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RAE 100 AIRFOIL (rae100-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RAE 100 AIRFOIL (rae100-il)
Reynolds number: 500,000
Max Cl/Cd: 60.92 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae100-il-500000-n5.txt
Download as CSV file: xf-rae100-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.9588   0.13975   0.13697   0.0234   1.0000   0.0105
 -17.250  -0.9892   0.12798   0.12507   0.0168   1.0000   0.0105
 -17.000  -1.0176   0.11714   0.11410   0.0106   1.0000   0.0105
 -16.750  -1.0441   0.10720   0.10402   0.0050   1.0000   0.0105
 -16.500  -1.0680   0.09817   0.09486  -0.0002   1.0000   0.0104
 -16.250  -1.0940   0.08910   0.08566  -0.0054   1.0000   0.0104
 -16.000  -1.1186   0.08068   0.07710  -0.0102   1.0000   0.0104
 -15.750  -1.1384   0.07327   0.06956  -0.0145   1.0000   0.0104
 -15.500  -1.1593   0.06587   0.06200  -0.0189   1.0000   0.0104
 -15.250  -1.1751   0.05946   0.05544  -0.0228   1.0000   0.0105
 -15.000  -1.1875   0.05382   0.04964  -0.0262   1.0000   0.0105
 -14.750  -1.1990   0.04861   0.04429  -0.0292   1.0000   0.0105
 -14.500  -1.2071   0.04418   0.03970  -0.0315   1.0000   0.0106
 -14.250  -1.2122   0.04053   0.03589  -0.0331   1.0000   0.0107
 -14.000  -1.2162   0.03737   0.03258  -0.0339   1.0000   0.0108
 -13.750  -1.2176   0.03485   0.02993  -0.0340   1.0000   0.0109
 -13.500  -1.2240   0.03226   0.02723  -0.0332   1.0000   0.0112
 -13.250  -1.2246   0.03045   0.02531  -0.0317   1.0000   0.0113
 -13.000  -1.2237   0.02895   0.02371  -0.0296   1.0000   0.0114
 -12.750  -1.2196   0.02778   0.02245  -0.0272   1.0000   0.0117
 -12.500  -1.2132   0.02674   0.02132  -0.0248   1.0000   0.0119
 -12.250  -1.2019   0.02575   0.02023  -0.0231   1.0000   0.0122
 -12.000  -1.1888   0.02478   0.01916  -0.0215   1.0000   0.0125
 -11.750  -1.1743   0.02386   0.01814  -0.0201   1.0000   0.0129
 -11.500  -1.1584   0.02297   0.01715  -0.0187   1.0000   0.0133
 -11.250  -1.1410   0.02218   0.01625  -0.0175   1.0000   0.0137
 -11.000  -1.1234   0.02136   0.01534  -0.0163   1.0000   0.0142
 -10.750  -1.1057   0.02051   0.01442  -0.0151   1.0000   0.0147
 -10.500  -1.0860   0.01982   0.01368  -0.0141   1.0000   0.0153
 -10.250  -1.0656   0.01919   0.01299  -0.0131   1.0000   0.0160
 -10.000  -1.0449   0.01856   0.01228  -0.0122   1.0000   0.0166
  -9.750  -1.0237   0.01797   0.01160  -0.0113   1.0000   0.0172
  -9.500  -1.0026   0.01733   0.01089  -0.0103   1.0000   0.0179
  -9.250  -0.9813   0.01672   0.01025  -0.0094   1.0000   0.0189
  -9.000  -0.9589   0.01622   0.00971  -0.0086   1.0000   0.0200
  -8.750  -0.9362   0.01575   0.00918  -0.0078   1.0000   0.0211
  -8.500  -0.9133   0.01529   0.00866  -0.0070   1.0000   0.0222
  -8.250  -0.8911   0.01475   0.00810  -0.0061   1.0000   0.0237
  -8.000  -0.8681   0.01431   0.00764  -0.0053   1.0000   0.0252
  -7.750  -0.8447   0.01394   0.00721  -0.0045   1.0000   0.0269
  -7.500  -0.8217   0.01349   0.00675  -0.0036   1.0000   0.0290
  -7.250  -0.7985   0.01311   0.00636  -0.0028   1.0000   0.0315
  -7.000  -0.7749   0.01279   0.00600  -0.0020   1.0000   0.0337
  -6.750  -0.7519   0.01239   0.00561  -0.0011   1.0000   0.0371
  -6.500  -0.7284   0.01207   0.00528  -0.0002   1.0000   0.0407
  -6.250  -0.7051   0.01172   0.00495   0.0007   1.0000   0.0453
  -6.000  -0.6816   0.01143   0.00466   0.0015   1.0000   0.0501
  -5.750  -0.6584   0.01110   0.00436   0.0025   1.0000   0.0567
  -5.500  -0.6351   0.01081   0.00409   0.0034   1.0000   0.0641
  -5.250  -0.6118   0.01054   0.00384   0.0043   1.0000   0.0728
  -5.000  -0.5889   0.01024   0.00360   0.0052   1.0000   0.0840
  -4.500  -0.5220   0.00961   0.00312   0.0026   0.9898   0.1172
  -4.250  -0.4878   0.00931   0.00291   0.0012   0.9838   0.1386
  -4.000  -0.4550   0.00899   0.00270   0.0000   0.9758   0.1628
  -3.750  -0.4201   0.00869   0.00251  -0.0015   0.9674   0.1902
  -3.500  -0.3849   0.00840   0.00234  -0.0032   0.9561   0.2197
  -3.250  -0.3497   0.00813   0.00217  -0.0047   0.9412   0.2505
  -3.000  -0.3162   0.00788   0.00202  -0.0059   0.9206   0.2812
  -2.500  -0.2584   0.00754   0.00175  -0.0060   0.8649   0.3403
  -2.250  -0.2325   0.00745   0.00165  -0.0053   0.8349   0.3672
  -2.000  -0.2070   0.00737   0.00156  -0.0046   0.8058   0.3951
  -1.750  -0.1815   0.00730   0.00148  -0.0039   0.7782   0.4222
  -1.500  -0.1559   0.00724   0.00142  -0.0033   0.7515   0.4482
  -1.250  -0.1301   0.00720   0.00137  -0.0027   0.7255   0.4750
  -1.000  -0.1042   0.00716   0.00132  -0.0021   0.7003   0.5009
  -0.750  -0.0783   0.00713   0.00129  -0.0016   0.6754   0.5263
  -0.500  -0.0522   0.00711   0.00127  -0.0011   0.6504   0.5516
  -0.250  -0.0262   0.00710   0.00125  -0.0005   0.6261   0.5766
   0.000   0.0000   0.00709   0.00125   0.0000   0.6012   0.6011
   0.250   0.0261   0.00710   0.00125   0.0005   0.5766   0.6262
   0.500   0.0521   0.00711   0.00127   0.0011   0.5516   0.6505
   1.000   0.1042   0.00716   0.00132   0.0021   0.5010   0.7002
   1.250   0.1301   0.00720   0.00137   0.0027   0.4749   0.7253
   1.500   0.1559   0.00724   0.00142   0.0033   0.4483   0.7516
   1.750   0.1815   0.00729   0.00148   0.0040   0.4223   0.7784
   2.000   0.2070   0.00737   0.00156   0.0046   0.3951   0.8058
   2.250   0.2325   0.00745   0.00165   0.0053   0.3675   0.8347
   2.500   0.2583   0.00754   0.00175   0.0060   0.3399   0.8649
   2.750   0.2855   0.00769   0.00188   0.0063   0.3109   0.8946
   3.000   0.3161   0.00788   0.00202   0.0059   0.2808   0.9206
   3.250   0.3497   0.00813   0.00217   0.0047   0.2502   0.9412
   3.500   0.3849   0.00840   0.00234   0.0031   0.2193   0.9561
   3.750   0.4201   0.00869   0.00252   0.0015   0.1900   0.9673
   4.000   0.4550   0.00899   0.00270   0.0000   0.1627   0.9757
   4.250   0.4877   0.00930   0.00291  -0.0011   0.1388   0.9837
   4.500   0.5219   0.00960   0.00312  -0.0026   0.1176   0.9898
   5.000   0.5891   0.01024   0.00360  -0.0053   0.0839   1.0000
   5.250   0.6121   0.01054   0.00384  -0.0043   0.0726   1.0000
   5.500   0.6353   0.01081   0.00409  -0.0034   0.0641   1.0000
   5.750   0.6586   0.01110   0.00436  -0.0025   0.0567   1.0000
   6.000   0.6818   0.01143   0.00466  -0.0016   0.0501   1.0000
   6.250   0.7053   0.01172   0.00495  -0.0007   0.0454   1.0000
   6.500   0.7285   0.01207   0.00528   0.0002   0.0408   1.0000
   6.750   0.7520   0.01239   0.00562   0.0010   0.0371   1.0000
   7.000   0.7750   0.01279   0.00600   0.0019   0.0337   1.0000
   7.250   0.7986   0.01311   0.00637   0.0028   0.0315   1.0000
   7.500   0.8218   0.01349   0.00675   0.0036   0.0290   1.0000
   7.750   0.8447   0.01394   0.00721   0.0045   0.0269   1.0000
   8.000   0.8680   0.01432   0.00764   0.0053   0.0252   1.0000
   8.250   0.8911   0.01475   0.00810   0.0061   0.0237   1.0000
   8.500   0.9133   0.01528   0.00865   0.0070   0.0222   1.0000
   8.750   0.9360   0.01575   0.00918   0.0078   0.0212   1.0000
   9.000   0.9587   0.01621   0.00970   0.0086   0.0200   1.0000
   9.250   0.9811   0.01671   0.01024   0.0094   0.0189   1.0000
   9.500   1.0024   0.01732   0.01088   0.0104   0.0180   1.0000
   9.750   1.0232   0.01798   0.01161   0.0113   0.0173   1.0000
  10.000   1.0444   0.01857   0.01229   0.0123   0.0167   1.0000
  10.250   1.0652   0.01918   0.01298   0.0132   0.0160   1.0000
  10.500   1.0855   0.01984   0.01370   0.0142   0.0154   1.0000
  10.750   1.1053   0.02050   0.01442   0.0152   0.0147   1.0000
  11.000   1.1230   0.02135   0.01533   0.0164   0.0141   1.0000
  11.250   1.1407   0.02216   0.01622   0.0176   0.0137   1.0000
  11.500   1.1576   0.02300   0.01717   0.0188   0.0134   1.0000
  11.750   1.1738   0.02384   0.01812   0.0202   0.0129   1.0000
  12.000   1.1888   0.02473   0.01911   0.0216   0.0125   1.0000
  12.250   1.2022   0.02567   0.02014   0.0231   0.0122   1.0000
  12.500   1.2130   0.02671   0.02129   0.0249   0.0119   1.0000
  12.750   1.2196   0.02773   0.02240   0.0273   0.0117   1.0000
  13.000   1.2236   0.02892   0.02367   0.0297   0.0114   1.0000
  13.250   1.2251   0.03038   0.02523   0.0317   0.0113   1.0000
  13.500   1.2232   0.03228   0.02724   0.0333   0.0111   1.0000
  13.750   1.2176   0.03481   0.02989   0.0340   0.0109   1.0000
  14.000   1.2159   0.03737   0.03257   0.0340   0.0108   1.0000
  14.250   1.2123   0.04048   0.03584   0.0331   0.0107   1.0000
  14.500   1.2070   0.04418   0.03969   0.0315   0.0106   1.0000
  14.750   1.1980   0.04873   0.04441   0.0291   0.0105   1.0000
  15.000   1.1876   0.05381   0.04964   0.0262   0.0105   1.0000
  15.250   1.1759   0.05937   0.05536   0.0228   0.0104   1.0000
  15.500   1.1595   0.06586   0.06200   0.0189   0.0104   1.0000
  15.750   1.1401   0.07304   0.06932   0.0146   0.0104   1.0000
  16.000   1.1181   0.08082   0.07725   0.0101   0.0104   1.0000
  16.250   1.0940   0.08922   0.08579   0.0052   0.0103   1.0000
  16.500   1.0706   0.09777   0.09447   0.0003   0.0104   1.0000
  16.750   1.0443   0.10720   0.10402  -0.0051   0.0105   1.0000
  17.000   1.0189   0.11696   0.11391  -0.0106   0.0105   1.0000
  17.250   0.9934   0.12707   0.12415  -0.0163   0.0105   1.0000
  17.500   0.9573   0.14030   0.13753  -0.0238   0.0105   1.0000
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