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WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 75-141 (fx75141-il)
Reynolds number: 100,000
Max Cl/Cd: 54.34 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx75141-il-100000.txt
Download as CSV file: xf-fx75141-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 75-141                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.4368   0.10083   0.09657  -0.0375   0.9932   0.1506
  -8.250  -0.4229   0.09782   0.09353  -0.0385   0.9903   0.1559
  -8.000  -0.4978   0.09318   0.08906  -0.0490   0.9819   0.1626
  -7.750  -0.4393   0.08997   0.08577  -0.0442   0.9820   0.1667
  -7.500  -0.4353   0.08705   0.08285  -0.0460   0.9784   0.1748
  -7.250  -0.5598   0.05639   0.05095  -0.0710   0.9679   0.0858
  -7.000  -0.5486   0.05160   0.04591  -0.0721   0.9645   0.0826
  -6.750  -0.5367   0.04619   0.03989  -0.0736   0.9607   0.0795
  -6.500  -0.5127   0.04300   0.03623  -0.0754   0.9572   0.0814
  -6.250  -0.4807   0.03958   0.03222  -0.0781   0.9542   0.0826
  -6.000  -0.4591   0.03718   0.02935  -0.0781   0.9503   0.0837
  -5.750  -0.4329   0.03556   0.02717  -0.0786   0.9462   0.0870
  -5.500  -0.4019   0.03353   0.02502  -0.0802   0.9426   0.0917
  -5.250  -0.3634   0.03230   0.02357  -0.0825   0.9394   0.0975
  -5.000  -0.3443   0.03135   0.02238  -0.0814   0.9345   0.1028
  -4.750  -0.3171   0.03035   0.02145  -0.0818   0.9299   0.1099
  -4.500  -0.2820   0.02944   0.02048  -0.0834   0.9260   0.1209
  -4.250  -0.2511   0.02879   0.01982  -0.0842   0.9220   0.1337
  -4.000  -0.2322   0.02828   0.01938  -0.0832   0.9162   0.1483
  -3.750  -0.2007   0.02756   0.01889  -0.0843   0.9116   0.1746
  -3.500  -0.1614   0.02655   0.01837  -0.0871   0.9081   0.2416
  -3.250  -0.1510   0.02531   0.01834  -0.0853   0.9018   0.4193
  -3.000  -0.1301   0.02566   0.01928  -0.0831   0.8960   0.5743
  -2.750  -0.0947   0.02672   0.02031  -0.0831   0.8917   0.6356
  -2.500  -0.0905   0.02746   0.02103  -0.0786   0.8834   0.6599
  -2.250  -0.0630   0.02837   0.02186  -0.0773   0.8779   0.6894
  -2.000  -0.0475   0.02912   0.02254  -0.0745   0.8710   0.7120
  -1.750  -0.0297   0.02970   0.02306  -0.0721   0.8641   0.7333
  -1.500   0.0013   0.03024   0.02354  -0.0712   0.8597   0.7541
  -1.250   0.0016   0.03065   0.02394  -0.0666   0.8508   0.7699
  -1.000   0.0266   0.03096   0.02418  -0.0652   0.8454   0.7903
  -0.750   0.0361   0.03131   0.02449  -0.0619   0.8375   0.8086
  -0.500   0.0541   0.03146   0.02461  -0.0597   0.8310   0.8262
  -0.250   0.0849   0.03154   0.02462  -0.0590   0.8271   0.8444
   0.000   0.0800   0.03173   0.02482  -0.0539   0.8164   0.8605
   0.250   0.1084   0.03171   0.02474  -0.0532   0.8121   0.8783
   0.500   0.1097   0.03193   0.02496  -0.0495   0.8024   0.8932
   0.750   0.1427   0.03196   0.02490  -0.0504   0.7974   0.9060
   1.000   0.1551   0.03226   0.02518  -0.0488   0.7888   0.9198
   1.250   0.1865   0.03239   0.02527  -0.0498   0.7829   0.9332
   1.500   0.2361   0.03245   0.02528  -0.0535   0.7796   0.9454
   1.750   0.2567   0.03311   0.02597  -0.0546   0.7690   0.9610
   2.000   0.3149   0.03335   0.02618  -0.0604   0.7652   0.9736
   2.250   0.3379   0.03412   0.02694  -0.0619   0.7554   1.0000
   2.500   0.3751   0.03440   0.02718  -0.0643   0.7502   1.0000
   2.750   0.4227   0.03450   0.02725  -0.0676   0.7471   1.0000
   3.000   0.4284   0.03552   0.02825  -0.0665   0.7352   1.0000
   3.250   0.4760   0.03554   0.02827  -0.0696   0.7321   1.0000
   3.500   0.4846   0.03663   0.02936  -0.0688   0.7204   1.0000
   3.750   0.5317   0.03654   0.02927  -0.0717   0.7169   1.0000
   4.000   0.5431   0.03762   0.03036  -0.0711   0.7055   1.0000
   4.250   0.5903   0.03736   0.03013  -0.0737   0.7017   1.0000
   4.500   0.6036   0.03838   0.03117  -0.0732   0.6903   1.0000
   4.750   0.6523   0.03786   0.03070  -0.0756   0.6866   1.0000
   5.000   0.6672   0.03875   0.03163  -0.0751   0.6749   1.0000
   5.250   0.7228   0.03748   0.03043  -0.0777   0.6714   1.0000
   5.500   0.7426   0.03786   0.03086  -0.0771   0.6591   1.0000
   5.750   0.8038   0.03577   0.02888  -0.0796   0.6563   1.0000
   6.000   0.8211   0.03627   0.02944  -0.0787   0.6439   1.0000
   6.250   0.8821   0.03389   0.02721  -0.0810   0.6417   1.0000
   6.500   0.9450   0.03131   0.02479  -0.0836   0.6400   1.0000
   6.750   0.9639   0.03132   0.02490  -0.0822   0.6276   1.0000
   7.000   0.9952   0.03057   0.02425  -0.0819   0.6176   1.0000
   7.250   1.0708   0.02708   0.02096  -0.0859   0.6123   1.0000
   7.500   1.1242   0.02479   0.01878  -0.0875   0.5973   1.0000
   7.750   1.1697   0.02303   0.01705  -0.0883   0.5760   1.0000
   8.000   1.1932   0.02257   0.01662  -0.0867   0.5508   1.0000
   8.250   1.2117   0.02242   0.01646  -0.0846   0.5234   1.0000
   8.500   1.2243   0.02253   0.01652  -0.0816   0.4923   1.0000
   8.750   1.2308   0.02297   0.01686  -0.0780   0.4574   1.0000
   9.000   1.2331   0.02370   0.01744  -0.0740   0.4177   1.0000
   9.250   1.2308   0.02483   0.01830  -0.0700   0.3735   1.0000
   9.500   1.2260   0.02637   0.01953  -0.0661   0.3287   1.0000
   9.750   1.2211   0.02819   0.02103  -0.0626   0.2883   1.0000
  10.000   1.2164   0.03021   0.02275  -0.0595   0.2525   1.0000
  10.250   1.2122   0.03237   0.02463  -0.0566   0.2203   1.0000
  10.500   1.2091   0.03463   0.02664  -0.0540   0.1906   1.0000
  10.750   1.2094   0.03683   0.02862  -0.0518   0.1654   1.0000
  11.000   1.2129   0.03889   0.03050  -0.0500   0.1461   1.0000
  11.250   1.2205   0.04079   0.03225  -0.0484   0.1307   1.0000
  11.500   1.2313   0.04254   0.03396  -0.0471   0.1183   1.0000
  11.750   1.2457   0.04423   0.03563  -0.0460   0.1082   1.0000
  12.000   1.2661   0.04581   0.03708  -0.0454   0.0999   1.0000
  12.250   1.2801   0.04750   0.03890  -0.0444   0.0931   1.0000
  12.500   1.3074   0.04923   0.04058  -0.0442   0.0865   1.0000
  12.750   1.3207   0.05115   0.04268  -0.0432   0.0816   1.0000
  13.000   1.3577   0.05323   0.04462  -0.0438   0.0760   1.0000
  13.250   1.3643   0.05565   0.04740  -0.0424   0.0734   1.0000
  13.500   1.3732   0.05811   0.05011  -0.0413   0.0705   1.0000
  13.750   1.3829   0.06046   0.05256  -0.0405   0.0677   1.0000
  14.000   1.4076   0.06417   0.05633  -0.0407   0.0647   1.0000
  14.250   1.3972   0.06746   0.05999  -0.0389   0.0640   1.0000
  14.500   1.3848   0.07112   0.06400  -0.0373   0.0633   1.0000
  14.750   1.3699   0.07518   0.06841  -0.0361   0.0627   1.0000
  15.000   1.3522   0.07961   0.07316  -0.0353   0.0621   1.0000
  15.250   1.3322   0.08448   0.07833  -0.0350   0.0617   1.0000
  15.500   1.3092   0.08989   0.08404  -0.0354   0.0615   1.0000
  15.750   1.2836   0.09601   0.09044  -0.0366   0.0616   1.0000
  16.000   1.2551   0.10297   0.09767  -0.0387   0.0619   1.0000
  16.250   1.2239   0.11090   0.10585  -0.0420   0.0624   1.0000
  16.500   1.1918   0.11983   0.11499  -0.0465   0.0632   1.0000
  16.750   1.1596   0.12977   0.12510  -0.0522   0.0640   1.0000
  17.000   1.1318   0.14006   0.13550  -0.0582   0.0648   1.0000
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