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NACA 65(2)-415 (naca652415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 65(2)-415 (naca652415-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.62 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca652415-il-1000000.txt
Download as CSV file: xf-naca652415-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.8295   0.07759   0.07523  -0.0679   1.0000   0.0122
 -16.250  -0.8556   0.06891   0.06636  -0.0735   1.0000   0.0122
 -16.000  -0.8847   0.06080   0.05805  -0.0783   1.0000   0.0122
 -15.750  -0.9015   0.05531   0.05243  -0.0812   1.0000   0.0123
 -15.500  -0.9225   0.04981   0.04674  -0.0834   1.0000   0.0123
 -15.250  -0.9270   0.04669   0.04354  -0.0844   1.0000   0.0125
 -15.000  -0.9313   0.04374   0.04050  -0.0850   1.0000   0.0126
 -14.750  -0.9308   0.04147   0.03815  -0.0854   1.0000   0.0127
 -14.500  -0.9274   0.03959   0.03622  -0.0855   1.0000   0.0128
 -14.250  -0.9244   0.03779   0.03436  -0.0853   1.0000   0.0130
 -14.000  -0.9227   0.03592   0.03241  -0.0849   1.0000   0.0131
 -13.750  -0.9191   0.03437   0.03079  -0.0843   1.0000   0.0133
 -13.500  -0.9142   0.03309   0.02944  -0.0835   1.0000   0.0135
 -13.250  -0.9126   0.03158   0.02784  -0.0823   1.0000   0.0137
 -13.000  -0.9118   0.03019   0.02636  -0.0805   1.0000   0.0138
 -12.750  -0.8997   0.02916   0.02527  -0.0803   0.9933   0.0142
 -12.500  -0.8783   0.02742   0.02335  -0.0824   0.9846   0.0146
 -12.250  -0.8509   0.02602   0.02180  -0.0852   0.9774   0.0149
 -12.000  -0.8176   0.02508   0.02073  -0.0887   0.9710   0.0151
 -11.750  -0.7934   0.02231   0.01776  -0.0912   0.9614   0.0158
 -11.500  -0.7636   0.02143   0.01682  -0.0934   0.9485   0.0161
 -11.250  -0.7430   0.02077   0.01605  -0.0935   0.9320   0.0164
 -11.000  -0.7295   0.02026   0.01543  -0.0918   0.9162   0.0168
 -10.750  -0.7173   0.01974   0.01479  -0.0898   0.9029   0.0171
 -10.500  -0.7023   0.01921   0.01415  -0.0882   0.8922   0.0175
 -10.250  -0.6847   0.01875   0.01359  -0.0870   0.8823   0.0179
 -10.000  -0.6659   0.01836   0.01310  -0.0859   0.8735   0.0183
  -9.750  -0.6462   0.01799   0.01263  -0.0849   0.8647   0.0186
  -9.500  -0.6289   0.01675   0.01127  -0.0838   0.8569   0.0191
  -9.250  -0.6102   0.01603   0.01049  -0.0828   0.8489   0.0196
  -9.000  -0.5895   0.01558   0.01000  -0.0820   0.8420   0.0201
  -8.750  -0.5679   0.01518   0.00955  -0.0813   0.8346   0.0205
  -8.500  -0.5458   0.01483   0.00914  -0.0807   0.8280   0.0211
  -8.250  -0.5232   0.01444   0.00870  -0.0801   0.8210   0.0217
  -8.000  -0.5006   0.01408   0.00826  -0.0795   0.8144   0.0222
  -7.750  -0.4773   0.01370   0.00783  -0.0790   0.8084   0.0226
  -7.500  -0.4530   0.01344   0.00751  -0.0786   0.8022   0.0230
  -7.250  -0.4353   0.01252   0.00652  -0.0774   0.7961   0.0238
  -7.000  -0.4121   0.01210   0.00607  -0.0769   0.7901   0.0246
  -6.750  -0.3878   0.01181   0.00574  -0.0766   0.7842   0.0254
  -6.500  -0.3630   0.01151   0.00541  -0.0763   0.7788   0.0261
  -6.250  -0.3378   0.01122   0.00508  -0.0761   0.7733   0.0270
  -6.000  -0.3124   0.01097   0.00477  -0.0759   0.7681   0.0276
  -5.750  -0.2867   0.01071   0.00447  -0.0758   0.7631   0.0282
  -5.500  -0.2623   0.01024   0.00396  -0.0755   0.7578   0.0299
  -5.250  -0.2362   0.01002   0.00371  -0.0755   0.7527   0.0314
  -5.000  -0.2094   0.00983   0.00349  -0.0755   0.7480   0.0330
  -4.750  -0.1822   0.00965   0.00329  -0.0756   0.7433   0.0342
  -4.500  -0.1558   0.00936   0.00297  -0.0755   0.7387   0.0379
  -4.250  -0.1287   0.00921   0.00278  -0.0756   0.7341   0.0413
  -4.000  -0.1016   0.00894   0.00257  -0.0757   0.7299   0.0518
  -3.750  -0.0759   0.00844   0.00231  -0.0758   0.7253   0.1099
  -3.500  -0.0516   0.00768   0.00199  -0.0759   0.7209   0.2371
  -3.250  -0.0276   0.00667   0.00163  -0.0762   0.7169   0.4187
  -3.000  -0.0004   0.00620   0.00153  -0.0766   0.7131   0.5244
  -2.750   0.0282   0.00612   0.00150  -0.0769   0.7090   0.5573
  -2.500   0.0569   0.00610   0.00148  -0.0772   0.7050   0.5778
  -2.250   0.0859   0.00609   0.00147  -0.0775   0.7012   0.5907
  -2.000   0.1149   0.00607   0.00147  -0.0779   0.6976   0.6065
  -1.750   0.1438   0.00608   0.00151  -0.0781   0.6939   0.6253
  -1.500   0.1726   0.00614   0.00156  -0.0784   0.6903   0.6420
  -1.250   0.2016   0.00620   0.00158  -0.0787   0.6866   0.6505
  -1.000   0.2307   0.00618   0.00159  -0.0790   0.6834   0.6548
  -0.750   0.2599   0.00618   0.00158  -0.0794   0.6798   0.6582
  -0.500   0.2890   0.00621   0.00158  -0.0798   0.6764   0.6616
  -0.250   0.3181   0.00626   0.00158  -0.0801   0.6731   0.6648
   0.000   0.3470   0.00626   0.00160  -0.0805   0.6698   0.6684
   0.250   0.3761   0.00626   0.00162  -0.0808   0.6666   0.6717
   0.500   0.4052   0.00627   0.00164  -0.0812   0.6633   0.6754
   0.750   0.4342   0.00631   0.00166  -0.0816   0.6601   0.6789
   1.000   0.4631   0.00637   0.00169  -0.0819   0.6567   0.6823
   1.250   0.4920   0.00638   0.00174  -0.0822   0.6537   0.6859
   1.500   0.5210   0.00639   0.00178  -0.0826   0.6505   0.6898
   1.750   0.5499   0.00642   0.00183  -0.0829   0.6472   0.6937
   2.000   0.5787   0.00648   0.00187  -0.0832   0.6430   0.6971
   2.250   0.6070   0.00650   0.00192  -0.0835   0.6381   0.7011
   2.500   0.6355   0.00650   0.00197  -0.0837   0.6329   0.7052
   2.750   0.6637   0.00656   0.00201  -0.0839   0.6268   0.7095
   3.000   0.6919   0.00659   0.00206  -0.0841   0.6190   0.7134
   3.250   0.7190   0.00663   0.00210  -0.0840   0.6087   0.7178
   3.500   0.7463   0.00666   0.00214  -0.0840   0.5957   0.7222
   3.750   0.7736   0.00673   0.00220  -0.0840   0.5818   0.7267
   4.000   0.8007   0.00682   0.00228  -0.0840   0.5672   0.7312
   4.250   0.8273   0.00691   0.00238  -0.0839   0.5518   0.7361
   4.500   0.8528   0.00707   0.00250  -0.0836   0.5306   0.7411
   4.750   0.8766   0.00736   0.00266  -0.0830   0.4947   0.7459
   5.000   0.8937   0.00799   0.00300  -0.0813   0.4222   0.7510
   5.250   0.9045   0.00904   0.00360  -0.0786   0.3248   0.7567
   5.500   0.9153   0.01007   0.00419  -0.0759   0.2375   0.7624
   5.750   0.9259   0.01099   0.00477  -0.0732   0.1646   0.7685
   6.000   0.9369   0.01184   0.00533  -0.0706   0.1060   0.7751
   6.250   0.9493   0.01255   0.00586  -0.0682   0.0665   0.7813
   6.500   0.9613   0.01312   0.00632  -0.0656   0.0440   0.7881
   7.000   0.9909   0.01396   0.00716  -0.0613   0.0314   0.8022
   7.250   1.0050   0.01446   0.00766  -0.0592   0.0281   0.8103
   7.500   1.0210   0.01486   0.00813  -0.0574   0.0263   0.8183
   8.000   1.0491   0.01591   0.00926  -0.0534   0.0226   0.8361
   8.250   1.0637   0.01643   0.00986  -0.0516   0.0217   0.8455
   8.500   1.0791   0.01692   0.01041  -0.0500   0.0208   0.8559
   8.750   1.0931   0.01747   0.01103  -0.0482   0.0199   0.8671
   9.000   1.1062   0.01807   0.01169  -0.0463   0.0193   0.8799
   9.250   1.1151   0.01889   0.01259  -0.0438   0.0184   0.8958
   9.500   1.1206   0.01986   0.01367  -0.0410   0.0179   0.9163
   9.750   1.1313   0.02040   0.01433  -0.0387   0.0176   0.9451
  10.000   1.1483   0.02115   0.01517  -0.0381   0.0172   1.0000
  10.250   1.1627   0.02200   0.01605  -0.0371   0.0168   1.0000
  10.500   1.1767   0.02288   0.01697  -0.0360   0.0162   1.0000
  10.750   1.1893   0.02388   0.01800  -0.0348   0.0159   1.0000
  11.000   1.2026   0.02483   0.01898  -0.0338   0.0155   1.0000
  11.250   1.2137   0.02597   0.02015  -0.0326   0.0151   1.0000
  11.500   1.2191   0.02757   0.02179  -0.0309   0.0146   1.0000
  11.750   1.2224   0.02939   0.02369  -0.0292   0.0143   1.0000
  12.000   1.2340   0.03059   0.02494  -0.0282   0.0142   1.0000
  12.250   1.2472   0.03167   0.02608  -0.0275   0.0140   1.0000
  12.500   1.2578   0.03299   0.02746  -0.0265   0.0138   1.0000
  12.750   1.2675   0.03443   0.02896  -0.0256   0.0137   1.0000
  13.000   1.2777   0.03585   0.03044  -0.0248   0.0134   1.0000
  13.250   1.2868   0.03739   0.03204  -0.0240   0.0133   1.0000
  13.500   1.2967   0.03889   0.03360  -0.0233   0.0130   1.0000
  13.750   1.3055   0.04053   0.03531  -0.0226   0.0128   1.0000
  14.000   1.3134   0.04230   0.03715  -0.0220   0.0126   1.0000
  14.250   1.3224   0.04398   0.03888  -0.0215   0.0124   1.0000
  14.500   1.3295   0.04589   0.04086  -0.0210   0.0123   1.0000
  14.750   1.3372   0.04778   0.04281  -0.0206   0.0121   1.0000
  15.000   1.3440   0.04981   0.04489  -0.0203   0.0120   1.0000
  15.250   1.3488   0.05209   0.04724  -0.0200   0.0118   1.0000
  15.500   1.3531   0.05448   0.04971  -0.0197   0.0117   1.0000
  15.750   1.3516   0.05767   0.05302  -0.0192   0.0114   1.0000
  16.000   1.3530   0.06060   0.05608  -0.0191   0.0112   1.0000
  16.250   1.3559   0.06334   0.05892  -0.0193   0.0112   1.0000
  16.500   1.3581   0.06625   0.06194  -0.0196   0.0111   1.0000
  16.750   1.3592   0.06937   0.06518  -0.0200   0.0110   1.0000
  17.000   1.3596   0.07266   0.06859  -0.0206   0.0110   1.0000
  17.250   1.3589   0.07619   0.07224  -0.0215   0.0109   1.0000
  17.500   1.3561   0.08010   0.07628  -0.0225   0.0108   1.0000
  17.750   1.3519   0.08437   0.08068  -0.0237   0.0107   1.0000
  18.000   1.3468   0.08889   0.08533  -0.0252   0.0106   1.0000
  18.250   1.3400   0.09379   0.09038  -0.0270   0.0106   1.0000
  18.500   1.3317   0.09905   0.09579  -0.0292   0.0105   1.0000
  18.750   1.3213   0.10489   0.10177  -0.0319   0.0104   1.0000
  19.000   1.3111   0.11087   0.10790  -0.0348   0.0104   1.0000
  19.250   1.2971   0.11773   0.11493  -0.0384   0.0103   1.0000
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