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GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: GOE 493 AIRFOIL (goe493-il)
Reynolds number: 100,000
Max Cl/Cd: 51.82 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe493-il-100000.txt
Download as CSV file: xf-goe493-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 493 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.4719   0.09959   0.09468  -0.0602   1.0000   0.0824
 -11.250  -0.5979   0.07518   0.07030  -0.0729   1.0000   0.0706
 -11.000  -0.6264   0.07110   0.06624  -0.0724   1.0000   0.0702
 -10.750  -0.6600   0.06765   0.06278  -0.0710   1.0000   0.0697
 -10.500  -0.6929   0.06525   0.06039  -0.0681   1.0000   0.0692
 -10.250  -0.7301   0.06321   0.05831  -0.0635   1.0000   0.0688
 -10.000  -0.7596   0.06026   0.05524  -0.0600   1.0000   0.0684
  -9.750  -0.7854   0.05684   0.05162  -0.0567   1.0000   0.0681
  -9.500  -0.8059   0.05314   0.04761  -0.0537   1.0000   0.0681
  -9.250  -0.8190   0.04947   0.04357  -0.0509   1.0000   0.0683
  -9.000  -0.8259   0.04593   0.03957  -0.0484   1.0000   0.0690
  -8.750  -0.8281   0.04284   0.03588  -0.0459   1.0000   0.0705
  -8.500  -0.8197   0.04051   0.03347  -0.0443   1.0000   0.0727
  -8.250  -0.8072   0.03946   0.03240  -0.0428   1.0000   0.0758
  -8.000  -0.7968   0.03755   0.03015  -0.0411   1.0000   0.0791
  -7.750  -0.7860   0.03537   0.02743  -0.0393   1.0000   0.0825
  -7.500  -0.7516   0.03434   0.02648  -0.0417   0.9948   0.0897
  -7.250  -0.7206   0.03280   0.02470  -0.0434   0.9890   0.0981
  -7.000  -0.6861   0.03176   0.02342  -0.0455   0.9835   0.1098
  -6.750  -0.6575   0.03094   0.02244  -0.0465   0.9769   0.1229
  -6.500  -0.6233   0.03026   0.02177  -0.0485   0.9713   0.1388
  -6.250  -0.5963   0.02969   0.02115  -0.0492   0.9643   0.1541
  -6.000  -0.5626   0.02924   0.02070  -0.0510   0.9583   0.1709
  -5.750  -0.5348   0.02880   0.02020  -0.0516   0.9515   0.1861
  -5.500  -0.5038   0.02840   0.01976  -0.0528   0.9450   0.2022
  -5.250  -0.4704   0.02808   0.01944  -0.0544   0.9394   0.2189
  -5.000  -0.4457   0.02769   0.01902  -0.0543   0.9318   0.2341
  -4.750  -0.4074   0.02738   0.01875  -0.0566   0.9268   0.2539
  -4.500  -0.3867   0.02703   0.01844  -0.0558   0.9187   0.2711
  -4.250  -0.3532   0.02672   0.01818  -0.0572   0.9129   0.2961
  -4.000  -0.3262   0.02650   0.01805  -0.0573   0.9062   0.3247
  -3.750  -0.3000   0.02625   0.01798  -0.0574   0.8990   0.3588
  -3.500  -0.2620   0.02617   0.01808  -0.0593   0.8947   0.4065
  -3.250  -0.2490   0.02618   0.01823  -0.0569   0.8853   0.4409
  -3.000  -0.2142   0.02626   0.01842  -0.0580   0.8801   0.4853
  -2.750  -0.1966   0.02644   0.01867  -0.0563   0.8719   0.5173
  -2.500  -0.1674   0.02657   0.01884  -0.0564   0.8658   0.5511
  -2.250  -0.1344   0.02670   0.01900  -0.0571   0.8608   0.5833
  -2.000  -0.1197   0.02688   0.01921  -0.0549   0.8517   0.6085
  -1.750  -0.0836   0.02692   0.01929  -0.0560   0.8475   0.6388
  -1.500  -0.0728   0.02721   0.01965  -0.0532   0.8386   0.6607
  -1.250  -0.0414   0.02727   0.01974  -0.0534   0.8332   0.6899
  -1.000  -0.0196   0.02746   0.02001  -0.0522   0.8265   0.7151
  -0.750   0.0009   0.02764   0.02023  -0.0508   0.8193   0.7423
  -0.500   0.0373   0.02756   0.02020  -0.0517   0.8156   0.7726
  -0.250   0.0446   0.02793   0.02065  -0.0483   0.8059   0.7986
   0.000   0.0779   0.02786   0.02064  -0.0488   0.8014   0.8331
   0.250   0.1155   0.02779   0.02066  -0.0501   0.7973   0.8740
   0.500   0.1574   0.02823   0.02121  -0.0536   0.7891   0.9225
   0.750   0.2480   0.02828   0.02125  -0.0655   0.7866   0.9645
   1.250   0.3261   0.02828   0.02100  -0.0723   0.7721   1.0000
   1.500   0.3763   0.02762   0.02024  -0.0758   0.7686   1.0000
   1.750   0.3813   0.02819   0.02070  -0.0726   0.7567   1.0000
   2.000   0.4288   0.02761   0.02006  -0.0754   0.7533   1.0000
   2.250   0.4837   0.02682   0.01923  -0.0794   0.7516   1.0000
   2.500   0.4769   0.02796   0.02031  -0.0744   0.7384   1.0000
   2.750   0.5303   0.02712   0.01946  -0.0779   0.7366   1.0000
   3.000   0.5262   0.02830   0.02060  -0.0734   0.7237   1.0000
   3.250   0.5790   0.02739   0.01970  -0.0767   0.7216   1.0000
   3.500   0.6376   0.02644   0.01877  -0.0811   0.7199   1.0000
   3.750   0.6301   0.02760   0.01992  -0.0757   0.7068   1.0000
   4.000   0.6352   0.02850   0.02082  -0.0724   0.6955   1.0000
   4.250   0.6848   0.02765   0.02001  -0.0752   0.6920   1.0000
   4.500   0.7445   0.02654   0.01897  -0.0795   0.6896   1.0000
   4.750   0.7463   0.02741   0.01985  -0.0754   0.6774   1.0000
   5.000   0.8037   0.02638   0.01891  -0.0795   0.6743   1.0000
   5.250   0.8104   0.02713   0.01970  -0.0762   0.6627   1.0000
   5.500   0.8682   0.02603   0.01868  -0.0802   0.6586   1.0000
   5.750   0.8793   0.02660   0.01931  -0.0774   0.6470   1.0000
   6.000   0.9370   0.02559   0.01839  -0.0815   0.6423   1.0000
   6.250   0.9462   0.02625   0.01913  -0.0784   0.6303   1.0000
   6.500   0.9923   0.02556   0.01851  -0.0806   0.6219   1.0000
   6.750   1.0406   0.02447   0.01746  -0.0828   0.6099   1.0000
   7.000   1.0769   0.02355   0.01655  -0.0830   0.5935   1.0000
   7.250   1.0951   0.02314   0.01615  -0.0803   0.5743   1.0000
   7.500   1.1115   0.02272   0.01572  -0.0774   0.5534   1.0000
   7.750   1.1315   0.02232   0.01528  -0.0751   0.5326   1.0000
   8.000   1.1498   0.02219   0.01513  -0.0728   0.5138   1.0000
   8.250   1.1579   0.02241   0.01540  -0.0690   0.4960   1.0000
   8.500   1.1628   0.02266   0.01571  -0.0648   0.4781   1.0000
   8.750   1.1659   0.02298   0.01607  -0.0603   0.4589   1.0000
   9.000   1.1695   0.02332   0.01641  -0.0560   0.4369   1.0000
   9.250   1.1673   0.02391   0.01701  -0.0511   0.4112   1.0000
   9.500   1.1621   0.02472   0.01772  -0.0461   0.3790   1.0000
   9.750   1.1513   0.02598   0.01877  -0.0407   0.3365   1.0000
  10.000   1.1316   0.02802   0.02047  -0.0349   0.2763   1.0000
  10.250   1.1048   0.03102   0.02288  -0.0294   0.1947   1.0000
  10.500   1.0814   0.03442   0.02575  -0.0251   0.1541   1.0000
  10.750   1.0673   0.03746   0.02852  -0.0218   0.1333   1.0000
  11.000   1.0629   0.03991   0.03085  -0.0194   0.1196   1.0000
  11.250   1.0658   0.04188   0.03281  -0.0176   0.1095   1.0000
  11.500   1.0713   0.04372   0.03458  -0.0159   0.1021   1.0000
  11.750   1.0820   0.04522   0.03605  -0.0145   0.0962   1.0000
  12.000   1.1022   0.04634   0.03705  -0.0133   0.0908   1.0000
  12.250   1.1219   0.04750   0.03825  -0.0124   0.0858   1.0000
  12.500   1.1653   0.04833   0.03883  -0.0127   0.0803   1.0000
  12.750   1.1851   0.04986   0.04060  -0.0119   0.0772   1.0000
  13.000   1.2056   0.05147   0.04233  -0.0113   0.0738   1.0000
  13.250   1.2722   0.05394   0.04461  -0.0142   0.0691   1.0000
  13.500   1.2736   0.05605   0.04706  -0.0122   0.0681   1.0000
  13.750   1.2743   0.05845   0.04978  -0.0104   0.0667   1.0000
  14.000   1.2760   0.06112   0.05274  -0.0088   0.0653   1.0000
  14.250   1.2767   0.06413   0.05604  -0.0074   0.0644   1.0000
  14.500   1.2736   0.06742   0.05961  -0.0060   0.0638   1.0000
  14.750   1.2664   0.07092   0.06338  -0.0047   0.0633   1.0000
  15.000   1.2557   0.07467   0.06740  -0.0036   0.0628   1.0000
  15.250   1.2443   0.07847   0.07143  -0.0028   0.0622   1.0000
  15.500   1.2242   0.08312   0.07635  -0.0023   0.0622   1.0000
  15.750   1.1984   0.08844   0.08197  -0.0025   0.0625   1.0000
  16.000   1.1671   0.09477   0.08861  -0.0037   0.0630   1.0000
  16.250   1.1314   0.10224   0.09637  -0.0060   0.0639   1.0000
  16.500   1.0934   0.11092   0.10530  -0.0097   0.0651   1.0000
  16.750   1.0549   0.12072   0.11530  -0.0148   0.0663   1.0000
  17.000   1.0204   0.13118   0.12588  -0.0205   0.0676   1.0000
  17.250   0.9991   0.14034   0.13511  -0.0252   0.0687   1.0000
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