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RAE 100 AIRFOIL (rae100-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: RAE 100 AIRFOIL (rae100-il)
Reynolds number: 200,000
Max Cl/Cd: 45.02 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae100-il-200000-n5.txt
Download as CSV file: xf-rae100-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 100 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9296   0.08939   0.08523  -0.0060   1.0000   0.0187
 -14.000  -0.9860   0.07364   0.06909  -0.0170   1.0000   0.0182
 -13.750  -1.0096   0.06562   0.06083  -0.0226   1.0000   0.0181
 -13.500  -1.0202   0.06045   0.05555  -0.0260   1.0000   0.0184
 -13.250  -1.0347   0.05500   0.04989  -0.0292   1.0000   0.0184
 -13.000  -1.0446   0.05071   0.04544  -0.0313   1.0000   0.0185
 -12.750  -1.0515   0.04723   0.04181  -0.0325   1.0000   0.0187
 -12.500  -1.0575   0.04418   0.03859  -0.0329   1.0000   0.0190
 -12.250  -1.0624   0.04153   0.03577  -0.0324   1.0000   0.0192
 -12.000  -1.0651   0.03931   0.03339  -0.0311   1.0000   0.0195
 -11.750  -1.0664   0.03735   0.03124  -0.0292   1.0000   0.0199
 -11.500  -1.0653   0.03556   0.02925  -0.0269   1.0000   0.0203
 -11.250  -1.0600   0.03378   0.02726  -0.0250   1.0000   0.0209
 -11.000  -1.0508   0.03215   0.02540  -0.0233   1.0000   0.0215
 -10.750  -1.0394   0.03063   0.02368  -0.0218   1.0000   0.0222
 -10.500  -1.0264   0.02936   0.02238  -0.0205   1.0000   0.0230
 -10.250  -1.0110   0.02828   0.02121  -0.0193   1.0000   0.0239
 -10.000  -0.9947   0.02716   0.01996  -0.0180   1.0000   0.0250
  -9.750  -0.9778   0.02598   0.01863  -0.0168   1.0000   0.0260
  -9.500  -0.9598   0.02488   0.01735  -0.0156   1.0000   0.0270
  -9.250  -0.9426   0.02372   0.01614  -0.0144   1.0000   0.0282
  -9.000  -0.9233   0.02289   0.01526  -0.0134   1.0000   0.0298
  -8.750  -0.9033   0.02207   0.01435  -0.0124   1.0000   0.0315
  -8.500  -0.8828   0.02126   0.01340  -0.0114   1.0000   0.0333
  -8.250  -0.8636   0.02030   0.01241  -0.0102   1.0000   0.0351
  -8.000  -0.8426   0.01959   0.01166  -0.0093   1.0000   0.0375
  -7.750  -0.8209   0.01895   0.01092  -0.0083   1.0000   0.0404
  -7.500  -0.8001   0.01819   0.01012  -0.0073   1.0000   0.0434
  -7.250  -0.7783   0.01756   0.00947  -0.0064   1.0000   0.0470
  -7.000  -0.7559   0.01701   0.00884  -0.0055   1.0000   0.0512
  -6.750  -0.7342   0.01638   0.00823  -0.0045   1.0000   0.0565
  -6.500  -0.7117   0.01586   0.00766  -0.0036   1.0000   0.0624
  -6.250  -0.6894   0.01533   0.00714  -0.0027   1.0000   0.0702
  -6.000  -0.6671   0.01482   0.00665  -0.0017   1.0000   0.0791
  -5.750  -0.6446   0.01435   0.00620  -0.0008   1.0000   0.0904
  -5.500  -0.6221   0.01389   0.00579   0.0002   1.0000   0.1040
  -5.250  -0.5996   0.01345   0.00541   0.0011   1.0000   0.1208
  -5.000  -0.5771   0.01305   0.00507   0.0021   1.0000   0.1403
  -4.750  -0.5548   0.01262   0.00474   0.0030   1.0000   0.1631
  -4.500  -0.5324   0.01223   0.00446   0.0040   1.0000   0.1883
  -4.250  -0.5101   0.01187   0.00420   0.0050   1.0000   0.2161
  -4.000  -0.4878   0.01153   0.00398   0.0060   1.0000   0.2452
  -3.750  -0.4658   0.01121   0.00378   0.0070   1.0000   0.2757
  -3.500  -0.4439   0.01092   0.00361   0.0081   1.0000   0.3069
  -3.250  -0.4190   0.01065   0.00347   0.0085   0.9985   0.3395
  -3.000  -0.3824   0.01037   0.00334   0.0065   0.9895   0.3782
  -2.750  -0.3461   0.01012   0.00323   0.0047   0.9800   0.4157
  -2.500  -0.3091   0.00988   0.00313   0.0028   0.9700   0.4526
  -2.250  -0.2742   0.00967   0.00303   0.0014   0.9571   0.4877
  -2.000  -0.2391   0.00947   0.00294   0.0000   0.9429   0.5208
  -1.750  -0.2040   0.00929   0.00286  -0.0013   0.9266   0.5531
  -1.500  -0.1696   0.00912   0.00279  -0.0024   0.9075   0.5842
  -1.250  -0.1370   0.00898   0.00273  -0.0030   0.8846   0.6141
  -1.000  -0.1062   0.00887   0.00267  -0.0031   0.8596   0.6428
  -0.750  -0.0779   0.00878   0.00262  -0.0027   0.8329   0.6702
  -0.500  -0.0513   0.00873   0.00258  -0.0019   0.8051   0.6969
  -0.250  -0.0255   0.00870   0.00256  -0.0010   0.7777   0.7239
   0.000   0.0000   0.00870   0.00255   0.0000   0.7508   0.7507
   0.250   0.0255   0.00870   0.00256   0.0010   0.7240   0.7776
   0.500   0.0513   0.00873   0.00258   0.0019   0.6970   0.8052
   0.750   0.0778   0.00878   0.00262   0.0027   0.6701   0.8329
   1.000   0.1062   0.00887   0.00267   0.0031   0.6428   0.8596
   1.250   0.1370   0.00898   0.00273   0.0030   0.6141   0.8846
   1.500   0.1697   0.00912   0.00279   0.0024   0.5842   0.9075
   1.750   0.2039   0.00929   0.00286   0.0013   0.5530   0.9265
   2.000   0.2391   0.00947   0.00294   0.0000   0.5209   0.9429
   2.250   0.2743   0.00967   0.00303  -0.0014   0.4876   0.9571
   2.500   0.3092   0.00989   0.00313  -0.0028   0.4526   0.9699
   2.750   0.3461   0.01012   0.00323  -0.0047   0.4157   0.9798
   3.000   0.3824   0.01037   0.00334  -0.0065   0.3784   0.9894
   3.250   0.4190   0.01065   0.00348  -0.0085   0.3397   0.9984
   3.500   0.4440   0.01092   0.00362  -0.0081   0.3068   1.0000
   3.750   0.4659   0.01121   0.00378  -0.0070   0.2755   1.0000
   4.000   0.4880   0.01153   0.00397  -0.0060   0.2452   1.0000
   4.250   0.5103   0.01187   0.00421  -0.0050   0.2160   1.0000
   4.500   0.5326   0.01224   0.00446  -0.0040   0.1881   1.0000
   4.750   0.5550   0.01262   0.00474  -0.0031   0.1632   1.0000
   5.000   0.5772   0.01305   0.00507  -0.0021   0.1402   1.0000
   5.250   0.5998   0.01345   0.00541  -0.0011   0.1208   1.0000
   5.500   0.6222   0.01389   0.00579  -0.0002   0.1040   1.0000
   5.750   0.6447   0.01435   0.00620   0.0007   0.0903   1.0000
   6.000   0.6672   0.01482   0.00665   0.0017   0.0790   1.0000
   6.250   0.6895   0.01533   0.00714   0.0026   0.0701   1.0000
   6.500   0.7117   0.01586   0.00765   0.0036   0.0624   1.0000
   6.750   0.7343   0.01638   0.00823   0.0045   0.0565   1.0000
   7.000   0.7559   0.01701   0.00884   0.0055   0.0512   1.0000
   7.250   0.7782   0.01756   0.00946   0.0064   0.0470   1.0000
   7.500   0.8000   0.01819   0.01013   0.0073   0.0434   1.0000
   7.750   0.8207   0.01895   0.01093   0.0084   0.0405   1.0000
   8.000   0.8424   0.01960   0.01166   0.0093   0.0376   1.0000
   8.250   0.8635   0.02030   0.01241   0.0102   0.0352   1.0000
   8.500   0.8826   0.02126   0.01340   0.0114   0.0334   1.0000
   8.750   0.9030   0.02208   0.01435   0.0124   0.0316   1.0000
   9.000   0.9231   0.02288   0.01526   0.0134   0.0298   1.0000
   9.250   0.9424   0.02373   0.01615   0.0144   0.0283   1.0000
   9.500   0.9596   0.02487   0.01734   0.0156   0.0270   1.0000
   9.750   0.9774   0.02599   0.01863   0.0169   0.0260   1.0000
  10.000   0.9943   0.02716   0.01996   0.0181   0.0250   1.0000
  10.250   1.0107   0.02826   0.02119   0.0193   0.0239   1.0000
  10.500   1.0260   0.02937   0.02239   0.0205   0.0231   1.0000
  10.750   1.0391   0.03060   0.02365   0.0219   0.0222   1.0000
  11.000   1.0505   0.03212   0.02536   0.0234   0.0215   1.0000
  11.250   1.0597   0.03375   0.02723   0.0250   0.0209   1.0000
  11.500   1.0652   0.03553   0.02921   0.0270   0.0204   1.0000
  11.750   1.0661   0.03732   0.03121   0.0293   0.0199   1.0000
  12.000   1.0649   0.03927   0.03335   0.0312   0.0195   1.0000
  12.250   1.0624   0.04147   0.03571   0.0324   0.0192   1.0000
  12.500   1.0577   0.04411   0.03852   0.0329   0.0190   1.0000
  12.750   1.0518   0.04715   0.04172   0.0326   0.0187   1.0000
  13.000   1.0451   0.05060   0.04532   0.0314   0.0185   1.0000
  13.250   1.0359   0.05478   0.04966   0.0293   0.0184   1.0000
  13.500   1.0237   0.05982   0.05488   0.0264   0.0183   1.0000
  13.750   1.0090   0.06571   0.06094   0.0225   0.0182   1.0000
  14.000   0.9860   0.07365   0.06910   0.0170   0.0182   1.0000
  14.250   0.9303   0.08928   0.08511   0.0060   0.0187   1.0000
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