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E475 (15.01%) (e475-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: E475 (15.01%) (e475-il)
Reynolds number: 100,000
Max Cl/Cd: 36.29 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e475-il-100000-n5.txt
Download as CSV file: xf-e475-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7125   0.13987   0.13370  -0.0104   1.0000   0.0844
 -15.500  -0.9536   0.07890   0.07251  -0.0429   1.0000   0.1063
 -15.250  -0.8251   0.09819   0.09196  -0.0307   1.0000   0.1075
 -15.000  -0.7857   0.10231   0.09608  -0.0278   1.0000   0.1083
 -14.750  -1.0155   0.06098   0.05438  -0.0519   1.0000   0.1134
 -14.500  -1.0497   0.05409   0.04726  -0.0550   1.0000   0.1153
 -14.250  -1.0760   0.04900   0.04191  -0.0562   1.0000   0.1175
 -14.000  -1.0879   0.04592   0.03868  -0.0560   1.0000   0.1200
 -13.750  -1.0862   0.04443   0.03719  -0.0550   1.0000   0.1227
 -13.500  -1.0898   0.04259   0.03528  -0.0537   1.0000   0.1256
 -13.250  -1.0973   0.04060   0.03311  -0.0517   1.0000   0.1288
 -13.000  -1.1078   0.03855   0.03078  -0.0490   1.0000   0.1320
 -12.750  -1.1015   0.03777   0.03005  -0.0469   1.0000   0.1347
 -12.500  -1.0982   0.03695   0.02918  -0.0442   1.0000   0.1377
 -12.250  -1.0988   0.03595   0.02807  -0.0410   1.0000   0.1411
 -12.000  -1.1037   0.03482   0.02672  -0.0369   1.0000   0.1446
 -11.750  -1.1011   0.03409   0.02594  -0.0334   1.0000   0.1474
 -11.500  -1.0937   0.03360   0.02546  -0.0305   1.0000   0.1505
 -11.250  -1.0878   0.03296   0.02473  -0.0273   1.0000   0.1541
 -11.000  -1.0837   0.03209   0.02366  -0.0240   1.0000   0.1581
 -10.750  -1.0751   0.03140   0.02287  -0.0211   1.0000   0.1614
 -10.500  -1.0632   0.03099   0.02246  -0.0186   1.0000   0.1648
 -10.250  -1.0528   0.03043   0.02182  -0.0159   1.0000   0.1686
 -10.000  -1.0439   0.02969   0.02086  -0.0130   1.0000   0.1729
  -9.750  -1.0312   0.02911   0.02022  -0.0106   1.0000   0.1764
  -9.500  -1.0168   0.02871   0.01981  -0.0084   1.0000   0.1800
  -9.250  -1.0032   0.02817   0.01918  -0.0061   1.0000   0.1840
  -9.000  -0.9908   0.02753   0.01832  -0.0036   1.0000   0.1885
  -8.750  -0.9748   0.02703   0.01780  -0.0016   1.0000   0.1920
  -8.500  -0.9584   0.02660   0.01736   0.0003   1.0000   0.1957
  -8.250  -0.9425   0.02611   0.01677   0.0024   1.0000   0.1999
  -8.000  -0.9272   0.02555   0.01600   0.0045   1.0000   0.2046
  -7.750  -0.9090   0.02509   0.01557   0.0061   1.0000   0.2080
  -7.500  -0.8910   0.02468   0.01514   0.0079   1.0000   0.2120
  -7.250  -0.8733   0.02423   0.01461   0.0096   1.0000   0.2164
  -7.000  -0.8557   0.02376   0.01395   0.0114   1.0000   0.2210
  -6.750  -0.8363   0.02334   0.01360   0.0129   1.0000   0.2246
  -6.500  -0.8173   0.02296   0.01321   0.0144   1.0000   0.2289
  -6.250  -0.7981   0.02257   0.01274   0.0160   1.0000   0.2335
  -6.000  -0.7788   0.02218   0.01224   0.0175   1.0000   0.2380
  -5.750  -0.7590   0.02181   0.01194   0.0189   1.0000   0.2420
  -5.500  -0.7393   0.02149   0.01160   0.0203   1.0000   0.2467
  -5.250  -0.7194   0.02118   0.01121   0.0217   1.0000   0.2518
  -5.000  -0.6991   0.02085   0.01089   0.0230   1.0000   0.2560
  -4.750  -0.6792   0.02057   0.01064   0.0244   1.0000   0.2606
  -4.500  -0.6592   0.02032   0.01038   0.0257   1.0000   0.2659
  -4.250  -0.6345   0.02008   0.01010   0.0261   0.9987   0.2715
  -4.000  -0.5887   0.01988   0.00998   0.0223   0.9900   0.2782
  -3.750  -0.5398   0.01972   0.00978   0.0180   0.9808   0.2869
  -3.500  -0.4954   0.01939   0.00957   0.0147   0.9701   0.2944
  -3.250  -0.4530   0.01911   0.00929   0.0118   0.9589   0.3031
  -3.000  -0.4117   0.01876   0.00905   0.0093   0.9480   0.3113
  -2.750  -0.3665   0.01845   0.00877   0.0061   0.9382   0.3220
  -2.500  -0.3328   0.01805   0.00850   0.0051   0.9248   0.3311
  -2.250  -0.2992   0.01769   0.00821   0.0043   0.9103   0.3415
  -2.000  -0.2679   0.01731   0.00792   0.0040   0.8936   0.3534
  -1.750  -0.2386   0.01691   0.00764   0.0041   0.8740   0.3659
  -1.500  -0.2136   0.01655   0.00738   0.0052   0.8481   0.3795
  -1.250  -0.1779   0.01611   0.00705   0.0042   0.8195   0.3974
  -1.000  -0.1337   0.01564   0.00665   0.0018   0.7819   0.4214
  -0.750  -0.0867   0.01521   0.00621  -0.0011   0.7279   0.4513
  -0.500  -0.0512   0.01503   0.00593  -0.0019   0.6663   0.4836
  -0.250  -0.0244   0.01498   0.00581  -0.0011   0.6103   0.5193
   0.000   0.0000   0.01498   0.00578   0.0000   0.5612   0.5613
   0.250   0.0244   0.01498   0.00581   0.0011   0.5192   0.6103
   0.500   0.0512   0.01503   0.00593   0.0019   0.4835   0.6665
   0.750   0.0868   0.01521   0.00622   0.0011   0.4512   0.7281
   1.000   0.1339   0.01564   0.00665  -0.0018   0.4213   0.7822
   1.250   0.1779   0.01612   0.00705  -0.0042   0.3972   0.8196
   1.500   0.2135   0.01655   0.00738  -0.0051   0.3795   0.8480
   1.750   0.2384   0.01691   0.00764  -0.0041   0.3660   0.8739
   2.000   0.2678   0.01731   0.00792  -0.0040   0.3535   0.8936
   2.250   0.2991   0.01769   0.00821  -0.0043   0.3416   0.9103
   2.500   0.3327   0.01805   0.00850  -0.0051   0.3311   0.9248
   2.750   0.3665   0.01844   0.00877  -0.0060   0.3220   0.9382
   3.000   0.4117   0.01876   0.00905  -0.0093   0.3114   0.9481
   3.250   0.4531   0.01911   0.00929  -0.0119   0.3030   0.9590
   3.500   0.4956   0.01939   0.00957  -0.0147   0.2943   0.9702
   3.750   0.5398   0.01971   0.00978  -0.0180   0.2869   0.9809
   4.000   0.5888   0.01988   0.00998  -0.0223   0.2782   0.9901
   4.250   0.6345   0.02008   0.01010  -0.0261   0.2716   0.9987
   4.500   0.6590   0.02032   0.01037  -0.0257   0.2660   1.0000
   4.750   0.6791   0.02057   0.01064  -0.0243   0.2606   1.0000
   5.000   0.6990   0.02085   0.01088  -0.0230   0.2560   1.0000
   5.250   0.7192   0.02118   0.01121  -0.0217   0.2518   1.0000
   5.500   0.7392   0.02149   0.01160  -0.0203   0.2467   1.0000
   5.750   0.7589   0.02181   0.01193  -0.0188   0.2420   1.0000
   6.000   0.7787   0.02217   0.01224  -0.0174   0.2381   1.0000
   6.250   0.7980   0.02257   0.01273  -0.0159   0.2336   1.0000
   6.500   0.8172   0.02296   0.01321  -0.0144   0.2289   1.0000
   6.750   0.8362   0.02333   0.01360  -0.0129   0.2247   1.0000
   7.000   0.8556   0.02376   0.01395  -0.0114   0.2211   1.0000
   7.250   0.8732   0.02422   0.01460  -0.0096   0.2164   1.0000
   7.500   0.8910   0.02468   0.01515  -0.0078   0.2120   1.0000
   7.750   0.9089   0.02508   0.01557  -0.0061   0.2080   1.0000
   8.000   0.9271   0.02555   0.01600  -0.0045   0.2046   1.0000
   8.250   0.9424   0.02610   0.01676  -0.0023   0.1999   1.0000
   8.500   0.9583   0.02660   0.01736  -0.0003   0.1957   1.0000
   8.750   0.9748   0.02702   0.01779   0.0016   0.1920   1.0000
   9.000   0.9907   0.02752   0.01831   0.0036   0.1885   1.0000
   9.250   1.0032   0.02817   0.01918   0.0061   0.1840   1.0000
   9.500   1.0167   0.02870   0.01980   0.0084   0.1799   1.0000
   9.750   1.0312   0.02911   0.02022   0.0106   0.1764   1.0000
  10.000   1.0439   0.02968   0.02086   0.0130   0.1729   1.0000
  10.250   1.0529   0.03043   0.02181   0.0159   0.1687   1.0000
  10.500   1.0633   0.03098   0.02245   0.0186   0.1648   1.0000
  10.750   1.0752   0.03140   0.02286   0.0211   0.1614   1.0000
  11.000   1.0838   0.03209   0.02365   0.0240   0.1581   1.0000
  11.250   1.0880   0.03295   0.02472   0.0273   0.1541   1.0000
  11.500   1.0939   0.03359   0.02544   0.0304   0.1504   1.0000
  11.750   1.1013   0.03408   0.02593   0.0334   0.1474   1.0000
  12.000   1.1039   0.03481   0.02671   0.0369   0.1445   1.0000
  12.250   1.0993   0.03595   0.02806   0.0409   0.1410   1.0000
  12.500   1.0987   0.03693   0.02916   0.0442   0.1376   1.0000
  12.750   1.1022   0.03775   0.03002   0.0468   0.1346   1.0000
  13.000   1.1082   0.03855   0.03079   0.0489   0.1319   1.0000
  13.250   1.0981   0.04059   0.03310   0.0516   0.1287   1.0000
  13.500   1.0908   0.04258   0.03526   0.0536   0.1256   1.0000
  13.750   1.0874   0.04437   0.03714   0.0549   0.1226   1.0000
  14.000   1.0896   0.04584   0.03859   0.0558   0.1199   1.0000
  14.250   1.0767   0.04902   0.04193   0.0561   0.1175   1.0000
  14.500   1.0509   0.05406   0.04723   0.0549   0.1152   1.0000
  14.750   1.0172   0.06089   0.05428   0.0518   0.1132   1.0000
  15.000   0.7903   0.10170   0.09547   0.0280   0.1084   1.0000
  15.250   0.8301   0.09752   0.09130   0.0309   0.1076   1.0000
  15.500   0.9512   0.07950   0.07312   0.0423   0.1062   1.0000
  16.500   0.7156   0.13950   0.13334   0.0104   0.0844   1.0000
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