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NACA 64(1)-212 (n64212-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64(1)-212 (n64212-il)
Reynolds number: 1,000,000
Max Cl/Cd: 73.26 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n64212-il-1000000-n5.txt
Download as CSV file: xf-n64212-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64(1)-212                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.0838   0.07549   0.07302  -0.0346   1.0000   0.0069
 -16.750  -1.1188   0.06527   0.06258  -0.0411   1.0000   0.0069
 -16.500  -1.1337   0.05934   0.05653  -0.0446   1.0000   0.0070
 -16.250  -1.1437   0.05454   0.05160  -0.0472   1.0000   0.0070
 -16.000  -1.1539   0.05002   0.04696  -0.0494   1.0000   0.0071
 -15.750  -1.1648   0.04568   0.04246  -0.0513   1.0000   0.0071
 -15.500  -1.1670   0.04261   0.03929  -0.0523   1.0000   0.0071
 -15.250  -1.1652   0.04012   0.03671  -0.0530   1.0000   0.0073
 -15.000  -1.1670   0.03737   0.03384  -0.0534   1.0000   0.0073
 -14.750  -1.1634   0.03530   0.03167  -0.0536   1.0000   0.0075
 -14.500  -1.1603   0.03327   0.02954  -0.0535   1.0000   0.0076
 -14.250  -1.1584   0.03124   0.02739  -0.0531   1.0000   0.0077
 -14.000  -1.1532   0.02961   0.02566  -0.0525   1.0000   0.0078
 -13.750  -1.1452   0.02829   0.02425  -0.0518   1.0000   0.0080
 -13.500  -1.1403   0.02679   0.02264  -0.0507   1.0000   0.0080
 -13.250  -1.1327   0.02560   0.02135  -0.0494   1.0000   0.0082
 -13.000  -1.1242   0.02459   0.02025  -0.0480   1.0000   0.0083
 -12.750  -1.1156   0.02370   0.01927  -0.0461   1.0000   0.0084
 -12.500  -1.1060   0.02289   0.01837  -0.0442   1.0000   0.0085
 -12.250  -1.0922   0.02202   0.01741  -0.0429   1.0000   0.0086
 -12.000  -1.0789   0.02102   0.01633  -0.0416   1.0000   0.0090
 -11.750  -1.0620   0.02027   0.01552  -0.0406   1.0000   0.0092
 -11.500  -1.0432   0.01964   0.01485  -0.0398   1.0000   0.0094
 -11.250  -1.0242   0.01899   0.01414  -0.0389   1.0000   0.0096
 -11.000  -1.0042   0.01841   0.01351  -0.0382   1.0000   0.0098
 -10.750  -0.9841   0.01781   0.01285  -0.0374   1.0000   0.0100
 -10.500  -0.9592   0.01724   0.01222  -0.0376   0.9909   0.0103
 -10.000  -0.8925   0.01597   0.01079  -0.0414   0.9591   0.0109
  -9.750  -0.8651   0.01551   0.01023  -0.0419   0.9410   0.0111
  -9.500  -0.8415   0.01512   0.00975  -0.0414   0.9237   0.0113
  -9.250  -0.8201   0.01456   0.00907  -0.0406   0.9083   0.0116
  -9.000  -0.7981   0.01403   0.00845  -0.0399   0.8945   0.0120
  -8.750  -0.7748   0.01360   0.00795  -0.0394   0.8826   0.0123
  -8.500  -0.7509   0.01324   0.00752  -0.0389   0.8712   0.0127
  -8.250  -0.7263   0.01290   0.00711  -0.0386   0.8604   0.0130
  -8.000  -0.7013   0.01258   0.00673  -0.0383   0.8503   0.0134
  -7.750  -0.6762   0.01228   0.00635  -0.0380   0.8406   0.0138
  -7.500  -0.6508   0.01196   0.00596  -0.0378   0.8307   0.0142
  -7.250  -0.6252   0.01165   0.00559  -0.0376   0.8217   0.0145
  -7.000  -0.5992   0.01138   0.00523  -0.0374   0.8123   0.0148
  -6.750  -0.5735   0.01101   0.00481  -0.0372   0.8036   0.0156
  -6.500  -0.5474   0.01073   0.00449  -0.0371   0.7950   0.0163
  -6.250  -0.5207   0.01049   0.00422  -0.0371   0.7864   0.0172
  -6.000  -0.4938   0.01028   0.00397  -0.0370   0.7787   0.0183
  -5.750  -0.4667   0.01008   0.00372  -0.0370   0.7705   0.0191
  -5.500  -0.4398   0.00984   0.00345  -0.0370   0.7625   0.0206
  -5.250  -0.4126   0.00964   0.00322  -0.0370   0.7540   0.0223
  -5.000  -0.3851   0.00947   0.00302  -0.0371   0.7464   0.0239
  -4.750  -0.3575   0.00931   0.00282  -0.0371   0.7386   0.0254
  -4.500  -0.3300   0.00913   0.00261  -0.0372   0.7316   0.0283
  -4.250  -0.3022   0.00897   0.00244  -0.0373   0.7241   0.0309
  -4.000  -0.2744   0.00884   0.00228  -0.0374   0.7171   0.0342
  -3.750  -0.2466   0.00867   0.00212  -0.0375   0.7095   0.0399
  -3.500  -0.2189   0.00851   0.00197  -0.0376   0.7022   0.0508
  -3.250  -0.1912   0.00827   0.00181  -0.0377   0.6945   0.0743
  -3.000  -0.1638   0.00798   0.00164  -0.0379   0.6876   0.1143
  -2.750  -0.1365   0.00761   0.00147  -0.0381   0.6808   0.1735
  -2.500  -0.1093   0.00722   0.00129  -0.0383   0.6741   0.2447
  -2.250  -0.0824   0.00666   0.00110  -0.0386   0.6679   0.3488
  -2.000  -0.0551   0.00626   0.00098  -0.0388   0.6612   0.4391
  -1.750  -0.0269   0.00611   0.00093  -0.0390   0.6552   0.4818
  -1.500   0.0014   0.00597   0.00091  -0.0392   0.6487   0.5217
  -1.250   0.0295   0.00586   0.00090  -0.0393   0.6423   0.5627
  -1.000   0.0582   0.00582   0.00090  -0.0395   0.6359   0.5811
  -0.750   0.0869   0.00582   0.00089  -0.0397   0.6296   0.5891
  -0.500   0.1158   0.00582   0.00088  -0.0399   0.6242   0.5971
  -0.250   0.1446   0.00582   0.00088  -0.0401   0.6185   0.6039
   0.000   0.1733   0.00584   0.00089  -0.0403   0.6130   0.6102
   0.250   0.2023   0.00585   0.00090  -0.0406   0.6079   0.6157
   0.500   0.2310   0.00586   0.00092  -0.0408   0.6019   0.6214
   0.750   0.2597   0.00589   0.00094  -0.0409   0.5954   0.6274
   1.000   0.2885   0.00591   0.00097  -0.0411   0.5878   0.6331
   1.250   0.3170   0.00594   0.00100  -0.0413   0.5808   0.6396
   1.500   0.3458   0.00598   0.00104  -0.0415   0.5726   0.6463
   1.750   0.3741   0.00603   0.00109  -0.0416   0.5595   0.6532
   2.000   0.4018   0.00615   0.00114  -0.0416   0.5355   0.6601
   2.250   0.4290   0.00632   0.00120  -0.0416   0.4986   0.6666
   2.500   0.4564   0.00649   0.00129  -0.0416   0.4681   0.6737
   2.750   0.4826   0.00682   0.00142  -0.0415   0.4108   0.6802
   3.000   0.5072   0.00735   0.00165  -0.0412   0.3337   0.6876
   3.250   0.5318   0.00791   0.00193  -0.0409   0.2592   0.6944
   3.500   0.5557   0.00852   0.00224  -0.0406   0.1815   0.7022
   3.750   0.5806   0.00902   0.00252  -0.0403   0.1252   0.7099
   4.000   0.6056   0.00947   0.00279  -0.0400   0.0809   0.7183
   4.250   0.6313   0.00983   0.00305  -0.0399   0.0535   0.7259
   4.500   0.6577   0.01008   0.00327  -0.0397   0.0415   0.7339
   4.750   0.6842   0.01032   0.00350  -0.0396   0.0344   0.7415
   5.000   0.7108   0.01053   0.00373  -0.0395   0.0305   0.7497
   5.250   0.7372   0.01076   0.00397  -0.0394   0.0271   0.7576
   5.500   0.7637   0.01095   0.00420  -0.0393   0.0252   0.7666
   5.750   0.7897   0.01120   0.00446  -0.0391   0.0227   0.7753
   6.000   0.8156   0.01145   0.00475  -0.0389   0.0206   0.7845
   6.250   0.8415   0.01168   0.00502  -0.0387   0.0189   0.7931
   6.500   0.8669   0.01197   0.00532  -0.0384   0.0170   0.8022
   6.750   0.8919   0.01226   0.00566  -0.0381   0.0157   0.8120
   7.000   0.9170   0.01253   0.00598  -0.0378   0.0147   0.8217
   7.500   0.9656   0.01318   0.00670  -0.0369   0.0130   0.8429
   7.750   0.9886   0.01358   0.00717  -0.0362   0.0123   0.8540
   8.000   1.0120   0.01392   0.00758  -0.0356   0.0121   0.8659
   8.250   1.0347   0.01427   0.00801  -0.0349   0.0118   0.8794
   8.500   1.0565   0.01465   0.00846  -0.0339   0.0116   0.8944
   8.750   1.0770   0.01503   0.00893  -0.0328   0.0113   0.9122
   9.000   1.0964   0.01540   0.00940  -0.0315   0.0111   0.9338
   9.250   1.1180   0.01580   0.00989  -0.0306   0.0109   0.9717
   9.500   1.1410   0.01630   0.01044  -0.0302   0.0107   1.0000
   9.750   1.1623   0.01681   0.01098  -0.0295   0.0104   1.0000
  10.000   1.1825   0.01737   0.01158  -0.0286   0.0102   1.0000
  10.250   1.2019   0.01795   0.01220  -0.0277   0.0099   1.0000
  10.500   1.2194   0.01864   0.01293  -0.0264   0.0097   1.0000
  10.750   1.2326   0.01952   0.01388  -0.0246   0.0094   1.0000
  11.000   1.2445   0.02029   0.01471  -0.0225   0.0093   1.0000
  11.250   1.2574   0.02098   0.01546  -0.0206   0.0092   1.0000
  11.500   1.2702   0.02171   0.01626  -0.0188   0.0091   1.0000
  11.750   1.2818   0.02254   0.01716  -0.0171   0.0091   1.0000
  12.000   1.2936   0.02340   0.01811  -0.0155   0.0089   1.0000
  12.250   1.3044   0.02438   0.01916  -0.0139   0.0088   1.0000
  12.500   1.3166   0.02528   0.02013  -0.0126   0.0087   1.0000
  12.750   1.3254   0.02648   0.02142  -0.0111   0.0086   1.0000
  13.000   1.3362   0.02757   0.02258  -0.0100   0.0084   1.0000
  13.250   1.3453   0.02883   0.02391  -0.0088   0.0083   1.0000
  13.500   1.3532   0.03023   0.02541  -0.0077   0.0082   1.0000
  13.750   1.3609   0.03172   0.02698  -0.0067   0.0081   1.0000
  14.000   1.3677   0.03331   0.02865  -0.0058   0.0080   1.0000
  14.250   1.3740   0.03501   0.03045  -0.0051   0.0079   1.0000
  14.500   1.3796   0.03683   0.03236  -0.0045   0.0077   1.0000
  14.750   1.3843   0.03880   0.03442  -0.0040   0.0077   1.0000
  15.000   1.3866   0.04111   0.03683  -0.0037   0.0076   1.0000
  15.250   1.3899   0.04336   0.03917  -0.0035   0.0075   1.0000
  15.500   1.3912   0.04592   0.04182  -0.0036   0.0074   1.0000
  15.750   1.3925   0.04857   0.04456  -0.0038   0.0073   1.0000
  16.000   1.3895   0.05183   0.04793  -0.0043   0.0072   1.0000
  16.250   1.3857   0.05535   0.05157  -0.0050   0.0072   1.0000
  16.500   1.3796   0.05936   0.05569  -0.0062   0.0071   1.0000
  16.750   1.3693   0.06416   0.06062  -0.0078   0.0070   1.0000
  17.000   1.3597   0.06914   0.06573  -0.0098   0.0069   1.0000
  17.250   1.3451   0.07515   0.07189  -0.0125   0.0068   1.0000
  17.500   1.3285   0.08185   0.07876  -0.0157   0.0068   1.0000
  17.750   1.3151   0.08842   0.08547  -0.0192   0.0068   1.0000
  18.000   1.3049   0.09469   0.09186  -0.0227   0.0068   1.0000
  18.250   1.2828   0.10366   0.10101  -0.0280   0.0068   1.0000
  18.500   1.2592   0.11345   0.11096  -0.0339   0.0068   1.0000
  18.750   1.2312   0.12465   0.12233  -0.0407   0.0068   1.0000
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