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EPPLER 603 AIRFOIL (e603-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 603 AIRFOIL (e603-il)
Reynolds number: 200,000
Max Cl/Cd: 62.96 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e603-il-200000-n5.txt
Download as CSV file: xf-e603-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 603 AIRFOIL                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.4878   0.06846   0.06411  -0.1012   0.9054   0.0136
 -13.750  -0.5069   0.05849   0.05359  -0.1116   0.8729   0.0136
 -13.500  -0.5183   0.05304   0.04770  -0.1155   0.8418   0.0136
 -13.250  -0.5249   0.04952   0.04385  -0.1169   0.8198   0.0136
 -13.000  -0.5304   0.04660   0.04065  -0.1171   0.8034   0.0138
 -12.500  -0.5361   0.04196   0.03552  -0.1159   0.7793   0.0141
 -12.250  -0.5352   0.04011   0.03344  -0.1150   0.7702   0.0144
 -12.000  -0.5333   0.03829   0.03140  -0.1138   0.7619   0.0148
 -11.750  -0.5294   0.03657   0.02941  -0.1126   0.7550   0.0151
 -11.500  -0.5235   0.03491   0.02750  -0.1113   0.7481   0.0155
 -11.250  -0.5155   0.03339   0.02566  -0.1100   0.7419   0.0160
 -11.000  -0.5029   0.03209   0.02421  -0.1090   0.7367   0.0163
 -10.750  -0.4893   0.03096   0.02302  -0.1081   0.7313   0.0166
 -10.500  -0.4747   0.02993   0.02187  -0.1072   0.7264   0.0170
 -10.250  -0.4592   0.02898   0.02078  -0.1063   0.7224   0.0173
 -10.000  -0.4428   0.02802   0.01970  -0.1054   0.7186   0.0179
  -9.750  -0.4255   0.02710   0.01867  -0.1045   0.7146   0.0186
  -9.500  -0.4080   0.02624   0.01769  -0.1036   0.7109   0.0192
  -9.250  -0.3913   0.02542   0.01677  -0.1026   0.7075   0.0197
  -9.000  -0.3755   0.02471   0.01601  -0.1016   0.7045   0.0206
  -8.750  -0.3586   0.02404   0.01529  -0.1006   0.7013   0.0217
  -8.500  -0.3411   0.02341   0.01457  -0.0996   0.6978   0.0232
  -8.250  -0.3255   0.02272   0.01386  -0.0985   0.6945   0.0244
  -8.000  -0.3093   0.02211   0.01320  -0.0973   0.6915   0.0259
  -7.750  -0.2929   0.02151   0.01250  -0.0961   0.6889   0.0279
  -7.500  -0.2776   0.02090   0.01186  -0.0947   0.6867   0.0296
  -7.250  -0.2614   0.02039   0.01130  -0.0934   0.6842   0.0325
  -7.000  -0.2463   0.01988   0.01081  -0.0920   0.6816   0.0362
  -6.750  -0.2317   0.01943   0.01036  -0.0904   0.6790   0.0410
  -6.500  -0.2174   0.01903   0.00995  -0.0886   0.6766   0.0468
  -6.250  -0.2021   0.01864   0.00955  -0.0871   0.6742   0.0549
  -6.000  -0.1858   0.01819   0.00914  -0.0858   0.6719   0.0668
  -5.750  -0.1687   0.01778   0.00876  -0.0846   0.6698   0.0836
  -5.500  -0.1516   0.01736   0.00843  -0.0834   0.6677   0.1052
  -5.250  -0.1347   0.01691   0.00813  -0.0822   0.6655   0.1339
  -5.000  -0.1182   0.01641   0.00780  -0.0810   0.6633   0.1740
  -4.750  -0.1026   0.01580   0.00746  -0.0798   0.6612   0.2328
  -4.500  -0.0882   0.01501   0.00705  -0.0786   0.6590   0.3194
  -4.250  -0.0754   0.01396   0.00665  -0.0772   0.6568   0.4560
  -4.000  -0.0560   0.01435   0.00779  -0.0742   0.6549   0.6031
  -3.750  -0.0281   0.01476   0.00814  -0.0739   0.6532   0.6427
  -3.500   0.0001   0.01492   0.00816  -0.0742   0.6516   0.6633
  -3.250   0.0273   0.01509   0.00824  -0.0743   0.6496   0.6779
  -3.000   0.0541   0.01557   0.00869  -0.0736   0.6474   0.6862
  -2.750   0.0812   0.01589   0.00893  -0.0733   0.6451   0.6972
  -2.500   0.1080   0.01636   0.00934  -0.0728   0.6429   0.7088
  -2.250   0.1342   0.01700   0.00996  -0.0715   0.6411   0.7159
  -2.000   0.1609   0.01737   0.01026  -0.0710   0.6393   0.7241
  -1.750   0.1881   0.01752   0.01033  -0.0709   0.6376   0.7299
  -1.500   0.2155   0.01768   0.01040  -0.0706   0.6359   0.7321
  -1.250   0.2421   0.01774   0.01042  -0.0706   0.6341   0.7344
  -1.000   0.2677   0.01776   0.01042  -0.0705   0.6319   0.7371
  -0.750   0.2943   0.01770   0.01033  -0.0708   0.6296   0.7402
  -0.500   0.3228   0.01753   0.01008  -0.0719   0.6273   0.7443
  -0.250   0.3499   0.01751   0.01002  -0.0722   0.6251   0.7459
   0.000   0.3770   0.01753   0.01000  -0.0722   0.6232   0.7470
   0.250   0.4045   0.01755   0.00998  -0.0724   0.6214   0.7484
   0.500   0.4328   0.01757   0.00994  -0.0727   0.6196   0.7499
   0.750   0.4610   0.01759   0.00992  -0.0732   0.6179   0.7513
   1.000   0.4859   0.01763   0.01000  -0.0731   0.6153   0.7531
   1.250   0.5118   0.01767   0.01006  -0.0732   0.6126   0.7551
   1.500   0.5391   0.01768   0.01006  -0.0737   0.6101   0.7573
   1.750   0.5679   0.01766   0.01001  -0.0744   0.6078   0.7593
   2.000   0.5980   0.01761   0.00993  -0.0755   0.6056   0.7613
   2.250   0.6272   0.01760   0.00989  -0.0762   0.6037   0.7626
   2.500   0.6558   0.01764   0.00991  -0.0766   0.6019   0.7637
   2.750   0.6789   0.01777   0.01012  -0.0761   0.5990   0.7649
   3.000   0.7030   0.01787   0.01028  -0.0758   0.5957   0.7661
   3.250   0.7289   0.01794   0.01039  -0.0758   0.5928   0.7673
   3.500   0.7563   0.01796   0.01043  -0.0762   0.5901   0.7686
   3.750   0.7852   0.01796   0.01043  -0.0767   0.5878   0.7699
   4.000   0.8154   0.01796   0.01041  -0.0775   0.5857   0.7715
   4.250   0.8385   0.01811   0.01065  -0.0772   0.5820   0.7734
   4.500   0.8627   0.01821   0.01082  -0.0771   0.5781   0.7752
   4.750   0.8902   0.01824   0.01089  -0.0776   0.5747   0.7767
   5.000   0.9200   0.01821   0.01085  -0.0784   0.5717   0.7781
   5.250   0.9507   0.01815   0.01078  -0.0792   0.5691   0.7791
   5.500   0.9679   0.01835   0.01114  -0.0778   0.5638   0.7803
   5.750   0.9907   0.01840   0.01127  -0.0772   0.5591   0.7815
   6.000   1.0175   0.01833   0.01123  -0.0772   0.5551   0.7828
   6.250   1.0408   0.01838   0.01136  -0.0768   0.5506   0.7842
   6.500   1.0598   0.01852   0.01160  -0.0756   0.5445   0.7856
   6.750   1.0850   0.01847   0.01160  -0.0755   0.5397   0.7869
   7.000   1.1066   0.01855   0.01176  -0.0748   0.5341   0.7884
   7.250   1.1251   0.01868   0.01198  -0.0736   0.5272   0.7900
   7.500   1.1513   0.01859   0.01190  -0.0737   0.5218   0.7915
   7.750   1.1634   0.01887   0.01231  -0.0715   0.5132   0.7935
   8.000   1.1856   0.01883   0.01228  -0.0709   0.5065   0.7953
   8.250   1.1926   0.01915   0.01272  -0.0677   0.4973   0.7967
   8.500   1.2077   0.01934   0.01295  -0.0659   0.4886   0.7981
   8.750   1.2203   0.01964   0.01332  -0.0639   0.4785   0.7995
   9.000   1.2312   0.02007   0.01381  -0.0617   0.4672   0.8011
   9.250   1.2423   0.02054   0.01429  -0.0597   0.4546   0.8028
   9.500   1.2524   0.02112   0.01486  -0.0577   0.4413   0.8046
   9.750   1.2602   0.02187   0.01561  -0.0556   0.4268   0.8065
  10.000   1.2661   0.02281   0.01653  -0.0535   0.4111   0.8086
  10.250   1.2704   0.02396   0.01765  -0.0515   0.3946   0.8109
  10.500   1.2725   0.02526   0.01893  -0.0493   0.3781   0.8126
  10.750   1.2724   0.02676   0.02041  -0.0470   0.3607   0.8142
  11.000   1.2724   0.02839   0.02201  -0.0450   0.3439   0.8159
  11.250   1.2714   0.03018   0.02378  -0.0431   0.3267   0.8177
  11.500   1.2700   0.03210   0.02566  -0.0414   0.3098   0.8195
  11.750   1.2687   0.03411   0.02764  -0.0398   0.2933   0.8214
  12.000   1.2676   0.03620   0.02969  -0.0385   0.2772   0.8233
  12.250   1.2672   0.03832   0.03179  -0.0373   0.2618   0.8251
  12.500   1.2673   0.04051   0.03395  -0.0363   0.2469   0.8270
  12.750   1.2674   0.04272   0.03615  -0.0353   0.2327   0.8286
  13.000   1.2684   0.04490   0.03834  -0.0345   0.2199   0.8304
  13.250   1.2694   0.04718   0.04061  -0.0337   0.2071   0.8324
  13.500   1.2704   0.04955   0.04297  -0.0331   0.1953   0.8345
  13.750   1.2731   0.05184   0.04528  -0.0327   0.1835   0.8367
  14.000   1.2759   0.05420   0.04766  -0.0324   0.1719   0.8388
  14.250   1.2776   0.05675   0.05021  -0.0322   0.1603   0.8409
  14.500   1.2786   0.05946   0.05290  -0.0321   0.1486   0.8429
  14.750   1.2783   0.06231   0.05574  -0.0321   0.1373   0.8447
  15.000   1.2790   0.06508   0.05852  -0.0320   0.1260   0.8466
  15.250   1.2810   0.06780   0.06127  -0.0321   0.1161   0.8486
  15.500   1.2824   0.07065   0.06413  -0.0323   0.1071   0.8508
  16.000   1.2858   0.07647   0.07002  -0.0330   0.0916   0.8556
  16.250   1.2868   0.07961   0.07319  -0.0335   0.0853   0.8581
  16.500   1.2892   0.08256   0.07621  -0.0340   0.0790   0.8605
  16.750   1.2896   0.08574   0.07946  -0.0345   0.0738   0.8630
  17.000   1.2910   0.08886   0.08265  -0.0352   0.0683   0.8659
  17.250   1.2908   0.09224   0.08609  -0.0359   0.0637   0.8692
  17.500   1.2921   0.09553   0.08947  -0.0368   0.0590   0.8727
  17.750   1.2907   0.09919   0.09319  -0.0378   0.0551   0.8762
  18.000   1.2912   0.10253   0.09663  -0.0386   0.0510   0.8802
  18.250   1.2881   0.10647   0.10063  -0.0398   0.0476   0.8845
  18.500   1.2887   0.10991   0.10420  -0.0409   0.0440   0.8894
  18.750   1.2853   0.11388   0.10825  -0.0422   0.0410   0.8947
  19.000   1.2832   0.11767   0.11214  -0.0435   0.0383   0.9015
  19.250   1.2804   0.12147   0.11605  -0.0447   0.0357   0.9105
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