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NACA 63012A AIRFOIL (n63012a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 63012A AIRFOIL (n63012a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 66.57 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63012a-il-1000000-n5.txt
Download as CSV file: xf-n63012a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63012A 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -1.0335   0.13926   0.13722   0.0225   1.0000   0.0068
 -18.000  -1.1168   0.11241   0.11007   0.0084   1.0000   0.0067
 -17.750  -1.1567   0.10012   0.09761   0.0019   1.0000   0.0066
 -17.500  -1.1884   0.08977   0.08708  -0.0038   1.0000   0.0066
 -17.250  -1.2125   0.08135   0.07851  -0.0083   1.0000   0.0066
 -17.000  -1.2328   0.07392   0.07093  -0.0123   1.0000   0.0066
 -16.750  -1.2476   0.06777   0.06464  -0.0154   1.0000   0.0067
 -16.500  -1.2596   0.06239   0.05912  -0.0180   1.0000   0.0067
 -16.250  -1.2688   0.05766   0.05427  -0.0201   1.0000   0.0067
 -16.000  -1.2828   0.05254   0.04899  -0.0220   1.0000   0.0068
 -15.750  -1.2940   0.04802   0.04433  -0.0235   1.0000   0.0068
 -15.500  -1.3010   0.04422   0.04040  -0.0244   1.0000   0.0069
 -15.250  -1.3038   0.04106   0.03713  -0.0250   1.0000   0.0070
 -15.000  -1.3040   0.03835   0.03430  -0.0252   1.0000   0.0071
 -14.750  -1.3011   0.03605   0.03191  -0.0252   1.0000   0.0072
 -14.500  -1.2964   0.03404   0.02980  -0.0250   1.0000   0.0073
 -14.250  -1.2900   0.03227   0.02794  -0.0246   1.0000   0.0074
 -14.000  -1.2826   0.03066   0.02625  -0.0240   1.0000   0.0075
 -13.750  -1.2741   0.02923   0.02473  -0.0232   1.0000   0.0076
 -13.500  -1.2649   0.02791   0.02333  -0.0223   1.0000   0.0077
 -13.250  -1.2550   0.02672   0.02205  -0.0212   1.0000   0.0079
 -13.000  -1.2444   0.02562   0.02087  -0.0200   1.0000   0.0080
 -12.750  -1.2330   0.02461   0.01978  -0.0186   1.0000   0.0081
 -12.500  -1.2209   0.02369   0.01877  -0.0171   1.0000   0.0083
 -12.250  -1.2076   0.02288   0.01787  -0.0156   1.0000   0.0084
 -12.000  -1.1930   0.02214   0.01706  -0.0141   1.0000   0.0086
 -11.750  -1.1763   0.02145   0.01630  -0.0129   1.0000   0.0088
 -11.500  -1.1582   0.02078   0.01556  -0.0119   1.0000   0.0090
 -11.250  -1.1394   0.02013   0.01483  -0.0110   1.0000   0.0091
 -11.000  -1.1201   0.01949   0.01413  -0.0101   1.0000   0.0092
 -10.750  -1.1002   0.01888   0.01345  -0.0092   1.0000   0.0092
 -10.500  -1.0836   0.01793   0.01241  -0.0079   1.0000   0.0095
 -10.250  -1.0648   0.01716   0.01158  -0.0069   1.0000   0.0097
 -10.000  -1.0445   0.01654   0.01091  -0.0060   1.0000   0.0100
  -9.750  -1.0232   0.01600   0.01033  -0.0052   1.0000   0.0102
  -9.500  -1.0015   0.01553   0.00983  -0.0044   1.0000   0.0105
  -9.250  -0.9795   0.01508   0.00934  -0.0037   1.0000   0.0108
  -9.000  -0.9578   0.01463   0.00886  -0.0028   1.0000   0.0110
  -8.750  -0.9364   0.01419   0.00838  -0.0019   1.0000   0.0112
  -8.500  -0.9152   0.01377   0.00792  -0.0009   1.0000   0.0115
  -8.250  -0.8876   0.01333   0.00745  -0.0013   0.9966   0.0117
  -8.000  -0.8570   0.01291   0.00697  -0.0023   0.9903   0.0120
  -7.750  -0.8258   0.01251   0.00654  -0.0034   0.9829   0.0123
  -7.500  -0.7948   0.01210   0.00609  -0.0044   0.9733   0.0127
  -7.250  -0.7650   0.01168   0.00565  -0.0051   0.9605   0.0135
  -7.000  -0.7372   0.01136   0.00528  -0.0053   0.9435   0.0142
  -6.750  -0.7116   0.01109   0.00496  -0.0050   0.9241   0.0149
  -6.500  -0.6868   0.01087   0.00466  -0.0045   0.9041   0.0157
  -6.250  -0.6617   0.01067   0.00438  -0.0040   0.8856   0.0164
  -6.000  -0.6366   0.01042   0.00408  -0.0035   0.8679   0.0185
  -5.750  -0.6109   0.01023   0.00384  -0.0032   0.8517   0.0207
  -5.500  -0.5851   0.01002   0.00359  -0.0029   0.8370   0.0240
  -5.250  -0.5590   0.00984   0.00337  -0.0027   0.8235   0.0277
  -4.750  -0.5064   0.00945   0.00294  -0.0023   0.7992   0.0400
  -4.500  -0.4799   0.00924   0.00274  -0.0021   0.7887   0.0504
  -4.250  -0.4537   0.00901   0.00254  -0.0020   0.7786   0.0657
  -4.000  -0.4274   0.00876   0.00235  -0.0018   0.7688   0.0869
  -3.750  -0.4014   0.00847   0.00215  -0.0016   0.7599   0.1173
  -3.500  -0.3763   0.00807   0.00194  -0.0013   0.7508   0.1695
  -3.250  -0.3514   0.00762   0.00171  -0.0011   0.7423   0.2333
  -3.000  -0.3270   0.00715   0.00150  -0.0007   0.7338   0.3072
  -2.750  -0.3016   0.00676   0.00134  -0.0004   0.7252   0.3720
  -2.500  -0.2760   0.00646   0.00121  -0.0002   0.7171   0.4287
  -2.250  -0.2494   0.00625   0.00113   0.0000   0.7084   0.4710
  -2.000  -0.2226   0.00610   0.00107   0.0001   0.7002   0.5072
  -1.750  -0.1953   0.00599   0.00101   0.0002   0.6914   0.5323
  -1.500  -0.1677   0.00592   0.00098   0.0002   0.6830   0.5539
  -1.000  -0.1123   0.00581   0.00092   0.0002   0.6653   0.5880
  -0.750  -0.0845   0.00578   0.00090   0.0002   0.6567   0.6026
  -0.250  -0.0282   0.00576   0.00088   0.0001   0.6395   0.6222
   0.000   0.0000   0.00576   0.00087   0.0000   0.6306   0.6307
   0.250   0.0282   0.00576   0.00088  -0.0001   0.6222   0.6396
   0.750   0.0845   0.00578   0.00090  -0.0002   0.6025   0.6567
   1.000   0.1123   0.00581   0.00092  -0.0002   0.5880   0.6654
   1.500   0.1677   0.00592   0.00098  -0.0002   0.5538   0.6830
   1.750   0.1953   0.00599   0.00102  -0.0002   0.5323   0.6914
   2.000   0.2226   0.00610   0.00107  -0.0001   0.5071   0.7003
   2.250   0.2494   0.00625   0.00113   0.0000   0.4708   0.7084
   2.500   0.2759   0.00646   0.00121   0.0002   0.4283   0.7172
   2.750   0.3016   0.00676   0.00134   0.0004   0.3727   0.7252
   3.000   0.3270   0.00714   0.00150   0.0007   0.3082   0.7338
   3.250   0.3514   0.00761   0.00171   0.0011   0.2342   0.7423
   3.500   0.3762   0.00808   0.00194   0.0014   0.1681   0.7508
   3.750   0.4014   0.00847   0.00215   0.0016   0.1175   0.7599
   4.000   0.4274   0.00876   0.00235   0.0018   0.0871   0.7688
   4.250   0.4536   0.00901   0.00254   0.0020   0.0655   0.7787
   4.500   0.4798   0.00924   0.00274   0.0022   0.0505   0.7889
   4.750   0.5062   0.00945   0.00294   0.0023   0.0401   0.7993
   5.250   0.5588   0.00984   0.00337   0.0027   0.0277   0.8234
   5.500   0.5850   0.01002   0.00359   0.0029   0.0240   0.8370
   5.750   0.6107   0.01023   0.00383   0.0032   0.0208   0.8520
   6.000   0.6364   0.01042   0.00408   0.0036   0.0185   0.8680
   6.250   0.6615   0.01067   0.00438   0.0040   0.0164   0.8857
   6.500   0.6866   0.01087   0.00466   0.0045   0.0157   0.9041
   6.750   0.7115   0.01109   0.00496   0.0050   0.0149   0.9240
   7.000   0.7371   0.01136   0.00528   0.0054   0.0142   0.9435
   7.250   0.7649   0.01168   0.00564   0.0051   0.0135   0.9605
   7.500   0.7947   0.01210   0.00609   0.0044   0.0127   0.9734
   7.750   0.8258   0.01251   0.00654   0.0034   0.0123   0.9829
   8.000   0.8569   0.01291   0.00697   0.0023   0.0120   0.9903
   8.250   0.8874   0.01333   0.00745   0.0013   0.0117   0.9965
   8.500   0.9152   0.01377   0.00792   0.0009   0.0115   1.0000
   8.750   0.9363   0.01419   0.00838   0.0019   0.0112   1.0000
   9.000   0.9578   0.01463   0.00885   0.0028   0.0110   1.0000
   9.250   0.9794   0.01508   0.00934   0.0037   0.0108   1.0000
   9.500   1.0013   0.01553   0.00983   0.0045   0.0105   1.0000
   9.750   1.0231   0.01600   0.01033   0.0052   0.0102   1.0000
  10.000   1.0442   0.01653   0.01090   0.0060   0.0100   1.0000
  10.250   1.0645   0.01716   0.01158   0.0069   0.0097   1.0000
  10.500   1.0833   0.01792   0.01240   0.0080   0.0095   1.0000
  10.750   1.0998   0.01888   0.01345   0.0093   0.0092   1.0000
  11.000   1.1198   0.01949   0.01412   0.0102   0.0092   1.0000
  11.250   1.1391   0.02012   0.01483   0.0111   0.0091   1.0000
  11.500   1.1579   0.02077   0.01555   0.0120   0.0090   1.0000
  11.750   1.1760   0.02144   0.01629   0.0130   0.0088   1.0000
  12.000   1.1927   0.02213   0.01705   0.0142   0.0086   1.0000
  12.250   1.2074   0.02287   0.01786   0.0157   0.0084   1.0000
  12.500   1.2208   0.02369   0.01876   0.0172   0.0083   1.0000
  12.750   1.2329   0.02461   0.01977   0.0186   0.0081   1.0000
  13.000   1.2444   0.02561   0.02086   0.0200   0.0080   1.0000
  13.250   1.2551   0.02670   0.02203   0.0212   0.0079   1.0000
  13.500   1.2651   0.02790   0.02331   0.0223   0.0077   1.0000
  13.750   1.2744   0.02921   0.02471   0.0232   0.0076   1.0000
  14.000   1.2829   0.03065   0.02623   0.0239   0.0075   1.0000
  14.250   1.2905   0.03224   0.02791   0.0245   0.0074   1.0000
  14.500   1.2970   0.03401   0.02977   0.0249   0.0073   1.0000
  14.750   1.3017   0.03602   0.03187   0.0251   0.0072   1.0000
  15.000   1.3046   0.03833   0.03428   0.0251   0.0071   1.0000
  15.250   1.3047   0.04103   0.03709   0.0249   0.0070   1.0000
  15.500   1.3018   0.04421   0.04039   0.0243   0.0069   1.0000
  15.750   1.2950   0.04798   0.04429   0.0234   0.0068   1.0000
  16.000   1.2839   0.05250   0.04895   0.0219   0.0068   1.0000
  16.250   1.2703   0.05758   0.05418   0.0199   0.0067   1.0000
  16.500   1.2616   0.06224   0.05897   0.0179   0.0067   1.0000
  16.750   1.2498   0.06759   0.06446   0.0153   0.0066   1.0000
  17.000   1.2344   0.07384   0.07085   0.0121   0.0066   1.0000
  17.250   1.2150   0.08112   0.07828   0.0082   0.0066   1.0000
  17.500   1.1915   0.08944   0.08675   0.0037   0.0066   1.0000
  17.750   1.1593   0.09988   0.09736  -0.0020   0.0066   1.0000
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