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RAE 102 AIRFOIL (rae102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE 102 AIRFOIL (rae102-il)
Reynolds number: 1,000,000
Max Cl/Cd: 68.29 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae102-il-1000000-n5.txt
Download as CSV file: xf-rae102-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 102 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9447   0.11912   0.11722   0.0069   1.0000   0.0043
 -16.250  -0.9911   0.10440   0.10237  -0.0005   1.0000   0.0041
 -16.000  -1.0566   0.08557   0.08333  -0.0106   1.0000   0.0041
 -15.750  -1.0905   0.07392   0.07151  -0.0177   1.0000   0.0040
 -15.500  -1.1141   0.06530   0.06274  -0.0232   1.0000   0.0040
 -15.250  -1.1354   0.05791   0.05519  -0.0278   1.0000   0.0040
 -15.000  -1.1564   0.05122   0.04832  -0.0316   1.0000   0.0040
 -14.750  -1.1732   0.04574   0.04266  -0.0342   1.0000   0.0040
 -14.500  -1.1795   0.04204   0.03883  -0.0355   1.0000   0.0040
 -14.250  -1.1836   0.03891   0.03556  -0.0362   1.0000   0.0041
 -14.000  -1.1907   0.03579   0.03228  -0.0363   1.0000   0.0041
 -13.750  -1.1917   0.03352   0.02988  -0.0357   1.0000   0.0041
 -13.500  -1.2014   0.03078   0.02695  -0.0341   1.0000   0.0042
 -13.250  -1.2051   0.02879   0.02480  -0.0319   1.0000   0.0042
 -13.000  -1.2075   0.02707   0.02293  -0.0291   1.0000   0.0043
 -12.750  -1.2071   0.02568   0.02141  -0.0260   1.0000   0.0044
 -12.500  -1.2013   0.02467   0.02030  -0.0233   1.0000   0.0045
 -12.250  -1.1913   0.02363   0.01916  -0.0211   1.0000   0.0046
 -12.000  -1.1776   0.02276   0.01819  -0.0195   1.0000   0.0047
 -11.750  -1.1637   0.02182   0.01714  -0.0179   1.0000   0.0048
 -11.500  -1.1476   0.02104   0.01627  -0.0165   1.0000   0.0049
 -11.250  -1.1302   0.02032   0.01548  -0.0152   1.0000   0.0050
 -11.000  -1.1128   0.01956   0.01463  -0.0139   1.0000   0.0052
 -10.750  -1.0941   0.01889   0.01389  -0.0127   1.0000   0.0053
 -10.500  -1.0754   0.01821   0.01312  -0.0115   1.0000   0.0055
 -10.250  -1.0556   0.01762   0.01246  -0.0104   1.0000   0.0058
 -10.000  -1.0357   0.01703   0.01178  -0.0093   1.0000   0.0059
  -9.750  -1.0151   0.01650   0.01119  -0.0083   1.0000   0.0061
  -9.500  -0.9940   0.01603   0.01065  -0.0073   1.0000   0.0063
  -9.250  -0.9753   0.01528   0.00982  -0.0059   1.0000   0.0065
  -9.000  -0.9558   0.01462   0.00909  -0.0046   1.0000   0.0068
  -8.750  -0.9350   0.01413   0.00855  -0.0035   1.0000   0.0071
  -8.500  -0.9137   0.01368   0.00808  -0.0024   1.0000   0.0075
  -8.250  -0.8921   0.01328   0.00763  -0.0014   1.0000   0.0079
  -8.000  -0.8704   0.01289   0.00719  -0.0004   1.0000   0.0082
  -7.750  -0.8487   0.01251   0.00677   0.0007   1.0000   0.0086
  -7.500  -0.8267   0.01217   0.00639   0.0017   1.0000   0.0090
  -7.250  -0.8051   0.01180   0.00599   0.0028   1.0000   0.0094
  -7.000  -0.7740   0.01134   0.00549   0.0018   0.9972   0.0104
  -6.750  -0.7435   0.01099   0.00514   0.0009   0.9930   0.0113
  -6.500  -0.7132   0.01070   0.00482   0.0002   0.9879   0.0124
  -6.000  -0.6496   0.01003   0.00413  -0.0020   0.9773   0.0153
  -5.750  -0.6154   0.00974   0.00383  -0.0035   0.9708   0.0171
  -5.500  -0.5816   0.00947   0.00354  -0.0050   0.9609   0.0195
  -5.250  -0.5473   0.00918   0.00326  -0.0066   0.9477   0.0233
  -5.000  -0.5155   0.00897   0.00301  -0.0075   0.9293   0.0272
  -4.750  -0.4881   0.00877   0.00278  -0.0075   0.9057   0.0324
  -4.500  -0.4627   0.00861   0.00257  -0.0070   0.8815   0.0404
  -4.250  -0.4377   0.00846   0.00238  -0.0064   0.8580   0.0498
  -4.000  -0.4126   0.00831   0.00219  -0.0058   0.8377   0.0622
  -3.750  -0.3875   0.00811   0.00201  -0.0053   0.8189   0.0823
  -3.500  -0.3625   0.00790   0.00184  -0.0048   0.8008   0.1081
  -3.250  -0.3378   0.00764   0.00166  -0.0043   0.7838   0.1459
  -3.000  -0.3131   0.00737   0.00149  -0.0038   0.7679   0.1911
  -2.750  -0.2888   0.00702   0.00132  -0.0032   0.7533   0.2518
  -2.500  -0.2646   0.00664   0.00115  -0.0027   0.7399   0.3222
  -2.250  -0.2406   0.00624   0.00101  -0.0021   0.7272   0.4013
  -2.000  -0.2151   0.00603   0.00094  -0.0017   0.7152   0.4555
  -1.750  -0.1887   0.00592   0.00088  -0.0014   0.7034   0.4878
  -1.500  -0.1621   0.00584   0.00084  -0.0012   0.6915   0.5127
  -1.000  -0.1082   0.00573   0.00078  -0.0008   0.6694   0.5535
  -0.750  -0.0811   0.00569   0.00076  -0.0006   0.6589   0.5716
  -0.500  -0.0541   0.00566   0.00075  -0.0004   0.6473   0.5887
  -0.250  -0.0270   0.00565   0.00074  -0.0002   0.6345   0.6051
   0.000   0.0000   0.00564   0.00073   0.0000   0.6202   0.6203
   0.250   0.0270   0.00565   0.00074   0.0002   0.6049   0.6344
   0.500   0.0541   0.00566   0.00075   0.0004   0.5887   0.6473
   0.750   0.0811   0.00569   0.00076   0.0006   0.5715   0.6590
   1.000   0.1082   0.00573   0.00078   0.0008   0.5535   0.6695
   1.500   0.1621   0.00584   0.00084   0.0012   0.5123   0.6914
   1.750   0.1888   0.00592   0.00088   0.0014   0.4874   0.7033
   2.000   0.2152   0.00602   0.00094   0.0017   0.4572   0.7152
   2.250   0.2407   0.00623   0.00101   0.0021   0.4049   0.7272
   2.500   0.2645   0.00665   0.00116   0.0027   0.3207   0.7399
   2.750   0.2888   0.00702   0.00132   0.0032   0.2514   0.7533
   3.000   0.3131   0.00737   0.00149   0.0038   0.1900   0.7678
   3.250   0.3380   0.00764   0.00166   0.0043   0.1470   0.7836
   3.500   0.3626   0.00790   0.00184   0.0048   0.1089   0.8008
   3.750   0.3876   0.00811   0.00201   0.0053   0.0822   0.8189
   4.000   0.4127   0.00830   0.00219   0.0058   0.0627   0.8377
   4.250   0.4377   0.00846   0.00238   0.0064   0.0498   0.8582
   4.500   0.4627   0.00862   0.00257   0.0070   0.0398   0.8815
   4.750   0.4882   0.00877   0.00278   0.0075   0.0325   0.9061
   5.000   0.5157   0.00897   0.00301   0.0075   0.0272   0.9293
   5.250   0.5474   0.00918   0.00326   0.0066   0.0234   0.9476
   5.500   0.5817   0.00947   0.00354   0.0050   0.0196   0.9610
   5.750   0.6157   0.00974   0.00383   0.0035   0.0171   0.9710
   6.000   0.6498   0.01003   0.00414   0.0019   0.0153   0.9777
   6.250   0.6811   0.01038   0.00448   0.0009   0.0134   0.9837
   6.500   0.7138   0.01069   0.00482  -0.0003   0.0124   0.9881
   6.750   0.7441   0.01099   0.00514  -0.0011   0.0113   0.9931
   7.000   0.7744   0.01134   0.00550  -0.0019   0.0103   0.9975
   7.250   0.8047   0.01180   0.00598  -0.0027   0.0094   1.0000
   7.500   0.8263   0.01216   0.00638  -0.0016   0.0090   1.0000
   7.750   0.8483   0.01251   0.00677  -0.0006   0.0086   1.0000
   8.000   0.8701   0.01288   0.00719   0.0004   0.0083   1.0000
   8.250   0.8919   0.01328   0.00762   0.0015   0.0079   1.0000
   8.500   0.9135   0.01369   0.00809   0.0025   0.0075   1.0000
   8.750   0.9350   0.01412   0.00855   0.0035   0.0072   1.0000
   9.000   0.9559   0.01462   0.00909   0.0046   0.0069   1.0000
   9.250   0.9756   0.01527   0.00980   0.0059   0.0065   1.0000
   9.500   0.9952   0.01593   0.01054   0.0071   0.0062   1.0000
   9.750   1.0151   0.01656   0.01125   0.0083   0.0061   1.0000
  10.000   1.0360   0.01706   0.01181   0.0092   0.0060   1.0000
  10.250   1.0563   0.01761   0.01245   0.0103   0.0058   1.0000
  10.500   1.0759   0.01823   0.01315   0.0114   0.0056   1.0000
  10.750   1.0951   0.01888   0.01387   0.0125   0.0054   1.0000
  11.000   1.1134   0.01959   0.01466   0.0137   0.0052   1.0000
  11.250   1.1314   0.02029   0.01545   0.0149   0.0051   1.0000
  11.500   1.1477   0.02113   0.01638   0.0164   0.0050   1.0000
  11.750   1.1646   0.02185   0.01718   0.0177   0.0048   1.0000
  12.000   1.1792   0.02273   0.01815   0.0192   0.0047   1.0000
  12.250   1.1929   0.02362   0.01915   0.0209   0.0046   1.0000
  12.500   1.2035   0.02464   0.02027   0.0229   0.0045   1.0000
  12.750   1.2091   0.02569   0.02142   0.0257   0.0044   1.0000
  13.000   1.2085   0.02714   0.02301   0.0289   0.0043   1.0000
  13.250   1.2116   0.02847   0.02445   0.0312   0.0043   1.0000
  13.500   1.2017   0.03093   0.02710   0.0338   0.0041   1.0000
  13.750   1.1968   0.03326   0.02960   0.0352   0.0041   1.0000
  14.000   1.1908   0.03600   0.03250   0.0359   0.0041   1.0000
  14.250   1.1865   0.03886   0.03550   0.0358   0.0041   1.0000
  14.500   1.1882   0.04132   0.03807   0.0354   0.0040   1.0000
  14.750   1.1768   0.04563   0.04255   0.0338   0.0040   1.0000
  15.000   1.1603   0.05109   0.04819   0.0312   0.0040   1.0000
  15.250   1.1435   0.05711   0.05437   0.0278   0.0040   1.0000
  15.500   1.1427   0.06096   0.05831   0.0255   0.0040   1.0000
  15.750   1.0952   0.07366   0.07125   0.0174   0.0040   1.0000
  16.000   1.0347   0.09114   0.08898   0.0068   0.0041   1.0000
  16.250   1.0050   0.10209   0.10004   0.0012   0.0042   1.0000
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