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Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il)
Reynolds number: 1,000,000
Max Cl/Cd: 123.41 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-eiffel385-il-1000000.txt
Download as CSV file: xf-eiffel385-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.8357   0.08945   0.08659  -0.0724   1.0000   0.0266
 -19.500  -0.8391   0.08593   0.08304  -0.0741   1.0000   0.0270
 -19.250  -0.8425   0.08238   0.07947  -0.0758   1.0000   0.0272
 -19.000  -0.8492   0.07838   0.07543  -0.0779   1.0000   0.0274
 -18.750  -0.8551   0.07458   0.07161  -0.0798   1.0000   0.0277
 -18.500  -0.8622   0.07073   0.06774  -0.0817   1.0000   0.0278
 -18.250  -0.8745   0.06631   0.06326  -0.0841   1.0000   0.0280
 -18.000  -0.8882   0.06204   0.05895  -0.0863   1.0000   0.0282
 -17.750  -0.9091   0.05717   0.05403  -0.0889   1.0000   0.0283
 -17.500  -0.9361   0.05194   0.04875  -0.0914   1.0000   0.0283
 -17.250  -0.9819   0.04579   0.04254  -0.0935   1.0000   0.0282
 -17.000  -1.0736   0.03326   0.02977  -0.1022   0.9987   0.0277
 -16.750  -1.0499   0.02823   0.02454  -0.1099   0.9963   0.0280
 -16.500  -1.0222   0.02618   0.02238  -0.1131   0.9943   0.0286
 -16.250  -0.9944   0.02458   0.02068  -0.1154   0.9925   0.0290
 -16.000  -0.9683   0.02333   0.01933  -0.1165   0.9895   0.0294
 -15.750  -0.9398   0.02219   0.01809  -0.1179   0.9869   0.0298
 -15.500  -0.9087   0.02129   0.01711  -0.1192   0.9850   0.0302
 -15.250  -0.8781   0.02019   0.01590  -0.1208   0.9833   0.0306
 -15.000  -0.8483   0.01874   0.01438  -0.1226   0.9819   0.0314
 -14.750  -0.8252   0.01786   0.01344  -0.1221   0.9771   0.0319
 -14.500  -0.7962   0.01709   0.01261  -0.1227   0.9744   0.0324
 -14.250  -0.7652   0.01639   0.01185  -0.1235   0.9725   0.0330
 -14.000  -0.7329   0.01577   0.01117  -0.1245   0.9710   0.0337
 -13.750  -0.6995   0.01519   0.01053  -0.1255   0.9697   0.0343
 -13.500  -0.6695   0.01470   0.00997  -0.1259   0.9669   0.0348
 -13.250  -0.6427   0.01410   0.00930  -0.1256   0.9622   0.0353
 -13.000  -0.6126   0.01333   0.00848  -0.1262   0.9589   0.0364
 -12.750  -0.5795   0.01277   0.00787  -0.1272   0.9562   0.0373
 -12.500  -0.5494   0.01233   0.00738  -0.1274   0.9517   0.0382
 -12.250  -0.5208   0.01195   0.00696  -0.1273   0.9454   0.0393
 -12.000  -0.4878   0.01158   0.00652  -0.1280   0.9409   0.0402
 -11.750  -0.4609   0.01108   0.00598  -0.1277   0.9338   0.0420
 -11.500  -0.4316   0.01068   0.00554  -0.1277   0.9267   0.0439
 -11.250  -0.4030   0.01038   0.00518  -0.1275   0.9191   0.0458
 -11.000  -0.3762   0.00996   0.00474  -0.1270   0.9103   0.0503
 -10.750  -0.3499   0.00956   0.00434  -0.1264   0.9020   0.0587
 -10.500  -0.3239   0.00917   0.00403  -0.1258   0.8928   0.0757
 -10.250  -0.2968   0.00902   0.00388  -0.1252   0.8835   0.0853
 -10.000  -0.2695   0.00888   0.00374  -0.1247   0.8732   0.0914
  -9.750  -0.2422   0.00884   0.00364  -0.1240   0.8625   0.0946
  -9.500  -0.2156   0.00870   0.00344  -0.1234   0.8510   0.0981
  -9.250  -0.1893   0.00859   0.00329  -0.1226   0.8374   0.1014
  -9.000  -0.1629   0.00852   0.00315  -0.1218   0.8220   0.1041
  -8.750  -0.1367   0.00848   0.00303  -0.1210   0.8047   0.1059
  -8.500  -0.1112   0.00844   0.00288  -0.1201   0.7846   0.1079
  -8.250  -0.0865   0.00834   0.00269  -0.1191   0.7619   0.1113
  -8.000  -0.0618   0.00829   0.00256  -0.1181   0.7378   0.1142
  -7.750  -0.0369   0.00829   0.00244  -0.1171   0.7152   0.1165
  -7.250   0.0143   0.00825   0.00222  -0.1154   0.6810   0.1220
  -7.000   0.0404   0.00817   0.00212  -0.1147   0.6691   0.1264
  -6.750   0.0665   0.00813   0.00203  -0.1141   0.6587   0.1304
  -6.500   0.0933   0.00807   0.00194  -0.1135   0.6496   0.1358
  -6.250   0.1195   0.00801   0.00188  -0.1129   0.6403   0.1452
  -6.000   0.1464   0.00795   0.00187  -0.1124   0.6319   0.1615
  -5.750   0.1732   0.00799   0.00189  -0.1118   0.6244   0.1738
  -5.500   0.2012   0.00797   0.00190  -0.1115   0.6195   0.1819
  -5.250   0.2290   0.00801   0.00192  -0.1112   0.6139   0.1876
  -5.000   0.2565   0.00809   0.00194  -0.1108   0.6083   0.1905
  -4.750   0.2839   0.00803   0.00190  -0.1104   0.6036   0.1957
  -4.500   0.3118   0.00803   0.00191  -0.1101   0.5987   0.1998
  -4.250   0.3393   0.00806   0.00192  -0.1098   0.5937   0.2028
  -4.000   0.3664   0.00812   0.00193  -0.1094   0.5884   0.2051
  -3.750   0.3946   0.00813   0.00193  -0.1092   0.5843   0.2065
  -3.500   0.4219   0.00808   0.00189  -0.1089   0.5794   0.2094
  -3.250   0.4489   0.00806   0.00186  -0.1085   0.5743   0.2125
  -3.000   0.4758   0.00808   0.00187  -0.1081   0.5693   0.2151
  -2.750   0.5036   0.00805   0.00187  -0.1079   0.5645   0.2174
  -2.500   0.5309   0.00806   0.00187  -0.1076   0.5591   0.2195
  -2.250   0.5577   0.00811   0.00188  -0.1072   0.5537   0.2216
  -2.000   0.5853   0.00811   0.00190  -0.1069   0.5486   0.2231
  -1.750   0.6125   0.00811   0.00190  -0.1066   0.5425   0.2255
  -1.500   0.6387   0.00812   0.00190  -0.1062   0.5363   0.2294
  -1.250   0.6659   0.00811   0.00192  -0.1059   0.5307   0.2322
  -1.000   0.6927   0.00813   0.00194  -0.1056   0.5236   0.2348
  -0.750   0.7189   0.00818   0.00197  -0.1051   0.5164   0.2373
  -0.500   0.7459   0.00820   0.00200  -0.1049   0.5083   0.2397
  -0.250   0.7716   0.00827   0.00204  -0.1044   0.4985   0.2422
   0.000   0.7977   0.00829   0.00208  -0.1040   0.4881   0.2488
   0.250   0.8231   0.00835   0.00214  -0.1034   0.4766   0.2562
   0.500   0.8478   0.00843   0.00222  -0.1028   0.4629   0.2690
   0.750   0.8719   0.00849   0.00233  -0.1021   0.4492   0.3016
   1.000   0.8964   0.00854   0.00247  -0.1015   0.4356   0.3504
   1.250   0.9210   0.00865   0.00260  -0.1008   0.4228   0.3761
   1.500   0.9449   0.00880   0.00273  -0.1001   0.4078   0.3933
   1.750   0.9682   0.00897   0.00288  -0.0993   0.3913   0.4078
   2.000   0.9912   0.00916   0.00303  -0.0984   0.3749   0.4228
   2.250   1.0140   0.00933   0.00319  -0.0976   0.3600   0.4428
   2.500   1.0355   0.00941   0.00339  -0.0965   0.3471   0.5065
   2.750   1.1008   0.00892   0.00386  -0.1054   0.3299   1.0000
   3.000   1.1237   0.00915   0.00404  -0.1045   0.3186   1.0000
   3.250   1.1467   0.00937   0.00422  -0.1037   0.3078   1.0000
   3.500   1.1688   0.00963   0.00442  -0.1028   0.2970   1.0000
   3.750   1.1913   0.00987   0.00461  -0.1019   0.2862   1.0000
   4.000   1.2135   0.01011   0.00482  -0.1010   0.2756   1.0000
   4.250   1.2346   0.01040   0.00505  -0.0999   0.2641   1.0000
   4.500   1.2558   0.01068   0.00528  -0.0989   0.2523   1.0000
   4.750   1.2761   0.01099   0.00554  -0.0977   0.2385   1.0000
   5.000   1.2938   0.01141   0.00585  -0.0961   0.2201   1.0000
   5.250   1.3085   0.01188   0.00621  -0.0938   0.1978   1.0000
   5.500   1.3160   0.01262   0.00673  -0.0904   0.1629   1.0000
   5.750   1.3167   0.01370   0.00753  -0.0859   0.1194   1.0000
   6.000   1.3215   0.01467   0.00830  -0.0823   0.0879   1.0000
   6.250   1.3300   0.01551   0.00901  -0.0795   0.0686   1.0000
   6.500   1.3441   0.01611   0.00957  -0.0776   0.0626   1.0000
   6.750   1.3591   0.01667   0.01013  -0.0760   0.0598   1.0000
   7.000   1.3732   0.01730   0.01076  -0.0742   0.0570   1.0000
   7.250   1.3884   0.01788   0.01137  -0.0727   0.0552   1.0000
   7.500   1.4046   0.01842   0.01195  -0.0715   0.0538   1.0000
   7.750   1.4190   0.01908   0.01263  -0.0701   0.0522   1.0000
   8.000   1.4321   0.01984   0.01341  -0.0686   0.0507   1.0000
   8.250   1.4430   0.02075   0.01434  -0.0669   0.0491   1.0000
   8.500   1.4552   0.02162   0.01526  -0.0655   0.0480   1.0000
   8.750   1.4696   0.02237   0.01605  -0.0644   0.0474   1.0000
   9.000   1.4831   0.02320   0.01693  -0.0633   0.0466   1.0000
   9.250   1.4957   0.02411   0.01788  -0.0622   0.0456   1.0000
   9.500   1.5068   0.02517   0.01897  -0.0610   0.0447   1.0000
   9.750   1.5164   0.02637   0.02021  -0.0599   0.0437   1.0000
  10.000   1.5230   0.02785   0.02173  -0.0586   0.0427   1.0000
  10.250   1.5276   0.02956   0.02351  -0.0573   0.0417   1.0000
  10.500   1.5403   0.03065   0.02465  -0.0568   0.0411   1.0000
  10.750   1.5507   0.03196   0.02602  -0.0561   0.0405   1.0000
  11.000   1.5603   0.03338   0.02749  -0.0555   0.0396   1.0000
  11.250   1.5685   0.03498   0.02914  -0.0549   0.0389   1.0000
  11.500   1.5757   0.03670   0.03090  -0.0544   0.0380   1.0000
  11.750   1.5800   0.03876   0.03299  -0.0539   0.0372   1.0000
  12.000   1.5784   0.04150   0.03580  -0.0534   0.0362   1.0000
  12.250   1.5859   0.04336   0.03772  -0.0532   0.0357   1.0000
  12.500   1.5940   0.04515   0.03958  -0.0530   0.0350   1.0000
  12.750   1.6011   0.04708   0.04157  -0.0530   0.0341   1.0000
  13.000   1.6047   0.04942   0.04396  -0.0528   0.0334   1.0000
  13.250   1.6087   0.05172   0.04630  -0.0528   0.0325   1.0000
  13.500   1.6073   0.05469   0.04931  -0.0528   0.0316   1.0000
  13.750   1.6068   0.05757   0.05227  -0.0528   0.0308   1.0000
  14.000   1.6102   0.06005   0.05482  -0.0530   0.0301   1.0000
  14.250   1.6123   0.06269   0.05753  -0.0531   0.0292   1.0000
  14.500   1.6122   0.06565   0.06054  -0.0534   0.0284   1.0000
  14.750   1.6097   0.06894   0.06387  -0.0537   0.0275   1.0000
  15.000   1.6022   0.07292   0.06791  -0.0542   0.0267   1.0000
  15.250   1.6015   0.07608   0.07115  -0.0546   0.0260   1.0000
  15.500   1.5998   0.07940   0.07455  -0.0552   0.0252   1.0000
  15.750   1.5954   0.08310   0.07831  -0.0558   0.0244   1.0000
  16.000   1.5887   0.08717   0.08244  -0.0566   0.0237   1.0000
  16.250   1.5787   0.09176   0.08709  -0.0575   0.0230   1.0000
  16.500   1.5726   0.09586   0.09128  -0.0585   0.0223   1.0000
  16.750   1.5666   0.09991   0.09542  -0.0595   0.0218   1.0000
  17.000   1.5593   0.10420   0.09978  -0.0606   0.0212   1.0000
  17.250   1.5513   0.10863   0.10428  -0.0618   0.0205   1.0000
  17.500   1.5413   0.11342   0.10913  -0.0632   0.0200   1.0000
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