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NACA 64A-010 10.0% (naca64a010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64A-010 10.0% (naca64a010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 63.07 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca64a010-il-1000000-n5.txt
Download as CSV file: xf-naca64a010-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64A-010 10.0%                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -1.0804   0.06300   0.06077  -0.0301   1.0000   0.0045
 -15.000  -1.1183   0.05342   0.05092  -0.0357   1.0000   0.0044
 -14.750  -1.1274   0.04907   0.04644  -0.0378   1.0000   0.0044
 -14.500  -1.1424   0.04437   0.04158  -0.0393   1.0000   0.0045
 -14.250  -1.1543   0.04050   0.03753  -0.0398   1.0000   0.0045
 -14.000  -1.1571   0.03794   0.03485  -0.0396   1.0000   0.0046
 -13.750  -1.1633   0.03523   0.03198  -0.0387   1.0000   0.0046
 -13.500  -1.1685   0.03283   0.02941  -0.0371   1.0000   0.0046
 -13.250  -1.1636   0.03148   0.02797  -0.0357   1.0000   0.0047
 -13.000  -1.1644   0.02972   0.02605  -0.0334   1.0000   0.0047
 -12.750  -1.1576   0.02867   0.02490  -0.0314   1.0000   0.0048
 -12.500  -1.1529   0.02750   0.02361  -0.0288   1.0000   0.0049
 -12.250  -1.1462   0.02655   0.02256  -0.0262   1.0000   0.0050
 -12.000  -1.1373   0.02566   0.02158  -0.0237   1.0000   0.0051
 -11.750  -1.1285   0.02434   0.02010  -0.0215   1.0000   0.0052
 -11.500  -1.1141   0.02351   0.01918  -0.0199   1.0000   0.0054
 -11.250  -1.1006   0.02250   0.01804  -0.0181   1.0000   0.0055
 -11.000  -1.0847   0.02169   0.01712  -0.0166   1.0000   0.0057
 -10.750  -1.0678   0.02094   0.01627  -0.0152   1.0000   0.0059
 -10.500  -1.0510   0.02013   0.01535  -0.0137   1.0000   0.0060
 -10.250  -1.0329   0.01947   0.01459  -0.0124   1.0000   0.0061
 -10.000  -1.0154   0.01871   0.01372  -0.0109   1.0000   0.0062
  -9.750  -0.9969   0.01805   0.01298  -0.0095   1.0000   0.0063
  -9.500  -0.9807   0.01713   0.01194  -0.0078   1.0000   0.0065
  -9.250  -0.9641   0.01627   0.01099  -0.0061   1.0000   0.0068
  -9.000  -0.9453   0.01566   0.01032  -0.0047   1.0000   0.0070
  -8.750  -0.9259   0.01512   0.00973  -0.0033   1.0000   0.0072
  -8.500  -0.9059   0.01467   0.00923  -0.0021   1.0000   0.0075
  -8.250  -0.8859   0.01423   0.00874  -0.0008   1.0000   0.0077
  -8.000  -0.8661   0.01380   0.00826   0.0006   1.0000   0.0080
  -7.750  -0.8432   0.01335   0.00776   0.0013   0.9995   0.0083
  -7.500  -0.8124   0.01289   0.00725   0.0002   0.9969   0.0087
  -7.250  -0.7828   0.01243   0.00674  -0.0005   0.9930   0.0090
  -7.000  -0.7526   0.01212   0.00639  -0.0013   0.9889   0.0093
  -6.750  -0.7237   0.01150   0.00571  -0.0020   0.9840   0.0101
  -6.500  -0.6932   0.01108   0.00527  -0.0029   0.9788   0.0106
  -6.250  -0.6605   0.01071   0.00488  -0.0042   0.9737   0.0113
  -6.000  -0.6274   0.01037   0.00450  -0.0057   0.9666   0.0120
  -5.750  -0.5936   0.01007   0.00416  -0.0072   0.9575   0.0128
  -5.500  -0.5598   0.00980   0.00386  -0.0087   0.9457   0.0133
  -5.250  -0.5294   0.00946   0.00347  -0.0095   0.9289   0.0153
  -5.000  -0.5019   0.00925   0.00320  -0.0095   0.9101   0.0168
  -4.750  -0.4760   0.00909   0.00297  -0.0092   0.8914   0.0181
  -4.500  -0.4508   0.00893   0.00274  -0.0086   0.8742   0.0201
  -4.250  -0.4258   0.00876   0.00253  -0.0081   0.8580   0.0236
  -4.000  -0.4004   0.00863   0.00235  -0.0076   0.8433   0.0276
  -3.750  -0.3752   0.00847   0.00218  -0.0072   0.8299   0.0348
  -3.500  -0.3499   0.00831   0.00201  -0.0067   0.8175   0.0457
  -3.250  -0.3247   0.00812   0.00184  -0.0063   0.8058   0.0634
  -3.000  -0.2998   0.00787   0.00168  -0.0058   0.7946   0.0945
  -2.750  -0.2760   0.00751   0.00150  -0.0052   0.7838   0.1532
  -2.500  -0.2533   0.00703   0.00131  -0.0044   0.7736   0.2411
  -2.250  -0.2304   0.00658   0.00112  -0.0036   0.7635   0.3262
  -2.000  -0.2083   0.00604   0.00096  -0.0028   0.7542   0.4345
  -1.750  -0.1846   0.00573   0.00088  -0.0021   0.7448   0.5104
  -1.500  -0.1595   0.00555   0.00083  -0.0016   0.7351   0.5582
  -1.250  -0.1342   0.00540   0.00080  -0.0011   0.7263   0.6016
  -1.000  -0.1081   0.00532   0.00077  -0.0007   0.7178   0.6277
  -0.750  -0.0813   0.00527   0.00076  -0.0005   0.7089   0.6471
  -0.500  -0.0546   0.00523   0.00075  -0.0002   0.7003   0.6632
  -0.250  -0.0273   0.00523   0.00074  -0.0001   0.6912   0.6744
   0.000   0.0000   0.00522   0.00074   0.0000   0.6831   0.6831
   0.250   0.0273   0.00523   0.00074   0.0001   0.6744   0.6912
   0.500   0.0546   0.00523   0.00075   0.0002   0.6632   0.7001
   0.750   0.0814   0.00527   0.00076   0.0005   0.6473   0.7089
   1.000   0.1081   0.00532   0.00077   0.0007   0.6281   0.7177
   1.250   0.1342   0.00540   0.00080   0.0011   0.6010   0.7262
   1.500   0.1595   0.00555   0.00083   0.0015   0.5583   0.7352
   1.750   0.1846   0.00573   0.00088   0.0020   0.5106   0.7449
   2.000   0.2083   0.00605   0.00096   0.0028   0.4332   0.7542
   2.250   0.2305   0.00657   0.00112   0.0036   0.3283   0.7635
   2.500   0.2535   0.00701   0.00130   0.0044   0.2430   0.7735
   2.750   0.2760   0.00751   0.00150   0.0052   0.1532   0.7837
   3.000   0.2998   0.00788   0.00168   0.0058   0.0930   0.7946
   3.250   0.3247   0.00812   0.00184   0.0062   0.0632   0.8058
   3.500   0.3499   0.00831   0.00201   0.0067   0.0460   0.8173
   3.750   0.3752   0.00847   0.00218   0.0072   0.0348   0.8299
   4.000   0.4005   0.00863   0.00235   0.0076   0.0279   0.8433
   4.250   0.4258   0.00876   0.00253   0.0081   0.0235   0.8580
   4.500   0.4508   0.00893   0.00274   0.0086   0.0202   0.8742
   4.750   0.4760   0.00909   0.00297   0.0092   0.0181   0.8918
   5.000   0.5019   0.00924   0.00320   0.0095   0.0167   0.9106
   5.250   0.5294   0.00946   0.00346   0.0095   0.0151   0.9291
   5.500   0.5599   0.00979   0.00385   0.0087   0.0133   0.9459
   5.750   0.5936   0.01006   0.00416   0.0072   0.0127   0.9574
   6.000   0.6274   0.01038   0.00451   0.0057   0.0120   0.9666
   6.250   0.6604   0.01071   0.00488   0.0043   0.0113   0.9736
   6.500   0.6931   0.01108   0.00526   0.0029   0.0106   0.9787
   6.750   0.7235   0.01150   0.00571   0.0020   0.0100   0.9841
   7.000   0.7522   0.01216   0.00643   0.0014   0.0093   0.9889
   7.250   0.7825   0.01246   0.00677   0.0006   0.0090   0.9930
   7.500   0.8123   0.01288   0.00724  -0.0002   0.0087   0.9968
   7.750   0.8429   0.01337   0.00779  -0.0012   0.0084   0.9995
   8.000   0.8658   0.01383   0.00830  -0.0005   0.0080   1.0000
   8.250   0.8858   0.01425   0.00876   0.0008   0.0077   1.0000
   8.500   0.9059   0.01468   0.00923   0.0021   0.0074   1.0000
   8.750   0.9258   0.01513   0.00974   0.0034   0.0072   1.0000
   9.000   0.9453   0.01565   0.01031   0.0047   0.0070   1.0000
   9.250   0.9643   0.01624   0.01096   0.0060   0.0068   1.0000
   9.500   0.9803   0.01718   0.01199   0.0079   0.0065   1.0000
   9.750   0.9961   0.01815   0.01308   0.0097   0.0063   1.0000
  10.000   1.0143   0.01882   0.01385   0.0111   0.0063   1.0000
  10.250   1.0328   0.01946   0.01458   0.0124   0.0062   1.0000
  10.500   1.0510   0.02011   0.01532   0.0137   0.0060   1.0000
  10.750   1.0684   0.02084   0.01617   0.0151   0.0058   1.0000
  11.000   1.0845   0.02168   0.01712   0.0166   0.0057   1.0000
  11.250   1.0995   0.02259   0.01814   0.0182   0.0056   1.0000
  11.500   1.1144   0.02345   0.01911   0.0198   0.0054   1.0000
  11.750   1.1271   0.02447   0.02025   0.0217   0.0052   1.0000
  12.000   1.1390   0.02546   0.02135   0.0236   0.0051   1.0000
  12.250   1.1486   0.02632   0.02231   0.0259   0.0050   1.0000
  12.500   1.1531   0.02747   0.02358   0.0288   0.0049   1.0000
  12.750   1.1558   0.02881   0.02506   0.0315   0.0049   1.0000
  13.000   1.1565   0.03041   0.02682   0.0341   0.0048   1.0000
  13.250   1.1661   0.03126   0.02773   0.0355   0.0047   1.0000
  13.500   1.1656   0.03310   0.02971   0.0373   0.0047   1.0000
  13.750   1.1659   0.03499   0.03171   0.0386   0.0046   1.0000
  14.000   1.1589   0.03776   0.03466   0.0395   0.0046   1.0000
  14.250   1.1558   0.04037   0.03740   0.0398   0.0045   1.0000
  14.500   1.1482   0.04372   0.04090   0.0394   0.0045   1.0000
  14.750   1.1353   0.04808   0.04542   0.0381   0.0044   1.0000
  15.000   1.1131   0.05428   0.05182   0.0352   0.0044   1.0000
  15.250   1.0924   0.06107   0.05877   0.0312   0.0044   1.0000
  15.500   1.0488   0.07360   0.07156   0.0227   0.0045   1.0000
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