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E475 (15.01%) (e475-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: E475 (15.01%) (e475-il)
Reynolds number: 500,000
Max Cl/Cd: 71.03 at α=10.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e475-il-500000-n5.txt
Download as CSV file: xf-e475-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E475  (15.01%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.1167   0.08840   0.08398  -0.0355   1.0000   0.0315
 -18.000  -1.1425   0.08133   0.07679  -0.0388   1.0000   0.0318
 -17.750  -1.1718   0.07391   0.06926  -0.0423   1.0000   0.0324
 -17.500  -1.1990   0.06692   0.06212  -0.0455   1.0000   0.0324
 -17.250  -1.2274   0.05976   0.05483  -0.0488   1.0000   0.0333
 -17.000  -1.2490   0.05361   0.04853  -0.0516   1.0000   0.0337
 -16.750  -1.2656   0.04823   0.04300  -0.0540   1.0000   0.0344
 -16.500  -1.2782   0.04362   0.03826  -0.0559   1.0000   0.0354
 -16.250  -1.2898   0.03944   0.03397  -0.0573   1.0000   0.0369
 -16.000  -1.2964   0.03619   0.03062  -0.0578   1.0000   0.0379
 -15.750  -1.3013   0.03345   0.02779  -0.0577   1.0000   0.0401
 -15.500  -1.3026   0.03128   0.02554  -0.0570   1.0000   0.0420
 -15.250  -1.3040   0.02931   0.02351  -0.0558   1.0000   0.0438
 -15.000  -1.3030   0.02770   0.02184  -0.0543   1.0000   0.0463
 -14.750  -1.2990   0.02643   0.02049  -0.0526   1.0000   0.0485
 -14.500  -1.2971   0.02510   0.01913  -0.0504   1.0000   0.0514
 -14.250  -1.2919   0.02406   0.01805  -0.0483   1.0000   0.0546
 -14.000  -1.2859   0.02313   0.01708  -0.0459   1.0000   0.0572
 -13.750  -1.2803   0.02225   0.01617  -0.0434   1.0000   0.0606
 -13.500  -1.2722   0.02156   0.01544  -0.0409   1.0000   0.0640
 -13.250  -1.2664   0.02082   0.01469  -0.0379   1.0000   0.0674
 -13.000  -1.2591   0.02023   0.01407  -0.0350   1.0000   0.0706
 -12.750  -1.2513   0.01975   0.01355  -0.0319   1.0000   0.0737
 -12.500  -1.2478   0.01923   0.01303  -0.0280   1.0000   0.0771
 -12.250  -1.2454   0.01884   0.01262  -0.0237   1.0000   0.0803
 -12.000  -1.2440   0.01856   0.01229  -0.0189   1.0000   0.0831
 -11.750  -1.2422   0.01822   0.01193  -0.0143   1.0000   0.0861
 -11.500  -1.2349   0.01782   0.01153  -0.0107   1.0000   0.0897
 -11.250  -1.2217   0.01747   0.01114  -0.0082   0.9998   0.0938
 -11.000  -1.1979   0.01700   0.01067  -0.0079   0.9984   0.0986
 -10.750  -1.1735   0.01660   0.01026  -0.0076   0.9970   0.1047
 -10.500  -1.1488   0.01619   0.00986  -0.0073   0.9955   0.1104
 -10.250  -1.1225   0.01584   0.00951  -0.0074   0.9941   0.1165
 -10.000  -1.0947   0.01552   0.00916  -0.0076   0.9929   0.1206
  -9.750  -1.0713   0.01518   0.00884  -0.0070   0.9914   0.1254
  -9.500  -1.0469   0.01491   0.00854  -0.0065   0.9898   0.1294
  -9.250  -1.0210   0.01466   0.00825  -0.0062   0.9882   0.1331
  -9.000  -0.9946   0.01436   0.00797  -0.0062   0.9865   0.1376
  -8.750  -0.9673   0.01413   0.00772  -0.0062   0.9852   0.1420
  -8.500  -0.9383   0.01393   0.00748  -0.0065   0.9839   0.1457
  -8.250  -0.9094   0.01366   0.00723  -0.0069   0.9827   0.1503
  -8.000  -0.8791   0.01345   0.00703  -0.0075   0.9818   0.1551
  -7.750  -0.8495   0.01327   0.00682  -0.0078   0.9805   0.1588
  -7.500  -0.8263   0.01306   0.00660  -0.0069   0.9775   0.1626
  -7.250  -0.7983   0.01285   0.00641  -0.0070   0.9750   0.1669
  -7.000  -0.7653   0.01265   0.00620  -0.0080   0.9728   0.1712
  -6.750  -0.7265   0.01244   0.00596  -0.0102   0.9706   0.1751
  -6.500  -0.6794   0.01209   0.00565  -0.0142   0.9685   0.1801
  -6.250  -0.6445   0.01181   0.00537  -0.0154   0.9612   0.1845
  -6.000  -0.6025   0.01151   0.00505  -0.0181   0.9554   0.1886
  -5.750  -0.5751   0.01128   0.00482  -0.0178   0.9479   0.1920
  -5.500  -0.5462   0.01105   0.00461  -0.0179   0.9414   0.1962
  -5.250  -0.5176   0.01087   0.00443  -0.0178   0.9363   0.2004
  -5.000  -0.4935   0.01074   0.00428  -0.0168   0.9289   0.2036
  -4.750  -0.4648   0.01055   0.00409  -0.0168   0.9227   0.2068
  -4.500  -0.4417   0.01039   0.00396  -0.0156   0.9138   0.2109
  -4.250  -0.4143   0.01022   0.00379  -0.0153   0.9050   0.2152
  -4.000  -0.3895   0.01009   0.00364  -0.0144   0.8910   0.2187
  -3.750  -0.3631   0.00994   0.00346  -0.0137   0.8668   0.2219
  -3.500  -0.3353   0.00977   0.00316  -0.0133   0.8154   0.2264
  -3.250  -0.3123   0.00984   0.00297  -0.0119   0.7488   0.2311
  -3.000  -0.2911   0.01001   0.00288  -0.0102   0.6834   0.2351
  -2.750  -0.2694   0.01017   0.00281  -0.0088   0.6247   0.2387
  -2.500  -0.2472   0.01027   0.00275  -0.0075   0.5742   0.2435
  -2.250  -0.2239   0.01036   0.00270  -0.0065   0.5317   0.2489
  -2.000  -0.1997   0.01045   0.00265  -0.0056   0.4958   0.2538
  -1.750  -0.1756   0.01049   0.00260  -0.0047   0.4630   0.2596
  -1.500  -0.1511   0.01055   0.00256  -0.0040   0.4319   0.2656
  -1.250  -0.1263   0.01061   0.00253  -0.0032   0.4042   0.2719
  -1.000  -0.1014   0.01062   0.00250  -0.0025   0.3823   0.2801
  -0.500  -0.0507   0.01065   0.00247  -0.0013   0.3477   0.2971
  -0.250  -0.0252   0.01068   0.00246  -0.0006   0.3325   0.3064
   0.000   0.0000   0.01069   0.00246   0.0000   0.3183   0.3183
   0.250   0.0252   0.01068   0.00246   0.0006   0.3064   0.3325
   0.500   0.0507   0.01065   0.00247   0.0013   0.2971   0.3477
   0.750   0.0759   0.01065   0.00248   0.0019   0.2881   0.3640
   1.000   0.1014   0.01062   0.00250   0.0025   0.2801   0.3826
   1.250   0.1262   0.01061   0.00253   0.0032   0.2720   0.4050
   1.500   0.1511   0.01055   0.00256   0.0039   0.2656   0.4314
   1.750   0.1757   0.01049   0.00260   0.0047   0.2596   0.4625
   2.000   0.1997   0.01045   0.00265   0.0056   0.2538   0.4958
   2.250   0.2239   0.01036   0.00270   0.0065   0.2489   0.5318
   2.500   0.2473   0.01027   0.00275   0.0075   0.2434   0.5738
   2.750   0.2694   0.01017   0.00281   0.0088   0.2387   0.6252
   3.000   0.2911   0.01001   0.00288   0.0102   0.2352   0.6837
   3.250   0.3123   0.00984   0.00297   0.0118   0.2310   0.7478
   3.500   0.3353   0.00977   0.00316   0.0132   0.2265   0.8155
   3.750   0.3631   0.00994   0.00345   0.0137   0.2219   0.8661
   4.000   0.3894   0.01009   0.00364   0.0144   0.2187   0.8905
   4.250   0.4143   0.01022   0.00379   0.0153   0.2151   0.9051
   4.500   0.4417   0.01039   0.00396   0.0156   0.2108   0.9138
   4.750   0.4648   0.01055   0.00408   0.0168   0.2067   0.9227
   5.000   0.4935   0.01074   0.00428   0.0168   0.2035   0.9290
   5.250   0.5178   0.01087   0.00443   0.0178   0.2003   0.9361
   5.500   0.5463   0.01105   0.00461   0.0178   0.1962   0.9415
   5.750   0.5751   0.01128   0.00482   0.0178   0.1920   0.9478
   6.000   0.6026   0.01151   0.00505   0.0181   0.1887   0.9554
   6.250   0.6445   0.01181   0.00537   0.0154   0.1846   0.9612
   6.500   0.6794   0.01209   0.00565   0.0142   0.1800   0.9685
   6.750   0.7266   0.01243   0.00596   0.0102   0.1751   0.9706
   7.000   0.7655   0.01265   0.00619   0.0080   0.1709   0.9728
   7.250   0.7984   0.01285   0.00641   0.0070   0.1669   0.9751
   7.500   0.8263   0.01306   0.00660   0.0069   0.1625   0.9775
   7.750   0.8494   0.01328   0.00682   0.0079   0.1590   0.9805
   8.000   0.8793   0.01345   0.00702   0.0074   0.1551   0.9818
   8.250   0.9095   0.01366   0.00723   0.0068   0.1504   0.9828
   8.500   0.9385   0.01393   0.00748   0.0064   0.1457   0.9840
   8.750   0.9675   0.01412   0.00772   0.0061   0.1420   0.9852
   9.000   0.9948   0.01436   0.00797   0.0061   0.1377   0.9866
   9.250   1.0212   0.01466   0.00825   0.0062   0.1330   0.9882
   9.500   1.0471   0.01491   0.00854   0.0064   0.1294   0.9899
   9.750   1.0715   0.01518   0.00883   0.0070   0.1253   0.9914
  10.000   1.0950   0.01552   0.00916   0.0076   0.1206   0.9930
  10.250   1.1228   0.01583   0.00950   0.0073   0.1165   0.9942
  10.500   1.1492   0.01618   0.00986   0.0073   0.1106   0.9956
  10.750   1.1738   0.01659   0.01026   0.0075   0.1044   0.9970
  11.000   1.1982   0.01701   0.01067   0.0078   0.0983   0.9985
  11.250   1.2222   0.01747   0.01113   0.0081   0.0937   0.9998
  11.500   1.2349   0.01782   0.01152   0.0107   0.0899   1.0000
  11.750   1.2425   0.01820   0.01192   0.0143   0.0863   1.0000
  12.000   1.2442   0.01855   0.01229   0.0189   0.0830   1.0000
  12.250   1.2456   0.01884   0.01261   0.0236   0.0803   1.0000
  12.500   1.2481   0.01922   0.01302   0.0279   0.0772   1.0000
  12.750   1.2517   0.01974   0.01354   0.0318   0.0738   1.0000
  13.000   1.2595   0.02022   0.01406   0.0349   0.0706   1.0000
  13.250   1.2667   0.02082   0.01469   0.0379   0.0672   1.0000
  13.500   1.2727   0.02155   0.01543   0.0408   0.0637   1.0000
  13.750   1.2810   0.02224   0.01616   0.0433   0.0607   1.0000
  14.000   1.2870   0.02311   0.01706   0.0458   0.0574   1.0000
  14.250   1.2929   0.02404   0.01803   0.0481   0.0547   1.0000
  14.500   1.2982   0.02507   0.01911   0.0503   0.0514   1.0000
  14.750   1.3004   0.02638   0.02045   0.0524   0.0486   1.0000
  15.000   1.3044   0.02767   0.02180   0.0542   0.0464   1.0000
  15.250   1.3060   0.02923   0.02343   0.0557   0.0442   1.0000
  15.500   1.3030   0.03132   0.02558   0.0569   0.0415   1.0000
  15.750   1.3026   0.03342   0.02776   0.0575   0.0398   1.0000
  16.000   1.2987   0.03608   0.03051   0.0576   0.0381   1.0000
  16.250   1.2911   0.03943   0.03396   0.0571   0.0367   1.0000
  16.500   1.2800   0.04355   0.03819   0.0557   0.0354   1.0000
  16.750   1.2684   0.04806   0.04283   0.0539   0.0344   1.0000
  17.000   1.2511   0.05353   0.04844   0.0514   0.0335   1.0000
  17.250   1.2264   0.06014   0.05519   0.0483   0.0324   1.0000
  17.500   1.2034   0.06656   0.06177   0.0454   0.0327   1.0000
  17.750   1.1730   0.07401   0.06935   0.0419   0.0321   1.0000
  18.000   1.1462   0.08107   0.07654   0.0387   0.0319   1.0000
  18.250   1.1192   0.08834   0.08391   0.0352   0.0315   1.0000
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