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EPPLER 395 AIRFOIL (e395-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 395 AIRFOIL (e395-il)
Reynolds number: 1,000,000
Max Cl/Cd: 144.11 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e395-il-1000000-n5.txt
Download as CSV file: xf-e395-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 395 AIRFOIL                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.4691   0.08554   0.08329  -0.0806   0.9918   0.0020
 -13.000  -0.4885   0.07679   0.07446  -0.0870   0.9891   0.0020
 -12.750  -0.5100   0.06764   0.06523  -0.0948   0.9857   0.0020
 -12.500  -0.5431   0.05745   0.05493  -0.1031   0.9785   0.0020
 -12.000  -0.5928   0.03056   0.02751  -0.1368   0.9422   0.0019
 -11.750  -0.5520   0.02331   0.01982  -0.1563   0.9271   0.0019
 -11.500  -0.5270   0.02121   0.01747  -0.1602   0.9095   0.0019
 -11.250  -0.5069   0.01980   0.01585  -0.1615   0.8935   0.0020
 -11.000  -0.4872   0.01865   0.01451  -0.1619   0.8801   0.0020
 -10.750  -0.4667   0.01764   0.01332  -0.1622   0.8682   0.0020
 -10.500  -0.4449   0.01678   0.01229  -0.1623   0.8574   0.0020
 -10.250  -0.4219   0.01600   0.01138  -0.1624   0.8481   0.0021
 -10.000  -0.3982   0.01533   0.01057  -0.1625   0.8397   0.0021
  -9.750  -0.3738   0.01470   0.00981  -0.1626   0.8312   0.0021
  -9.500  -0.3497   0.01385   0.00879  -0.1628   0.8235   0.0023
  -9.250  -0.3242   0.01326   0.00808  -0.1630   0.8161   0.0024
  -9.000  -0.2984   0.01275   0.00746  -0.1631   0.8094   0.0026
  -8.750  -0.2718   0.01230   0.00693  -0.1633   0.8027   0.0028
  -8.250  -0.2181   0.01155   0.00600  -0.1636   0.7906   0.0032
  -8.000  -0.1908   0.01122   0.00559  -0.1637   0.7845   0.0035
  -7.750  -0.1636   0.01089   0.00518  -0.1639   0.7790   0.0039
  -7.500  -0.1359   0.01056   0.00480  -0.1641   0.7734   0.0047
  -7.250  -0.1083   0.01028   0.00445  -0.1643   0.7678   0.0058
  -7.000  -0.0804   0.01000   0.00413  -0.1645   0.7628   0.0076
  -6.750  -0.0523   0.00971   0.00382  -0.1647   0.7576   0.0105
  -6.500  -0.0244   0.00947   0.00354  -0.1649   0.7525   0.0139
  -6.250   0.0037   0.00923   0.00328  -0.1652   0.7478   0.0183
  -6.000   0.0321   0.00902   0.00306  -0.1654   0.7428   0.0232
  -5.750   0.0603   0.00881   0.00285  -0.1657   0.7379   0.0298
  -5.500   0.0886   0.00861   0.00265  -0.1659   0.7335   0.0387
  -5.250   0.1172   0.00839   0.00246  -0.1662   0.7289   0.0501
  -5.000   0.1456   0.00821   0.00230  -0.1665   0.7242   0.0611
  -4.750   0.1739   0.00808   0.00216  -0.1667   0.7197   0.0708
  -4.500   0.2027   0.00793   0.00203  -0.1670   0.7155   0.0818
  -4.250   0.2314   0.00781   0.00192  -0.1672   0.7110   0.0925
  -4.000   0.2598   0.00771   0.00181  -0.1674   0.7065   0.1035
  -3.750   0.2884   0.00762   0.00172  -0.1676   0.7025   0.1143
  -3.500   0.3172   0.00752   0.00164  -0.1679   0.6982   0.1263
  -3.250   0.3458   0.00743   0.00157  -0.1681   0.6936   0.1411
  -3.000   0.3741   0.00738   0.00150  -0.1682   0.6894   0.1544
  -2.750   0.4030   0.00729   0.00145  -0.1685   0.6853   0.1690
  -2.500   0.4316   0.00723   0.00141  -0.1687   0.6808   0.1831
  -2.250   0.4600   0.00718   0.00137  -0.1689   0.6763   0.1986
  -2.000   0.4886   0.00713   0.00135  -0.1691   0.6721   0.2134
  -1.750   0.5173   0.00709   0.00133  -0.1693   0.6675   0.2288
  -1.500   0.5456   0.00706   0.00131  -0.1694   0.6627   0.2429
  -1.250   0.5739   0.00704   0.00131  -0.1696   0.6583   0.2588
  -1.000   0.6026   0.00701   0.00131  -0.1698   0.6535   0.2738
  -0.750   0.6309   0.00700   0.00132  -0.1699   0.6485   0.2898
  -0.500   0.6589   0.00700   0.00133  -0.1700   0.6438   0.3046
  -0.250   0.6875   0.00698   0.00135  -0.1702   0.6389   0.3216
   0.000   0.7156   0.00698   0.00138  -0.1703   0.6334   0.3389
   0.250   0.7435   0.00700   0.00141  -0.1703   0.6283   0.3556
   0.500   0.7719   0.00699   0.00145  -0.1705   0.6225   0.3737
   0.750   0.7996   0.00701   0.00150  -0.1705   0.6162   0.3924
   1.000   0.8276   0.00702   0.00155  -0.1706   0.6101   0.4125
   1.250   0.8552   0.00705   0.00161  -0.1706   0.6029   0.4328
   1.500   0.8828   0.00708   0.00168  -0.1706   0.5959   0.4544
   1.750   0.9103   0.00712   0.00176  -0.1706   0.5877   0.4769
   2.000   0.9376   0.00717   0.00184  -0.1706   0.5795   0.5003
   2.250   0.9643   0.00724   0.00193  -0.1704   0.5697   0.5252
   2.500   0.9914   0.00730   0.00204  -0.1703   0.5595   0.5507
   2.750   1.0181   0.00738   0.00215  -0.1702   0.5493   0.5772
   3.000   1.0443   0.00748   0.00227  -0.1699   0.5378   0.6044
   3.250   1.0703   0.00759   0.00242  -0.1697   0.5250   0.6325
   3.500   1.0963   0.00770   0.00256  -0.1694   0.5118   0.6618
   3.750   1.1219   0.00782   0.00272  -0.1690   0.4985   0.6928
   4.000   1.1471   0.00796   0.00290  -0.1686   0.4840   0.7264
   4.250   1.1715   0.00813   0.00310  -0.1680   0.4677   0.7619
   4.750   1.2167   0.00852   0.00355  -0.1661   0.4286   0.8498
   5.000   1.2329   0.00868   0.00377  -0.1636   0.4070   0.9223
   5.250   1.2531   0.00896   0.00399  -0.1622   0.3829   1.0000
   5.500   1.2739   0.00940   0.00430  -0.1610   0.3557   1.0000
   5.750   1.2931   0.00990   0.00465  -0.1596   0.3238   1.0000
   6.000   1.3120   0.01041   0.00501  -0.1581   0.2954   1.0000
   6.250   1.3299   0.01095   0.00541  -0.1564   0.2664   1.0000
   6.500   1.3464   0.01152   0.00583  -0.1545   0.2372   1.0000
   6.750   1.3603   0.01211   0.00628  -0.1520   0.2095   1.0000
   7.000   1.3717   0.01278   0.00679  -0.1492   0.1789   1.0000
   7.250   1.3845   0.01340   0.00728  -0.1466   0.1552   1.0000
   7.500   1.3990   0.01395   0.00776  -0.1444   0.1385   1.0000
   7.750   1.4125   0.01456   0.00828  -0.1420   0.1202   1.0000
   8.000   1.4236   0.01529   0.00891  -0.1394   0.1009   1.0000
   8.250   1.4350   0.01603   0.00956  -0.1368   0.0830   1.0000
   8.500   1.4461   0.01680   0.01026  -0.1343   0.0681   1.0000
   8.750   1.4580   0.01755   0.01096  -0.1320   0.0569   1.0000
   9.000   1.4690   0.01837   0.01173  -0.1296   0.0464   1.0000
   9.250   1.4803   0.01921   0.01254  -0.1274   0.0381   1.0000
   9.500   1.4913   0.02010   0.01341  -0.1252   0.0309   1.0000
   9.750   1.5024   0.02101   0.01431  -0.1231   0.0254   1.0000
  10.000   1.5131   0.02199   0.01528  -0.1211   0.0209   1.0000
  10.250   1.5233   0.02302   0.01632  -0.1191   0.0168   1.0000
  10.500   1.5341   0.02407   0.01737  -0.1172   0.0138   1.0000
  10.750   1.5449   0.02514   0.01847  -0.1155   0.0115   1.0000
  11.000   1.5546   0.02632   0.01967  -0.1137   0.0093   1.0000
  11.250   1.5644   0.02755   0.02092  -0.1120   0.0076   1.0000
  11.500   1.5746   0.02877   0.02219  -0.1104   0.0064   1.0000
  11.750   1.5837   0.03012   0.02357  -0.1088   0.0053   1.0000
  12.000   1.5931   0.03147   0.02496  -0.1074   0.0045   1.0000
  12.250   1.6015   0.03296   0.02650  -0.1059   0.0039   1.0000
  12.500   1.6105   0.03443   0.02803  -0.1046   0.0035   1.0000
  12.750   1.6189   0.03599   0.02965  -0.1033   0.0031   1.0000
  13.000   1.6264   0.03767   0.03138  -0.1020   0.0028   1.0000
  13.250   1.6337   0.03943   0.03320  -0.1009   0.0025   1.0000
  13.500   1.6411   0.04122   0.03505  -0.0998   0.0023   1.0000
  13.750   1.6480   0.04309   0.03700  -0.0988   0.0022   1.0000
  14.000   1.6542   0.04509   0.03906  -0.0978   0.0020   1.0000
  14.250   1.6598   0.04722   0.04126  -0.0969   0.0018   1.0000
  14.500   1.6644   0.04951   0.04363  -0.0961   0.0017   1.0000
  14.750   1.6682   0.05194   0.04613  -0.0954   0.0015   1.0000
  15.000   1.6731   0.05430   0.04857  -0.0948   0.0015   1.0000
  15.250   1.6771   0.05682   0.05117  -0.0942   0.0014   1.0000
  15.500   1.6805   0.05948   0.05392  -0.0938   0.0013   1.0000
  15.750   1.6833   0.06230   0.05682  -0.0935   0.0012   1.0000
  16.000   1.6856   0.06522   0.05983  -0.0933   0.0012   1.0000
  16.250   1.6870   0.06832   0.06302  -0.0932   0.0011   1.0000
  16.500   1.6877   0.07160   0.06638  -0.0933   0.0011   1.0000
  16.750   1.6877   0.07506   0.06994  -0.0934   0.0010   1.0000
  17.000   1.6867   0.07873   0.07371  -0.0938   0.0010   1.0000
  17.250   1.6852   0.08255   0.07763  -0.0943   0.0009   1.0000
  17.500   1.6826   0.08661   0.08179  -0.0949   0.0009   1.0000
  17.750   1.6790   0.09092   0.08621  -0.0958   0.0008   1.0000
  18.000   1.6748   0.09541   0.09081  -0.0968   0.0008   1.0000
  18.250   1.6690   0.10025   0.09577  -0.0981   0.0008   1.0000
  18.500   1.6621   0.10536   0.10099  -0.0996   0.0008   1.0000
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