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E210 (13.64%) (e210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E210 (13.64%) (e210-il)
Reynolds number: 1,000,000
Max Cl/Cd: 129.52 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e210-il-1000000-n5.txt
Download as CSV file: xf-e210-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.8459   0.06567   0.06318  -0.0694   1.0000   0.0059
 -14.750  -0.8897   0.05545   0.05279  -0.0750   1.0000   0.0058
 -14.500  -0.9204   0.04711   0.04427  -0.0809   0.9996   0.0059
 -14.250  -0.9307   0.04055   0.03753  -0.0879   0.9981   0.0058
 -14.000  -0.9329   0.03505   0.03186  -0.0948   0.9959   0.0059
 -13.750  -0.9210   0.03141   0.02809  -0.1008   0.9941   0.0061
 -13.500  -0.9139   0.02810   0.02461  -0.1056   0.9891   0.0061
 -13.250  -0.8854   0.02633   0.02275  -0.1099   0.9861   0.0064
 -13.000  -0.8512   0.02491   0.02124  -0.1139   0.9844   0.0066
 -12.750  -0.8306   0.02362   0.01985  -0.1150   0.9813   0.0067
 -12.500  -0.8102   0.02272   0.01889  -0.1153   0.9780   0.0069
 -12.250  -0.7861   0.02169   0.01775  -0.1164   0.9758   0.0071
 -12.000  -0.7586   0.02089   0.01688  -0.1177   0.9743   0.0074
 -11.750  -0.7297   0.02002   0.01591  -0.1192   0.9731   0.0076
 -11.500  -0.7000   0.01918   0.01498  -0.1208   0.9721   0.0078
 -11.250  -0.6842   0.01858   0.01431  -0.1192   0.9678   0.0080
 -11.000  -0.6615   0.01787   0.01352  -0.1191   0.9642   0.0081
 -10.750  -0.6349   0.01696   0.01252  -0.1200   0.9618   0.0085
 -10.500  -0.6048   0.01635   0.01186  -0.1211   0.9602   0.0088
 -10.250  -0.5730   0.01582   0.01130  -0.1225   0.9588   0.0090
 -10.000  -0.5608   0.01546   0.01090  -0.1196   0.9502   0.0093
  -9.750  -0.5328   0.01493   0.01032  -0.1202   0.9466   0.0096
  -9.500  -0.5116   0.01448   0.00982  -0.1191   0.9389   0.0099
  -9.250  -0.4803   0.01398   0.00926  -0.1202   0.9338   0.0102
  -9.000  -0.4462   0.01349   0.00870  -0.1219   0.9278   0.0106
  -8.750  -0.4060   0.01307   0.00821  -0.1248   0.9204   0.0109
  -8.500  -0.3657   0.01239   0.00742  -0.1280   0.9082   0.0114
  -8.250  -0.3291   0.01189   0.00681  -0.1302   0.8896   0.0119
  -8.000  -0.2997   0.01159   0.00638  -0.1307   0.8640   0.0123
  -7.750  -0.2743   0.01139   0.00602  -0.1304   0.8373   0.0126
  -7.500  -0.2503   0.01120   0.00569  -0.1297   0.8128   0.0130
  -7.250  -0.2261   0.01103   0.00540  -0.1291   0.7904   0.0135
  -7.000  -0.2021   0.01087   0.00510  -0.1284   0.7687   0.0140
  -6.750  -0.1774   0.01072   0.00484  -0.1279   0.7491   0.0143
  -6.500  -0.1524   0.01056   0.00457  -0.1274   0.7310   0.0145
  -6.250  -0.1276   0.01028   0.00417  -0.1269   0.7143   0.0151
  -6.000  -0.1024   0.01006   0.00386  -0.1265   0.6982   0.0157
  -5.750  -0.0765   0.00989   0.00361  -0.1262   0.6839   0.0164
  -5.500  -0.0503   0.00975   0.00339  -0.1259   0.6709   0.0171
  -5.250  -0.0240   0.00961   0.00318  -0.1257   0.6581   0.0176
  -5.000   0.0025   0.00950   0.00298  -0.1254   0.6460   0.0182
  -4.750   0.0295   0.00939   0.00280  -0.1253   0.6350   0.0188
  -4.500   0.0564   0.00926   0.00261  -0.1251   0.6249   0.0198
  -4.250   0.0832   0.00915   0.00244  -0.1250   0.6148   0.0216
  -4.000   0.1106   0.00904   0.00230  -0.1249   0.6055   0.0238
  -3.750   0.1376   0.00889   0.00216  -0.1248   0.5972   0.0331
  -3.500   0.1647   0.00872   0.00202  -0.1248   0.5885   0.0526
  -3.250   0.1921   0.00859   0.00192  -0.1247   0.5809   0.0689
  -3.000   0.2194   0.00846   0.00182  -0.1247   0.5733   0.0894
  -2.750   0.2468   0.00833   0.00174  -0.1247   0.5666   0.1162
  -2.500   0.2743   0.00818   0.00166  -0.1248   0.5594   0.1484
  -2.250   0.3016   0.00802   0.00159  -0.1248   0.5532   0.1887
  -2.000   0.3293   0.00784   0.00154  -0.1249   0.5473   0.2342
  -1.750   0.3568   0.00773   0.00149  -0.1249   0.5408   0.2733
  -1.500   0.3844   0.00759   0.00146  -0.1250   0.5353   0.3168
  -1.250   0.4119   0.00738   0.00145  -0.1251   0.5296   0.3935
  -0.750   0.4674   0.00734   0.00149  -0.1251   0.5187   0.4515
  -0.500   0.4952   0.00737   0.00151  -0.1251   0.5130   0.4641
  -0.250   0.5227   0.00740   0.00153  -0.1250   0.5081   0.4757
   0.000   0.5508   0.00742   0.00156  -0.1251   0.5032   0.4862
   0.500   0.6059   0.00751   0.00163  -0.1249   0.4925   0.5065
   0.750   0.6338   0.00753   0.00167  -0.1249   0.4880   0.5165
   1.000   0.6614   0.00758   0.00171  -0.1249   0.4827   0.5259
   1.250   0.6887   0.00764   0.00177  -0.1248   0.4775   0.5343
   1.500   0.7164   0.00768   0.00182  -0.1248   0.4729   0.5442
   1.750   0.7438   0.00772   0.00188  -0.1247   0.4677   0.5555
   2.000   0.7709   0.00779   0.00195  -0.1246   0.4624   0.5653
   2.500   0.8256   0.00790   0.00210  -0.1244   0.4524   0.5833
   2.750   0.8525   0.00798   0.00218  -0.1243   0.4471   0.5924
   3.000   0.8798   0.00804   0.00226  -0.1242   0.4418   0.6025
   3.250   0.9066   0.00812   0.00236  -0.1240   0.4358   0.6137
   3.500   0.9333   0.00819   0.00246  -0.1238   0.4299   0.6261
   3.750   0.9599   0.00828   0.00256  -0.1236   0.4224   0.6389
   4.000   0.9861   0.00838   0.00268  -0.1234   0.4146   0.6528
   4.250   1.0122   0.00849   0.00281  -0.1231   0.4059   0.6686
   4.500   1.0382   0.00858   0.00294  -0.1228   0.3984   0.6874
   4.750   1.0638   0.00870   0.00308  -0.1224   0.3895   0.7087
   5.000   1.0895   0.00879   0.00324  -0.1221   0.3811   0.7315
   5.250   1.1144   0.00892   0.00340  -0.1216   0.3721   0.7572
   5.500   1.1390   0.00904   0.00358  -0.1210   0.3611   0.7878
   5.750   1.1627   0.00915   0.00377  -0.1203   0.3504   0.8266
   6.000   1.1837   0.00924   0.00397  -0.1189   0.3390   0.8814
   6.250   1.2058   0.00931   0.00414  -0.1178   0.3261   1.0000
   6.500   1.2294   0.00958   0.00435  -0.1171   0.3126   1.0000
   6.750   1.2520   0.00990   0.00460  -0.1163   0.2948   1.0000
   7.000   1.2735   0.01027   0.00489  -0.1153   0.2745   1.0000
   7.250   1.2937   0.01071   0.00521  -0.1140   0.2525   1.0000
   7.500   1.3114   0.01126   0.00562  -0.1124   0.2248   1.0000
   7.750   1.3267   0.01185   0.00606  -0.1102   0.1974   1.0000
   8.000   1.3404   0.01247   0.00654  -0.1078   0.1710   1.0000
   8.250   1.3548   0.01304   0.00700  -0.1056   0.1496   1.0000
   8.500   1.3679   0.01367   0.00752  -0.1031   0.1288   1.0000
   8.750   1.3817   0.01424   0.00801  -0.1009   0.1119   1.0000
   9.000   1.3948   0.01487   0.00855  -0.0985   0.0957   1.0000
   9.250   1.4079   0.01547   0.00910  -0.0962   0.0830   1.0000
   9.500   1.4205   0.01611   0.00969  -0.0939   0.0712   1.0000
   9.750   1.4317   0.01682   0.01034  -0.0914   0.0597   1.0000
  10.000   1.4434   0.01751   0.01099  -0.0890   0.0506   1.0000
  10.250   1.4541   0.01826   0.01171  -0.0866   0.0431   1.0000
  10.750   1.4758   0.01979   0.01324  -0.0822   0.0322   1.0000
  11.000   1.4854   0.02066   0.01412  -0.0799   0.0278   1.0000
  11.250   1.4945   0.02160   0.01506  -0.0777   0.0240   1.0000
  11.500   1.5038   0.02255   0.01603  -0.0756   0.0211   1.0000
  11.750   1.5114   0.02366   0.01716  -0.0735   0.0183   1.0000
  12.000   1.5184   0.02486   0.01839  -0.0715   0.0152   1.0000
  12.250   1.5238   0.02624   0.01979  -0.0694   0.0125   1.0000
  12.500   1.5279   0.02779   0.02137  -0.0675   0.0098   1.0000
  12.750   1.5315   0.02948   0.02309  -0.0657   0.0075   1.0000
  13.000   1.5345   0.03130   0.02496  -0.0642   0.0059   1.0000
  13.250   1.5389   0.03310   0.02682  -0.0628   0.0051   1.0000
  13.500   1.5432   0.03501   0.02879  -0.0617   0.0046   1.0000
  13.750   1.5460   0.03714   0.03098  -0.0607   0.0041   1.0000
  14.000   1.5496   0.03928   0.03319  -0.0599   0.0038   1.0000
  14.250   1.5531   0.04151   0.03550  -0.0592   0.0037   1.0000
  14.500   1.5555   0.04393   0.03799  -0.0587   0.0035   1.0000
  14.750   1.5578   0.04645   0.04059  -0.0583   0.0033   1.0000
  15.000   1.5586   0.04919   0.04341  -0.0580   0.0032   1.0000
  15.250   1.5587   0.05210   0.04640  -0.0578   0.0030   1.0000
  15.500   1.5580   0.05519   0.04957  -0.0578   0.0029   1.0000
  15.750   1.5578   0.05830   0.05276  -0.0579   0.0028   1.0000
  16.000   1.5551   0.06181   0.05636  -0.0582   0.0027   1.0000
  16.250   1.5548   0.06508   0.05972  -0.0585   0.0027   1.0000
  16.500   1.5541   0.06848   0.06320  -0.0590   0.0026   1.0000
  16.750   1.5525   0.07207   0.06688  -0.0596   0.0025   1.0000
  17.000   1.5504   0.07579   0.07070  -0.0604   0.0025   1.0000
  17.250   1.5482   0.07962   0.07461  -0.0612   0.0024   1.0000
  17.500   1.5456   0.08358   0.07867  -0.0622   0.0024   1.0000
  17.750   1.5418   0.08779   0.08299  -0.0634   0.0024   1.0000
  18.000   1.5382   0.09203   0.08731  -0.0647   0.0023   1.0000
  18.250   1.5339   0.09646   0.09184  -0.0661   0.0023   1.0000
  18.500   1.5293   0.10099   0.09647  -0.0677   0.0022   1.0000
  18.750   1.5249   0.10556   0.10113  -0.0693   0.0022   1.0000
  19.000   1.5193   0.11037   0.10604  -0.0712   0.0022   1.0000
  19.250   1.5141   0.11515   0.11092  -0.0732   0.0021   1.0000
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