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NACA 63(2)-615 (naca632615-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(2)-615 (naca632615-il)
Reynolds number: 1,000,000
Max Cl/Cd: 134.4 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca632615-il-1000000.txt
Download as CSV file: xf-naca632615-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)-615                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.7552   0.10643   0.10419  -0.0529   1.0000   0.0125
 -17.250  -0.8168   0.09042   0.08794  -0.0621   1.0000   0.0124
 -17.000  -0.8536   0.07983   0.07718  -0.0685   1.0000   0.0123
 -16.750  -0.8735   0.07254   0.06975  -0.0730   1.0000   0.0124
 -16.500  -0.8913   0.06591   0.06299  -0.0771   1.0000   0.0124
 -16.250  -0.9083   0.05982   0.05676  -0.0808   1.0000   0.0124
 -16.000  -0.9183   0.05502   0.05184  -0.0836   1.0000   0.0125
 -15.750  -0.9283   0.05057   0.04728  -0.0860   1.0000   0.0126
 -15.500  -0.9337   0.04692   0.04353  -0.0879   1.0000   0.0127
 -15.250  -0.9394   0.04344   0.03994  -0.0894   1.0000   0.0127
 -15.000  -0.9421   0.04045   0.03685  -0.0905   1.0000   0.0129
 -14.750  -0.9420   0.03792   0.03423  -0.0912   1.0000   0.0130
 -14.500  -0.9445   0.03529   0.03149  -0.0917   1.0000   0.0131
 -14.250  -0.9433   0.03319   0.02931  -0.0917   1.0000   0.0132
 -14.000  -0.9391   0.03154   0.02758  -0.0914   1.0000   0.0134
 -13.750  -0.9385   0.02982   0.02577  -0.0906   1.0000   0.0134
 -13.500  -0.9402   0.02822   0.02410  -0.0892   1.0000   0.0135
 -13.000  -0.9266   0.02400   0.01971  -0.0913   0.9951   0.0142
 -12.750  -0.9016   0.02267   0.01832  -0.0938   0.9882   0.0145
 -12.500  -0.8723   0.02153   0.01713  -0.0967   0.9830   0.0149
 -12.250  -0.8449   0.02046   0.01599  -0.0989   0.9741   0.0153
 -12.000  -0.8094   0.01948   0.01492  -0.1024   0.9700   0.0158
 -11.750  -0.7763   0.01865   0.01400  -0.1049   0.9613   0.0162
 -11.500  -0.7427   0.01763   0.01288  -0.1078   0.9517   0.0168
 -11.250  -0.7132   0.01671   0.01189  -0.1097   0.9377   0.0175
 -11.000  -0.6867   0.01624   0.01134  -0.1103   0.9232   0.0181
 -10.500  -0.6415   0.01539   0.01032  -0.1096   0.8968   0.0193
 -10.250  -0.6185   0.01503   0.00985  -0.1092   0.8861   0.0198
  -9.750  -0.5753   0.01393   0.00862  -0.1083   0.8658   0.0213
  -9.500  -0.5506   0.01365   0.00828  -0.1080   0.8571   0.0222
  -9.250  -0.5255   0.01336   0.00793  -0.1079   0.8487   0.0231
  -9.000  -0.4996   0.01317   0.00765  -0.1077   0.8407   0.0238
  -8.750  -0.4762   0.01256   0.00701  -0.1075   0.8327   0.0251
  -8.500  -0.4503   0.01231   0.00672  -0.1074   0.8253   0.0263
  -8.250  -0.4238   0.01205   0.00641  -0.1074   0.8181   0.0274
  -8.000  -0.3970   0.01187   0.00616  -0.1074   0.8109   0.0283
  -7.750  -0.3715   0.01136   0.00562  -0.1075   0.8042   0.0300
  -7.500  -0.3444   0.01112   0.00535  -0.1076   0.7972   0.0315
  -7.250  -0.3172   0.01095   0.00512  -0.1076   0.7907   0.0329
  -7.000  -0.2897   0.01064   0.00478  -0.1078   0.7843   0.0344
  -6.750  -0.2625   0.01032   0.00442  -0.1080   0.7776   0.0364
  -6.500  -0.2346   0.01013   0.00420  -0.1081   0.7715   0.0382
  -6.250  -0.2063   0.00997   0.00400  -0.1083   0.7649   0.0397
  -6.000  -0.1786   0.00965   0.00364  -0.1086   0.7586   0.0427
  -5.750  -0.1501   0.00946   0.00343  -0.1088   0.7526   0.0453
  -5.500  -0.1217   0.00927   0.00321  -0.1091   0.7461   0.0481
  -5.250  -0.0933   0.00906   0.00298  -0.1094   0.7402   0.0529
  -5.000  -0.0644   0.00884   0.00278  -0.1097   0.7342   0.0601
  -4.750  -0.0358   0.00860   0.00257  -0.1101   0.7279   0.0746
  -4.500  -0.0069   0.00827   0.00236  -0.1106   0.7220   0.1087
  -4.250   0.0223   0.00788   0.00215  -0.1113   0.7159   0.1601
  -4.000   0.0515   0.00746   0.00195  -0.1120   0.7099   0.2268
  -3.750   0.0813   0.00695   0.00175  -0.1129   0.7041   0.3166
  -3.500   0.1111   0.00662   0.00163  -0.1137   0.6979   0.3904
  -3.250   0.1404   0.00651   0.00157  -0.1141   0.6920   0.4279
  -3.000   0.1701   0.00642   0.00154  -0.1145   0.6865   0.4535
  -2.750   0.1995   0.00639   0.00151  -0.1149   0.6804   0.4735
  -2.500   0.2287   0.00638   0.00149  -0.1151   0.6745   0.4890
  -2.250   0.2584   0.00635   0.00147  -0.1155   0.6688   0.5027
  -2.000   0.2877   0.00634   0.00148  -0.1158   0.6630   0.5211
  -1.750   0.3169   0.00636   0.00149  -0.1161   0.6574   0.5374
  -1.500   0.3464   0.00635   0.00149  -0.1164   0.6516   0.5473
  -1.000   0.4047   0.00640   0.00152  -0.1169   0.6403   0.5678
  -0.750   0.4341   0.00642   0.00153  -0.1172   0.6346   0.5757
  -0.500   0.4630   0.00645   0.00155  -0.1174   0.6287   0.5828
  -0.250   0.4922   0.00650   0.00157  -0.1177   0.6234   0.5898
   0.000   0.5215   0.00651   0.00160  -0.1180   0.6177   0.5967
   0.250   0.5503   0.00656   0.00163  -0.1182   0.6119   0.6036
   0.500   0.5794   0.00660   0.00167  -0.1185   0.6065   0.6098
   0.750   0.6085   0.00662   0.00171  -0.1187   0.6008   0.6164
   1.000   0.6371   0.00670   0.00175  -0.1189   0.5948   0.6229
   1.250   0.6662   0.00673   0.00180  -0.1192   0.5894   0.6290
   1.500   0.6951   0.00677   0.00186  -0.1194   0.5834   0.6355
   1.750   0.7234   0.00688   0.00192  -0.1195   0.5775   0.6420
   2.000   0.7526   0.00689   0.00199  -0.1198   0.5722   0.6484
   2.250   0.7812   0.00695   0.00206  -0.1200   0.5663   0.6550
   2.500   0.8095   0.00705   0.00214  -0.1201   0.5604   0.6615
   2.750   0.8383   0.00708   0.00222  -0.1204   0.5540   0.6684
   3.000   0.8661   0.00720   0.00231  -0.1204   0.5462   0.6752
   3.250   0.8947   0.00724   0.00239  -0.1206   0.5387   0.6816
   3.500   0.9225   0.00735   0.00249  -0.1207   0.5309   0.6886
   3.750   0.9509   0.00742   0.00259  -0.1208   0.5237   0.6955
   4.000   0.9783   0.00754   0.00271  -0.1208   0.5144   0.7025
   4.250   1.0061   0.00764   0.00281  -0.1209   0.5031   0.7097
   4.500   1.0333   0.00776   0.00294  -0.1208   0.4911   0.7163
   4.750   1.0601   0.00792   0.00308  -0.1207   0.4783   0.7238
   5.000   1.0866   0.00810   0.00323  -0.1205   0.4627   0.7309
   5.250   1.1128   0.00828   0.00340  -0.1204   0.4472   0.7381
   5.750   1.1646   0.00871   0.00378  -0.1199   0.4147   0.7528
   6.000   1.1894   0.00900   0.00401  -0.1195   0.3920   0.7606
   6.250   1.2121   0.00940   0.00431  -0.1187   0.3615   0.7679
   6.500   1.2321   0.01001   0.00472  -0.1176   0.3197   0.7761
   6.750   1.2495   0.01076   0.00525  -0.1161   0.2712   0.7840
   7.000   1.2649   0.01163   0.00585  -0.1142   0.2207   0.7927
   7.250   1.2796   0.01247   0.00647  -0.1123   0.1769   0.8011
   7.500   1.2939   0.01329   0.00709  -0.1103   0.1405   0.8107
   7.750   1.3082   0.01402   0.00769  -0.1082   0.1121   0.8203
   8.000   1.3218   0.01472   0.00828  -0.1061   0.0898   0.8306
   8.250   1.3329   0.01532   0.00883  -0.1034   0.0732   0.8425
   8.500   1.3419   0.01599   0.00946  -0.1004   0.0591   0.8560
   8.750   1.3512   0.01665   0.01011  -0.0975   0.0490   0.8719
   9.250   1.3695   0.01781   0.01139  -0.0918   0.0389   0.9222
   9.500   1.3765   0.01836   0.01202  -0.0887   0.0361   1.0000
   9.750   1.3895   0.01915   0.01281  -0.0870   0.0334   1.0000
  10.000   1.4035   0.01990   0.01359  -0.0856   0.0315   1.0000
  10.250   1.4150   0.02083   0.01453  -0.0839   0.0296   1.0000
  10.500   1.4268   0.02179   0.01551  -0.0824   0.0280   1.0000
  10.750   1.4403   0.02265   0.01642  -0.0811   0.0268   1.0000
  11.000   1.4516   0.02370   0.01748  -0.0797   0.0254   1.0000
  11.250   1.4589   0.02507   0.01888  -0.0780   0.0237   1.0000
  11.500   1.4723   0.02605   0.01991  -0.0769   0.0228   1.0000
  11.750   1.4835   0.02722   0.02112  -0.0758   0.0216   1.0000
  12.000   1.4915   0.02868   0.02259  -0.0745   0.0203   1.0000
  12.250   1.4995   0.03020   0.02416  -0.0732   0.0192   1.0000
  12.500   1.5099   0.03155   0.02557  -0.0723   0.0183   1.0000
  12.750   1.5188   0.03307   0.02712  -0.0713   0.0174   1.0000
  13.000   1.5240   0.03495   0.02903  -0.0702   0.0166   1.0000
  13.250   1.5287   0.03694   0.03110  -0.0692   0.0159   1.0000
  13.500   1.5374   0.03862   0.03283  -0.0685   0.0154   1.0000
  13.750   1.5453   0.04040   0.03467  -0.0679   0.0149   1.0000
  14.000   1.5520   0.04236   0.03667  -0.0673   0.0143   1.0000
  14.250   1.5572   0.04452   0.03889  -0.0668   0.0139   1.0000
  14.500   1.5587   0.04717   0.04160  -0.0663   0.0134   1.0000
  14.750   1.5579   0.05016   0.04467  -0.0658   0.0131   1.0000
  15.000   1.5634   0.05251   0.04710  -0.0656   0.0129   1.0000
  15.250   1.5683   0.05499   0.04965  -0.0655   0.0126   1.0000
  15.500   1.5718   0.05769   0.05243  -0.0655   0.0124   1.0000
  15.750   1.5746   0.06053   0.05534  -0.0656   0.0121   1.0000
  16.000   1.5769   0.06352   0.05842  -0.0658   0.0119   1.0000
  16.250   1.5790   0.06660   0.06157  -0.0662   0.0117   1.0000
  16.500   1.5804   0.06983   0.06487  -0.0666   0.0115   1.0000
  16.750   1.5805   0.07329   0.06841  -0.0672   0.0113   1.0000
  17.000   1.5789   0.07708   0.07229  -0.0679   0.0112   1.0000
  17.250   1.5760   0.08115   0.07644  -0.0688   0.0110   1.0000
  17.500   1.5709   0.08564   0.08102  -0.0700   0.0108   1.0000
  17.750   1.5630   0.09063   0.08611  -0.0714   0.0107   1.0000
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