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NACA 63A010 AIRFOIL (n63010a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63A010 AIRFOIL (n63010a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 64.25 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63010a-il-1000000-n5.txt
Download as CSV file: xf-n63010a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63A010 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -1.1604   0.08072   0.07868  -0.0006   1.0000   0.0041
 -15.750  -1.2040   0.06763   0.06534  -0.0091   1.0000   0.0040
 -15.500  -1.2307   0.05906   0.05657  -0.0145   1.0000   0.0040
 -15.250  -1.2502   0.05243   0.04977  -0.0182   1.0000   0.0040
 -15.000  -1.2642   0.04721   0.04437  -0.0207   1.0000   0.0041
 -14.750  -1.2727   0.04313   0.04014  -0.0221   1.0000   0.0041
 -14.500  -1.2773   0.03983   0.03670  -0.0228   1.0000   0.0042
 -14.250  -1.2775   0.03726   0.03401  -0.0228   1.0000   0.0043
 -14.000  -1.2753   0.03514   0.03178  -0.0224   1.0000   0.0044
 -13.750  -1.2715   0.03331   0.02984  -0.0216   1.0000   0.0044
 -13.500  -1.2661   0.03175   0.02817  -0.0205   1.0000   0.0045
 -13.250  -1.2590   0.03041   0.02673  -0.0191   1.0000   0.0046
 -13.000  -1.2510   0.02918   0.02540  -0.0175   1.0000   0.0047
 -12.750  -1.2411   0.02806   0.02417  -0.0159   1.0000   0.0048
 -12.500  -1.2282   0.02698   0.02296  -0.0146   1.0000   0.0050
 -12.250  -1.2136   0.02590   0.02177  -0.0135   1.0000   0.0051
 -12.000  -1.1978   0.02486   0.02061  -0.0125   1.0000   0.0053
 -11.750  -1.1810   0.02385   0.01948  -0.0115   1.0000   0.0055
 -11.500  -1.1631   0.02290   0.01842  -0.0106   1.0000   0.0056
 -11.250  -1.1442   0.02202   0.01742  -0.0098   1.0000   0.0058
 -11.000  -1.1244   0.02121   0.01651  -0.0090   1.0000   0.0059
 -10.750  -1.1037   0.02048   0.01567  -0.0084   1.0000   0.0060
 -10.500  -1.0850   0.01942   0.01450  -0.0074   1.0000   0.0062
 -10.250  -1.0646   0.01859   0.01357  -0.0067   1.0000   0.0065
 -10.000  -1.0417   0.01809   0.01304  -0.0063   1.0000   0.0068
  -9.750  -1.0184   0.01765   0.01256  -0.0059   1.0000   0.0071
  -9.500  -0.9950   0.01719   0.01205  -0.0054   1.0000   0.0074
  -9.250  -0.9720   0.01665   0.01146  -0.0049   1.0000   0.0077
  -9.000  -0.9491   0.01608   0.01082  -0.0044   1.0000   0.0079
  -8.750  -0.9261   0.01553   0.01020  -0.0038   1.0000   0.0082
  -8.500  -0.9029   0.01500   0.00960  -0.0032   1.0000   0.0085
  -8.250  -0.8796   0.01451   0.00905  -0.0027   1.0000   0.0087
  -8.000  -0.8561   0.01407   0.00855  -0.0021   1.0000   0.0089
  -7.750  -0.8322   0.01371   0.00815  -0.0016   1.0000   0.0090
  -7.500  -0.8116   0.01291   0.00727  -0.0005   1.0000   0.0095
  -7.250  -0.7896   0.01237   0.00668   0.0004   1.0000   0.0100
  -7.000  -0.7673   0.01194   0.00621   0.0013   1.0000   0.0104
  -6.750  -0.7358   0.01152   0.00575   0.0002   0.9957   0.0108
  -6.500  -0.7047   0.01114   0.00534  -0.0008   0.9901   0.0112
  -6.250  -0.6729   0.01079   0.00497  -0.0020   0.9838   0.0118
  -6.000  -0.6414   0.01046   0.00459  -0.0030   0.9753   0.0124
  -5.750  -0.6104   0.01015   0.00423  -0.0039   0.9642   0.0127
  -5.500  -0.5808   0.00988   0.00392  -0.0044   0.9499   0.0130
  -5.250  -0.5538   0.00959   0.00356  -0.0043   0.9321   0.0137
  -5.000  -0.5280   0.00935   0.00326  -0.0039   0.9130   0.0150
  -4.750  -0.5024   0.00916   0.00301  -0.0034   0.8943   0.0164
  -4.500  -0.4764   0.00900   0.00279  -0.0031   0.8770   0.0183
  -4.250  -0.4503   0.00882   0.00257  -0.0027   0.8604   0.0235
  -4.000  -0.4240   0.00865   0.00238  -0.0025   0.8451   0.0303
  -3.750  -0.3975   0.00849   0.00219  -0.0023   0.8309   0.0388
  -3.500  -0.3709   0.00831   0.00202  -0.0021   0.8178   0.0520
  -3.000  -0.3182   0.00783   0.00168  -0.0018   0.7934   0.1077
  -2.750  -0.2923   0.00749   0.00149  -0.0016   0.7824   0.1619
  -2.500  -0.2670   0.00706   0.00130  -0.0014   0.7719   0.2365
  -2.000  -0.2173   0.00610   0.00097  -0.0008   0.7514   0.4242
  -1.750  -0.1915   0.00580   0.00088  -0.0005   0.7416   0.4937
  -1.500  -0.1655   0.00557   0.00083  -0.0003   0.7316   0.5536
  -1.250  -0.1383   0.00546   0.00079  -0.0002   0.7214   0.5843
  -1.000  -0.1109   0.00539   0.00076  -0.0001   0.7114   0.6083
  -0.750  -0.0834   0.00535   0.00074   0.0000   0.7013   0.6284
  -0.500  -0.0557   0.00531   0.00073   0.0000   0.6909   0.6461
  -0.250  -0.0278   0.00530   0.00072   0.0000   0.6806   0.6595
   0.000   0.0000   0.00529   0.00072   0.0000   0.6704   0.6704
   0.250   0.0279   0.00530   0.00072   0.0000   0.6595   0.6807
   0.500   0.0557   0.00531   0.00073   0.0000   0.6461   0.6909
   0.750   0.0834   0.00535   0.00074   0.0000   0.6284   0.7014
   1.000   0.1109   0.00539   0.00076   0.0001   0.6082   0.7115
   1.250   0.1383   0.00546   0.00079   0.0002   0.5844   0.7214
   1.500   0.1655   0.00557   0.00083   0.0003   0.5537   0.7316
   1.750   0.1916   0.00579   0.00088   0.0005   0.4963   0.7416
   2.000   0.2174   0.00610   0.00097   0.0008   0.4255   0.7514
   2.500   0.2671   0.00706   0.00130   0.0014   0.2359   0.7719
   2.750   0.2924   0.00749   0.00149   0.0016   0.1610   0.7824
   3.000   0.3183   0.00783   0.00168   0.0018   0.1083   0.7934
   3.500   0.3710   0.00831   0.00202   0.0021   0.0519   0.8177
   3.750   0.3976   0.00849   0.00219   0.0023   0.0388   0.8308
   4.000   0.4241   0.00866   0.00238   0.0025   0.0303   0.8450
   4.250   0.4505   0.00882   0.00257   0.0027   0.0234   0.8602
   4.500   0.4765   0.00901   0.00279   0.0030   0.0183   0.8768
   4.750   0.5025   0.00916   0.00301   0.0034   0.0164   0.8942
   5.000   0.5282   0.00935   0.00326   0.0038   0.0149   0.9130
   5.250   0.5539   0.00959   0.00356   0.0042   0.0137   0.9320
   5.500   0.5809   0.00988   0.00391   0.0044   0.0130   0.9496
   5.750   0.6104   0.01015   0.00423   0.0039   0.0127   0.9639
   6.000   0.6414   0.01046   0.00459   0.0030   0.0123   0.9752
   6.250   0.6730   0.01079   0.00497   0.0019   0.0118   0.9837
   6.500   0.7048   0.01114   0.00534   0.0008   0.0112   0.9902
   6.750   0.7359   0.01152   0.00575  -0.0002   0.0108   0.9958
   7.000   0.7671   0.01194   0.00621  -0.0013   0.0103   1.0000
   7.250   0.7895   0.01237   0.00668  -0.0004   0.0100   1.0000
   7.500   0.8116   0.01291   0.00727   0.0005   0.0095   1.0000
   7.750   0.8321   0.01372   0.00816   0.0016   0.0090   1.0000
   8.000   0.8562   0.01407   0.00855   0.0021   0.0089   1.0000
   8.250   0.8797   0.01452   0.00905   0.0026   0.0087   1.0000
   8.500   0.9032   0.01501   0.00960   0.0032   0.0085   1.0000
   8.750   0.9264   0.01553   0.01021   0.0038   0.0082   1.0000
   9.000   0.9494   0.01609   0.01083   0.0043   0.0080   1.0000
   9.250   0.9724   0.01666   0.01147   0.0049   0.0077   1.0000
   9.500   0.9955   0.01719   0.01206   0.0054   0.0074   1.0000
   9.750   1.0188   0.01766   0.01257   0.0058   0.0071   1.0000
  10.000   1.0423   0.01808   0.01303   0.0062   0.0068   1.0000
  10.250   1.0651   0.01860   0.01358   0.0066   0.0065   1.0000
  10.500   1.0855   0.01943   0.01450   0.0073   0.0062   1.0000
  10.750   1.1043   0.02049   0.01568   0.0082   0.0060   1.0000
  11.000   1.1250   0.02122   0.01652   0.0089   0.0059   1.0000
  11.250   1.1449   0.02202   0.01743   0.0096   0.0058   1.0000
  11.500   1.1638   0.02291   0.01842   0.0104   0.0056   1.0000
  11.750   1.1817   0.02386   0.01949   0.0113   0.0055   1.0000
  12.000   1.1986   0.02487   0.02062   0.0123   0.0053   1.0000
  12.250   1.2144   0.02591   0.02177   0.0133   0.0051   1.0000
  12.500   1.2291   0.02698   0.02296   0.0144   0.0050   1.0000
  12.750   1.2421   0.02807   0.02418   0.0157   0.0048   1.0000
  13.000   1.2520   0.02919   0.02541   0.0173   0.0047   1.0000
  13.250   1.2602   0.03041   0.02673   0.0189   0.0046   1.0000
  13.500   1.2675   0.03173   0.02815   0.0203   0.0045   1.0000
  13.750   1.2729   0.03329   0.02982   0.0214   0.0044   1.0000
  14.000   1.2770   0.03509   0.03173   0.0222   0.0044   1.0000
  14.250   1.2790   0.03724   0.03399   0.0226   0.0043   1.0000
  14.500   1.2786   0.03983   0.03670   0.0225   0.0042   1.0000
  14.750   1.2746   0.04306   0.04007   0.0219   0.0041   1.0000
  15.000   1.2658   0.04718   0.04435   0.0205   0.0041   1.0000
  15.250   1.2518   0.05242   0.04976   0.0180   0.0040   1.0000
  15.500   1.2325   0.05905   0.05657   0.0142   0.0040   1.0000
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