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E203 (13.64%) (e203-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: E203 (13.64%) (e203-il)
Reynolds number: 100,000
Max Cl/Cd: 54.97 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e203-il-100000-n5.txt
Download as CSV file: xf-e203-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E203  (13.64%)                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.5730   0.07002   0.06456  -0.0677   1.0000   0.0276
 -11.250  -0.5950   0.06431   0.05876  -0.0711   1.0000   0.0275
 -11.000  -0.6157   0.05958   0.05392  -0.0734   1.0000   0.0274
 -10.750  -0.6363   0.05575   0.04998  -0.0743   1.0000   0.0274
 -10.500  -0.6576   0.05284   0.04696  -0.0732   1.0000   0.0273
 -10.250  -0.6784   0.05051   0.04451  -0.0703   1.0000   0.0273
 -10.000  -0.6924   0.04795   0.04175  -0.0677   1.0000   0.0274
  -9.750  -0.7022   0.04546   0.03903  -0.0650   1.0000   0.0274
  -9.500  -0.7079   0.04309   0.03640  -0.0623   1.0000   0.0276
  -9.250  -0.7094   0.04070   0.03382  -0.0598   1.0000   0.0278
  -9.000  -0.7075   0.03855   0.03151  -0.0574   1.0000   0.0281
  -8.750  -0.7033   0.03672   0.02953  -0.0551   1.0000   0.0285
  -8.500  -0.6767   0.03446   0.02704  -0.0569   0.9947   0.0293
  -8.250  -0.6465   0.03242   0.02479  -0.0591   0.9879   0.0303
  -8.000  -0.6142   0.03077   0.02287  -0.0613   0.9814   0.0322
  -7.750  -0.5834   0.02918   0.02103  -0.0629   0.9736   0.0342
  -7.500  -0.5523   0.02769   0.01930  -0.0643   0.9661   0.0356
  -7.250  -0.5222   0.02604   0.01763  -0.0657   0.9583   0.0373
  -7.000  -0.4940   0.02482   0.01633  -0.0667   0.9487   0.0394
  -6.750  -0.4609   0.02364   0.01503  -0.0684   0.9419   0.0426
  -6.500  -0.4330   0.02256   0.01384  -0.0691   0.9315   0.0471
  -6.250  -0.4030   0.02156   0.01278  -0.0702   0.9225   0.0553
  -6.000  -0.3713   0.02038   0.01162  -0.0716   0.9148   0.0709
  -5.750  -0.3435   0.01941   0.01069  -0.0722   0.9043   0.0965
  -5.500  -0.3130   0.01850   0.00992  -0.0734   0.8955   0.1362
  -5.250  -0.2835   0.01750   0.00926  -0.0747   0.8865   0.2034
  -5.000  -0.2560   0.01670   0.00877  -0.0753   0.8761   0.2741
  -4.750  -0.2249   0.01622   0.00843  -0.0761   0.8676   0.3343
  -4.500  -0.1946   0.01601   0.00824  -0.0766   0.8577   0.3842
  -4.250  -0.1648   0.01591   0.00807  -0.0768   0.8477   0.4209
  -4.000  -0.1329   0.01582   0.00786  -0.0774   0.8392   0.4499
  -3.750  -0.1042   0.01576   0.00768  -0.0775   0.8289   0.4726
  -3.500  -0.0750   0.01571   0.00750  -0.0776   0.8194   0.4922
  -3.250  -0.0446   0.01564   0.00733  -0.0778   0.8111   0.5096
  -3.000  -0.0173   0.01560   0.00720  -0.0776   0.8011   0.5250
  -2.750   0.0117   0.01555   0.00705  -0.0777   0.7927   0.5398
  -2.500   0.0399   0.01551   0.00691  -0.0776   0.7839   0.5537
  -2.250   0.0677   0.01548   0.00679  -0.0775   0.7753   0.5670
  -2.000   0.0962   0.01543   0.00667  -0.0775   0.7676   0.5788
  -1.750   0.1230   0.01540   0.00661  -0.0772   0.7591   0.5901
  -1.500   0.1516   0.01537   0.00649  -0.0772   0.7521   0.6018
  -1.250   0.1781   0.01537   0.00645  -0.0770   0.7438   0.6137
  -1.000   0.2065   0.01534   0.00637  -0.0769   0.7372   0.6254
  -0.750   0.2326   0.01535   0.00637  -0.0766   0.7293   0.6361
  -0.500   0.2607   0.01533   0.00632  -0.0765   0.7228   0.6474
  -0.250   0.2872   0.01536   0.00634  -0.0763   0.7154   0.6593
   0.000   0.3146   0.01537   0.00633  -0.0761   0.7090   0.6719
   0.250   0.3409   0.01540   0.00638  -0.0758   0.7023   0.6843
   0.500   0.3674   0.01543   0.00643  -0.0755   0.6956   0.6980
   0.750   0.3945   0.01546   0.00648  -0.0752   0.6898   0.7130
   1.000   0.4199   0.01552   0.00660  -0.0747   0.6828   0.7297
   1.250   0.4472   0.01554   0.00664  -0.0744   0.6775   0.7483
   1.500   0.4713   0.01561   0.00682  -0.0736   0.6705   0.7691
   1.750   0.4970   0.01565   0.00692  -0.0730   0.6647   0.7935
   2.000   0.5219   0.01570   0.00706  -0.0722   0.6587   0.8217
   2.250   0.5473   0.01575   0.00724  -0.0715   0.6523   0.8549
   2.500   0.5795   0.01577   0.00731  -0.0721   0.6473   0.8937
   2.750   0.6158   0.01589   0.00754  -0.0739   0.6398   0.9404
   3.000   0.6590   0.01597   0.00765  -0.0773   0.6340   0.9982
   3.250   0.6830   0.01621   0.00789  -0.0769   0.6273   1.0000
   3.500   0.7081   0.01641   0.00809  -0.0765   0.6209   1.0000
   3.750   0.7336   0.01663   0.00833  -0.0763   0.6146   1.0000
   4.000   0.7578   0.01686   0.00860  -0.0757   0.6072   1.0000
   4.250   0.7838   0.01705   0.00879  -0.0754   0.6004   1.0000
   4.500   0.8076   0.01727   0.00907  -0.0748   0.5919   1.0000
   4.750   0.8325   0.01746   0.00932  -0.0743   0.5838   1.0000
   5.000   0.8576   0.01763   0.00953  -0.0738   0.5751   1.0000
   5.250   0.8806   0.01785   0.00984  -0.0729   0.5654   1.0000
   5.500   0.9056   0.01799   0.01001  -0.0723   0.5559   1.0000
   5.750   0.9294   0.01813   0.01025  -0.0715   0.5450   1.0000
   6.000   0.9514   0.01832   0.01054  -0.0705   0.5328   1.0000
   6.250   0.9737   0.01849   0.01080  -0.0694   0.5200   1.0000
   6.500   0.9956   0.01866   0.01105  -0.0683   0.5062   1.0000
   6.750   1.0169   0.01883   0.01130  -0.0670   0.4906   1.0000
   7.000   1.0374   0.01902   0.01157  -0.0656   0.4733   1.0000
   7.250   1.0566   0.01925   0.01186  -0.0640   0.4535   1.0000
   7.500   1.0741   0.01954   0.01220  -0.0622   0.4302   1.0000
   7.750   1.0901   0.01991   0.01258  -0.0602   0.4029   1.0000
   8.000   1.1037   0.02039   0.01301  -0.0578   0.3703   1.0000
   8.250   1.1139   0.02106   0.01358  -0.0550   0.3316   1.0000
   8.500   1.1198   0.02197   0.01429  -0.0518   0.2912   1.0000
   8.750   1.1213   0.02303   0.01515  -0.0480   0.2557   1.0000
   9.000   1.1221   0.02425   0.01622  -0.0444   0.2245   1.0000
   9.250   1.1229   0.02560   0.01744  -0.0411   0.1958   1.0000
   9.500   1.1242   0.02703   0.01878  -0.0382   0.1709   1.0000
   9.750   1.1254   0.02858   0.02025  -0.0356   0.1487   1.0000
  10.000   1.1256   0.03031   0.02189  -0.0332   0.1289   1.0000
  10.250   1.1264   0.03212   0.02363  -0.0312   0.1098   1.0000
  10.500   1.1271   0.03406   0.02552  -0.0294   0.0924   1.0000
  10.750   1.1276   0.03614   0.02750  -0.0279   0.0770   1.0000
  11.000   1.1294   0.03821   0.02955  -0.0267   0.0650   1.0000
  11.250   1.1313   0.04037   0.03174  -0.0256   0.0552   1.0000
  11.500   1.1323   0.04271   0.03410  -0.0245   0.0473   1.0000
  11.750   1.1312   0.04533   0.03669  -0.0237   0.0413   1.0000
  12.000   1.1328   0.04778   0.03928  -0.0230   0.0363   1.0000
  12.250   1.1309   0.05066   0.04220  -0.0224   0.0331   1.0000
  12.500   1.1295   0.05359   0.04524  -0.0219   0.0303   1.0000
  12.750   1.1295   0.05643   0.04822  -0.0215   0.0281   1.0000
  13.000   1.1291   0.05940   0.05128  -0.0214   0.0262   1.0000
  13.250   1.1265   0.06268   0.05462  -0.0214   0.0249   1.0000
  13.500   1.1273   0.06567   0.05777  -0.0213   0.0237   1.0000
  13.750   1.1290   0.06866   0.06093  -0.0215   0.0220   1.0000
  14.000   1.1297   0.07183   0.06423  -0.0218   0.0209   1.0000
  14.250   1.1297   0.07516   0.06768  -0.0222   0.0201   1.0000
  14.500   1.1293   0.07861   0.07123  -0.0229   0.0195   1.0000
  14.750   1.1280   0.08225   0.07495  -0.0236   0.0189   1.0000
  15.000   1.1283   0.08576   0.07857  -0.0241   0.0185   1.0000
  15.250   1.1286   0.08944   0.08245  -0.0248   0.0182   1.0000
  15.500   1.1270   0.09354   0.08677  -0.0258   0.0178   1.0000
  15.750   1.1241   0.09793   0.09137  -0.0271   0.0175   1.0000
  16.000   1.1188   0.10284   0.09650  -0.0289   0.0173   1.0000
  16.250   1.1114   0.10829   0.10217  -0.0312   0.0170   1.0000
  16.500   1.1024   0.11420   0.10830  -0.0340   0.0169   1.0000
  16.750   1.0911   0.12076   0.11508  -0.0374   0.0169   1.0000
  17.000   1.0771   0.12821   0.12275  -0.0416   0.0168   1.0000
  17.250   1.0614   0.13642   0.13116  -0.0465   0.0169   1.0000
  17.500   1.0420   0.14611   0.14106  -0.0526   0.0171   1.0000
  17.750   1.0182   0.15780   0.15294  -0.0601   0.0173   1.0000
  18.000   0.9904   0.17194   0.16721  -0.0688   0.0178   1.0000
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