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NACA 65(1)-212 a=0.6 (naca651212a06-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 65(1)-212 a=0.6 (naca651212a06-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.74 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca651212a06-il-1000000-n5.txt
Download as CSV file: xf-naca651212a06-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 65(1)-212 a=0.6                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -1.0513   0.06033   0.05803  -0.0482   1.0000   0.0059
 -15.750  -1.0746   0.05335   0.05087  -0.0524   1.0000   0.0059
 -15.500  -1.0958   0.04753   0.04487  -0.0552   1.0000   0.0060
 -15.250  -1.1142   0.04267   0.03983  -0.0569   1.0000   0.0060
 -15.000  -1.1231   0.03926   0.03627  -0.0574   1.0000   0.0060
 -14.750  -1.1319   0.03612   0.03298  -0.0573   1.0000   0.0061
 -14.500  -1.1344   0.03379   0.03053  -0.0568   1.0000   0.0062
 -14.250  -1.1311   0.03212   0.02878  -0.0561   1.0000   0.0064
 -14.000  -1.1295   0.03043   0.02698  -0.0548   1.0000   0.0065
 -13.750  -1.1245   0.02908   0.02554  -0.0533   1.0000   0.0066
 -13.500  -1.1168   0.02801   0.02439  -0.0518   1.0000   0.0067
 -13.000  -1.0892   0.02585   0.02201  -0.0508   0.9591   0.0070
 -12.750  -1.0776   0.02496   0.02097  -0.0493   0.9327   0.0071
 -12.500  -1.0682   0.02430   0.02017  -0.0469   0.9160   0.0073
 -12.250  -1.0559   0.02347   0.01920  -0.0451   0.9026   0.0075
 -12.000  -1.0403   0.02282   0.01842  -0.0437   0.8909   0.0077
 -11.750  -1.0237   0.02212   0.01759  -0.0424   0.8809   0.0080
 -11.500  -1.0070   0.02135   0.01668  -0.0412   0.8720   0.0081
 -11.250  -0.9891   0.02060   0.01579  -0.0401   0.8632   0.0083
 -11.000  -0.9699   0.01994   0.01499  -0.0392   0.8553   0.0084
 -10.750  -0.9525   0.01901   0.01393  -0.0380   0.8472   0.0087
 -10.500  -0.9315   0.01845   0.01329  -0.0373   0.8407   0.0090
 -10.250  -0.9097   0.01793   0.01271  -0.0367   0.8338   0.0092
 -10.000  -0.8873   0.01750   0.01219  -0.0362   0.8274   0.0094
  -9.750  -0.8640   0.01708   0.01170  -0.0357   0.8212   0.0097
  -9.500  -0.8411   0.01661   0.01114  -0.0352   0.8150   0.0100
  -9.250  -0.8176   0.01617   0.01062  -0.0348   0.8097   0.0103
  -9.000  -0.7940   0.01571   0.01008  -0.0344   0.8037   0.0106
  -8.750  -0.7698   0.01535   0.00963  -0.0340   0.7981   0.0110
  -8.500  -0.7456   0.01492   0.00913  -0.0337   0.7931   0.0112
  -8.250  -0.7209   0.01454   0.00868  -0.0334   0.7877   0.0114
  -8.000  -0.6990   0.01380   0.00782  -0.0326   0.7825   0.0118
  -7.750  -0.6748   0.01333   0.00730  -0.0323   0.7778   0.0122
  -7.500  -0.6496   0.01300   0.00694  -0.0321   0.7729   0.0126
  -7.250  -0.6243   0.01268   0.00658  -0.0318   0.7684   0.0129
  -7.000  -0.5985   0.01241   0.00626  -0.0317   0.7642   0.0134
  -6.750  -0.5730   0.01206   0.00586  -0.0315   0.7597   0.0138
  -6.500  -0.5474   0.01173   0.00548  -0.0312   0.7550   0.0142
  -6.000  -0.4955   0.01113   0.00477  -0.0309   0.7471   0.0149
  -5.750  -0.4689   0.01091   0.00451  -0.0308   0.7432   0.0152
  -5.500  -0.4436   0.01049   0.00404  -0.0306   0.7391   0.0161
  -5.250  -0.4173   0.01024   0.00374  -0.0305   0.7353   0.0168
  -5.000  -0.3904   0.01000   0.00349  -0.0304   0.7316   0.0175
  -4.750  -0.3634   0.00980   0.00326  -0.0304   0.7277   0.0182
  -4.500  -0.3363   0.00960   0.00304  -0.0304   0.7241   0.0190
  -4.250  -0.3091   0.00943   0.00283  -0.0304   0.7207   0.0198
  -4.000  -0.2818   0.00925   0.00262  -0.0305   0.7176   0.0206
  -3.750  -0.2545   0.00904   0.00241  -0.0305   0.7140   0.0225
  -3.500  -0.2270   0.00888   0.00225  -0.0305   0.7103   0.0246
  -3.250  -0.1994   0.00876   0.00210  -0.0306   0.7068   0.0264
  -3.000  -0.1718   0.00863   0.00195  -0.0307   0.7037   0.0292
  -2.750  -0.1440   0.00847   0.00182  -0.0308   0.7007   0.0334
  -2.500  -0.1162   0.00834   0.00170  -0.0309   0.6972   0.0397
  -2.250  -0.0890   0.00812   0.00157  -0.0310   0.6936   0.0659
  -2.000  -0.0629   0.00775   0.00142  -0.0309   0.6903   0.1345
  -1.750  -0.0370   0.00730   0.00127  -0.0309   0.6874   0.2259
  -1.500  -0.0139   0.00647   0.00106  -0.0305   0.6841   0.4052
  -1.250   0.0107   0.00595   0.00098  -0.0302   0.6805   0.5360
  -1.000   0.0377   0.00579   0.00098  -0.0301   0.6771   0.5916
  -0.750   0.0650   0.00569   0.00098  -0.0301   0.6740   0.6256
  -0.500   0.0933   0.00564   0.00098  -0.0303   0.6708   0.6415
  -0.250   0.1217   0.00561   0.00098  -0.0304   0.6673   0.6551
   0.000   0.1501   0.00560   0.00098  -0.0306   0.6638   0.6645
   0.250   0.1786   0.00561   0.00098  -0.0308   0.6604   0.6699
   0.500   0.2072   0.00561   0.00099  -0.0310   0.6573   0.6758
   0.750   0.2359   0.00561   0.00101  -0.0313   0.6539   0.6817
   1.000   0.2644   0.00561   0.00103  -0.0315   0.6502   0.6876
   1.250   0.2928   0.00562   0.00105  -0.0317   0.6466   0.6941
   1.500   0.3213   0.00563   0.00108  -0.0319   0.6424   0.7003
   1.750   0.3495   0.00563   0.00112  -0.0320   0.6347   0.7074
   2.250   0.4053   0.00571   0.00119  -0.0322   0.6086   0.7220
   2.750   0.4582   0.00605   0.00133  -0.0319   0.5389   0.7386
   3.000   0.4812   0.00659   0.00154  -0.0313   0.4503   0.7464
   3.250   0.5007   0.00752   0.00194  -0.0303   0.3226   0.7542
   3.500   0.5205   0.00840   0.00234  -0.0294   0.2084   0.7607
   3.750   0.5418   0.00907   0.00268  -0.0286   0.1264   0.7669
   4.000   0.5645   0.00963   0.00299  -0.0281   0.0690   0.7721
   4.250   0.5883   0.01001   0.00324  -0.0276   0.0397   0.7761
   4.500   0.6136   0.01026   0.00346  -0.0273   0.0307   0.7804
   4.750   0.6395   0.01047   0.00366  -0.0272   0.0274   0.7846
   5.000   0.6646   0.01069   0.00388  -0.0269   0.0240   0.7883
   5.250   0.6897   0.01089   0.00411  -0.0266   0.0218   0.7922
   5.500   0.7148   0.01110   0.00433  -0.0263   0.0199   0.7960
   6.000   0.7632   0.01161   0.00487  -0.0254   0.0164   0.8033
   6.250   0.7871   0.01183   0.00514  -0.0249   0.0155   0.8080
   6.750   0.8321   0.01232   0.00577  -0.0233   0.0139   0.8229
   7.000   0.8498   0.01272   0.00632  -0.0214   0.0131   0.8394
   7.250   0.8715   0.01323   0.00686  -0.0206   0.0124   0.8871
   7.500   0.8944   0.01357   0.00721  -0.0201   0.0122   0.8917
   7.750   0.9163   0.01395   0.00761  -0.0193   0.0119   0.8957
   8.000   0.9371   0.01439   0.00807  -0.0184   0.0116   0.8986
   8.250   0.9564   0.01480   0.00853  -0.0172   0.0114   0.9007
   8.500   0.9749   0.01524   0.00902  -0.0158   0.0110   0.9028
   8.750   0.9922   0.01567   0.00950  -0.0143   0.0108   0.9047
   9.000   1.0072   0.01611   0.00998  -0.0123   0.0107   0.9065
   9.250   1.0217   0.01663   0.01052  -0.0104   0.0105   0.9081
   9.500   1.0354   0.01717   0.01111  -0.0084   0.0103   0.9096
   9.750   1.0499   0.01769   0.01168  -0.0066   0.0101   0.9111
  10.000   1.0629   0.01835   0.01240  -0.0047   0.0100   0.9124
  10.250   1.0770   0.01897   0.01307  -0.0030   0.0098   0.9137
  10.500   1.0891   0.01975   0.01390  -0.0012   0.0095   0.9151
  10.750   1.1001   0.02064   0.01486   0.0007   0.0094   0.9170
  11.000   1.1083   0.02179   0.01609   0.0028   0.0091   0.9188
  11.250   1.1220   0.02252   0.01688   0.0042   0.0091   0.9206
  11.500   1.1369   0.02315   0.01758   0.0054   0.0089   0.9222
  11.750   1.1482   0.02412   0.01865   0.0069   0.0089   0.9235
  12.000   1.1596   0.02511   0.01973   0.0084   0.0088   0.9248
  12.250   1.1718   0.02605   0.02075   0.0096   0.0087   0.9260
  12.500   1.1832   0.02709   0.02187   0.0108   0.0086   0.9267
  12.750   1.1950   0.02812   0.02298   0.0119   0.0084   0.9270
  13.000   1.2045   0.02942   0.02437   0.0131   0.0083   0.9271
  13.250   1.2173   0.03036   0.02538   0.0139   0.0081   0.9272
  13.500   1.2243   0.03193   0.02705   0.0151   0.0080   0.9272
  13.750   1.2355   0.03305   0.02823   0.0158   0.0078   0.9273
  14.000   1.2438   0.03447   0.02976   0.0167   0.0077   0.9275
  14.250   1.2509   0.03607   0.03144   0.0175   0.0076   0.9275
  14.500   1.2593   0.03752   0.03297   0.0181   0.0074   0.9275
  14.750   1.2660   0.03920   0.03473   0.0186   0.0073   0.9274
  15.000   1.2723   0.04093   0.03653   0.0191   0.0072   0.9273
  15.250   1.2743   0.04319   0.03891   0.0196   0.0072   0.9272
  15.500   1.2776   0.04536   0.04117   0.0198   0.0071   0.9271
  15.750   1.2811   0.04759   0.04348   0.0199   0.0069   0.9269
  16.000   1.2835   0.05002   0.04599   0.0198   0.0069   0.9268
  16.250   1.2787   0.05342   0.04952   0.0195   0.0068   0.9266
  16.500   1.2726   0.05718   0.05340   0.0189   0.0067   0.9265
  16.750   1.2567   0.06242   0.05883   0.0176   0.0065   0.9263
  17.000   1.2479   0.06705   0.06361   0.0161   0.0065   0.9261
  17.250   1.2518   0.06996   0.06659   0.0149   0.0065   0.9260
  17.500   1.2379   0.07580   0.07261   0.0124   0.0065   0.9258
  17.750   1.2367   0.07986   0.07678   0.0104   0.0064   0.9257
  18.000   1.2186   0.08712   0.08421   0.0066   0.0064   0.9255
  18.250   1.1947   0.09597   0.09324   0.0016   0.0064   0.9254
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