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E203 (13.64%) (e203-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: E203 (13.64%) (e203-il)
Reynolds number: 500,000
Max Cl/Cd: 101.31 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e203-il-500000-n5.txt
Download as CSV file: xf-e203-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7072   0.08458   0.08171  -0.0535   1.0000   0.0093
 -14.500  -0.7400   0.07441   0.07134  -0.0596   1.0000   0.0092
 -14.250  -0.7635   0.06681   0.06359  -0.0642   1.0000   0.0092
 -14.000  -0.7783   0.06114   0.05780  -0.0675   1.0000   0.0092
 -13.750  -0.7925   0.05588   0.05241  -0.0705   1.0000   0.0093
 -13.500  -0.8045   0.05122   0.04763  -0.0730   1.0000   0.0093
 -13.250  -0.8152   0.04696   0.04324  -0.0751   1.0000   0.0093
 -13.000  -0.8205   0.04365   0.03983  -0.0766   1.0000   0.0095
 -12.750  -0.8293   0.04015   0.03619  -0.0777   1.0000   0.0095
 -12.500  -0.8347   0.03737   0.03331  -0.0782   1.0000   0.0096
 -12.250  -0.8392   0.03506   0.03090  -0.0781   1.0000   0.0097
 -12.000  -0.8497   0.03272   0.02842  -0.0768   1.0000   0.0097
 -11.750  -0.8579   0.03144   0.02706  -0.0742   1.0000   0.0099
 -11.500  -0.8706   0.03027   0.02580  -0.0698   0.9998   0.0100
 -11.250  -0.8478   0.02843   0.02378  -0.0721   0.9962   0.0103
 -11.000  -0.8237   0.02692   0.02212  -0.0739   0.9926   0.0106
 -10.750  -0.8004   0.02553   0.02057  -0.0751   0.9885   0.0109
 -10.500  -0.7738   0.02423   0.01911  -0.0767   0.9850   0.0112
 -10.250  -0.7474   0.02299   0.01772  -0.0780   0.9815   0.0114
 -10.000  -0.7236   0.02197   0.01658  -0.0784   0.9757   0.0116
  -9.750  -0.6944   0.02103   0.01551  -0.0798   0.9718   0.0117
  -9.500  -0.6748   0.01949   0.01386  -0.0797   0.9640   0.0121
  -9.000  -0.6239   0.01756   0.01178  -0.0807   0.9483   0.0129
  -8.750  -0.5946   0.01681   0.01097  -0.0818   0.9395   0.0133
  -8.500  -0.5637   0.01612   0.01020  -0.0831   0.9288   0.0139
  -8.250  -0.5326   0.01541   0.00939  -0.0843   0.9154   0.0144
  -8.000  -0.5019   0.01476   0.00861  -0.0854   0.8992   0.0148
  -7.750  -0.4745   0.01422   0.00794  -0.0856   0.8794   0.0152
  -7.500  -0.4490   0.01379   0.00737  -0.0854   0.8596   0.0155
  -7.250  -0.4243   0.01343   0.00685  -0.0850   0.8409   0.0158
  -7.000  -0.4009   0.01296   0.00625  -0.0844   0.8230   0.0164
  -6.750  -0.3769   0.01257   0.00574  -0.0839   0.8068   0.0173
  -6.500  -0.3522   0.01226   0.00533  -0.0834   0.7923   0.0183
  -6.250  -0.3272   0.01200   0.00496  -0.0830   0.7786   0.0195
  -6.000  -0.3018   0.01177   0.00461  -0.0826   0.7659   0.0209
  -5.750  -0.2764   0.01149   0.00427  -0.0823   0.7540   0.0238
  -5.500  -0.2509   0.01119   0.00395  -0.0820   0.7431   0.0312
  -5.250  -0.2256   0.01087   0.00365  -0.0817   0.7329   0.0484
  -5.000  -0.1999   0.01059   0.00338  -0.0815   0.7230   0.0664
  -4.750  -0.1740   0.01030   0.00314  -0.0813   0.7139   0.0885
  -4.500  -0.1482   0.01001   0.00292  -0.0811   0.7055   0.1169
  -4.250  -0.1221   0.00972   0.00271  -0.0810   0.6969   0.1501
  -4.000  -0.0960   0.00943   0.00251  -0.0809   0.6894   0.1866
  -3.750  -0.0699   0.00911   0.00232  -0.0808   0.6818   0.2329
  -3.500  -0.0436   0.00885   0.00216  -0.0807   0.6748   0.2751
  -3.250  -0.0172   0.00859   0.00205  -0.0806   0.6677   0.3242
  -3.000   0.0095   0.00842   0.00198  -0.0805   0.6614   0.3734
  -2.750   0.0370   0.00833   0.00195  -0.0805   0.6548   0.4065
  -2.500   0.0646   0.00831   0.00191  -0.0804   0.6486   0.4231
  -2.250   0.0926   0.00829   0.00187  -0.0804   0.6429   0.4350
  -2.000   0.1206   0.00829   0.00183  -0.0805   0.6369   0.4463
  -1.750   0.1483   0.00828   0.00180  -0.0804   0.6314   0.4567
  -1.500   0.1764   0.00827   0.00178  -0.0805   0.6257   0.4660
  -1.250   0.2043   0.00828   0.00176  -0.0805   0.6203   0.4753
  -1.000   0.2321   0.00827   0.00175  -0.0805   0.6152   0.4841
  -0.750   0.2602   0.00828   0.00174  -0.0805   0.6097   0.4925
  -0.500   0.2880   0.00829   0.00174  -0.0805   0.6046   0.5005
  -0.250   0.3160   0.00830   0.00175  -0.0805   0.5997   0.5084
   0.000   0.3440   0.00830   0.00176  -0.0805   0.5943   0.5173
   0.250   0.3717   0.00832   0.00178  -0.0805   0.5894   0.5263
   0.500   0.3996   0.00834   0.00181  -0.0806   0.5846   0.5353
   0.750   0.4275   0.00834   0.00184  -0.0806   0.5793   0.5434
   1.250   0.4830   0.00839   0.00193  -0.0805   0.5696   0.5605
   1.500   0.5108   0.00841   0.00198  -0.0805   0.5642   0.5697
   1.750   0.5383   0.00846   0.00203  -0.0805   0.5593   0.5797
   2.000   0.5660   0.00847   0.00210  -0.0805   0.5541   0.5902
   2.250   0.5935   0.00850   0.00217  -0.0804   0.5485   0.6024
   2.500   0.6206   0.00855   0.00225  -0.0803   0.5427   0.6151
   2.750   0.6480   0.00857   0.00234  -0.0802   0.5353   0.6287
   3.000   0.6746   0.00862   0.00242  -0.0800   0.5276   0.6442
   3.250   0.7016   0.00864   0.00252  -0.0799   0.5196   0.6619
   3.500   0.7280   0.00869   0.00263  -0.0796   0.5120   0.6814
   4.000   0.7804   0.00877   0.00287  -0.0790   0.4932   0.7262
   4.250   0.8057   0.00882   0.00301  -0.0785   0.4830   0.7541
   4.500   0.8304   0.00886   0.00315  -0.0778   0.4720   0.7866
   4.750   0.8544   0.00890   0.00331  -0.0770   0.4599   0.8238
   5.000   0.8766   0.00895   0.00347  -0.0757   0.4466   0.8677
   5.250   0.8991   0.00902   0.00363  -0.0745   0.4306   0.9269
   5.500   0.9351   0.00923   0.00382  -0.0764   0.4084   1.0000
   5.750   0.9580   0.00954   0.00405  -0.0756   0.3844   1.0000
   6.000   0.9794   0.00993   0.00431  -0.0746   0.3533   1.0000
   6.250   0.9977   0.01053   0.00469  -0.0731   0.3065   1.0000
   6.500   1.0144   0.01124   0.00515  -0.0714   0.2586   1.0000
   6.750   1.0307   0.01197   0.00566  -0.0697   0.2150   1.0000
   7.000   1.0469   0.01269   0.00618  -0.0679   0.1767   1.0000
   7.250   1.0629   0.01338   0.00669  -0.0661   0.1438   1.0000
   7.500   1.0797   0.01399   0.00718  -0.0645   0.1194   1.0000
   7.750   1.0955   0.01463   0.00770  -0.0627   0.0974   1.0000
   8.000   1.1085   0.01534   0.00827  -0.0604   0.0746   1.0000
   8.250   1.1212   0.01594   0.00882  -0.0580   0.0593   1.0000
   8.500   1.1344   0.01653   0.00936  -0.0558   0.0487   1.0000
   8.750   1.1474   0.01714   0.00994  -0.0535   0.0403   1.0000
   9.250   1.1714   0.01850   0.01126  -0.0491   0.0252   1.0000
   9.500   1.1819   0.01930   0.01204  -0.0468   0.0184   1.0000
   9.750   1.1915   0.02017   0.01291  -0.0445   0.0132   1.0000
  10.000   1.2014   0.02106   0.01382  -0.0423   0.0108   1.0000
  10.250   1.2120   0.02195   0.01476  -0.0404   0.0094   1.0000
  10.500   1.2214   0.02297   0.01581  -0.0385   0.0083   1.0000
  10.750   1.2296   0.02411   0.01701  -0.0366   0.0075   1.0000
  11.000   1.2400   0.02515   0.01812  -0.0351   0.0072   1.0000
  11.250   1.2492   0.02633   0.01938  -0.0336   0.0068   1.0000
  11.500   1.2576   0.02762   0.02075  -0.0322   0.0066   1.0000
  11.750   1.2656   0.02901   0.02222  -0.0309   0.0062   1.0000
  12.000   1.2733   0.03047   0.02376  -0.0297   0.0061   1.0000
  12.250   1.2799   0.03208   0.02545  -0.0286   0.0060   1.0000
  12.500   1.2846   0.03392   0.02737  -0.0276   0.0057   1.0000
  12.750   1.2891   0.03584   0.02937  -0.0266   0.0055   1.0000
  13.000   1.2918   0.03800   0.03162  -0.0258   0.0054   1.0000
  13.250   1.2914   0.04052   0.03425  -0.0250   0.0052   1.0000
  13.500   1.2929   0.04296   0.03677  -0.0245   0.0051   1.0000
  13.750   1.2950   0.04538   0.03929  -0.0241   0.0050   1.0000
  14.000   1.2966   0.04795   0.04196  -0.0238   0.0050   1.0000
  14.250   1.2983   0.05056   0.04467  -0.0237   0.0049   1.0000
  14.500   1.2999   0.05327   0.04750  -0.0237   0.0049   1.0000
  14.750   1.2994   0.05633   0.05067  -0.0238   0.0048   1.0000
  15.000   1.2985   0.05952   0.05396  -0.0241   0.0048   1.0000
  15.250   1.2982   0.06273   0.05727  -0.0245   0.0047   1.0000
  15.500   1.2958   0.06632   0.06098  -0.0252   0.0046   1.0000
  15.750   1.2937   0.06998   0.06475  -0.0260   0.0046   1.0000
  16.000   1.2914   0.07376   0.06864  -0.0269   0.0045   1.0000
  16.250   1.2875   0.07788   0.07288  -0.0280   0.0045   1.0000
  16.500   1.2847   0.08196   0.07707  -0.0293   0.0044   1.0000
  16.750   1.2806   0.08634   0.08157  -0.0308   0.0043   1.0000
  17.000   1.2747   0.09111   0.08646  -0.0325   0.0043   1.0000
  17.250   1.2710   0.09564   0.09111  -0.0343   0.0043   1.0000
  17.500   1.2646   0.10073   0.09631  -0.0365   0.0042   1.0000
  17.750   1.2587   0.10585   0.10155  -0.0387   0.0041   1.0000
  18.000   1.2522   0.11116   0.10698  -0.0412   0.0041   1.0000
  18.250   1.2463   0.11648   0.11242  -0.0438   0.0041   1.0000
  18.500   1.2377   0.12238   0.11845  -0.0467   0.0040   1.0000
  18.750   1.2313   0.12800   0.12420  -0.0497   0.0040   1.0000
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