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NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(3)-618 (naca633618-il)
Reynolds number: 1,000,000
Max Cl/Cd: 133.17 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633618-il-1000000.txt
Download as CSV file: xf-naca633618-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(3)-618                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.9337   0.09845   0.09521  -0.0633   1.0000   0.0152
 -19.500  -0.9489   0.09246   0.08912  -0.0665   1.0000   0.0153
 -19.250  -0.9621   0.08687   0.08345  -0.0695   1.0000   0.0154
 -19.000  -0.9770   0.08114   0.07764  -0.0725   1.0000   0.0155
 -18.750  -0.9868   0.07624   0.07265  -0.0751   1.0000   0.0157
 -18.500  -0.9958   0.07161   0.06794  -0.0774   1.0000   0.0159
 -18.250  -1.0017   0.06751   0.06376  -0.0795   1.0000   0.0160
 -18.000  -1.0061   0.06370   0.05987  -0.0813   1.0000   0.0161
 -17.750  -1.0082   0.06023   0.05634  -0.0829   1.0000   0.0165
 -17.500  -1.0111   0.05681   0.05284  -0.0844   1.0000   0.0166
 -17.250  -1.0114   0.05376   0.04972  -0.0857   1.0000   0.0169
 -17.000  -1.0112   0.05086   0.04675  -0.0868   1.0000   0.0171
 -16.750  -1.0062   0.04859   0.04442  -0.0876   1.0000   0.0174
 -16.500  -1.0034   0.04612   0.04187  -0.0884   1.0000   0.0176
 -16.250  -1.0032   0.04348   0.03916  -0.0891   1.0000   0.0179
 -16.000  -1.0077   0.04047   0.03611  -0.0899   1.0000   0.0184
 -15.750  -1.0052   0.03831   0.03391  -0.0902   1.0000   0.0187
 -15.500  -1.0017   0.03635   0.03190  -0.0903   1.0000   0.0190
 -15.250  -0.9967   0.03459   0.03011  -0.0903   1.0000   0.0194
 -15.000  -0.9909   0.03299   0.02847  -0.0900   1.0000   0.0198
 -14.750  -0.9846   0.03153   0.02696  -0.0896   1.0000   0.0203
 -14.500  -0.9795   0.03010   0.02548  -0.0889   1.0000   0.0206
 -14.250  -0.9738   0.02888   0.02422  -0.0878   1.0000   0.0210
 -14.000  -0.9561   0.02679   0.02211  -0.0904   0.9899   0.0218
 -13.750  -0.9282   0.02549   0.02079  -0.0934   0.9776   0.0227
 -13.500  -0.8918   0.02433   0.01958  -0.0975   0.9665   0.0237
 -13.250  -0.8482   0.02323   0.01840  -0.1030   0.9576   0.0246
 -13.000  -0.8029   0.02174   0.01689  -0.1097   0.9454   0.0261
 -12.750  -0.7587   0.02096   0.01602  -0.1147   0.9282   0.0275
 -12.500  -0.7300   0.02043   0.01535  -0.1162   0.9060   0.0284
 -12.250  -0.7232   0.01930   0.01409  -0.1151   0.8840   0.0292
 -12.000  -0.7123   0.01854   0.01327  -0.1139   0.8682   0.0301
 -11.750  -0.6989   0.01793   0.01259  -0.1128   0.8554   0.0310
 -11.500  -0.6858   0.01734   0.01192  -0.1115   0.8441   0.0318
 -11.250  -0.6719   0.01682   0.01132  -0.1102   0.8335   0.0326
 -11.000  -0.6616   0.01622   0.01064  -0.1084   0.8239   0.0331
 -10.750  -0.6580   0.01546   0.00982  -0.1060   0.8137   0.0341
 -10.500  -0.6410   0.01497   0.00929  -0.1051   0.8062   0.0351
 -10.250  -0.6206   0.01462   0.00889  -0.1045   0.7986   0.0362
 -10.000  -0.5991   0.01432   0.00851  -0.1039   0.7916   0.0372
  -9.750  -0.5759   0.01403   0.00818  -0.1036   0.7849   0.0380
  -9.500  -0.5564   0.01347   0.00758  -0.1030   0.7781   0.0395
  -9.250  -0.5332   0.01312   0.00719  -0.1027   0.7719   0.0407
  -9.000  -0.5085   0.01283   0.00687  -0.1025   0.7656   0.0419
  -8.750  -0.4832   0.01260   0.00658  -0.1023   0.7592   0.0431
  -8.500  -0.4589   0.01222   0.00616  -0.1022   0.7533   0.0448
  -8.250  -0.4334   0.01188   0.00582  -0.1022   0.7473   0.0467
  -8.000  -0.4072   0.01165   0.00554  -0.1022   0.7412   0.0485
  -7.750  -0.3806   0.01142   0.00526  -0.1022   0.7356   0.0504
  -7.500  -0.3540   0.01108   0.00493  -0.1024   0.7297   0.0534
  -7.250  -0.3269   0.01087   0.00468  -0.1025   0.7240   0.0562
  -7.000  -0.2999   0.01058   0.00438  -0.1027   0.7184   0.0611
  -6.750  -0.2722   0.01030   0.00412  -0.1029   0.7129   0.0679
  -6.500  -0.2448   0.00999   0.00385  -0.1032   0.7071   0.0796
  -6.250  -0.2173   0.00969   0.00359  -0.1035   0.7016   0.0977
  -6.000  -0.1891   0.00933   0.00334  -0.1040   0.6967   0.1227
  -5.750  -0.1609   0.00897   0.00310  -0.1044   0.6910   0.1530
  -5.500  -0.1327   0.00862   0.00286  -0.1049   0.6853   0.1886
  -5.250  -0.1037   0.00819   0.00261  -0.1056   0.6806   0.2369
  -5.000  -0.0745   0.00777   0.00238  -0.1064   0.6754   0.2900
  -4.750  -0.0452   0.00743   0.00220  -0.1071   0.6701   0.3422
  -4.500  -0.0156   0.00722   0.00210  -0.1077   0.6650   0.3841
  -4.250   0.0144   0.00709   0.00203  -0.1082   0.6600   0.4100
  -4.000   0.0441   0.00703   0.00197  -0.1086   0.6547   0.4274
  -3.750   0.0736   0.00703   0.00193  -0.1090   0.6495   0.4409
  -3.500   0.1037   0.00697   0.00190  -0.1095   0.6453   0.4536
  -3.250   0.1336   0.00693   0.00188  -0.1099   0.6403   0.4660
  -3.000   0.1632   0.00694   0.00186  -0.1103   0.6351   0.4796
  -2.750   0.1928   0.00696   0.00186  -0.1106   0.6302   0.4905
  -2.500   0.2228   0.00693   0.00185  -0.1111   0.6256   0.4990
  -2.250   0.2525   0.00694   0.00185  -0.1114   0.6208   0.5061
  -2.000   0.2819   0.00699   0.00184  -0.1117   0.6160   0.5124
  -1.750   0.3116   0.00699   0.00186  -0.1121   0.6117   0.5207
  -1.500   0.3415   0.00702   0.00186  -0.1125   0.6072   0.5274
  -1.250   0.3710   0.00702   0.00187  -0.1129   0.6023   0.5333
  -1.000   0.4001   0.00707   0.00189  -0.1131   0.5971   0.5386
  -0.750   0.4300   0.00709   0.00190  -0.1136   0.5933   0.5437
  -0.500   0.4597   0.00711   0.00191  -0.1139   0.5890   0.5486
  -0.250   0.4891   0.00713   0.00194  -0.1143   0.5844   0.5542
   0.000   0.5180   0.00721   0.00199  -0.1145   0.5794   0.5595
   0.250   0.5478   0.00723   0.00201  -0.1149   0.5756   0.5641
   0.500   0.5774   0.00724   0.00204  -0.1153   0.5713   0.5695
   0.750   0.6065   0.00729   0.00209  -0.1156   0.5668   0.5744
   1.000   0.6352   0.00738   0.00215  -0.1158   0.5618   0.5791
   1.250   0.6649   0.00741   0.00218  -0.1162   0.5580   0.5832
   1.500   0.6942   0.00743   0.00224  -0.1165   0.5534   0.5889
   1.750   0.7229   0.00750   0.00230  -0.1168   0.5485   0.5940
   2.000   0.7516   0.00759   0.00237  -0.1170   0.5439   0.5987
   2.250   0.7810   0.00762   0.00243  -0.1173   0.5399   0.6032
   2.500   0.8100   0.00766   0.00250  -0.1176   0.5353   0.6084
   2.750   0.8383   0.00775   0.00258  -0.1178   0.5306   0.6138
   3.000   0.8669   0.00784   0.00267  -0.1180   0.5262   0.6189
   3.250   0.8960   0.00787   0.00275  -0.1183   0.5220   0.6243
   3.500   0.9245   0.00794   0.00284  -0.1185   0.5170   0.6296
   3.750   0.9521   0.00808   0.00295  -0.1186   0.5113   0.6350
   4.000   0.9809   0.00813   0.00303  -0.1189   0.5062   0.6398
   4.250   1.0090   0.00820   0.00314  -0.1190   0.4997   0.6455
   4.500   1.0361   0.00834   0.00326  -0.1190   0.4933   0.6514
   4.750   1.0647   0.00840   0.00336  -0.1192   0.4879   0.6570
   5.000   1.0921   0.00850   0.00349  -0.1192   0.4812   0.6629
   5.250   1.1193   0.00862   0.00363  -0.1192   0.4746   0.6688
   5.500   1.1467   0.00873   0.00375  -0.1193   0.4667   0.6745
   5.750   1.1730   0.00889   0.00390  -0.1191   0.4577   0.6803
   6.000   1.1994   0.00902   0.00406  -0.1190   0.4477   0.6866
   6.250   1.2252   0.00920   0.00422  -0.1188   0.4358   0.6930
   6.500   1.2499   0.00942   0.00442  -0.1184   0.4224   0.6990
   6.750   1.2741   0.00966   0.00464  -0.1179   0.4098   0.7053
   7.000   1.2987   0.00988   0.00485  -0.1174   0.3968   0.7118
   7.250   1.3218   0.01015   0.00510  -0.1168   0.3813   0.7182
   7.500   1.3426   0.01052   0.00542  -0.1158   0.3619   0.7250
   7.750   1.3613   0.01099   0.00579  -0.1144   0.3365   0.7315
   8.000   1.3760   0.01158   0.00626  -0.1124   0.3087   0.7383
   8.250   1.3868   0.01224   0.00679  -0.1097   0.2810   0.7458
   8.500   1.3946   0.01286   0.00732  -0.1064   0.2559   0.7530
   8.750   1.3999   0.01363   0.00798  -0.1028   0.2313   0.7609
   9.250   1.4089   0.01536   0.00954  -0.0961   0.1868   0.7775
   9.500   1.4135   0.01633   0.01043  -0.0931   0.1670   0.7865
   9.750   1.4171   0.01740   0.01145  -0.0901   0.1486   0.7961
  10.000   1.4205   0.01858   0.01258  -0.0873   0.1322   0.8059
  10.250   1.4233   0.01987   0.01382  -0.0846   0.1167   0.8168
  10.500   1.4258   0.02127   0.01518  -0.0822   0.1016   0.8286
  10.750   1.4297   0.02265   0.01656  -0.0800   0.0899   0.8419
  11.000   1.4332   0.02412   0.01803  -0.0779   0.0792   0.8573
  11.250   1.4358   0.02565   0.01958  -0.0758   0.0697   0.8773
  11.500   1.4364   0.02717   0.02117  -0.0734   0.0617   0.9126
  12.000   1.4433   0.03047   0.02453  -0.0702   0.0491   1.0000
  12.250   1.4494   0.03222   0.02628  -0.0692   0.0448   1.0000
  12.500   1.4541   0.03414   0.02820  -0.0681   0.0411   1.0000
  12.750   1.4621   0.03582   0.02991  -0.0674   0.0389   1.0000
  13.000   1.4671   0.03781   0.03192  -0.0666   0.0367   1.0000
  13.250   1.4738   0.03973   0.03387  -0.0660   0.0351   1.0000
  13.500   1.4814   0.04159   0.03577  -0.0654   0.0337   1.0000
  13.750   1.4866   0.04374   0.03795  -0.0649   0.0323   1.0000
  14.000   1.4900   0.04613   0.04037  -0.0644   0.0309   1.0000
  14.250   1.4984   0.04805   0.04235  -0.0642   0.0301   1.0000
  14.500   1.5052   0.05019   0.04454  -0.0640   0.0293   1.0000
  14.750   1.5110   0.05246   0.04685  -0.0638   0.0283   1.0000
  15.000   1.5145   0.05504   0.04947  -0.0637   0.0275   1.0000
  15.250   1.5160   0.05793   0.05240  -0.0636   0.0265   1.0000
  15.500   1.5235   0.06015   0.05469  -0.0637   0.0259   1.0000
  15.750   1.5294   0.06260   0.05720  -0.0638   0.0252   1.0000
  16.000   1.5343   0.06519   0.05984  -0.0640   0.0245   1.0000
  16.250   1.5369   0.06813   0.06283  -0.0643   0.0238   1.0000
  16.500   1.5369   0.07146   0.06621  -0.0647   0.0230   1.0000
  16.750   1.5404   0.07438   0.06920  -0.0651   0.0224   1.0000
  17.000   1.5458   0.07708   0.07197  -0.0656   0.0218   1.0000
  17.250   1.5495   0.08004   0.07498  -0.0661   0.0211   1.0000
  17.500   1.5513   0.08331   0.07831  -0.0668   0.0204   1.0000
  17.750   1.5504   0.08701   0.08206  -0.0676   0.0197   1.0000
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