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NACA 64(3)-418 (naca643418-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 64(3)-418 (naca643418-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.15 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca643418-il-1000000-n5.txt
Download as CSV file: xf-naca643418-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 64(3)-418                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0946   0.08244   0.07873  -0.0603   1.0000   0.0150
 -19.500  -1.1024   0.07794   0.07414  -0.0624   1.0000   0.0151
 -19.250  -1.1059   0.07415   0.07028  -0.0641   1.0000   0.0152
 -19.000  -1.1076   0.07065   0.06670  -0.0656   1.0000   0.0154
 -18.750  -1.1118   0.06692   0.06289  -0.0671   1.0000   0.0155
 -18.500  -1.1118   0.06380   0.05969  -0.0684   1.0000   0.0156
 -18.250  -1.1121   0.06071   0.05653  -0.0695   1.0000   0.0158
 -18.000  -1.1113   0.05780   0.05355  -0.0706   1.0000   0.0159
 -17.750  -1.1098   0.05505   0.05072  -0.0715   1.0000   0.0160
 -17.500  -1.1068   0.05252   0.04813  -0.0722   1.0000   0.0162
 -17.250  -1.1025   0.05019   0.04572  -0.0729   1.0000   0.0163
 -17.000  -1.0982   0.04789   0.04336  -0.0734   1.0000   0.0165
 -16.750  -1.0936   0.04568   0.04108  -0.0739   1.0000   0.0166
 -16.500  -1.0874   0.04369   0.03903  -0.0743   1.0000   0.0167
 -16.250  -1.0825   0.04162   0.03690  -0.0746   1.0000   0.0168
 -16.000  -1.0787   0.03948   0.03471  -0.0748   1.0000   0.0170
 -15.750  -1.0734   0.03757   0.03275  -0.0750   1.0000   0.0172
 -15.500  -1.0661   0.03592   0.03107  -0.0749   1.0000   0.0175
 -15.250  -1.0586   0.03431   0.02942  -0.0748   1.0000   0.0177
 -15.000  -1.0497   0.03288   0.02795  -0.0747   1.0000   0.0178
 -14.500  -1.0269   0.03008   0.02508  -0.0748   0.9747   0.0184
 -14.250  -0.9806   0.02852   0.02345  -0.0817   0.9587   0.0188
 -14.000  -0.9343   0.02702   0.02186  -0.0886   0.9423   0.0192
 -13.750  -0.8998   0.02584   0.02052  -0.0928   0.9128   0.0195
 -13.500  -0.8869   0.02488   0.01941  -0.0924   0.8851   0.0196
 -13.250  -0.8760   0.02398   0.01839  -0.0914   0.8666   0.0199
 -13.000  -0.8673   0.02297   0.01729  -0.0903   0.8506   0.0202
 -12.750  -0.8573   0.02203   0.01628  -0.0892   0.8371   0.0205
 -12.500  -0.8452   0.02123   0.01541  -0.0882   0.8256   0.0209
 -12.250  -0.8334   0.02045   0.01455  -0.0871   0.8147   0.0212
 -12.000  -0.8207   0.01968   0.01373  -0.0861   0.8045   0.0217
 -11.750  -0.8075   0.01901   0.01299  -0.0850   0.7943   0.0220
 -11.500  -0.7942   0.01834   0.01225  -0.0839   0.7836   0.0224
 -11.250  -0.7807   0.01770   0.01155  -0.0827   0.7748   0.0226
 -11.000  -0.7671   0.01708   0.01086  -0.0814   0.7656   0.0229
 -10.750  -0.7531   0.01654   0.01025  -0.0801   0.7578   0.0233
 -10.500  -0.7416   0.01590   0.00957  -0.0784   0.7501   0.0238
 -10.250  -0.7314   0.01536   0.00898  -0.0764   0.7420   0.0243
 -10.000  -0.7208   0.01494   0.00853  -0.0742   0.7350   0.0249
  -9.750  -0.7031   0.01457   0.00811  -0.0731   0.7271   0.0254
  -9.500  -0.6836   0.01424   0.00772  -0.0722   0.7206   0.0262
  -9.250  -0.6624   0.01392   0.00737  -0.0715   0.7139   0.0267
  -9.000  -0.6411   0.01360   0.00700  -0.0708   0.7074   0.0275
  -8.750  -0.6191   0.01327   0.00665  -0.0702   0.7016   0.0284
  -8.500  -0.5960   0.01298   0.00633  -0.0698   0.6955   0.0294
  -8.250  -0.5722   0.01272   0.00603  -0.0694   0.6893   0.0305
  -8.000  -0.5476   0.01249   0.00576  -0.0692   0.6839   0.0314
  -7.750  -0.5232   0.01220   0.00546  -0.0689   0.6780   0.0330
  -7.500  -0.4982   0.01196   0.00520  -0.0687   0.6720   0.0348
  -7.250  -0.4726   0.01174   0.00495  -0.0686   0.6667   0.0367
  -7.000  -0.4468   0.01149   0.00470  -0.0686   0.6613   0.0393
  -6.750  -0.4207   0.01129   0.00447  -0.0685   0.6553   0.0421
  -6.500  -0.3946   0.01107   0.00425  -0.0685   0.6497   0.0460
  -6.250  -0.3680   0.01085   0.00403  -0.0685   0.6441   0.0509
  -6.000  -0.3413   0.01064   0.00383  -0.0686   0.6382   0.0570
  -5.750  -0.3147   0.01043   0.00363  -0.0686   0.6328   0.0653
  -5.500  -0.2876   0.01019   0.00343  -0.0688   0.6283   0.0760
  -5.250  -0.2603   0.00996   0.00324  -0.0689   0.6232   0.0884
  -5.000  -0.2332   0.00973   0.00305  -0.0691   0.6181   0.1050
  -4.750  -0.2062   0.00945   0.00285  -0.0693   0.6137   0.1301
  -4.500  -0.1788   0.00913   0.00265  -0.0696   0.6093   0.1608
  -4.250  -0.1517   0.00876   0.00243  -0.0699   0.6046   0.2022
  -4.000  -0.1247   0.00835   0.00220  -0.0702   0.5999   0.2563
  -3.750  -0.0976   0.00786   0.00196  -0.0706   0.5959   0.3258
  -3.500  -0.0698   0.00742   0.00176  -0.0711   0.5920   0.3916
  -3.250  -0.0410   0.00721   0.00170  -0.0715   0.5877   0.4416
  -3.000  -0.0119   0.00715   0.00167  -0.0719   0.5835   0.4613
  -2.750   0.0173   0.00714   0.00164  -0.0722   0.5795   0.4719
  -2.500   0.0469   0.00711   0.00162  -0.0726   0.5762   0.4836
  -2.250   0.0763   0.00707   0.00162  -0.0730   0.5724   0.4982
  -2.000   0.1057   0.00706   0.00161  -0.0733   0.5684   0.5090
  -1.750   0.1349   0.00708   0.00161  -0.0737   0.5644   0.5146
  -1.500   0.1644   0.00710   0.00160  -0.0740   0.5609   0.5179
  -1.250   0.1941   0.00711   0.00159  -0.0744   0.5576   0.5210
  -1.000   0.2235   0.00710   0.00159  -0.0748   0.5543   0.5249
  -0.750   0.2529   0.00711   0.00160  -0.0752   0.5509   0.5281
  -0.500   0.2821   0.00714   0.00161  -0.0755   0.5476   0.5310
  -0.250   0.3114   0.00718   0.00162  -0.0758   0.5446   0.5339
   0.000   0.3410   0.00719   0.00163  -0.0762   0.5422   0.5365
   0.250   0.3705   0.00721   0.00165  -0.0766   0.5395   0.5389
   0.500   0.3999   0.00722   0.00168  -0.0770   0.5366   0.5419
   0.750   0.4292   0.00725   0.00171  -0.0773   0.5338   0.5450
   1.000   0.4583   0.00729   0.00174  -0.0776   0.5310   0.5482
   1.250   0.4873   0.00734   0.00179  -0.0779   0.5282   0.5513
   1.500   0.5167   0.00737   0.00183  -0.0783   0.5260   0.5543
   1.750   0.5460   0.00740   0.00187  -0.0787   0.5230   0.5572
   2.000   0.5751   0.00742   0.00192  -0.0790   0.5195   0.5608
   2.250   0.6041   0.00747   0.00198  -0.0793   0.5160   0.5645
   2.500   0.6327   0.00753   0.00205  -0.0795   0.5125   0.5683
   2.750   0.6616   0.00759   0.00211  -0.0798   0.5094   0.5720
   3.000   0.6908   0.00762   0.00218  -0.0802   0.5069   0.5758
   3.250   0.7197   0.00766   0.00225  -0.0805   0.5035   0.5803
   3.500   0.7479   0.00774   0.00233  -0.0806   0.4970   0.5849
   3.750   0.7762   0.00781   0.00241  -0.0808   0.4896   0.5892
   4.250   0.8318   0.00800   0.00260  -0.0810   0.4713   0.5974
   4.500   0.8593   0.00811   0.00270  -0.0811   0.4622   0.6023
   4.750   0.8871   0.00820   0.00281  -0.0812   0.4539   0.6071
   5.000   0.9136   0.00837   0.00294  -0.0811   0.4379   0.6113
   5.250   0.9366   0.00871   0.00315  -0.0805   0.3982   0.6162
   5.500   0.9527   0.00948   0.00361  -0.0787   0.3363   0.6215
   5.750   0.9711   0.01009   0.00403  -0.0774   0.2947   0.6266
   6.000   0.9880   0.01075   0.00448  -0.0758   0.2513   0.6312
   6.250   1.0045   0.01137   0.00494  -0.0742   0.2151   0.6368
   6.500   1.0216   0.01191   0.00536  -0.0726   0.1864   0.6426
   6.750   1.0382   0.01243   0.00578  -0.0710   0.1620   0.6479
   7.000   1.0521   0.01298   0.00623  -0.0689   0.1385   0.6536
   7.250   1.0620   0.01349   0.00666  -0.0660   0.1184   0.6599
   7.500   1.0709   0.01409   0.00718  -0.0630   0.1011   0.6664
   7.750   1.0800   0.01472   0.00777  -0.0603   0.0849   0.6732
   8.000   1.0900   0.01536   0.00837  -0.0578   0.0724   0.6804
   8.500   1.1130   0.01666   0.00964  -0.0537   0.0560   0.6939
   8.750   1.1248   0.01736   0.01034  -0.0519   0.0499   0.7011
   9.000   1.1365   0.01810   0.01109  -0.0502   0.0447   0.7077
   9.500   1.1608   0.01966   0.01269  -0.0471   0.0368   0.7227
   9.750   1.1723   0.02053   0.01359  -0.0456   0.0337   0.7300
  10.000   1.1847   0.02139   0.01448  -0.0443   0.0314   0.7382
  10.250   1.1965   0.02232   0.01544  -0.0430   0.0294   0.7457
  10.500   1.2085   0.02326   0.01643  -0.0418   0.0277   0.7544
  10.750   1.2194   0.02431   0.01752  -0.0405   0.0261   0.7629
  11.000   1.2314   0.02530   0.01857  -0.0395   0.0250   0.7732
  11.250   1.2426   0.02638   0.01970  -0.0384   0.0237   0.7827
  11.500   1.2530   0.02754   0.02091  -0.0373   0.0227   0.7927
  11.750   1.2635   0.02872   0.02216  -0.0363   0.0218   0.8034
  12.000   1.2742   0.02991   0.02342  -0.0354   0.0209   0.8157
  12.250   1.2839   0.03116   0.02475  -0.0344   0.0199   0.8309
  12.500   1.2927   0.03249   0.02616  -0.0334   0.0191   0.8495
  12.750   1.3011   0.03384   0.02761  -0.0324   0.0183   0.8712
  13.000   1.3097   0.03514   0.02901  -0.0313   0.0177   0.8949
  13.250   1.3167   0.03648   0.03049  -0.0301   0.0170   0.9368
  13.750   1.3376   0.03974   0.03384  -0.0300   0.0156   1.0000
  14.000   1.3475   0.04135   0.03549  -0.0296   0.0150   1.0000
  14.250   1.3563   0.04308   0.03726  -0.0293   0.0145   1.0000
  14.500   1.3647   0.04488   0.03909  -0.0290   0.0140   1.0000
  14.750   1.3729   0.04673   0.04098  -0.0288   0.0137   1.0000
  15.000   1.3802   0.04872   0.04300  -0.0287   0.0133   1.0000
  15.250   1.3876   0.05073   0.04506  -0.0285   0.0128   1.0000
  15.500   1.3952   0.05274   0.04712  -0.0285   0.0125   1.0000
  15.750   1.4026   0.05482   0.04924  -0.0285   0.0123   1.0000
  16.000   1.4094   0.05699   0.05147  -0.0286   0.0120   1.0000
  16.250   1.4156   0.05927   0.05379  -0.0287   0.0117   1.0000
  16.500   1.4216   0.06161   0.05618  -0.0289   0.0115   1.0000
  16.750   1.4269   0.06406   0.05868  -0.0292   0.0113   1.0000
  17.000   1.4316   0.06661   0.06128  -0.0296   0.0111   1.0000
  17.250   1.4352   0.06936   0.06409  -0.0300   0.0109   1.0000
  17.500   1.4381   0.07225   0.06704  -0.0305   0.0107   1.0000
  17.750   1.4422   0.07502   0.06987  -0.0311   0.0106   1.0000
  18.000   1.4455   0.07792   0.07284  -0.0317   0.0105   1.0000
  18.250   1.4489   0.08087   0.07585  -0.0325   0.0104   1.0000
  18.500   1.4512   0.08402   0.07908  -0.0333   0.0103   1.0000
  18.750   1.4536   0.08719   0.08232  -0.0342   0.0102   1.0000
  19.000   1.4544   0.09062   0.08583  -0.0353   0.0101   1.0000
  19.250   1.4557   0.09399   0.08927  -0.0364   0.0099   1.0000
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