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Eiffel 371 (Monge) (eiffel371-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Eiffel 371 (Monge) (eiffel371-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.53 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-eiffel371-il-1000000.txt
Download as CSV file: xf-eiffel371-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Eiffel 371 (Monge)                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.6398   0.05535   0.05334  -0.0718   1.0000   0.0098
 -12.250  -0.6878   0.04675   0.04453  -0.0769   1.0000   0.0097
 -12.000  -0.7324   0.04195   0.03955  -0.0746   1.0000   0.0095
 -11.750  -0.7615   0.03964   0.03711  -0.0700   1.0000   0.0096
 -11.500  -0.7658   0.03616   0.03335  -0.0703   0.9974   0.0097
 -11.250  -0.7722   0.03195   0.02875  -0.0697   0.9922   0.0097
 -11.000  -0.7632   0.02908   0.02555  -0.0691   0.9873   0.0098
 -10.750  -0.7430   0.02716   0.02342  -0.0693   0.9848   0.0099
 -10.500  -0.7198   0.02551   0.02155  -0.0697   0.9831   0.0100
 -10.250  -0.7133   0.02251   0.01818  -0.0675   0.9772   0.0101
 -10.000  -0.6931   0.02039   0.01586  -0.0671   0.9742   0.0104
  -9.750  -0.6644   0.01952   0.01494  -0.0676   0.9724   0.0107
  -9.500  -0.6335   0.01892   0.01428  -0.0684   0.9709   0.0110
  -9.250  -0.6046   0.01803   0.01330  -0.0689   0.9688   0.0113
  -9.000  -0.5805   0.01747   0.01268  -0.0681   0.9637   0.0117
  -8.750  -0.5506   0.01663   0.01175  -0.0687   0.9606   0.0120
  -8.500  -0.5177   0.01600   0.01103  -0.0697   0.9578   0.0125
  -8.250  -0.4825   0.01535   0.01028  -0.0711   0.9553   0.0128
  -8.000  -0.4592   0.01482   0.00969  -0.0701   0.9474   0.0129
  -7.750  -0.4317   0.01339   0.00815  -0.0703   0.9420   0.0134
  -7.500  -0.4058   0.01289   0.00762  -0.0699   0.9347   0.0139
  -7.250  -0.3774   0.01246   0.00715  -0.0699   0.9271   0.0145
  -7.000  -0.3520   0.01206   0.00670  -0.0692   0.9186   0.0150
  -6.750  -0.3257   0.01167   0.00624  -0.0687   0.9095   0.0155
  -6.500  -0.3020   0.01140   0.00591  -0.0676   0.8986   0.0161
  -6.250  -0.2793   0.01097   0.00541  -0.0664   0.8871   0.0166
  -6.000  -0.2570   0.01060   0.00499  -0.0651   0.8742   0.0177
  -5.750  -0.2338   0.01038   0.00472  -0.0639   0.8594   0.0187
  -5.500  -0.2112   0.01017   0.00444  -0.0625   0.8411   0.0195
  -5.250  -0.1892   0.01002   0.00418  -0.0610   0.8156   0.0203
  -5.000  -0.1710   0.00974   0.00376  -0.0588   0.7815   0.0219
  -4.750  -0.1521   0.00971   0.00356  -0.0567   0.7416   0.0234
  -4.500  -0.1317   0.00970   0.00340  -0.0549   0.7099   0.0248
  -4.250  -0.1119   0.00956   0.00315  -0.0530   0.6835   0.0278
  -4.000  -0.0896   0.00951   0.00300  -0.0517   0.6622   0.0306
  -3.750  -0.0678   0.00936   0.00280  -0.0503   0.6434   0.0366
  -3.500  -0.0460   0.00918   0.00264  -0.0489   0.6279   0.0519
  -3.250  -0.0240   0.00900   0.00253  -0.0476   0.6155   0.0806
  -3.000  -0.0011   0.00884   0.00243  -0.0465   0.6042   0.1063
  -2.750   0.0212   0.00865   0.00234  -0.0453   0.5943   0.1436
  -2.500   0.0417   0.00839   0.00223  -0.0438   0.5852   0.1989
  -2.250   0.0532   0.00769   0.00210  -0.0407   0.5779   0.3622
  -2.000   0.0724   0.00745   0.00203  -0.0389   0.5700   0.4227
  -1.750   0.0932   0.00727   0.00207  -0.0374   0.5631   0.4980
  -1.500   0.1206   0.00735   0.00214  -0.0371   0.5559   0.5279
  -1.250   0.1478   0.00745   0.00219  -0.0369   0.5493   0.5417
  -1.000   0.1751   0.00751   0.00222  -0.0367   0.5427   0.5519
  -0.750   0.2021   0.00762   0.00225  -0.0364   0.5364   0.5589
  -0.500   0.2284   0.00762   0.00223  -0.0360   0.5298   0.5628
  -0.250   0.2546   0.00767   0.00223  -0.0356   0.5220   0.5677
   0.000   0.2812   0.00773   0.00224  -0.0353   0.5155   0.5721
   0.250   0.3073   0.00774   0.00222  -0.0350   0.5077   0.5766
   0.500   0.3327   0.00776   0.00221  -0.0345   0.5010   0.5825
   0.750   0.3597   0.00780   0.00222  -0.0343   0.4944   0.5879
   1.000   0.3847   0.00779   0.00218  -0.0338   0.4875   0.5911
   1.250   0.4109   0.00779   0.00218  -0.0335   0.4804   0.5929
   1.500   0.4364   0.00783   0.00218  -0.0331   0.4718   0.5946
   1.750   0.4626   0.00786   0.00219  -0.0329   0.4639   0.5961
   2.000   0.4879   0.00792   0.00220  -0.0325   0.4544   0.5977
   2.250   0.5139   0.00796   0.00222  -0.0322   0.4437   0.5992
   2.500   0.5391   0.00805   0.00225  -0.0318   0.4306   0.6009
   2.750   0.5639   0.00814   0.00229  -0.0314   0.4164   0.6025
   3.000   0.5876   0.00823   0.00232  -0.0307   0.3995   0.6048
   3.250   0.6109   0.00836   0.00238  -0.0300   0.3812   0.6069
   3.500   0.6342   0.00851   0.00246  -0.0294   0.3643   0.6089
   3.750   0.6574   0.00867   0.00255  -0.0287   0.3486   0.6108
   4.000   0.6808   0.00882   0.00265  -0.0281   0.3352   0.6130
   4.250   0.7042   0.00898   0.00276  -0.0275   0.3229   0.6151
   4.750   0.7513   0.00923   0.00296  -0.0263   0.3045   0.6209
   5.000   0.7738   0.00935   0.00308  -0.0256   0.2960   0.6256
   5.500   0.8163   0.00954   0.00351  -0.0236   0.2817   0.7353
   5.750   0.8404   0.00970   0.00368  -0.0231   0.2753   0.7402
   6.000   0.8633   0.00990   0.00385  -0.0225   0.2676   0.7432
   6.250   0.8867   0.01007   0.00401  -0.0220   0.2611   0.7454
   6.500   0.9086   0.01026   0.00417  -0.0212   0.2536   0.7473
   6.750   0.9299   0.01044   0.00433  -0.0203   0.2464   0.7490
   7.000   0.9507   0.01062   0.00450  -0.0194   0.2389   0.7503
   7.250   0.9705   0.01084   0.00469  -0.0182   0.2290   0.7515
   7.500   0.9887   0.01113   0.00493  -0.0168   0.2167   0.7528
   7.750   1.0063   0.01145   0.00521  -0.0153   0.2041   0.7541
   8.000   1.0232   0.01181   0.00551  -0.0137   0.1892   0.7552
   8.250   1.0389   0.01221   0.00584  -0.0119   0.1731   0.7566
   8.500   1.0528   0.01267   0.00622  -0.0098   0.1562   0.7577
   8.750   1.0672   0.01312   0.00662  -0.0079   0.1445   0.7589
   9.000   1.0818   0.01355   0.00701  -0.0061   0.1365   0.7601
   9.250   1.0982   0.01393   0.00737  -0.0046   0.1307   0.7613
   9.500   1.1138   0.01432   0.00776  -0.0030   0.1263   0.7624
   9.750   1.1278   0.01478   0.00821  -0.0012   0.1206   0.7634
  10.000   1.1452   0.01511   0.00856  -0.0001   0.1177   0.7642
  10.250   1.1616   0.01548   0.00895   0.0012   0.1153   0.7648
  10.500   1.1750   0.01596   0.00942   0.0029   0.1107   0.7655
  10.750   1.1884   0.01642   0.00990   0.0046   0.1065   0.7665
  11.000   1.2055   0.01675   0.01027   0.0056   0.1031   0.7674
  11.250   1.2155   0.01739   0.01087   0.0076   0.0950   0.7682
  11.500   1.2251   0.01807   0.01149   0.0096   0.0827   0.7689
  11.750   1.2133   0.01976   0.01296   0.0144   0.0525   0.7695
  12.000   1.1905   0.02218   0.01521   0.0200   0.0213   0.7700
  12.250   1.1901   0.02359   0.01664   0.0225   0.0158   0.7707
  12.500   1.1950   0.02479   0.01790   0.0242   0.0144   0.7713
  12.750   1.1978   0.02619   0.01938   0.0260   0.0131   0.7719
  13.000   1.2035   0.02748   0.02073   0.0272   0.0125   0.7725
  13.250   1.2081   0.02893   0.02225   0.0284   0.0119   0.7731
  13.500   1.2136   0.03038   0.02377   0.0293   0.0118   0.7736
  13.750   1.2156   0.03216   0.02564   0.0302   0.0112   0.7742
  14.000   1.2168   0.03412   0.02766   0.0310   0.0109   0.7745
  14.250   1.2163   0.03630   0.02991   0.0316   0.0104   0.7751
  14.500   1.2075   0.03937   0.03311   0.0324   0.0099   0.7754
  14.750   1.2070   0.04179   0.03562   0.0326   0.0098   0.7757
  15.000   1.2115   0.04379   0.03767   0.0326   0.0095   0.7761
  15.250   1.2083   0.04663   0.04060   0.0325   0.0094   0.7764
  15.500   1.2096   0.04906   0.04311   0.0323   0.0093   0.7768
  15.750   1.2049   0.05226   0.04639   0.0320   0.0090   0.7770
  16.000   1.2036   0.05513   0.04934   0.0315   0.0088   0.7773
  16.250   1.1980   0.05859   0.05288   0.0308   0.0085   0.7775
  16.500   1.1917   0.06225   0.05663   0.0300   0.0083   0.7777
  16.750   1.1841   0.06622   0.06069   0.0290   0.0084   0.7778
  17.000   1.1744   0.07058   0.06515   0.0278   0.0083   0.7780
  17.250   1.1633   0.07530   0.06997   0.0264   0.0081   0.7781
  17.500   1.1576   0.07938   0.07414   0.0249   0.0080   0.7783
  17.750   1.1417   0.08508   0.07995   0.0230   0.0079   0.7784
  18.000   1.1208   0.09174   0.08673   0.0206   0.0078   0.7784
  18.250   1.1131   0.09647   0.09156   0.0187   0.0078   0.7786
  18.500   1.0996   0.10221   0.09740   0.0164   0.0078   0.7788
  18.750   1.0870   0.10790   0.10319   0.0140   0.0078   0.7789
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