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NACA 65(2)-415 (naca652415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 65(2)-415 (naca652415-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.92 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca652415-il-1000000-n5.txt
Download as CSV file: xf-naca652415-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 65(2)-415                                  
  
 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  -1.0231   0.07641   0.07356  -0.0675   1.0000   0.0088
 -18.250  -1.0473   0.06866   0.06565  -0.0720   1.0000   0.0089
 -18.000  -1.0645   0.06248   0.05934  -0.0755   1.0000   0.0089
 -17.750  -1.0764   0.05749   0.05423  -0.0781   1.0000   0.0090
 -17.500  -1.0852   0.05320   0.04982  -0.0800   1.0000   0.0090
 -17.250  -1.0906   0.04957   0.04609  -0.0815   1.0000   0.0092
 -17.000  -1.0915   0.04667   0.04311  -0.0825   1.0000   0.0092
 -16.750  -1.0902   0.04414   0.04051  -0.0832   1.0000   0.0094
 -16.500  -1.0901   0.04162   0.03790  -0.0837   1.0000   0.0095
 -16.250  -1.0861   0.03959   0.03581  -0.0839   1.0000   0.0097
 -16.000  -1.0835   0.03747   0.03361  -0.0840   1.0000   0.0098
 -15.750  -1.0768   0.03583   0.03189  -0.0839   1.0000   0.0100
 -15.500  -1.0728   0.03398   0.02995  -0.0837   1.0000   0.0100
 -15.250  -1.0647   0.03256   0.02847  -0.0834   1.0000   0.0103
 -15.000  -1.0563   0.03121   0.02705  -0.0830   1.0000   0.0105
 -14.750  -1.0501   0.02972   0.02548  -0.0823   1.0000   0.0107
 -14.500  -1.0401   0.02861   0.02430  -0.0816   1.0000   0.0109
 -14.250  -1.0319   0.02741   0.02303  -0.0807   1.0000   0.0110
 -14.000  -1.0250   0.02627   0.02181  -0.0792   0.9916   0.0111
 -13.750  -0.9979   0.02482   0.02028  -0.0823   0.9780   0.0115
 -13.500  -0.9632   0.02361   0.01899  -0.0863   0.9684   0.0117
 -13.250  -0.9266   0.02256   0.01788  -0.0903   0.9584   0.0120
 -13.000  -0.8914   0.02173   0.01696  -0.0938   0.9450   0.0123
 -12.750  -0.8663   0.02101   0.01614  -0.0950   0.9262   0.0126
 -12.500  -0.8496   0.02040   0.01541  -0.0944   0.9083   0.0129
 -12.250  -0.8361   0.01976   0.01465  -0.0931   0.8933   0.0132
 -12.000  -0.8223   0.01919   0.01398  -0.0917   0.8807   0.0134
 -11.750  -0.8092   0.01858   0.01327  -0.0902   0.8691   0.0136
 -11.500  -0.7942   0.01810   0.01270  -0.0888   0.8591   0.0138
 -11.250  -0.7794   0.01767   0.01217  -0.0873   0.8492   0.0140
 -11.000  -0.7687   0.01704   0.01146  -0.0852   0.8391   0.0143
 -10.750  -0.7573   0.01657   0.01092  -0.0830   0.8304   0.0147
 -10.500  -0.7406   0.01612   0.01041  -0.0817   0.8226   0.0149
 -10.250  -0.7217   0.01573   0.00996  -0.0807   0.8158   0.0152
 -10.000  -0.7013   0.01538   0.00956  -0.0799   0.8087   0.0155
  -9.500  -0.6591   0.01470   0.00876  -0.0784   0.7952   0.0162
  -9.250  -0.6377   0.01433   0.00833  -0.0777   0.7888   0.0165
  -9.000  -0.6151   0.01402   0.00796  -0.0772   0.7833   0.0169
  -8.750  -0.5923   0.01369   0.00757  -0.0767   0.7772   0.0172
  -8.500  -0.5696   0.01336   0.00717  -0.0761   0.7711   0.0174
  -8.250  -0.5470   0.01296   0.00672  -0.0756   0.7655   0.0177
  -8.000  -0.5241   0.01257   0.00630  -0.0751   0.7594   0.0183
  -7.750  -0.5000   0.01229   0.00598  -0.0748   0.7540   0.0188
  -7.500  -0.4752   0.01202   0.00568  -0.0746   0.7492   0.0193
  -7.250  -0.4502   0.01175   0.00537  -0.0744   0.7439   0.0197
  -7.000  -0.4252   0.01150   0.00507  -0.0741   0.7385   0.0201
  -6.750  -0.3995   0.01126   0.00479  -0.0740   0.7338   0.0206
  -6.500  -0.3736   0.01104   0.00454  -0.0740   0.7288   0.0210
  -6.250  -0.3475   0.01085   0.00430  -0.0739   0.7240   0.0214
  -6.000  -0.3218   0.01057   0.00398  -0.0738   0.7200   0.0222
  -5.750  -0.2954   0.01033   0.00374  -0.0738   0.7157   0.0231
  -5.500  -0.2687   0.01014   0.00352  -0.0738   0.7110   0.0239
  -5.250  -0.2419   0.00997   0.00332  -0.0738   0.7066   0.0248
  -5.000  -0.2147   0.00981   0.00314  -0.0740   0.7026   0.0258
  -4.750  -0.1873   0.00964   0.00296  -0.0741   0.6986   0.0268
  -4.500  -0.1601   0.00947   0.00278  -0.0742   0.6946   0.0291
  -4.250  -0.1327   0.00933   0.00262  -0.0743   0.6907   0.0314
  -4.000  -0.1050   0.00918   0.00248  -0.0745   0.6872   0.0347
  -3.750  -0.0772   0.00903   0.00234  -0.0747   0.6832   0.0393
  -3.500  -0.0496   0.00886   0.00220  -0.0749   0.6791   0.0506
  -3.250  -0.0224   0.00864   0.00205  -0.0751   0.6755   0.0749
  -3.000   0.0048   0.00835   0.00190  -0.0753   0.6723   0.1164
  -2.750   0.0319   0.00795   0.00174  -0.0756   0.6690   0.1842
  -2.500   0.0586   0.00743   0.00155  -0.0760   0.6654   0.2818
  -2.250   0.0851   0.00682   0.00133  -0.0765   0.6616   0.4000
  -1.750   0.1408   0.00618   0.00124  -0.0772   0.6552   0.5737
  -1.500   0.1698   0.00615   0.00126  -0.0776   0.6520   0.6000
  -1.250   0.1988   0.00614   0.00127  -0.0779   0.6488   0.6134
  -1.000   0.2278   0.00616   0.00126  -0.0782   0.6455   0.6178
  -0.500   0.2858   0.00618   0.00126  -0.0789   0.6393   0.6243
  -0.250   0.3150   0.00619   0.00127  -0.0793   0.6363   0.6276
   0.000   0.3441   0.00621   0.00128  -0.0797   0.6332   0.6308
   0.500   0.4017   0.00627   0.00132  -0.0803   0.6269   0.6370
   0.750   0.4308   0.00628   0.00135  -0.0807   0.6242   0.6402
   1.000   0.4599   0.00630   0.00138  -0.0810   0.6213   0.6436
   1.250   0.4889   0.00633   0.00142  -0.0814   0.6181   0.6472
   1.500   0.5177   0.00637   0.00146  -0.0817   0.6148   0.6503
   1.750   0.5462   0.00641   0.00151  -0.0820   0.6117   0.6537
   2.000   0.5750   0.00643   0.00156  -0.0823   0.6077   0.6571
   2.250   0.6036   0.00647   0.00161  -0.0825   0.6016   0.6609
   2.500   0.6315   0.00655   0.00167  -0.0827   0.5947   0.6646
   2.750   0.6599   0.00658   0.00173  -0.0829   0.5862   0.6681
   3.000   0.6872   0.00666   0.00180  -0.0829   0.5722   0.6718
   3.250   0.7141   0.00677   0.00187  -0.0829   0.5545   0.6756
   3.500   0.7393   0.00698   0.00198  -0.0825   0.5250   0.6795
   3.750   0.7613   0.00739   0.00216  -0.0817   0.4729   0.6834
   4.000   0.7767   0.00822   0.00258  -0.0797   0.3800   0.6876
   4.250   0.7918   0.00909   0.00307  -0.0778   0.2955   0.6921
   4.500   0.8084   0.00983   0.00350  -0.0761   0.2280   0.6964
   4.750   0.8261   0.01047   0.00389  -0.0746   0.1751   0.7002
   5.000   0.8437   0.01106   0.00429  -0.0731   0.1290   0.7046
   5.250   0.8608   0.01165   0.00470  -0.0715   0.0884   0.7095
   5.500   0.8795   0.01213   0.00506  -0.0701   0.0629   0.7144
   5.750   0.8983   0.01256   0.00542  -0.0688   0.0449   0.7192
   6.000   0.9179   0.01293   0.00576  -0.0675   0.0348   0.7244
   6.250   0.9372   0.01324   0.00606  -0.0662   0.0302   0.7295
   6.500   0.9546   0.01354   0.00637  -0.0645   0.0268   0.7344
   6.750   0.9729   0.01384   0.00670  -0.0630   0.0249   0.7399
   7.000   0.9905   0.01418   0.00706  -0.0615   0.0230   0.7459
   7.250   1.0075   0.01457   0.00747  -0.0598   0.0211   0.7518
   7.500   1.0254   0.01491   0.00786  -0.0584   0.0201   0.7586
   7.750   1.0425   0.01532   0.00829  -0.0569   0.0188   0.7652
   8.000   1.0585   0.01577   0.00878  -0.0553   0.0175   0.7718
   8.250   1.0750   0.01622   0.00927  -0.0538   0.0167   0.7790
   8.500   1.0916   0.01668   0.00977  -0.0524   0.0158   0.7858
   8.750   1.1075   0.01719   0.01032  -0.0509   0.0152   0.7939
   9.000   1.1230   0.01773   0.01091  -0.0495   0.0145   0.8017
   9.250   1.1371   0.01837   0.01159  -0.0479   0.0139   0.8111
   9.500   1.1518   0.01898   0.01226  -0.0464   0.0135   0.8198
   9.750   1.1671   0.01959   0.01294  -0.0451   0.0132   0.8292
  10.000   1.1814   0.02026   0.01367  -0.0436   0.0129   0.8386
  10.250   1.1954   0.02097   0.01445  -0.0422   0.0126   0.8491
  10.500   1.2089   0.02170   0.01525  -0.0408   0.0122   0.8615
  10.750   1.2212   0.02249   0.01613  -0.0393   0.0120   0.8759
  11.000   1.2334   0.02327   0.01699  -0.0377   0.0117   0.8932
  11.250   1.2435   0.02412   0.01793  -0.0359   0.0115   0.9156
  11.500   1.2539   0.02498   0.01892  -0.0342   0.0112   0.9534
  11.750   1.2667   0.02613   0.02013  -0.0335   0.0109   1.0000
  12.000   1.2775   0.02732   0.02136  -0.0324   0.0108   1.0000
  12.250   1.2900   0.02838   0.02248  -0.0314   0.0107   1.0000
  12.500   1.3014   0.02957   0.02371  -0.0305   0.0106   1.0000
  12.750   1.3131   0.03075   0.02495  -0.0296   0.0104   1.0000
  13.000   1.3236   0.03203   0.02629  -0.0287   0.0103   1.0000
  13.250   1.3341   0.03335   0.02767  -0.0279   0.0102   1.0000
  13.500   1.3444   0.03472   0.02909  -0.0271   0.0100   1.0000
  13.750   1.3548   0.03610   0.03053  -0.0264   0.0099   1.0000
  14.000   1.3635   0.03767   0.03215  -0.0257   0.0097   1.0000
  14.250   1.3727   0.03923   0.03377  -0.0250   0.0096   1.0000
  14.500   1.3809   0.04092   0.03553  -0.0244   0.0095   1.0000
  14.750   1.3891   0.04265   0.03733  -0.0239   0.0094   1.0000
  15.000   1.3965   0.04449   0.03923  -0.0235   0.0093   1.0000
  15.250   1.4035   0.04641   0.04122  -0.0231   0.0092   1.0000
  15.500   1.4105   0.04839   0.04325  -0.0228   0.0091   1.0000
  15.750   1.4162   0.05056   0.04549  -0.0225   0.0090   1.0000
  16.000   1.4211   0.05284   0.04785  -0.0224   0.0089   1.0000
  16.250   1.4250   0.05529   0.05037  -0.0223   0.0088   1.0000
  16.500   1.4278   0.05794   0.05310  -0.0223   0.0087   1.0000
  16.750   1.4293   0.06083   0.05607  -0.0225   0.0086   1.0000
  17.000   1.4288   0.06403   0.05937  -0.0228   0.0085   1.0000
  17.250   1.4274   0.06742   0.06285  -0.0232   0.0084   1.0000
  17.500   1.4247   0.07108   0.06662  -0.0238   0.0083   1.0000
  17.750   1.4251   0.07445   0.07008  -0.0246   0.0083   1.0000
  18.000   1.4245   0.07801   0.07375  -0.0255   0.0083   1.0000
  18.250   1.4228   0.08183   0.07768  -0.0266   0.0082   1.0000
  18.500   1.4224   0.08553   0.08148  -0.0278   0.0082   1.0000
  18.750   1.4187   0.08985   0.08591  -0.0293   0.0082   1.0000
  19.000   1.4150   0.09427   0.09043  -0.0310   0.0081   1.0000
  19.250   1.4113   0.09877   0.09506  -0.0328   0.0081   1.0000
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