   0.02794   0.0079   0.0086   1.0000
  15.750   1.4787   0.03528   0.02989   0.0089   0.0074   1.0000
  16.000   1.4801   0.03739   0.03208   0.0097   0.0065   1.0000
  16.250   1.4812   0.03961   0.03437   0.0104   0.0059   1.0000
  16.500   1.4811   0.04204   0.03689   0.0108   0.0054   1.0000
  16.750   1.4802   0.04470   0.03964   0.0111   0.0051   1.0000
  17.000   1.4778   0.04766   0.04270   0.0110   0.0046   1.0000
  17.250   1.4780   0.05044   0.04557   0.0108   0.0047   1.0000
  17.500   1.4744   0.05382   0.04906   0.0102   0.0045   1.0000
  17.750   1.4712   0.05728   0.05263   0.0095   0.0044   1.0000
  18.000   1.4630   0.06157   0.05703   0.0082   0.0042   1.0000
  18.250   1.4540   0.06615   0.06173   0.0067   0.0041   1.0000
  18.500   1.4435   0.07116   0.06687   0.0047   0.0040   1.0000
  18.750   1.4320   0.07651   0.07234   0.0025   0.0039   1.0000
  19.000   1.4159   0.08278   0.07874  -0.0004   0.0038   1.0000
  19.250   1.4011   0.08907   0.08517  -0.0034   0.0039   1.0000
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