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E210 (13.64%) (e210-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: E210 (13.64%) (e210-il)
Reynolds number: 500,000
Max Cl/Cd: 109.02 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e210-il-500000-n5.txt
Download as CSV file: xf-e210-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.6800   0.04928   0.04638  -0.0791   0.9967   0.0089
 -11.750  -0.6848   0.04187   0.03873  -0.0892   0.9931   0.0089
 -11.500  -0.6854   0.03670   0.03333  -0.0965   0.9877   0.0090
 -11.250  -0.6718   0.03299   0.02938  -0.1034   0.9836   0.0092
 -11.000  -0.6630   0.03056   0.02675  -0.1046   0.9771   0.0094
 -10.750  -0.6420   0.02835   0.02430  -0.1072   0.9737   0.0097
 -10.500  -0.6163   0.02635   0.02204  -0.1099   0.9716   0.0101
 -10.250  -0.6042   0.02488   0.02039  -0.1088   0.9647   0.0104
 -10.000  -0.5783   0.02354   0.01883  -0.1101   0.9614   0.0108
  -9.500  -0.5343   0.02116   0.01618  -0.1106   0.9515   0.0115
  -9.250  -0.5061   0.02043   0.01539  -0.1115   0.9477   0.0119
  -9.000  -0.4823   0.01964   0.01451  -0.1115   0.9419   0.0123
  -8.750  -0.4586   0.01886   0.01364  -0.1113   0.9351   0.0128
  -8.500  -0.4331   0.01802   0.01268  -0.1114   0.9290   0.0132
  -8.250  -0.4070   0.01721   0.01175  -0.1116   0.9216   0.0137
  -8.000  -0.3755   0.01642   0.01083  -0.1128   0.9159   0.0142
  -7.750  -0.3424   0.01584   0.01014  -0.1142   0.9085   0.0146
  -7.500  -0.3031   0.01471   0.00894  -0.1174   0.9022   0.0155
  -7.250  -0.2623   0.01405   0.00821  -0.1205   0.8928   0.0162
  -7.000  -0.2216   0.01340   0.00745  -0.1236   0.8805   0.0170
  -6.750  -0.1839   0.01285   0.00677  -0.1259   0.8635   0.0176
  -6.500  -0.1514   0.01246   0.00622  -0.1271   0.8433   0.0183
  -6.250  -0.1230   0.01217   0.00577  -0.1273   0.8218   0.0189
  -6.000  -0.0974   0.01173   0.00519  -0.1272   0.8006   0.0199
  -5.750  -0.0719   0.01147   0.00480  -0.1268   0.7803   0.0207
  -5.500  -0.0466   0.01125   0.00445  -0.1264   0.7612   0.0216
  -5.250  -0.0213   0.01107   0.00414  -0.1259   0.7437   0.0226
  -5.000   0.0042   0.01091   0.00386  -0.1255   0.7269   0.0236
  -4.750   0.0297   0.01073   0.00358  -0.1251   0.7114   0.0257
  -4.500   0.0555   0.01057   0.00334  -0.1247   0.6972   0.0288
  -4.250   0.0815   0.01039   0.00312  -0.1244   0.6839   0.0359
  -4.000   0.1074   0.01019   0.00292  -0.1241   0.6713   0.0533
  -3.750   0.1335   0.01003   0.00275  -0.1239   0.6597   0.0723
  -3.500   0.1599   0.00987   0.00261  -0.1237   0.6485   0.0938
  -3.250   0.1865   0.00968   0.00247  -0.1236   0.6382   0.1244
  -3.000   0.2129   0.00948   0.00235  -0.1235   0.6284   0.1641
  -2.750   0.2395   0.00926   0.00224  -0.1235   0.6191   0.2112
  -2.500   0.2664   0.00909   0.00214  -0.1234   0.6104   0.2557
  -2.250   0.2929   0.00887   0.00207  -0.1234   0.6017   0.3160
  -2.000   0.3199   0.00868   0.00205  -0.1234   0.5941   0.3862
  -1.750   0.3469   0.00863   0.00206  -0.1233   0.5863   0.4300
  -1.500   0.3743   0.00862   0.00208  -0.1232   0.5792   0.4575
  -1.250   0.4015   0.00865   0.00208  -0.1230   0.5720   0.4760
  -1.000   0.4290   0.00868   0.00209  -0.1229   0.5658   0.4894
  -0.750   0.4564   0.00872   0.00210  -0.1228   0.5590   0.5014
  -0.500   0.4836   0.00877   0.00212  -0.1227   0.5529   0.5130
  -0.250   0.5113   0.00880   0.00214  -0.1226   0.5468   0.5242
   0.000   0.5384   0.00885   0.00218  -0.1225   0.5408   0.5352
   0.250   0.5658   0.00889   0.00222  -0.1224   0.5352   0.5463
   0.500   0.5932   0.00894   0.00226  -0.1223   0.5293   0.5567
   0.750   0.6201   0.00901   0.00231  -0.1221   0.5240   0.5667
   1.000   0.6476   0.00904   0.00237  -0.1220   0.5187   0.5779
   1.500   0.7015   0.00917   0.00250  -0.1217   0.5078   0.6000
   1.750   0.7289   0.00921   0.00257  -0.1216   0.5026   0.6101
   2.250   0.7824   0.00936   0.00274  -0.1212   0.4920   0.6324
   2.500   0.8095   0.00941   0.00284  -0.1211   0.4868   0.6448
   2.750   0.8360   0.00948   0.00294  -0.1208   0.4813   0.6590
   3.000   0.8625   0.00956   0.00305  -0.1206   0.4764   0.6741
   3.250   0.8891   0.00961   0.00317  -0.1204   0.4709   0.6905
   3.500   0.9151   0.00969   0.00330  -0.1200   0.4655   0.7097
   3.750   0.9410   0.00976   0.00344  -0.1197   0.4603   0.7319
   4.000   0.9667   0.00981   0.00358  -0.1193   0.4543   0.7573
   4.250   0.9910   0.00990   0.00373  -0.1186   0.4482   0.7859
   4.500   1.0155   0.00993   0.00388  -0.1179   0.4415   0.8208
   4.750   1.0363   0.00997   0.00403  -0.1163   0.4341   0.8689
   5.000   1.0613   0.00992   0.00413  -0.1156   0.4262   1.0000
   5.500   1.1119   0.01027   0.00445  -0.1149   0.4103   1.0000
   5.750   1.1362   0.01047   0.00463  -0.1143   0.4020   1.0000
   6.000   1.1610   0.01066   0.00483  -0.1138   0.3925   1.0000
   6.250   1.1850   0.01087   0.00503  -0.1132   0.3827   1.0000
   6.500   1.2082   0.01112   0.00525  -0.1125   0.3721   1.0000
   6.750   1.2311   0.01137   0.00549  -0.1117   0.3600   1.0000
   7.000   1.2538   0.01164   0.00574  -0.1108   0.3477   1.0000
   7.250   1.2756   0.01193   0.00601  -0.1098   0.3346   1.0000
   7.500   1.2955   0.01227   0.00631  -0.1085   0.3188   1.0000
   7.750   1.3139   0.01266   0.00664  -0.1069   0.3016   1.0000
   8.000   1.3309   0.01311   0.00703  -0.1051   0.2816   1.0000
   8.250   1.3452   0.01370   0.00750  -0.1029   0.2564   1.0000
   8.500   1.3582   0.01436   0.00805  -0.1005   0.2296   1.0000
   8.750   1.3695   0.01512   0.00866  -0.0979   0.2027   1.0000
   9.000   1.3817   0.01583   0.00929  -0.0955   0.1821   1.0000
   9.250   1.3925   0.01660   0.00998  -0.0930   0.1614   1.0000
   9.500   1.4017   0.01747   0.01074  -0.0902   0.1409   1.0000
   9.750   1.4107   0.01834   0.01154  -0.0876   0.1222   1.0000
  10.000   1.4181   0.01932   0.01243  -0.0848   0.1051   1.0000
  10.500   1.4333   0.02131   0.01433  -0.0796   0.0792   1.0000
  10.750   1.4400   0.02241   0.01541  -0.0771   0.0684   1.0000
  11.000   1.4472   0.02353   0.01652  -0.0749   0.0599   1.0000
  11.250   1.4530   0.02478   0.01777  -0.0726   0.0521   1.0000
  11.500   1.4575   0.02619   0.01918  -0.0704   0.0453   1.0000
  11.750   1.4645   0.02750   0.02053  -0.0686   0.0405   1.0000
  12.000   1.4685   0.02911   0.02216  -0.0668   0.0356   1.0000
  12.250   1.4731   0.03076   0.02384  -0.0652   0.0313   1.0000
  12.500   1.4768   0.03257   0.02569  -0.0637   0.0279   1.0000
  12.750   1.4799   0.03453   0.02770  -0.0624   0.0243   1.0000
  13.000   1.4829   0.03659   0.02981  -0.0613   0.0219   1.0000
  13.250   1.4857   0.03877   0.03205  -0.0603   0.0193   1.0000
  13.500   1.4867   0.04121   0.03455  -0.0595   0.0170   1.0000
  13.750   1.4877   0.04375   0.03716  -0.0588   0.0145   1.0000
  14.000   1.4877   0.04650   0.03996  -0.0583   0.0125   1.0000
  14.250   1.4869   0.04941   0.04294  -0.0580   0.0107   1.0000
  14.500   1.4860   0.05242   0.04603  -0.0578   0.0093   1.0000
  14.750   1.4851   0.05554   0.04922  -0.0577   0.0083   1.0000
  15.000   1.4830   0.05887   0.05263  -0.0578   0.0074   1.0000
  15.250   1.4817   0.06220   0.05605  -0.0580   0.0067   1.0000
  15.500   1.4794   0.06573   0.05968  -0.0584   0.0062   1.0000
  15.750   1.4763   0.06947   0.06351  -0.0589   0.0058   1.0000
  16.000   1.4739   0.07319   0.06734  -0.0595   0.0054   1.0000
  16.250   1.4723   0.07686   0.07111  -0.0602   0.0052   1.0000
  16.500   1.4702   0.08071   0.07507  -0.0611   0.0050   1.0000
  16.750   1.4668   0.08480   0.07925  -0.0621   0.0047   1.0000
  17.000   1.4632   0.08901   0.08357  -0.0633   0.0045   1.0000
  17.250   1.4591   0.09337   0.08803  -0.0646   0.0044   1.0000
  17.500   1.4538   0.09799   0.09276  -0.0661   0.0042   1.0000
  17.750   1.4487   0.10269   0.09756  -0.0677   0.0041   1.0000
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