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Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il)
Reynolds number: 200,000
Max Cl/Cd: 74.33 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eiffel385-il-200000-n5.txt
Download as CSV file: xf-eiffel385-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Eiffel 385 (S.T. Ae)                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.6700   0.07464   0.06989  -0.0747   1.0000   0.0422
 -16.250  -0.7030   0.06726   0.06240  -0.0793   1.0000   0.0423
 -16.000  -0.7292   0.06134   0.05640  -0.0825   1.0000   0.0424
 -15.750  -0.7550   0.05595   0.05093  -0.0852   1.0000   0.0425
 -15.500  -0.7841   0.05084   0.04576  -0.0872   1.0000   0.0426
 -15.250  -0.8201   0.04635   0.04126  -0.0875   1.0000   0.0425
 -15.000  -0.8562   0.04112   0.03593  -0.0894   1.0000   0.0424
 -14.750  -0.8654   0.03680   0.03139  -0.0921   0.9994   0.0427
 -14.500  -0.8398   0.03423   0.02875  -0.0962   0.9945   0.0435
 -14.250  -0.8141   0.03205   0.02645  -0.0994   0.9890   0.0444
 -14.000  -0.7868   0.03017   0.02442  -0.1021   0.9841   0.0454
 -13.750  -0.7615   0.02854   0.02265  -0.1037   0.9794   0.0464
 -13.500  -0.7365   0.02711   0.02107  -0.1048   0.9743   0.0474
 -13.250  -0.7070   0.02579   0.01957  -0.1065   0.9706   0.0485
 -13.000  -0.6833   0.02461   0.01830  -0.1068   0.9646   0.0497
 -12.750  -0.6552   0.02349   0.01711  -0.1078   0.9598   0.0512
 -12.500  -0.6234   0.02246   0.01596  -0.1092   0.9566   0.0534
 -12.250  -0.5998   0.02162   0.01499  -0.1088   0.9499   0.0554
 -12.000  -0.5705   0.02070   0.01403  -0.1096   0.9454   0.0578
 -11.750  -0.5375   0.01986   0.01311  -0.1109   0.9422   0.0613
 -11.500  -0.5119   0.01918   0.01237  -0.1106   0.9353   0.0651
 -11.250  -0.4805   0.01854   0.01168  -0.1113   0.9302   0.0709
 -11.000  -0.4452   0.01801   0.01111  -0.1127   0.9266   0.0783
 -10.750  -0.4167   0.01761   0.01065  -0.1126   0.9199   0.0854
 -10.500  -0.3850   0.01722   0.01013  -0.1131   0.9138   0.0923
 -10.250  -0.3491   0.01680   0.00965  -0.1144   0.9092   0.0985
 -10.000  -0.3212   0.01650   0.00917  -0.1141   0.9003   0.1033
  -9.750  -0.2880   0.01603   0.00870  -0.1149   0.8938   0.1080
  -9.500  -0.2580   0.01570   0.00829  -0.1151   0.8854   0.1129
  -9.250  -0.2258   0.01537   0.00782  -0.1156   0.8768   0.1173
  -9.000  -0.1966   0.01501   0.00746  -0.1156   0.8668   0.1217
  -8.750  -0.1647   0.01470   0.00708  -0.1160   0.8570   0.1265
  -8.500  -0.1367   0.01445   0.00675  -0.1157   0.8451   0.1322
  -8.250  -0.1069   0.01425   0.00656  -0.1158   0.8334   0.1393
  -8.000  -0.0769   0.01405   0.00626  -0.1158   0.8207   0.1454
  -7.750  -0.0491   0.01393   0.00612  -0.1154   0.8063   0.1505
  -7.500  -0.0209   0.01376   0.00587  -0.1150   0.7921   0.1553
  -7.250   0.0072   0.01362   0.00564  -0.1147   0.7777   0.1597
  -7.000   0.0352   0.01355   0.00549  -0.1143   0.7635   0.1653
  -6.750   0.0631   0.01346   0.00528  -0.1139   0.7499   0.1720
  -6.500   0.0902   0.01343   0.00518  -0.1133   0.7364   0.1777
  -6.250   0.1175   0.01339   0.00500  -0.1128   0.7240   0.1847
  -6.000   0.1446   0.01335   0.00490  -0.1123   0.7129   0.1901
  -5.750   0.1716   0.01335   0.00479  -0.1118   0.7023   0.1962
  -5.500   0.1986   0.01334   0.00466  -0.1113   0.6927   0.2018
  -5.250   0.2253   0.01330   0.00459  -0.1108   0.6837   0.2070
  -5.000   0.2522   0.01330   0.00452  -0.1104   0.6753   0.2126
  -4.750   0.2792   0.01332   0.00443  -0.1099   0.6669   0.2173
  -4.500   0.3056   0.01325   0.00435  -0.1094   0.6586   0.2215
  -4.250   0.3319   0.01323   0.00429  -0.1089   0.6497   0.2256
  -4.000   0.3585   0.01323   0.00424  -0.1084   0.6415   0.2298
  -3.750   0.3850   0.01324   0.00419  -0.1079   0.6336   0.2336
  -3.250   0.4379   0.01320   0.00415  -0.1070   0.6202   0.2416
  -3.000   0.4644   0.01321   0.00415  -0.1065   0.6136   0.2470
  -2.750   0.4912   0.01326   0.00414  -0.1061   0.6077   0.2517
  -2.500   0.5173   0.01324   0.00417  -0.1056   0.6009   0.2562
  -2.250   0.5434   0.01324   0.00420  -0.1052   0.5944   0.2613
  -2.000   0.5698   0.01327   0.00423  -0.1047   0.5884   0.2663
  -1.750   0.5957   0.01329   0.00428  -0.1042   0.5813   0.2716
  -1.500   0.6216   0.01331   0.00434  -0.1037   0.5748   0.2787
  -1.250   0.6474   0.01333   0.00442  -0.1032   0.5680   0.2876
  -1.000   0.6729   0.01335   0.00451  -0.1027   0.5607   0.2967
  -0.750   0.6987   0.01341   0.00458  -0.1022   0.5543   0.3080
  -0.500   0.7238   0.01342   0.00471  -0.1016   0.5461   0.3228
  -0.250   0.7490   0.01348   0.00480  -0.1010   0.5385   0.3408
   0.000   0.7740   0.01352   0.00493  -0.1004   0.5306   0.3605
   0.250   0.7986   0.01358   0.00503  -0.0997   0.5222   0.3798
   0.500   0.8231   0.01362   0.00515  -0.0990   0.5133   0.3984
   0.750   0.8470   0.01367   0.00524  -0.0982   0.5041   0.4172
   1.000   0.8711   0.01371   0.00538  -0.0975   0.4947   0.4384
   1.500   0.9476   0.01297   0.00581  -0.1021   0.4709   1.0000
   1.750   0.9702   0.01317   0.00597  -0.1011   0.4580   1.0000
   2.000   0.9924   0.01340   0.00613  -0.1001   0.4450   1.0000
   2.250   1.0140   0.01365   0.00631  -0.0990   0.4319   1.0000
   2.500   1.0351   0.01393   0.00652  -0.0978   0.4187   1.0000
   2.750   1.0562   0.01421   0.00675  -0.0966   0.4048   1.0000
   3.000   1.0768   0.01451   0.00700  -0.0954   0.3915   1.0000
   3.250   1.0973   0.01484   0.00728  -0.0941   0.3801   1.0000
   3.500   1.1172   0.01518   0.00758  -0.0929   0.3692   1.0000
   3.750   1.1373   0.01552   0.00789  -0.0916   0.3576   1.0000
   4.000   1.1562   0.01589   0.00822  -0.0902   0.3466   1.0000
   4.250   1.1733   0.01631   0.00858  -0.0885   0.3341   1.0000
   4.500   1.1909   0.01670   0.00895  -0.0869   0.3210   1.0000
   4.750   1.2075   0.01710   0.00933  -0.0851   0.3097   1.0000
   5.000   1.2220   0.01755   0.00974  -0.0830   0.2993   1.0000
   5.250   1.2377   0.01797   0.01017  -0.0811   0.2883   1.0000
   5.500   1.2524   0.01843   0.01062  -0.0791   0.2770   1.0000
   5.750   1.2655   0.01896   0.01113  -0.0769   0.2645   1.0000
   6.000   1.2790   0.01950   0.01166  -0.0749   0.2525   1.0000
   6.250   1.2930   0.02005   0.01223  -0.0730   0.2401   1.0000
   6.500   1.3045   0.02071   0.01287  -0.0709   0.2253   1.0000
   6.750   1.3141   0.02150   0.01361  -0.0686   0.2079   1.0000
   7.000   1.3204   0.02249   0.01452  -0.0661   0.1858   1.0000
   7.250   1.3221   0.02381   0.01569  -0.0632   0.1567   1.0000
   7.500   1.3195   0.02550   0.01719  -0.0602   0.1282   1.0000
   7.750   1.3193   0.02718   0.01877  -0.0576   0.1097   1.0000
   8.000   1.3214   0.02881   0.02037  -0.0555   0.0970   1.0000
   8.250   1.3247   0.03044   0.02199  -0.0537   0.0879   1.0000
   8.500   1.3276   0.03218   0.02373  -0.0521   0.0815   1.0000
   8.750   1.3319   0.03388   0.02548  -0.0508   0.0769   1.0000
   9.000   1.3348   0.03579   0.02743  -0.0495   0.0735   1.0000
   9.250   1.3368   0.03785   0.02955  -0.0485   0.0709   1.0000
   9.500   1.3402   0.03988   0.03165  -0.0476   0.0688   1.0000
   9.750   1.3426   0.04207   0.03392  -0.0469   0.0670   1.0000
  10.000   1.3436   0.04448   0.03640  -0.0463   0.0654   1.0000
  10.250   1.3431   0.04712   0.03910  -0.0458   0.0640   1.0000
  10.500   1.3411   0.04999   0.04202  -0.0454   0.0627   1.0000
  10.750   1.3414   0.05268   0.04480  -0.0451   0.0616   1.0000
  11.000   1.3431   0.05526   0.04749  -0.0449   0.0604   1.0000
  11.250   1.3440   0.05798   0.05030  -0.0449   0.0591   1.0000
  11.500   1.3445   0.06081   0.05321  -0.0449   0.0578   1.0000
  11.750   1.3438   0.06382   0.05629  -0.0450   0.0566   1.0000
  12.000   1.3420   0.06700   0.05952  -0.0451   0.0553   1.0000
  12.250   1.3395   0.07028   0.06282  -0.0453   0.0542   1.0000
  12.500   1.3404   0.07321   0.06584  -0.0456   0.0531   1.0000
  12.750   1.3428   0.07605   0.06879  -0.0460   0.0520   1.0000
  13.000   1.3444   0.07899   0.07183  -0.0464   0.0509   1.0000
  13.250   1.3454   0.08205   0.07498  -0.0469   0.0497   1.0000
  13.500   1.3466   0.08512   0.07812  -0.0475   0.0487   1.0000
  13.750   1.3469   0.08834   0.08140  -0.0481   0.0476   1.0000
  14.000   1.3475   0.09143   0.08451  -0.0487   0.0466   1.0000
  14.250   1.3492   0.09442   0.08756  -0.0493   0.0457   1.0000
  14.500   1.3506   0.09767   0.09096  -0.0502   0.0446   1.0000
  14.750   1.3520   0.10089   0.09429  -0.0511   0.0436   1.0000
  15.000   1.3527   0.10426   0.09776  -0.0522   0.0425   1.0000
  15.250   1.3530   0.10770   0.10128  -0.0534   0.0414   1.0000
  15.500   1.3538   0.11100   0.10464  -0.0545   0.0406   1.0000
  15.750   1.3549   0.11420   0.10786  -0.0556   0.0397   1.0000
  16.000   1.3545   0.11788   0.11167  -0.0571   0.0387   1.0000
  16.250   1.3540   0.12160   0.11555  -0.0586   0.0377   1.0000
  16.500   1.3532   0.12539   0.11946  -0.0602   0.0367   1.0000
  16.750   1.3524   0.12917   0.12334  -0.0620   0.0357   1.0000
  17.000   1.3519   0.13291   0.12714  -0.0638   0.0348   1.0000
  17.250   1.3517   0.13655   0.13082  -0.0656   0.0341   1.0000
  17.500   1.3499   0.14059   0.13499  -0.0677   0.0332   1.0000
  17.750   1.3467   0.14497   0.13953  -0.0699   0.0321   1.0000
  18.000   1.3446   0.14912   0.14380  -0.0722   0.0312   1.0000
  18.250   1.3423   0.15335   0.14813  -0.0746   0.0304   1.0000
  18.500   1.3409   0.15741   0.15225  -0.0770   0.0297   1.0000
  18.750   1.3400   0.16133   0.15621  -0.0793   0.0291   1.0000
  19.000   1.3347   0.16623   0.16127  -0.0822   0.0283   1.0000
  19.250   1.3277   0.17159   0.16680  -0.0854   0.0274   1.0000
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