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RG 15A-1.8/11.0 AIRFOIL (rg15a111-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RG 15A-1.8/11.0 AIRFOIL (rg15a111-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.87 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rg15a111-il-1000000.txt
Download as CSV file: xf-rg15a111-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RG 15A-1.8/11.0 AIRFOIL                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.8747   0.05598   0.05351  -0.0562   1.0000   0.0066
 -13.500  -0.8942   0.04836   0.04572  -0.0622   1.0000   0.0066
 -13.250  -0.9094   0.04287   0.04010  -0.0660   1.0000   0.0067
 -13.000  -0.9248   0.03839   0.03545  -0.0680   1.0000   0.0067
 -12.750  -0.9359   0.03518   0.03210  -0.0683   1.0000   0.0068
 -12.500  -0.9418   0.03312   0.02995  -0.0672   1.0000   0.0068
 -12.250  -0.9572   0.03113   0.02783  -0.0639   1.0000   0.0069
 -12.000  -0.9640   0.02999   0.02661  -0.0599   1.0000   0.0069
 -11.750  -0.9614   0.02878   0.02531  -0.0573   1.0000   0.0071
 -11.500  -0.9546   0.02780   0.02426  -0.0549   1.0000   0.0072
 -11.250  -0.9496   0.02648   0.02281  -0.0524   1.0000   0.0073
 -11.000  -0.9426   0.02520   0.02139  -0.0499   1.0000   0.0074
 -10.750  -0.9308   0.02435   0.02045  -0.0479   1.0000   0.0076
 -10.500  -0.9199   0.02331   0.01928  -0.0457   1.0000   0.0078
 -10.250  -0.9094   0.02211   0.01794  -0.0434   1.0000   0.0079
 -10.000  -0.8966   0.02112   0.01683  -0.0414   1.0000   0.0081
  -9.750  -0.8729   0.02012   0.01571  -0.0415   0.9992   0.0083
  -9.500  -0.8424   0.01916   0.01462  -0.0428   0.9977   0.0086
  -9.250  -0.8106   0.01845   0.01380  -0.0442   0.9962   0.0088
  -9.000  -0.7827   0.01652   0.01166  -0.0456   0.9946   0.0094
  -8.750  -0.7519   0.01581   0.01091  -0.0468   0.9930   0.0099
  -8.500  -0.7212   0.01530   0.01036  -0.0478   0.9908   0.0104
  -8.250  -0.6892   0.01485   0.00986  -0.0490   0.9888   0.0110
  -8.000  -0.6562   0.01440   0.00936  -0.0503   0.9870   0.0116
  -7.750  -0.6222   0.01403   0.00893  -0.0518   0.9856   0.0120
  -7.500  -0.5910   0.01270   0.00749  -0.0533   0.9841   0.0131
  -7.250  -0.5563   0.01222   0.00698  -0.0550   0.9831   0.0140
  -7.000  -0.5299   0.01176   0.00650  -0.0548   0.9784   0.0148
  -6.750  -0.4974   0.01137   0.00606  -0.0560   0.9758   0.0156
  -6.500  -0.4639   0.01079   0.00541  -0.0574   0.9738   0.0167
  -6.250  -0.4295   0.01026   0.00486  -0.0590   0.9721   0.0185
  -6.000  -0.3936   0.00987   0.00445  -0.0608   0.9709   0.0199
  -5.750  -0.3658   0.00956   0.00410  -0.0608   0.9653   0.0209
  -5.500  -0.3342   0.00909   0.00361  -0.0616   0.9612   0.0241
  -5.250  -0.3005   0.00876   0.00327  -0.0629   0.9579   0.0272
  -5.000  -0.2724   0.00832   0.00293  -0.0630   0.9508   0.0431
  -4.750  -0.2406   0.00794   0.00264  -0.0639   0.9448   0.0654
  -4.250  -0.1794   0.00740   0.00221  -0.0652   0.9282   0.1029
  -4.000  -0.1513   0.00717   0.00203  -0.0652   0.9165   0.1250
  -3.750  -0.1237   0.00693   0.00186  -0.0652   0.9043   0.1553
  -3.500  -0.0967   0.00668   0.00171  -0.0650   0.8914   0.1934
  -3.250  -0.0699   0.00646   0.00158  -0.0648   0.8783   0.2311
  -3.000  -0.0433   0.00626   0.00145  -0.0646   0.8649   0.2713
  -2.750  -0.0174   0.00600   0.00134  -0.0643   0.8511   0.3303
  -2.500   0.0082   0.00571   0.00124  -0.0639   0.8372   0.4017
  -2.250   0.0343   0.00551   0.00115  -0.0635   0.8230   0.4564
  -2.000   0.0602   0.00532   0.00108  -0.0632   0.8084   0.5144
  -1.750   0.0861   0.00515   0.00106  -0.0627   0.7938   0.5782
  -1.500   0.1125   0.00508   0.00105  -0.0623   0.7791   0.6255
  -1.250   0.1394   0.00508   0.00105  -0.0620   0.7642   0.6512
  -1.000   0.1665   0.00510   0.00105  -0.0617   0.7493   0.6698
  -0.750   0.1936   0.00513   0.00105  -0.0614   0.7340   0.6847
  -0.500   0.2208   0.00517   0.00105  -0.0612   0.7186   0.6975
  -0.250   0.2479   0.00522   0.00106  -0.0609   0.7026   0.7094
   0.000   0.2750   0.00528   0.00108  -0.0606   0.6862   0.7207
   0.250   0.3020   0.00533   0.00110  -0.0603   0.6691   0.7312
   0.500   0.3290   0.00540   0.00112  -0.0600   0.6517   0.7407
   0.750   0.3559   0.00548   0.00115  -0.0598   0.6335   0.7502
   1.000   0.3826   0.00556   0.00119  -0.0594   0.6149   0.7596
   1.250   0.4094   0.00564   0.00123  -0.0592   0.5951   0.7684
   1.500   0.4361   0.00575   0.00128  -0.0589   0.5751   0.7778
   1.750   0.4626   0.00585   0.00134  -0.0585   0.5549   0.7872
   2.000   0.4891   0.00596   0.00141  -0.0582   0.5335   0.7968
   2.250   0.5154   0.00609   0.00148  -0.0578   0.5124   0.8070
   2.500   0.5416   0.00620   0.00157  -0.0574   0.4909   0.8171
   2.750   0.5676   0.00634   0.00166  -0.0570   0.4690   0.8277
   3.000   0.5937   0.00648   0.00175  -0.0566   0.4469   0.8393
   3.250   0.6189   0.00664   0.00186  -0.0561   0.4222   0.8518
   3.500   0.6441   0.00680   0.00198  -0.0555   0.3978   0.8646
   3.750   0.6693   0.00695   0.00210  -0.0549   0.3775   0.8777
   4.000   0.6941   0.00710   0.00223  -0.0543   0.3565   0.8923
   4.250   0.7179   0.00728   0.00237  -0.0534   0.3346   0.9097
   4.500   0.7407   0.00742   0.00251  -0.0523   0.3147   0.9317
   4.750   0.7658   0.00758   0.00265  -0.0517   0.2947   0.9605
   5.000   0.8007   0.00786   0.00284  -0.0534   0.2676   0.9875
   5.250   0.8293   0.00818   0.00303  -0.0538   0.2410   1.0000
   5.500   0.8537   0.00850   0.00324  -0.0533   0.2167   1.0000
   5.750   0.8784   0.00881   0.00345  -0.0529   0.1954   1.0000
   6.250   0.9274   0.00945   0.00394  -0.0519   0.1576   1.0000
   6.500   0.9515   0.00981   0.00420  -0.0513   0.1390   1.0000
   6.750   0.9755   0.01017   0.00448  -0.0507   0.1228   1.0000
   7.000   0.9993   0.01054   0.00479  -0.0501   0.1077   1.0000
   7.250   1.0230   0.01092   0.00510  -0.0495   0.0938   1.0000
   7.500   1.0465   0.01130   0.00542  -0.0489   0.0819   1.0000
   7.750   1.0699   0.01168   0.00576  -0.0482   0.0717   1.0000
   8.000   1.0930   0.01207   0.00613  -0.0475   0.0617   1.0000
   8.250   1.1157   0.01250   0.00651  -0.0468   0.0517   1.0000
   8.500   1.1380   0.01294   0.00691  -0.0460   0.0434   1.0000
   8.750   1.1596   0.01344   0.00736  -0.0450   0.0364   1.0000
   9.000   1.1820   0.01384   0.00777  -0.0442   0.0326   1.0000
   9.250   1.2028   0.01437   0.00829  -0.0432   0.0283   1.0000
   9.500   1.2252   0.01473   0.00869  -0.0424   0.0263   1.0000
   9.750   1.2457   0.01524   0.00919  -0.0414   0.0237   1.0000
  10.000   1.2656   0.01577   0.00974  -0.0402   0.0214   1.0000
  10.250   1.2869   0.01615   0.01017  -0.0393   0.0199   1.0000
  10.500   1.3061   0.01668   0.01070  -0.0381   0.0179   1.0000
  10.750   1.3241   0.01725   0.01132  -0.0366   0.0160   1.0000
  11.000   1.3429   0.01773   0.01181  -0.0354   0.0141   1.0000
  11.250   1.3563   0.01842   0.01252  -0.0332   0.0121   1.0000
  11.500   1.3711   0.01895   0.01310  -0.0312   0.0109   1.0000
  11.750   1.3811   0.01976   0.01392  -0.0286   0.0094   1.0000
  12.000   1.3929   0.02047   0.01470  -0.0263   0.0085   1.0000
  12.250   1.4051   0.02116   0.01545  -0.0242   0.0079   1.0000
  12.500   1.4144   0.02204   0.01637  -0.0219   0.0073   1.0000
  12.750   1.4171   0.02335   0.01778  -0.0189   0.0066   1.0000
  13.000   1.4260   0.02430   0.01881  -0.0168   0.0064   1.0000
  13.250   1.4353   0.02525   0.01984  -0.0149   0.0061   1.0000
  13.500   1.4412   0.02648   0.02116  -0.0129   0.0059   1.0000
  13.750   1.4471   0.02777   0.02253  -0.0110   0.0056   1.0000
  14.000   1.4516   0.02922   0.02407  -0.0093   0.0054   1.0000
  14.250   1.4546   0.03089   0.02582  -0.0078   0.0053   1.0000
  14.500   1.4553   0.03285   0.02788  -0.0064   0.0051   1.0000
  14.750   1.4522   0.03529   0.03043  -0.0052   0.0050   1.0000
  15.000   1.4437   0.03845   0.03372  -0.0043   0.0048   1.0000
  15.250   1.4294   0.04252   0.03795  -0.0041   0.0046   1.0000
  15.500   1.4216   0.04617   0.04173  -0.0043   0.0045   1.0000
  15.750   1.4151   0.04994   0.04563  -0.0050   0.0045   1.0000
  16.000   1.4066   0.05419   0.05001  -0.0062   0.0045   1.0000
  16.250   1.3987   0.05861   0.05456  -0.0077   0.0045   1.0000
  16.500   1.3863   0.06397   0.06005  -0.0099   0.0045   1.0000
  16.750   1.3779   0.06896   0.06516  -0.0121   0.0044   1.0000
  17.000   1.3584   0.07600   0.07236  -0.0155   0.0045   1.0000
  17.250   1.3469   0.08198   0.07846  -0.0185   0.0044   1.0000
  17.500   1.3238   0.09022   0.08686  -0.0228   0.0044   1.0000
  17.750   1.3092   0.09723   0.09399  -0.0265   0.0044   1.0000
  18.000   1.2909   0.10506   0.10195  -0.0308   0.0044   1.0000
  18.250   1.2691   0.11382   0.11084  -0.0357   0.0044   1.0000
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