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E385 (8.41%) (e385-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: E385 (8.41%) (e385-il)
Reynolds number: 500,000
Max Cl/Cd: 133.12 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e385-il-500000-n5.txt
Download as CSV file: xf-e385-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E385  (8.41%)                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.2874   0.12974   0.12737  -0.0377   1.0000   0.0075
 -11.000  -0.2834   0.12706   0.12471  -0.0380   1.0000   0.0075
 -10.750  -0.2798   0.12440   0.12206  -0.0382   1.0000   0.0075
 -10.500  -0.2704   0.12094   0.11862  -0.0403   0.9992   0.0076
 -10.250  -0.2577   0.11645   0.11413  -0.0428   0.9976   0.0077
 -10.000  -0.2439   0.11272   0.11039  -0.0455   0.9948   0.0078
  -9.750  -0.2309   0.10935   0.10702  -0.0478   0.9919   0.0079
  -9.500  -0.2175   0.10582   0.10350  -0.0508   0.9883   0.0080
  -9.000  -0.1916   0.09917   0.09685  -0.0563   0.9777   0.0082
  -8.500  -0.1633   0.09240   0.09009  -0.0626   0.9625   0.0087
  -8.250  -0.1447   0.08866   0.08634  -0.0671   0.9530   0.0088
  -8.000  -0.1199   0.08440   0.08204  -0.0736   0.9437   0.0091
  -7.750  -0.0907   0.07964   0.07724  -0.0817   0.9297   0.0104
  -7.500  -0.0612   0.07484   0.07235  -0.0908   0.9075   0.0108
  -7.250  -0.0442   0.07103   0.06842  -0.0959   0.8785   0.0110
  -7.000  -0.0357   0.06844   0.06573  -0.0974   0.8534   0.0109
  -6.750  -0.0264   0.06541   0.06259  -0.0999   0.8319   0.0110
  -6.500  -0.0154   0.06234   0.05945  -0.1027   0.8145   0.0110
  -6.250   0.0069   0.04238   0.03947  -0.0923   0.7621   0.0118
  -5.750   0.0255   0.05182   0.04873  -0.1141   0.7742   0.0116
  -5.500   0.0434   0.05025   0.04711  -0.1157   0.7638   0.0126
  -5.250   0.0667   0.04660   0.04337  -0.1210   0.7542   0.0133
  -5.000   0.0942   0.04221   0.03887  -0.1274   0.7450   0.0136
  -4.000   0.2450   0.01558   0.01002  -0.1524   0.7170   0.0075
  -3.750   0.2765   0.01356   0.00753  -0.1537   0.7105   0.0077
  -3.500   0.3066   0.01228   0.00597  -0.1545   0.7037   0.0080
  -3.250   0.3356   0.01159   0.00511  -0.1549   0.6976   0.0084
  -3.000   0.3647   0.01105   0.00445  -0.1552   0.6912   0.0089
  -2.750   0.3936   0.01061   0.00387  -0.1555   0.6851   0.0094
  -2.500   0.4224   0.01032   0.00350  -0.1557   0.6792   0.0104
  -2.250   0.4511   0.01009   0.00318  -0.1559   0.6733   0.0111
  -2.000   0.4806   0.00966   0.00265  -0.1563   0.6679   0.0115
  -1.750   0.5098   0.00939   0.00232  -0.1566   0.6622   0.0123
  -1.500   0.5385   0.00925   0.00209  -0.1568   0.6568   0.0136
  -1.250   0.5672   0.00913   0.00190  -0.1570   0.6517   0.0156
  -1.000   0.5963   0.00892   0.00178  -0.1573   0.6461   0.0433
  -0.750   0.6250   0.00876   0.00173  -0.1576   0.6412   0.0938
  -0.500   0.6538   0.00862   0.00171  -0.1579   0.6361   0.1465
  -0.250   0.6828   0.00843   0.00173  -0.1584   0.6308   0.2398
   0.000   0.7116   0.00824   0.00178  -0.1588   0.6260   0.3507
   0.250   0.7407   0.00803   0.00185  -0.1593   0.6210   0.4735
   0.500   0.7694   0.00777   0.00196  -0.1597   0.6157   0.6303
   0.750   0.7956   0.00755   0.00207  -0.1593   0.6111   0.7742
   1.000   0.8134   0.00720   0.00204  -0.1567   0.6061   1.0000
   1.250   0.8415   0.00729   0.00207  -0.1568   0.6008   1.0000
   1.500   0.8695   0.00740   0.00212  -0.1569   0.5959   1.0000
   1.750   0.8977   0.00749   0.00218  -0.1570   0.5904   1.0000
   2.000   0.9255   0.00760   0.00224  -0.1570   0.5846   1.0000
   2.250   0.9532   0.00770   0.00231  -0.1570   0.5781   1.0000
   2.500   0.9807   0.00782   0.00240  -0.1570   0.5704   1.0000
   2.750   1.0083   0.00793   0.00249  -0.1570   0.5627   1.0000
   3.000   1.0355   0.00806   0.00259  -0.1569   0.5550   1.0000
   3.250   1.0629   0.00818   0.00270  -0.1569   0.5467   1.0000
   3.500   1.0897   0.00833   0.00283  -0.1567   0.5373   1.0000
   3.750   1.1167   0.00847   0.00296  -0.1566   0.5270   1.0000
   4.000   1.1436   0.00862   0.00310  -0.1565   0.5174   1.0000
   4.250   1.1701   0.00879   0.00327  -0.1563   0.5072   1.0000
   4.500   1.1963   0.00899   0.00344  -0.1561   0.4948   1.0000
   4.750   1.2222   0.00920   0.00363  -0.1558   0.4798   1.0000
   5.000   1.2468   0.00950   0.00385  -0.1554   0.4541   1.0000
   5.250   1.2698   0.00994   0.00415  -0.1546   0.4172   1.0000
   5.500   1.2902   0.01064   0.00457  -0.1535   0.3624   1.0000
   5.750   1.3063   0.01179   0.00526  -0.1519   0.2828   1.0000
   6.000   1.3227   0.01291   0.00599  -0.1503   0.2152   1.0000
   6.250   1.3402   0.01390   0.00670  -0.1489   0.1625   1.0000
   6.500   1.3589   0.01474   0.00733  -0.1477   0.1256   1.0000
   6.750   1.3766   0.01562   0.00802  -0.1463   0.0909   1.0000
   7.000   1.3938   0.01651   0.00874  -0.1448   0.0605   1.0000
   7.250   1.4088   0.01753   0.00959  -0.1430   0.0317   1.0000
   7.500   1.4233   0.01854   0.01049  -0.1410   0.0128   1.0000
   7.750   1.4410   0.01924   0.01121  -0.1395   0.0097   1.0000
   8.000   1.4582   0.01991   0.01194  -0.1379   0.0086   1.0000
   8.250   1.4735   0.02061   0.01271  -0.1360   0.0079   1.0000
   8.500   1.4864   0.02137   0.01355  -0.1337   0.0075   1.0000
   8.750   1.4993   0.02211   0.01437  -0.1315   0.0073   1.0000
   9.000   1.5111   0.02294   0.01531  -0.1292   0.0071   1.0000
   9.250   1.5218   0.02387   0.01633  -0.1268   0.0069   1.0000
   9.500   1.5315   0.02491   0.01747  -0.1245   0.0067   1.0000
   9.750   1.5402   0.02607   0.01872  -0.1221   0.0065   1.0000
  10.000   1.5478   0.02736   0.02011  -0.1198   0.0064   1.0000
  10.250   1.5545   0.02880   0.02165  -0.1176   0.0062   1.0000
  10.500   1.5603   0.03038   0.02334  -0.1155   0.0061   1.0000
  10.750   1.5653   0.03212   0.02519  -0.1135   0.0059   1.0000
  11.000   1.5697   0.03399   0.02716  -0.1117   0.0058   1.0000
  11.250   1.5733   0.03604   0.02931  -0.1100   0.0056   1.0000
  11.500   1.5759   0.03828   0.03165  -0.1084   0.0054   1.0000
  11.750   1.5766   0.04082   0.03431  -0.1070   0.0053   1.0000
  12.000   1.5750   0.04372   0.03732  -0.1056   0.0051   1.0000
  12.250   1.5723   0.04686   0.04058  -0.1043   0.0050   1.0000
  12.500   1.5687   0.05025   0.04410  -0.1032   0.0049   1.0000
  12.750   1.5686   0.05328   0.04725  -0.1024   0.0049   1.0000
  13.000   1.5705   0.05616   0.05026  -0.1018   0.0049   1.0000
  13.250   1.5721   0.05915   0.05339  -0.1013   0.0048   1.0000
  13.500   1.5729   0.06232   0.05669  -0.1010   0.0048   1.0000
  13.750   1.5734   0.06562   0.06013  -0.1007   0.0047   1.0000
  14.000   1.5732   0.06911   0.06377  -0.1007   0.0047   1.0000
  14.250   1.5727   0.07272   0.06752  -0.1007   0.0046   1.0000
  14.500   1.5710   0.07660   0.07155  -0.1009   0.0046   1.0000
  14.750   1.5691   0.08061   0.07571  -0.1013   0.0045   1.0000
  15.000   1.5663   0.08487   0.08014  -0.1019   0.0044   1.0000
  15.250   1.5627   0.08935   0.08478  -0.1027   0.0044   1.0000
  15.500   1.5581   0.09408   0.08967  -0.1038   0.0043   1.0000
  15.750   1.5529   0.09904   0.09480  -0.1051   0.0043   1.0000
  16.000   1.5466   0.10434   0.10028  -0.1067   0.0043   1.0000
  16.250   1.5399   0.10981   0.10592  -0.1086   0.0042   1.0000
  16.500   1.5321   0.11562   0.11190  -0.1108   0.0042   1.0000
  16.750   1.5233   0.12176   0.11824  -0.1135   0.0041   1.0000
  17.000   1.5146   0.12807   0.12473  -0.1165   0.0041   1.0000
  17.250   1.5050   0.13472   0.13155  -0.1199   0.0041   1.0000
  17.500   1.4950   0.14173   0.13874  -0.1238   0.0040   1.0000
  17.750   1.4843   0.14897   0.14615  -0.1280   0.0040   1.0000
  18.000   1.4733   0.15655   0.15390  -0.1327   0.0041   1.0000
  18.250   1.4623   0.16439   0.16191  -0.1378   0.0040   1.0000
  18.500   1.4501   0.17290   0.17059  -0.1435   0.0041   1.0000
  18.750   1.4376   0.18186   0.17971  -0.1496   0.0041   1.0000
  19.000   1.4263   0.19089   0.18888  -0.1559   0.0041   1.0000
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