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J5012 12% (j5012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: J5012 12% (j5012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.4 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-j5012-il-1000000-n5.txt
Download as CSV file: xf-j5012-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: J5012   12%                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.1128   0.11015   0.10730  -0.0173   1.0000   0.0088
 -19.000  -1.1438   0.10074   0.09775  -0.0222   1.0000   0.0087
 -18.750  -1.1783   0.09094   0.08779  -0.0272   1.0000   0.0087
 -18.500  -1.2077   0.08222   0.07892  -0.0318   1.0000   0.0086
 -18.250  -1.2311   0.07472   0.07128  -0.0357   1.0000   0.0086
 -18.000  -1.2545   0.06741   0.06382  -0.0395   1.0000   0.0087
 -17.750  -1.2700   0.06157   0.05785  -0.0424   1.0000   0.0086
 -17.500  -1.2825   0.05641   0.05257  -0.0449   1.0000   0.0088
 -17.250  -1.2895   0.05221   0.04827  -0.0467   1.0000   0.0089
 -17.000  -1.2958   0.04831   0.04426  -0.0482   1.0000   0.0090
 -16.750  -1.3021   0.04460   0.04044  -0.0493   1.0000   0.0090
 -16.500  -1.3062   0.04137   0.03709  -0.0501   1.0000   0.0091
 -16.250  -1.3020   0.03922   0.03486  -0.0503   1.0000   0.0093
 -16.000  -1.3036   0.03656   0.03210  -0.0503   1.0000   0.0094
 -15.750  -1.3018   0.03440   0.02985  -0.0500   1.0000   0.0095
 -15.500  -1.2983   0.03254   0.02790  -0.0494   1.0000   0.0096
 -15.250  -1.2930   0.03092   0.02619  -0.0486   1.0000   0.0098
 -15.000  -1.2881   0.02937   0.02456  -0.0476   1.0000   0.0099
 -14.750  -1.2828   0.02793   0.02303  -0.0463   1.0000   0.0101
 -14.500  -1.2757   0.02672   0.02174  -0.0449   1.0000   0.0102
 -14.250  -1.2673   0.02566   0.02060  -0.0433   1.0000   0.0103
 -14.000  -1.2598   0.02459   0.01945  -0.0415   1.0000   0.0104
 -13.750  -1.2507   0.02369   0.01847  -0.0397   1.0000   0.0105
 -13.500  -1.2404   0.02290   0.01761  -0.0378   1.0000   0.0106
 -13.250  -1.2333   0.02197   0.01661  -0.0354   1.0000   0.0108
 -13.000  -1.2258   0.02112   0.01570  -0.0328   1.0000   0.0111
 -12.750  -1.2171   0.02040   0.01492  -0.0302   1.0000   0.0113
 -12.500  -1.2069   0.01981   0.01430  -0.0276   1.0000   0.0116
 -12.250  -1.1967   0.01930   0.01375  -0.0249   1.0000   0.0119
 -12.000  -1.1887   0.01880   0.01319  -0.0216   1.0000   0.0120
 -11.750  -1.1807   0.01835   0.01270  -0.0181   1.0000   0.0123
 -11.500  -1.1696   0.01790   0.01220  -0.0153   1.0000   0.0125
 -11.250  -1.1569   0.01746   0.01171  -0.0127   1.0000   0.0128
 -11.000  -1.1442   0.01702   0.01124  -0.0101   1.0000   0.0131
 -10.750  -1.1309   0.01664   0.01080  -0.0075   1.0000   0.0132
 -10.500  -1.1173   0.01627   0.01038  -0.0050   1.0000   0.0135
 -10.250  -1.0981   0.01586   0.00994  -0.0036   0.9996   0.0137
 -10.000  -1.0708   0.01529   0.00933  -0.0041   0.9983   0.0145
  -9.750  -1.0425   0.01482   0.00885  -0.0047   0.9966   0.0152
  -9.500  -1.0137   0.01439   0.00840  -0.0053   0.9948   0.0157
  -9.250  -0.9855   0.01400   0.00797  -0.0058   0.9930   0.0163
  -9.000  -0.9583   0.01363   0.00757  -0.0060   0.9906   0.0169
  -8.750  -0.9300   0.01326   0.00718  -0.0064   0.9883   0.0175
  -8.500  -0.9011   0.01286   0.00677  -0.0070   0.9862   0.0186
  -8.250  -0.8710   0.01249   0.00640  -0.0078   0.9844   0.0201
  -8.000  -0.8401   0.01217   0.00606  -0.0087   0.9830   0.0216
  -7.750  -0.8146   0.01182   0.00573  -0.0084   0.9793   0.0239
  -7.500  -0.7866   0.01152   0.00542  -0.0087   0.9760   0.0262
  -7.250  -0.7568   0.01119   0.00510  -0.0093   0.9734   0.0293
  -7.000  -0.7253   0.01089   0.00481  -0.0103   0.9714   0.0326
  -6.750  -0.6922   0.01057   0.00452  -0.0117   0.9697   0.0370
  -6.500  -0.6656   0.01033   0.00428  -0.0116   0.9644   0.0404
  -6.250  -0.6349   0.01003   0.00401  -0.0124   0.9603   0.0466
  -6.000  -0.6020   0.00975   0.00376  -0.0136   0.9569   0.0528
  -5.750  -0.5722   0.00950   0.00353  -0.0142   0.9517   0.0595
  -5.500  -0.5428   0.00923   0.00330  -0.0147   0.9452   0.0686
  -5.250  -0.5120   0.00897   0.00308  -0.0155   0.9391   0.0793
  -5.000  -0.4852   0.00871   0.00287  -0.0153   0.9301   0.0943
  -4.750  -0.4579   0.00843   0.00267  -0.0153   0.9211   0.1135
  -4.500  -0.4318   0.00818   0.00247  -0.0151   0.9108   0.1343
  -4.250  -0.4064   0.00797   0.00231  -0.0146   0.8999   0.1529
  -4.000  -0.3815   0.00775   0.00215  -0.0140   0.8886   0.1747
  -3.750  -0.3569   0.00754   0.00200  -0.0133   0.8765   0.2000
  -3.500  -0.3328   0.00734   0.00186  -0.0125   0.8637   0.2274
  -3.250  -0.3087   0.00716   0.00173  -0.0118   0.8504   0.2522
  -3.000  -0.2846   0.00699   0.00162  -0.0110   0.8364   0.2786
  -2.750  -0.2611   0.00681   0.00151  -0.0101   0.8216   0.3104
  -2.500  -0.2378   0.00662   0.00141  -0.0091   0.8066   0.3463
  -2.250  -0.2141   0.00648   0.00132  -0.0082   0.7910   0.3772
  -2.000  -0.1905   0.00635   0.00125  -0.0073   0.7748   0.4086
  -1.750  -0.1666   0.00624   0.00118  -0.0064   0.7586   0.4363
  -1.500  -0.1428   0.00614   0.00113  -0.0055   0.7414   0.4643
  -1.250  -0.1191   0.00606   0.00108  -0.0046   0.7234   0.4937
  -1.000  -0.0953   0.00599   0.00104  -0.0037   0.7049   0.5217
  -0.750  -0.0714   0.00593   0.00101  -0.0028   0.6851   0.5483
  -0.500  -0.0478   0.00589   0.00099  -0.0018   0.6638   0.5741
  -0.250  -0.0239   0.00588   0.00098  -0.0009   0.6423   0.5976
   0.000   0.0000   0.00587   0.00098   0.0000   0.6199   0.6200
   0.250   0.0239   0.00589   0.00098   0.0009   0.5971   0.6416
   0.500   0.0478   0.00590   0.00099   0.0018   0.5733   0.6633
   0.750   0.0714   0.00593   0.00101   0.0028   0.5485   0.6850
   1.000   0.0951   0.00600   0.00104   0.0037   0.5206   0.7049
   1.250   0.1192   0.00606   0.00108   0.0046   0.4938   0.7231
   1.500   0.1427   0.00614   0.00113   0.0055   0.4644   0.7416
   1.750   0.1666   0.00624   0.00118   0.0064   0.4368   0.7585
   2.000   0.1903   0.00635   0.00125   0.0073   0.4072   0.7751
   2.250   0.2140   0.00648   0.00133   0.0082   0.3757   0.7912
   2.500   0.2378   0.00662   0.00141   0.0091   0.3466   0.8067
   2.750   0.2610   0.00681   0.00151   0.0101   0.3104   0.8216
   3.000   0.2845   0.00699   0.00162   0.0110   0.2775   0.8367
   3.250   0.3086   0.00716   0.00173   0.0118   0.2519   0.8503
   3.500   0.3328   0.00734   0.00186   0.0126   0.2274   0.8637
   3.750   0.3568   0.00754   0.00200   0.0133   0.1995   0.8766
   4.000   0.3814   0.00775   0.00215   0.0140   0.1751   0.8885
   4.500   0.4316   0.00819   0.00248   0.0151   0.1330   0.9108
   4.750   0.4581   0.00842   0.00266   0.0153   0.1149   0.9212
   5.000   0.4852   0.00871   0.00287   0.0153   0.0947   0.9302
   5.250   0.5119   0.00897   0.00308   0.0155   0.0793   0.9392
   5.500   0.5428   0.00923   0.00330   0.0147   0.0687   0.9452
   5.750   0.5722   0.00950   0.00353   0.0142   0.0596   0.9517
   6.000   0.6019   0.00976   0.00376   0.0137   0.0522   0.9569
   6.250   0.6348   0.01003   0.00401   0.0124   0.0461   0.9603
   6.500   0.6655   0.01033   0.00428   0.0116   0.0404   0.9643
   6.750   0.6921   0.01058   0.00452   0.0117   0.0366   0.9697
   7.000   0.7253   0.01089   0.00481   0.0103   0.0324   0.9714
   7.250   0.7568   0.01119   0.00510   0.0093   0.0292   0.9734
   7.500   0.7865   0.01152   0.00542   0.0087   0.0262   0.9760
   7.750   0.8146   0.01182   0.00573   0.0084   0.0239   0.9793
   8.000   0.8400   0.01218   0.00607   0.0087   0.0215   0.9830
   8.250   0.8710   0.01250   0.00640   0.0078   0.0201   0.9844
   8.500   0.9011   0.01285   0.00677   0.0070   0.0188   0.9862
   8.750   0.9300   0.01327   0.00718   0.0064   0.0174   0.9883
   9.000   0.9583   0.01363   0.00758   0.0060   0.0168   0.9907
   9.250   0.9855   0.01400   0.00797   0.0058   0.0162   0.9930
   9.500   1.0137   0.01440   0.00841   0.0053   0.0156   0.9948
   9.750   1.0425   0.01483   0.00886   0.0047   0.0150   0.9966
  10.000   1.0708   0.01530   0.00934   0.0041   0.0144   0.9983
  10.250   1.0982   0.01587   0.00995   0.0036   0.0137   0.9996
  10.500   1.1177   0.01625   0.01037   0.0049   0.0135   1.0000
  10.750   1.1308   0.01664   0.01081   0.0075   0.0132   1.0000
  11.000   1.1438   0.01705   0.01126   0.0101   0.0130   1.0000
  11.250   1.1569   0.01746   0.01172   0.0127   0.0128   1.0000
  11.500   1.1692   0.01792   0.01223   0.0153   0.0126   1.0000
  11.750   1.1806   0.01836   0.01271   0.0181   0.0123   1.0000
  12.000   1.1884   0.01881   0.01320   0.0216   0.0121   1.0000
  12.250   1.1969   0.01930   0.01374   0.0248   0.0119   1.0000
  12.500   1.2066   0.01983   0.01432   0.0276   0.0116   1.0000
  12.750   1.2166   0.02043   0.01497   0.0303   0.0114   1.0000
  13.000   1.2264   0.02110   0.01568   0.0327   0.0112   1.0000
  13.250   1.2347   0.02190   0.01654   0.0352   0.0109   1.0000
  13.500   1.2408   0.02290   0.01761   0.0377   0.0106   1.0000
  13.750   1.2496   0.02378   0.01857   0.0398   0.0105   1.0000
  14.000   1.2587   0.02469   0.01955   0.0416   0.0105   1.0000
  14.250   1.2685   0.02560   0.02055   0.0432   0.0103   1.0000
  14.500   1.2758   0.02675   0.02177   0.0448   0.0102   1.0000
  14.750   1.2827   0.02798   0.02309   0.0462   0.0101   1.0000
  15.000   1.2881   0.02941   0.02461   0.0475   0.0100   1.0000
  15.250   1.2940   0.03089   0.02616   0.0485   0.0099   1.0000
  15.500   1.3001   0.03244   0.02779   0.0492   0.0096   1.0000
  15.750   1.3022   0.03444   0.02989   0.0499   0.0096   1.0000
  16.000   1.3069   0.03632   0.03185   0.0501   0.0094   1.0000
  16.250   1.3093   0.03855   0.03416   0.0502   0.0092   1.0000
  16.500   1.3070   0.04139   0.03712   0.0498   0.0091   1.0000
  16.750   1.3045   0.04446   0.04029   0.0492   0.0090   1.0000
  17.000   1.3001   0.04793   0.04386   0.0481   0.0089   1.0000
  17.250   1.2928   0.05196   0.04800   0.0466   0.0088   1.0000
  17.500   1.2852   0.05624   0.05239   0.0447   0.0087   1.0000
  17.750   1.2721   0.06150   0.05778   0.0422   0.0087   1.0000
  18.000   1.2558   0.06747   0.06389   0.0391   0.0087   1.0000
  18.250   1.2350   0.07437   0.07092   0.0356   0.0087   1.0000
  18.500   1.2102   0.08213   0.07883   0.0315   0.0087   1.0000
  18.750   1.1813   0.09079   0.08764   0.0270   0.0087   1.0000
  19.000   1.1490   0.10021   0.09721   0.0221   0.0086   1.0000
  19.250   1.1151   0.11015   0.10730   0.0169   0.0088   1.0000
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