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E210 (13.64%) (e210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: E210 (13.64%) (e210-il)
Reynolds number: 1,000,000
Max Cl/Cd: 140.31 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e210-il-1000000.txt
Download as CSV file: xf-e210-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E210  (13.64%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.2499   0.11898   0.11743  -0.0471   0.9965   0.0141
 -12.250  -0.7329   0.05010   0.04789  -0.0711   1.0000   0.0089
 -12.000  -0.7375   0.04227   0.03985  -0.0820   0.9972   0.0090
 -11.750  -0.7306   0.03647   0.03382  -0.0923   0.9941   0.0091
 -11.500  -0.7173   0.03438   0.03166  -0.0962   0.9894   0.0093
 -11.250  -0.6985   0.03064   0.02766  -0.1027   0.9856   0.0094
 -11.000  -0.6680   0.02926   0.02618  -0.1062   0.9843   0.0098
 -10.750  -0.6533   0.02708   0.02379  -0.1072   0.9797   0.0100
 -10.500  -0.6295   0.02528   0.02179  -0.1090   0.9765   0.0103
 -10.250  -0.6012   0.02368   0.01998  -0.1113   0.9746   0.0106
 -10.000  -0.5693   0.02259   0.01873  -0.1135   0.9733   0.0108
  -9.750  -0.5423   0.01978   0.01565  -0.1162   0.9720   0.0114
  -9.500  -0.5247   0.01889   0.01470  -0.1150   0.9662   0.0116
  -9.250  -0.4944   0.01817   0.01393  -0.1162   0.9637   0.0120
  -9.000  -0.4617   0.01739   0.01306  -0.1179   0.9619   0.0124
  -8.750  -0.4277   0.01664   0.01224  -0.1198   0.9606   0.0130
  -8.500  -0.3928   0.01580   0.01130  -0.1218   0.9595   0.0134
  -8.250  -0.3728   0.01524   0.01067  -0.1204   0.9528   0.0138
  -8.000  -0.3408   0.01495   0.01032  -0.1214   0.9494   0.0141
  -7.750  -0.3112   0.01329   0.00856  -0.1228   0.9467   0.0151
  -7.500  -0.2900   0.01277   0.00802  -0.1216   0.9381   0.0156
  -7.250  -0.2561   0.01217   0.00738  -0.1231   0.9331   0.0163
  -7.000  -0.2241   0.01166   0.00681  -0.1242   0.9250   0.0169
  -6.750  -0.1837   0.01111   0.00619  -0.1270   0.9178   0.0176
  -6.500  -0.1453   0.01079   0.00579  -0.1293   0.9048   0.0181
  -6.250  -0.1122   0.00988   0.00473  -0.1309   0.8865   0.0194
  -6.000  -0.0825   0.00957   0.00429  -0.1314   0.8631   0.0203
  -5.750  -0.0558   0.00936   0.00395  -0.1312   0.8391   0.0212
  -5.500  -0.0305   0.00920   0.00365  -0.1307   0.8156   0.0220
  -5.250  -0.0054   0.00910   0.00342  -0.1301   0.7938   0.0228
  -5.000   0.0193   0.00884   0.00302  -0.1295   0.7728   0.0247
  -4.750   0.0442   0.00870   0.00279  -0.1289   0.7531   0.0266
  -4.500   0.0698   0.00861   0.00259  -0.1284   0.7353   0.0284
  -4.250   0.0955   0.00844   0.00237  -0.1280   0.7185   0.0357
  -4.000   0.1210   0.00816   0.00216  -0.1277   0.7026   0.0686
  -3.750   0.1469   0.00796   0.00202  -0.1274   0.6882   0.1006
  -3.500   0.1730   0.00780   0.00191  -0.1272   0.6747   0.1335
  -3.250   0.1996   0.00764   0.00180  -0.1271   0.6619   0.1690
  -3.000   0.2263   0.00745   0.00171  -0.1270   0.6502   0.2147
  -2.750   0.2530   0.00725   0.00163  -0.1269   0.6394   0.2676
  -2.500   0.2793   0.00699   0.00156  -0.1268   0.6290   0.3445
  -2.250   0.3066   0.00685   0.00154  -0.1268   0.6192   0.4019
  -2.000   0.3339   0.00684   0.00154  -0.1267   0.6104   0.4333
  -1.750   0.3614   0.00684   0.00155  -0.1266   0.6017   0.4603
  -1.500   0.3890   0.00686   0.00156  -0.1265   0.5938   0.4783
  -1.250   0.4165   0.00690   0.00157  -0.1264   0.5857   0.4910
  -1.000   0.4442   0.00693   0.00159  -0.1264   0.5788   0.5060
  -0.750   0.4718   0.00696   0.00160  -0.1263   0.5716   0.5164
  -0.500   0.4994   0.00701   0.00162  -0.1262   0.5650   0.5257
  -0.250   0.5272   0.00704   0.00165  -0.1262   0.5584   0.5357
   0.000   0.5544   0.00710   0.00168  -0.1260   0.5521   0.5448
   0.250   0.5825   0.00713   0.00171  -0.1260   0.5463   0.5546
   0.500   0.6099   0.00717   0.00175  -0.1260   0.5401   0.5645
   0.750   0.6373   0.00723   0.00179  -0.1259   0.5345   0.5748
   1.000   0.6651   0.00725   0.00184  -0.1259   0.5289   0.5856
   1.250   0.6923   0.00731   0.00189  -0.1257   0.5231   0.5963
   1.500   0.7198   0.00735   0.00195  -0.1257   0.5178   0.6082
   1.750   0.7474   0.00739   0.00201  -0.1256   0.5123   0.6219
   2.000   0.7742   0.00746   0.00208  -0.1254   0.5067   0.6361
   2.250   0.8018   0.00749   0.00215  -0.1254   0.5016   0.6507
   2.500   0.8290   0.00753   0.00223  -0.1253   0.4961   0.6669
   2.750   0.8554   0.00761   0.00233  -0.1250   0.4904   0.6849
   3.000   0.8829   0.00762   0.00241  -0.1250   0.4853   0.7055
   3.250   0.9096   0.00766   0.00251  -0.1248   0.4796   0.7293
   3.500   0.9357   0.00772   0.00263  -0.1244   0.4738   0.7565
   3.750   0.9622   0.00773   0.00273  -0.1242   0.4675   0.7872
   4.000   0.9868   0.00778   0.00285  -0.1235   0.4606   0.8241
   4.250   1.0108   0.00775   0.00297  -0.1227   0.4543   0.8724
   4.500   1.0347   0.00767   0.00304  -0.1217   0.4476   0.9918
   4.750   1.0612   0.00779   0.00315  -0.1215   0.4411   1.0000
   5.000   1.0877   0.00792   0.00326  -0.1213   0.4339   1.0000
   5.250   1.1138   0.00806   0.00339  -0.1210   0.4267   1.0000
   5.500   1.1398   0.00820   0.00351  -0.1208   0.4188   1.0000
   5.750   1.1656   0.00835   0.00365  -0.1205   0.4111   1.0000
   6.000   1.1909   0.00852   0.00380  -0.1201   0.4023   1.0000
   6.250   1.2165   0.00867   0.00395  -0.1197   0.3939   1.0000
   6.500   1.2408   0.00889   0.00413  -0.1192   0.3842   1.0000
   6.750   1.2657   0.00906   0.00430  -0.1187   0.3738   1.0000
   7.000   1.2901   0.00927   0.00449  -0.1181   0.3633   1.0000
   7.250   1.3135   0.00951   0.00470  -0.1174   0.3512   1.0000
   7.500   1.3362   0.00979   0.00494  -0.1166   0.3362   1.0000
   7.750   1.3582   0.01010   0.00520  -0.1157   0.3200   1.0000
   8.000   1.3790   0.01045   0.00548  -0.1145   0.3017   1.0000
   8.250   1.3970   0.01090   0.00583  -0.1128   0.2790   1.0000
   8.500   1.4111   0.01151   0.00627  -0.1105   0.2470   1.0000
   8.750   1.4220   0.01226   0.00682  -0.1076   0.2126   1.0000
   9.000   1.4332   0.01299   0.00739  -0.1049   0.1840   1.0000
   9.250   1.4443   0.01369   0.00797  -0.1021   0.1596   1.0000
   9.500   1.4545   0.01445   0.00860  -0.0993   0.1367   1.0000
   9.750   1.4650   0.01518   0.00923  -0.0966   0.1176   1.0000
  10.000   1.4749   0.01595   0.00991  -0.0939   0.1010   1.0000
  10.250   1.4849   0.01671   0.01060  -0.0912   0.0874   1.0000
  10.500   1.4950   0.01748   0.01132  -0.0886   0.0759   1.0000
  10.750   1.5056   0.01823   0.01205  -0.0863   0.0670   1.0000
  11.000   1.5153   0.01904   0.01285  -0.0838   0.0590   1.0000
  11.250   1.5233   0.01997   0.01376  -0.0813   0.0513   1.0000
  11.500   1.5313   0.02094   0.01472  -0.0789   0.0452   1.0000
  11.750   1.5397   0.02193   0.01572  -0.0766   0.0399   1.0000
  12.000   1.5450   0.02315   0.01693  -0.0742   0.0346   1.0000
  12.250   1.5520   0.02432   0.01813  -0.0721   0.0304   1.0000
  12.500   1.5568   0.02571   0.01954  -0.0700   0.0265   1.0000
  12.750   1.5613   0.02720   0.02105  -0.0680   0.0230   1.0000
  13.000   1.5644   0.02889   0.02276  -0.0662   0.0193   1.0000
  13.250   1.5646   0.03091   0.02479  -0.0643   0.0153   1.0000
  13.500   1.5641   0.03312   0.02703  -0.0627   0.0121   1.0000
  13.750   1.5629   0.03553   0.02948  -0.0613   0.0100   1.0000
  14.000   1.5644   0.03780   0.03182  -0.0603   0.0087   1.0000
  14.250   1.5606   0.04072   0.03480  -0.0592   0.0074   1.0000
  14.500   1.5627   0.04314   0.03731  -0.0586   0.0071   1.0000
  14.750   1.5646   0.04569   0.03994  -0.0582   0.0068   1.0000
  15.000   1.5646   0.04850   0.04283  -0.0578   0.0064   1.0000
  15.250   1.5626   0.05164   0.04605  -0.0576   0.0060   1.0000
  15.500   1.5604   0.05492   0.04941  -0.0576   0.0058   1.0000
  15.750   1.5530   0.05894   0.05354  -0.0577   0.0054   1.0000
  16.000   1.5505   0.06244   0.05713  -0.0580   0.0053   1.0000
  16.250   1.5497   0.06582   0.06060  -0.0584   0.0052   1.0000
  16.500   1.5469   0.06954   0.06442  -0.0590   0.0051   1.0000
  16.750   1.5437   0.07340   0.06838  -0.0597   0.0050   1.0000
  17.000   1.5406   0.07731   0.07239  -0.0605   0.0049   1.0000
  17.250   1.5358   0.08158   0.07675  -0.0615   0.0047   1.0000
  17.500   1.5310   0.08594   0.08121  -0.0627   0.0046   1.0000
  17.750   1.5264   0.09033   0.08570  -0.0640   0.0045   1.0000
  18.000   1.5214   0.09486   0.09033  -0.0654   0.0044   1.0000
  18.250   1.5143   0.09983   0.09540  -0.0671   0.0044   1.0000
  18.500   1.5074   0.10485   0.10051  -0.0690   0.0043   1.0000
  18.750   1.5007   0.10988   0.10565  -0.0709   0.0043   1.0000
  19.000   1.4924   0.11527   0.11114  -0.0731   0.0042   1.0000
  19.250   1.4840   0.12076   0.11673  -0.0755   0.0041   1.0000
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