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EPPLER 603 AIRFOIL (e603-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 603 AIRFOIL (e603-il)
Reynolds number: 100,000
Max Cl/Cd: 22.56 at α=12°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e603-il-100000-n5.txt
Download as CSV file: xf-e603-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.3313   0.08952   0.08461  -0.0890   0.9153   0.0260
 -12.500  -0.3861   0.07233   0.06709  -0.1028   0.9010   0.0250
 -12.250  -0.4189   0.06305   0.05736  -0.1102   0.8816   0.0246
 -12.000  -0.4379   0.05739   0.05127  -0.1134   0.8624   0.0246
 -11.750  -0.4520   0.05330   0.04680  -0.1142   0.8459   0.0245
 -11.500  -0.4617   0.05015   0.04331  -0.1138   0.8322   0.0247
 -11.250  -0.4683   0.04737   0.04021  -0.1129   0.8213   0.0249
 -11.000  -0.4713   0.04497   0.03749  -0.1116   0.8116   0.0251
 -10.750  -0.4712   0.04272   0.03493  -0.1101   0.8036   0.0255
 -10.500  -0.4676   0.04063   0.03253  -0.1086   0.7958   0.0259
 -10.250  -0.4602   0.03874   0.03028  -0.1072   0.7896   0.0266
 -10.000  -0.4522   0.03682   0.02794  -0.1055   0.7828   0.0278
  -9.750  -0.4363   0.03565   0.02674  -0.1050   0.7770   0.0289
  -9.500  -0.4182   0.03440   0.02532  -0.1044   0.7724   0.0300
  -9.250  -0.3974   0.03306   0.02379  -0.1039   0.7672   0.0312
  -9.000  -0.3717   0.03167   0.02214  -0.1038   0.7628   0.0327
  -8.750  -0.3485   0.03057   0.02100  -0.1036   0.7589   0.0340
  -8.500  -0.3274   0.02968   0.02003  -0.1031   0.7555   0.0361
  -8.250  -0.3065   0.02889   0.01909  -0.1024   0.7513   0.0392
  -8.000  -0.2892   0.02812   0.01837  -0.1015   0.7470   0.0420
  -7.750  -0.2696   0.02735   0.01748  -0.1005   0.7432   0.0456
  -7.500  -0.2529   0.02664   0.01677  -0.0994   0.7398   0.0496
  -7.250  -0.2361   0.02601   0.01606  -0.0982   0.7365   0.0554
  -7.000  -0.2216   0.02546   0.01553  -0.0967   0.7328   0.0624
  -6.750  -0.2076   0.02489   0.01501  -0.0950   0.7294   0.0713
  -6.500  -0.1934   0.02436   0.01451  -0.0934   0.7264   0.0835
  -6.250  -0.1786   0.02386   0.01404  -0.0917   0.7237   0.1002
  -6.000  -0.1635   0.02331   0.01360  -0.0901   0.7212   0.1251
  -5.750  -0.1506   0.02284   0.01334  -0.0883   0.7178   0.1602
  -5.500  -0.1406   0.02229   0.01310  -0.0860   0.7143   0.2130
  -5.250  -0.1359   0.02158   0.01281  -0.0831   0.7111   0.2880
  -5.000  -0.1348   0.02076   0.01257  -0.0795   0.7084   0.3942
  -4.750  -0.0825   0.02323   0.01597  -0.0775   0.7067   0.5780
  -4.500  -0.0690   0.02349   0.01609  -0.0752   0.7045   0.6182
  -4.250  -0.0605   0.02353   0.01599  -0.0728   0.7017   0.6472
  -4.000  -0.0424   0.02416   0.01653  -0.0708   0.6983   0.6658
  -3.750  -0.0221   0.02477   0.01702  -0.0691   0.6952   0.6819
  -3.500  -0.0005   0.02537   0.01749  -0.0675   0.6927   0.6970
  -3.250   0.0219   0.02598   0.01797  -0.0660   0.6905   0.7119
  -3.000   0.0561   0.02690   0.01876  -0.0654   0.6885   0.7224
  -2.750   0.0840   0.02731   0.01902  -0.0647   0.6866   0.7324
  -2.500   0.0991   0.02762   0.01929  -0.0626   0.6834   0.7423
  -2.250   0.1191   0.02793   0.01955  -0.0611   0.6803   0.7486
  -2.000   0.1415   0.02815   0.01970  -0.0601   0.6776   0.7542
  -1.750   0.1531   0.02806   0.01952  -0.0582   0.6747   0.7628
  -1.500   0.1807   0.02811   0.01947  -0.0580   0.6725   0.7656
  -1.250   0.2069   0.02808   0.01933  -0.0579   0.6706   0.7692
  -1.000   0.2281   0.02802   0.01918  -0.0572   0.6688   0.7739
  -0.750   0.2290   0.02823   0.01943  -0.0537   0.6643   0.7800
  -0.500   0.2458   0.02840   0.01958  -0.0521   0.6608   0.7826
  -0.250   0.2656   0.02844   0.01958  -0.0511   0.6580   0.7857
   0.000   0.2871   0.02840   0.01946  -0.0506   0.6557   0.7890
   0.250   0.3103   0.02826   0.01924  -0.0506   0.6537   0.7928
   0.500   0.3357   0.02811   0.01900  -0.0509   0.6519   0.7958
   0.750   0.3308   0.02880   0.01981  -0.0462   0.6458   0.7985
   1.000   0.3457   0.02901   0.02002  -0.0446   0.6422   0.8012
   1.250   0.3685   0.02901   0.01998  -0.0443   0.6395   0.8035
   1.500   0.3956   0.02893   0.01984  -0.0447   0.6374   0.8056
   1.750   0.4256   0.02881   0.01965  -0.0457   0.6358   0.8081
   2.000   0.4127   0.02983   0.02078  -0.0409   0.6281   0.8122
   2.250   0.4293   0.03006   0.02101  -0.0396   0.6243   0.8138
   2.500   0.4552   0.03006   0.02100  -0.0397   0.6219   0.8153
   2.750   0.4855   0.02996   0.02087  -0.0404   0.6201   0.8169
   3.000   0.5187   0.02980   0.02069  -0.0415   0.6186   0.8187
   3.500   0.5150   0.03155   0.02256  -0.0350   0.6050   0.8243
   3.750   0.5513   0.03136   0.02236  -0.0369   0.6034   0.8257
   4.000   0.5899   0.03114   0.02211  -0.0390   0.6021   0.8273
   4.500   0.5778   0.03321   0.02432  -0.0311   0.5872   0.8322
   4.750   0.6140   0.03285   0.02399  -0.0325   0.5859   0.8333
   5.250   0.6188   0.03536   0.02660  -0.0286   0.5708   0.8380
   5.500   0.6555   0.03487   0.02614  -0.0298   0.5696   0.8396
   6.000   0.6710   0.03739   0.02877  -0.0281   0.5542   0.8440
   6.250   0.7062   0.03670   0.02812  -0.0288   0.5532   0.8451
   6.750   0.7166   0.03938   0.03095  -0.0262   0.5364   0.8487
   7.250   0.7335   0.04188   0.03359  -0.0246   0.5197   0.8532
   7.750   0.7750   0.04265   0.03450  -0.0247   0.5082   0.8571
   8.000   0.8115   0.04177   0.03368  -0.0256   0.5068   0.8586
   8.250   0.8065   0.04420   0.03620  -0.0243   0.4937   0.8605
   8.500   0.8398   0.04329   0.03537  -0.0246   0.4919   0.8620
   9.000   0.8708   0.04458   0.03683  -0.0237   0.4771   0.8658
   9.500   0.9058   0.04563   0.03806  -0.0232   0.4622   0.8705
  10.000   0.9458   0.04639   0.03901  -0.0232   0.4470   0.8750
  10.500   0.9849   0.04682   0.03962  -0.0224   0.4311   0.8791
  10.750   0.9909   0.04843   0.04133  -0.0218   0.4191   0.8814
  11.000   1.0304   0.04677   0.03975  -0.0221   0.4142   0.8839
  11.250   1.0372   0.04838   0.04145  -0.0216   0.4012   0.8864
  11.500   1.0518   0.04930   0.04244  -0.0214   0.3892   0.8891
  11.750   1.0759   0.04907   0.04229  -0.0211   0.3788   0.8919
  12.000   1.0998   0.04875   0.04199  -0.0207   0.3672   0.8952
  12.250   1.1103   0.04991   0.04322  -0.0201   0.3531   0.8988
  12.500   1.1227   0.05098   0.04432  -0.0198   0.3387   0.9024
  12.750   1.1348   0.05208   0.04546  -0.0194   0.3240   0.9061
  13.000   1.1446   0.05329   0.04669  -0.0188   0.3093   0.9098
  13.250   1.1537   0.05470   0.04812  -0.0183   0.2946   0.9140
  13.500   1.1619   0.05629   0.04972  -0.0180   0.2796   0.9186
  13.750   1.1685   0.05799   0.05143  -0.0176   0.2653   0.9236
  14.000   1.1742   0.05986   0.05333  -0.0173   0.2513   0.9299
  14.250   1.1788   0.06189   0.05537  -0.0171   0.2376   0.9377
  14.500   1.1825   0.06396   0.05745  -0.0169   0.2246   0.9503
  14.750   1.1836   0.06614   0.05965  -0.0168   0.2121   1.0000
  15.000   1.1876   0.06891   0.06247  -0.0175   0.1995   1.0000
  15.250   1.1915   0.07175   0.06534  -0.0183   0.1876   1.0000
  15.500   1.1952   0.07462   0.06824  -0.0190   0.1764   1.0000
  15.750   1.1981   0.07760   0.07119  -0.0199   0.1660   1.0000
  16.000   1.2003   0.08080   0.07447  -0.0208   0.1556   1.0000
  16.250   1.2020   0.08406   0.07778  -0.0218   0.1459   1.0000
  16.500   1.2028   0.08744   0.08114  -0.0228   0.1371   1.0000
  16.750   1.2031   0.09102   0.08480  -0.0240   0.1280   1.0000
  17.000   1.2031   0.09466   0.08849  -0.0253   0.1197   1.0000
  17.250   1.2015   0.09851   0.09234  -0.0267   0.1121   1.0000
  17.500   1.2008   0.10239   0.09633  -0.0282   0.1042   1.0000
  17.750   1.1988   0.10639   0.10033  -0.0298   0.0977   1.0000
  18.000   1.1975   0.11046   0.10451  -0.0315   0.0909   1.0000
  18.250   1.1954   0.11458   0.10864  -0.0334   0.0853   1.0000
  18.500   1.1939   0.11872   0.11289  -0.0353   0.0794   1.0000
  18.750   1.1916   0.12291   0.11708  -0.0373   0.0748   1.0000
  19.000   1.1905   0.12706   0.12137  -0.0394   0.0697   1.0000
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