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HQ 3.5/12 AIRFOIL (hq3512-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.5/12 AIRFOIL (hq3512-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.86 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3512-il-1000000-n5.txt
Download as CSV file: xf-hq3512-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.5/12 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.6968   0.03735   0.03513  -0.0935   0.9833   0.0044
 -11.750  -0.6827   0.03248   0.03002  -0.1027   0.9733   0.0045
 -11.500  -0.6687   0.02871   0.02594  -0.1080   0.9598   0.0047
 -11.250  -0.6518   0.02672   0.02375  -0.1095   0.9465   0.0048
 -11.000  -0.6383   0.02493   0.02173  -0.1097   0.9318   0.0049
 -10.750  -0.6247   0.02335   0.01993  -0.1092   0.9187   0.0050
 -10.500  -0.6089   0.02204   0.01842  -0.1086   0.9087   0.0051
 -10.250  -0.5909   0.02093   0.01712  -0.1080   0.9001   0.0053
 -10.000  -0.5721   0.01982   0.01583  -0.1074   0.8917   0.0054
  -9.750  -0.5525   0.01875   0.01458  -0.1069   0.8844   0.0054
  -9.500  -0.5307   0.01792   0.01359  -0.1065   0.8772   0.0055
  -9.250  -0.5086   0.01710   0.01261  -0.1061   0.8708   0.0056
  -9.000  -0.4854   0.01638   0.01176  -0.1057   0.8642   0.0056
  -8.750  -0.4620   0.01566   0.01090  -0.1054   0.8581   0.0057
  -8.500  -0.4375   0.01508   0.01021  -0.1051   0.8525   0.0057
  -8.250  -0.4133   0.01442   0.00944  -0.1048   0.8463   0.0058
  -8.000  -0.3902   0.01347   0.00832  -0.1044   0.8406   0.0059
  -7.750  -0.3655   0.01278   0.00751  -0.1042   0.8346   0.0060
  -7.500  -0.3405   0.01218   0.00681  -0.1039   0.8289   0.0062
  -7.250  -0.3147   0.01170   0.00625  -0.1038   0.8232   0.0064
  -7.000  -0.2885   0.01130   0.00579  -0.1037   0.8172   0.0067
  -6.750  -0.2621   0.01092   0.00534  -0.1035   0.8118   0.0069
  -6.500  -0.2354   0.01056   0.00491  -0.1034   0.8057   0.0070
  -6.250  -0.2087   0.01024   0.00451  -0.1033   0.7998   0.0072
  -6.000  -0.1816   0.00993   0.00415  -0.1032   0.7942   0.0074
  -5.750  -0.1545   0.00966   0.00382  -0.1031   0.7882   0.0077
  -5.500  -0.1273   0.00943   0.00353  -0.1031   0.7826   0.0079
  -5.250  -0.0997   0.00921   0.00326  -0.1030   0.7767   0.0082
  -5.000  -0.0723   0.00900   0.00299  -0.1030   0.7710   0.0087
  -4.750  -0.0447   0.00880   0.00275  -0.1030   0.7654   0.0095
  -4.500  -0.0170   0.00862   0.00254  -0.1029   0.7595   0.0105
  -4.250   0.0106   0.00844   0.00234  -0.1029   0.7540   0.0135
  -4.000   0.0382   0.00822   0.00217  -0.1030   0.7480   0.0233
  -3.750   0.0660   0.00813   0.00204  -0.1030   0.7420   0.0277
  -3.500   0.0940   0.00800   0.00192  -0.1030   0.7356   0.0329
  -3.250   0.1216   0.00792   0.00181  -0.1030   0.7273   0.0368
  -3.000   0.1493   0.00783   0.00169  -0.1029   0.7166   0.0420
  -2.750   0.1768   0.00777   0.00160  -0.1029   0.7054   0.0472
  -2.500   0.2043   0.00769   0.00151  -0.1028   0.6957   0.0560
  -2.250   0.2323   0.00761   0.00143  -0.1028   0.6874   0.0665
  -2.000   0.2599   0.00753   0.00135  -0.1028   0.6791   0.0822
  -1.750   0.2875   0.00738   0.00128  -0.1029   0.6710   0.1168
  -1.500   0.3148   0.00711   0.00121  -0.1029   0.6635   0.1877
  -1.250   0.3421   0.00693   0.00115  -0.1030   0.6550   0.2480
  -1.000   0.3692   0.00659   0.00108  -0.1031   0.6467   0.3508
  -0.750   0.3963   0.00641   0.00106  -0.1031   0.6383   0.4223
  -0.500   0.4238   0.00629   0.00106  -0.1031   0.6288   0.4766
  -0.250   0.4508   0.00618   0.00109  -0.1030   0.6174   0.5408
   0.000   0.4776   0.00614   0.00116  -0.1028   0.6042   0.5989
   0.250   0.5048   0.00619   0.00120  -0.1027   0.5907   0.6232
   0.500   0.5322   0.00626   0.00124  -0.1026   0.5784   0.6345
   0.750   0.5594   0.00634   0.00129  -0.1025   0.5645   0.6437
   1.000   0.5864   0.00646   0.00133  -0.1023   0.5467   0.6504
   1.250   0.6128   0.00660   0.00140  -0.1020   0.5254   0.6557
   1.500   0.6391   0.00676   0.00148  -0.1018   0.5039   0.6614
   1.750   0.6652   0.00695   0.00157  -0.1015   0.4812   0.6670
   2.000   0.6909   0.00715   0.00168  -0.1011   0.4565   0.6728
   2.250   0.7161   0.00739   0.00181  -0.1007   0.4295   0.6787
   2.500   0.7414   0.00762   0.00195  -0.1003   0.4046   0.6843
   2.750   0.7668   0.00784   0.00208  -0.0999   0.3817   0.6906
   3.000   0.7916   0.00811   0.00224  -0.0994   0.3548   0.6968
   3.250   0.8159   0.00840   0.00242  -0.0989   0.3245   0.7034
   3.500   0.8402   0.00870   0.00261  -0.0983   0.2983   0.7103
   3.750   0.8648   0.00895   0.00279  -0.0978   0.2794   0.7173
   4.000   0.8900   0.00916   0.00296  -0.0974   0.2669   0.7245
   4.250   0.9154   0.00934   0.00313  -0.0971   0.2575   0.7317
   4.500   0.9409   0.00952   0.00330  -0.0967   0.2495   0.7392
   4.750   0.9665   0.00967   0.00347  -0.0964   0.2433   0.7469
   5.250   1.0169   0.01001   0.00383  -0.0956   0.2302   0.7635
   5.500   1.0418   0.01019   0.00401  -0.0952   0.2222   0.7725
   5.750   1.0663   0.01039   0.00421  -0.0947   0.2132   0.7826
   6.000   1.0899   0.01062   0.00443  -0.0940   0.2026   0.7933
   6.250   1.1135   0.01083   0.00465  -0.0934   0.1919   0.8057
   6.500   1.1366   0.01105   0.00488  -0.0926   0.1809   0.8205
   6.750   1.1584   0.01130   0.00513  -0.0917   0.1678   0.8414
   7.000   1.1769   0.01149   0.00541  -0.0900   0.1529   0.8917
   7.250   1.2030   0.01181   0.00575  -0.0901   0.1364   1.0000
   7.500   1.2221   0.01232   0.00615  -0.0887   0.1163   1.0000
   7.750   1.2395   0.01290   0.00661  -0.0872   0.0961   1.0000
   8.000   1.2565   0.01349   0.00708  -0.0855   0.0769   1.0000
   8.250   1.2694   0.01419   0.00764  -0.0831   0.0561   1.0000
   8.500   1.2806   0.01492   0.00826  -0.0805   0.0373   1.0000
   8.750   1.2909   0.01573   0.00895  -0.0777   0.0208   1.0000
   9.000   1.3033   0.01643   0.00961  -0.0754   0.0118   1.0000
   9.250   1.3158   0.01716   0.01031  -0.0731   0.0049   1.0000
   9.500   1.3313   0.01772   0.01089  -0.0714   0.0039   1.0000
   9.750   1.3469   0.01827   0.01148  -0.0697   0.0035   1.0000
  10.000   1.3622   0.01885   0.01211  -0.0681   0.0033   1.0000
  10.250   1.3762   0.01952   0.01283  -0.0663   0.0030   1.0000
  10.500   1.3905   0.02019   0.01354  -0.0647   0.0029   1.0000
  10.750   1.4037   0.02094   0.01435  -0.0630   0.0027   1.0000
  11.000   1.4153   0.02181   0.01529  -0.0611   0.0025   1.0000
  11.250   1.4290   0.02256   0.01609  -0.0596   0.0025   1.0000
  11.500   1.4409   0.02346   0.01704  -0.0580   0.0024   1.0000
  11.750   1.4524   0.02440   0.01805  -0.0564   0.0023   1.0000
  12.000   1.4631   0.02542   0.01914  -0.0548   0.0022   1.0000
  12.250   1.4740   0.02646   0.02024  -0.0533   0.0021   1.0000
  12.500   1.4828   0.02768   0.02154  -0.0517   0.0020   1.0000
  12.750   1.4914   0.02896   0.02288  -0.0502   0.0020   1.0000
  13.000   1.4993   0.03032   0.02432  -0.0488   0.0019   1.0000
  13.250   1.5052   0.03191   0.02598  -0.0473   0.0018   1.0000
  13.500   1.5118   0.03346   0.02762  -0.0461   0.0018   1.0000
  13.750   1.5162   0.03528   0.02952  -0.0448   0.0018   1.0000
  14.000   1.5209   0.03712   0.03144  -0.0437   0.0017   1.0000
  14.250   1.5236   0.03921   0.03363  -0.0427   0.0017   1.0000
  14.500   1.5241   0.04163   0.03615  -0.0418   0.0016   1.0000
  14.750   1.5238   0.04421   0.03883  -0.0410   0.0016   1.0000
  15.000   1.5226   0.04701   0.04173  -0.0405   0.0016   1.0000
  15.250   1.5217   0.04992   0.04474  -0.0402   0.0016   1.0000
  15.500   1.5176   0.05333   0.04826  -0.0401   0.0015   1.0000
  15.750   1.5120   0.05708   0.05213  -0.0403   0.0015   1.0000
  16.000   1.5024   0.06156   0.05674  -0.0409   0.0015   1.0000
  16.250   1.4935   0.06618   0.06149  -0.0418   0.0015   1.0000
  16.500   1.4798   0.07175   0.06720  -0.0433   0.0014   1.0000
  16.750   1.4647   0.07783   0.07343  -0.0453   0.0014   1.0000
  17.000   1.4606   0.08235   0.07805  -0.0469   0.0014   1.0000
  17.250   1.4457   0.08889   0.08473  -0.0495   0.0014   1.0000
  17.500   1.4271   0.09633   0.09232  -0.0528   0.0014   1.0000
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