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RAE 103 AIRFOIL (rae103-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE 103 AIRFOIL (rae103-il)
Reynolds number: 1,000,000
Max Cl/Cd: 66 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae103-il-1000000-n5.txt
Download as CSV file: xf-rae103-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 103 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.9789   0.09057   0.08867  -0.0117   1.0000   0.0041
 -15.250  -1.0544   0.06810   0.06590  -0.0259   1.0000   0.0039
 -15.000  -1.0880   0.05795   0.05553  -0.0327   1.0000   0.0038
 -14.750  -1.1005   0.05261   0.05006  -0.0356   1.0000   0.0039
 -14.500  -1.1243   0.04637   0.04360  -0.0383   1.0000   0.0039
 -14.250  -1.1338   0.04252   0.03959  -0.0393   1.0000   0.0039
 -14.000  -1.1384   0.03953   0.03646  -0.0395   1.0000   0.0040
 -13.750  -1.1499   0.03612   0.03286  -0.0390   1.0000   0.0040
 -13.500  -1.1534   0.03376   0.03034  -0.0379   1.0000   0.0040
 -13.250  -1.1574   0.03154   0.02796  -0.0362   1.0000   0.0040
 -13.000  -1.1556   0.02995   0.02623  -0.0343   1.0000   0.0041
 -12.750  -1.1547   0.02838   0.02451  -0.0319   1.0000   0.0041
 -12.500  -1.1499   0.02719   0.02320  -0.0294   1.0000   0.0042
 -12.250  -1.1492   0.02577   0.02162  -0.0261   1.0000   0.0042
 -12.000  -1.1402   0.02494   0.02068  -0.0237   1.0000   0.0043
 -11.750  -1.1303   0.02383   0.01945  -0.0215   1.0000   0.0043
 -11.500  -1.1175   0.02287   0.01836  -0.0196   1.0000   0.0043
 -11.250  -1.1028   0.02202   0.01740  -0.0180   1.0000   0.0044
 -11.000  -1.0939   0.02049   0.01569  -0.0155   1.0000   0.0046
 -10.750  -1.0794   0.01950   0.01456  -0.0137   1.0000   0.0047
 -10.500  -1.0630   0.01866   0.01364  -0.0122   1.0000   0.0049
 -10.250  -1.0449   0.01799   0.01290  -0.0108   1.0000   0.0051
 -10.000  -1.0261   0.01740   0.01224  -0.0096   1.0000   0.0052
  -9.750  -1.0075   0.01676   0.01153  -0.0082   1.0000   0.0054
  -9.500  -0.9881   0.01621   0.01092  -0.0069   1.0000   0.0056
  -9.250  -0.9685   0.01569   0.01034  -0.0057   1.0000   0.0058
  -9.000  -0.9482   0.01525   0.00983  -0.0045   1.0000   0.0061
  -8.750  -0.9281   0.01477   0.00930  -0.0032   1.0000   0.0064
  -8.500  -0.9082   0.01428   0.00875  -0.0019   1.0000   0.0065
  -8.250  -0.8878   0.01387   0.00829  -0.0007   1.0000   0.0067
  -8.000  -0.8680   0.01335   0.00770   0.0006   0.9999   0.0069
  -7.750  -0.8385   0.01271   0.00701  -0.0002   0.9969   0.0075
  -7.500  -0.8099   0.01226   0.00653  -0.0007   0.9923   0.0081
  -7.250  -0.7806   0.01187   0.00610  -0.0014   0.9873   0.0086
  -6.750  -0.7177   0.01115   0.00530  -0.0036   0.9771   0.0098
  -6.500  -0.6843   0.01073   0.00485  -0.0051   0.9710   0.0108
  -6.250  -0.6515   0.01037   0.00448  -0.0065   0.9625   0.0122
  -6.000  -0.6173   0.01008   0.00416  -0.0081   0.9522   0.0137
  -5.750  -0.5853   0.00980   0.00384  -0.0092   0.9373   0.0151
  -5.500  -0.5572   0.00954   0.00354  -0.0094   0.9176   0.0176
  -5.250  -0.5313   0.00936   0.00328  -0.0091   0.8974   0.0197
  -5.000  -0.5064   0.00918   0.00304  -0.0085   0.8777   0.0234
  -4.750  -0.4816   0.00901   0.00283  -0.0079   0.8602   0.0276
  -4.500  -0.4567   0.00885   0.00263  -0.0074   0.8447   0.0333
  -4.250  -0.4314   0.00869   0.00244  -0.0069   0.8307   0.0402
  -4.000  -0.4064   0.00850   0.00225  -0.0064   0.8179   0.0534
  -3.750  -0.3812   0.00830   0.00207  -0.0060   0.8063   0.0690
  -3.500  -0.3562   0.00808   0.00190  -0.0055   0.7952   0.0929
  -3.250  -0.3315   0.00783   0.00173  -0.0050   0.7843   0.1263
  -3.000  -0.3069   0.00752   0.00156  -0.0045   0.7741   0.1725
  -2.750  -0.2827   0.00718   0.00140  -0.0040   0.7650   0.2292
  -2.500  -0.2591   0.00678   0.00124  -0.0034   0.7563   0.3021
  -2.250  -0.2356   0.00636   0.00107  -0.0028   0.7484   0.3826
  -1.750  -0.1883   0.00562   0.00087  -0.0014   0.7332   0.5457
  -1.500  -0.1621   0.00553   0.00083  -0.0010   0.7257   0.5783
  -1.250  -0.1353   0.00545   0.00080  -0.0009   0.7183   0.6008
  -1.000  -0.1084   0.00541   0.00078  -0.0006   0.7108   0.6193
  -0.750  -0.0813   0.00538   0.00077  -0.0005   0.7025   0.6348
  -0.500  -0.0542   0.00536   0.00076  -0.0003   0.6937   0.6486
  -0.250  -0.0272   0.00535   0.00075  -0.0001   0.6835   0.6610
   0.000   0.0000   0.00534   0.00075   0.0000   0.6725   0.6725
   0.250   0.0272   0.00535   0.00075   0.0001   0.6609   0.6835
   0.500   0.0542   0.00536   0.00076   0.0003   0.6485   0.6937
   0.750   0.0813   0.00538   0.00077   0.0005   0.6349   0.7025
   1.000   0.1085   0.00541   0.00078   0.0006   0.6194   0.7109
   1.250   0.1353   0.00545   0.00080   0.0009   0.6008   0.7183
   1.750   0.1884   0.00562   0.00087   0.0014   0.5469   0.7332
   2.250   0.2356   0.00635   0.00107   0.0027   0.3832   0.7484
   2.500   0.2590   0.00679   0.00124   0.0034   0.3000   0.7563
   2.750   0.2827   0.00719   0.00140   0.0040   0.2283   0.7650
   3.000   0.3068   0.00754   0.00157   0.0046   0.1697   0.7740
   3.250   0.3315   0.00783   0.00173   0.0050   0.1261   0.7842
   3.500   0.3564   0.00807   0.00190   0.0055   0.0948   0.7951
   3.750   0.3812   0.00830   0.00207   0.0060   0.0689   0.8063
   4.000   0.4063   0.00851   0.00225   0.0065   0.0523   0.8180
   4.250   0.4314   0.00869   0.00243   0.0069   0.0403   0.8307
   4.500   0.4567   0.00885   0.00263   0.0074   0.0332   0.8448
   4.750   0.4817   0.00901   0.00283   0.0079   0.0276   0.8602
   5.000   0.5064   0.00918   0.00304   0.0085   0.0234   0.8776
   5.250   0.5313   0.00936   0.00328   0.0091   0.0198   0.8973
   5.500   0.5572   0.00954   0.00354   0.0094   0.0176   0.9178
   5.750   0.5853   0.00980   0.00384   0.0092   0.0151   0.9373
   6.000   0.6173   0.01008   0.00416   0.0081   0.0137   0.9522
   6.250   0.6515   0.01037   0.00448   0.0065   0.0122   0.9625
   6.500   0.6842   0.01074   0.00486   0.0051   0.0107   0.9711
   6.750   0.7176   0.01115   0.00530   0.0036   0.0098   0.9773
   7.250   0.7804   0.01187   0.00611   0.0014   0.0087   0.9873
   7.500   0.8098   0.01227   0.00654   0.0008   0.0082   0.9922
   7.750   0.8382   0.01270   0.00699   0.0002   0.0075   0.9967
   8.000   0.8676   0.01330   0.00765  -0.0006   0.0070   0.9997
   8.250   0.8878   0.01388   0.00829   0.0007   0.0067   1.0000
   8.500   0.9079   0.01431   0.00878   0.0020   0.0066   1.0000
   8.750   0.9280   0.01478   0.00931   0.0033   0.0064   1.0000
   9.000   0.9486   0.01519   0.00977   0.0044   0.0061   1.0000
   9.250   0.9685   0.01568   0.01033   0.0056   0.0058   1.0000
   9.500   0.9882   0.01620   0.01091   0.0069   0.0056   1.0000
   9.750   1.0078   0.01672   0.01149   0.0081   0.0053   1.0000
  10.000   1.0263   0.01737   0.01221   0.0095   0.0052   1.0000
  10.250   1.0453   0.01795   0.01286   0.0108   0.0051   1.0000
  10.500   1.0633   0.01864   0.01361   0.0121   0.0049   1.0000
  10.750   1.0801   0.01943   0.01450   0.0136   0.0047   1.0000
  11.000   1.0941   0.02049   0.01567   0.0155   0.0045   1.0000
  11.250   1.1051   0.02180   0.01716   0.0177   0.0044   1.0000
  11.500   1.1182   0.02283   0.01831   0.0195   0.0044   1.0000
  11.750   1.1301   0.02388   0.01949   0.0215   0.0043   1.0000
  12.000   1.1413   0.02488   0.02062   0.0235   0.0043   1.0000
  12.250   1.1484   0.02587   0.02173   0.0262   0.0042   1.0000
  12.500   1.1514   0.02713   0.02313   0.0292   0.0042   1.0000
  12.750   1.1569   0.02826   0.02438   0.0316   0.0041   1.0000
  13.000   1.1592   0.02972   0.02598   0.0339   0.0041   1.0000
  13.250   1.1590   0.03148   0.02789   0.0360   0.0040   1.0000
  13.500   1.1548   0.03373   0.03032   0.0377   0.0040   1.0000
  13.750   1.1520   0.03602   0.03276   0.0388   0.0040   1.0000
  14.000   1.1459   0.03888   0.03577   0.0393   0.0039   1.0000
  14.250   1.1384   0.04216   0.03922   0.0392   0.0038   1.0000
  14.500   1.1195   0.04718   0.04445   0.0378   0.0039   1.0000
  14.750   1.1145   0.05086   0.04826   0.0363   0.0039   1.0000
  15.000   1.1001   0.05631   0.05386   0.0334   0.0038   1.0000
  15.250   1.0639   0.06659   0.06435   0.0266   0.0039   1.0000
  15.500   1.0143   0.08266   0.08067   0.0158   0.0040   1.0000
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