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WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 75-141 (fx75141-il)
Reynolds number: 50,000
Max Cl/Cd: 26.74 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75141-il-50000-n5.txt
Download as CSV file: xf-fx75141-il-50000-n5.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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.3949   0.10694   0.10005  -0.0579   1.0000   0.0625
 -10.500  -0.4108   0.10448   0.09769  -0.0561   1.0000   0.0624
 -10.250  -0.4273   0.10193   0.09524  -0.0543   1.0000   0.0623
 -10.000  -0.4432   0.09912   0.09250  -0.0529   1.0000   0.0621
  -9.750  -0.4571   0.09515   0.08860  -0.0533   0.9992   0.0618
  -9.500  -0.4627   0.08814   0.08158  -0.0588   0.9935   0.0614
  -9.250  -0.4773   0.08091   0.07432  -0.0652   0.9867   0.0609
  -9.000  -0.4973   0.07488   0.06820  -0.0704   0.9787   0.0604
  -8.750  -0.5186   0.06958   0.06275  -0.0743   0.9700   0.0601
  -8.500  -0.5308   0.06447   0.05738  -0.0773   0.9627   0.0600
  -8.250  -0.5359   0.05962   0.05216  -0.0798   0.9563   0.0604
  -8.000  -0.5361   0.05522   0.04726  -0.0814   0.9507   0.0613
  -7.750  -0.5322   0.05127   0.04271  -0.0823   0.9451   0.0629
  -7.500  -0.5119   0.04912   0.04051  -0.0834   0.9416   0.0653
  -7.250  -0.4921   0.04668   0.03777  -0.0844   0.9379   0.0677
  -7.000  -0.4782   0.04429   0.03501  -0.0840   0.9331   0.0696
  -6.750  -0.4567   0.04190   0.03204  -0.0847   0.9290   0.0733
  -6.500  -0.4301   0.04003   0.02998  -0.0858   0.9258   0.0772
  -6.250  -0.4034   0.03849   0.02823  -0.0865   0.9227   0.0812
  -6.000  -0.3850   0.03725   0.02666  -0.0854   0.9179   0.0862
  -5.750  -0.3608   0.03610   0.02547  -0.0854   0.9139   0.0918
  -5.500  -0.3322   0.03505   0.02421  -0.0858   0.9106   0.0992
  -5.250  -0.3011   0.03408   0.02322  -0.0868   0.9078   0.1081
  -5.000  -0.2852   0.03348   0.02245  -0.0848   0.9023   0.1165
  -4.750  -0.2621   0.03275   0.02175  -0.0845   0.8978   0.1283
  -4.500  -0.2336   0.03197   0.02095  -0.0852   0.8941   0.1450
  -4.250  -0.2054   0.03113   0.02024  -0.0860   0.8905   0.1685
  -4.000  -0.1893   0.03048   0.01973  -0.0850   0.8846   0.1980
  -3.750  -0.1630   0.02947   0.01909  -0.0860   0.8802   0.2600
  -3.500  -0.1351   0.02850   0.01903  -0.0868   0.8767   0.3943
  -3.250  -0.1215   0.02869   0.01961  -0.0838   0.8707   0.4987
  -3.000  -0.1039   0.02921   0.02023  -0.0809   0.8649   0.5649
  -2.750  -0.0783   0.02986   0.02079  -0.0794   0.8607   0.6171
  -2.500  -0.0646   0.03049   0.02133  -0.0764   0.8541   0.6509
  -2.250  -0.0459   0.03107   0.02177  -0.0739   0.8482   0.6810
  -2.000  -0.0213   0.03156   0.02214  -0.0721   0.8441   0.7089
  -1.750  -0.0109   0.03196   0.02244  -0.0690   0.8366   0.7317
  -1.500   0.0081   0.03222   0.02260  -0.0667   0.8311   0.7518
  -1.250   0.0348   0.03235   0.02260  -0.0657   0.8274   0.7726
  -1.000   0.0408   0.03261   0.02280  -0.0620   0.8188   0.7898
  -0.750   0.0649   0.03267   0.02274  -0.0611   0.8139   0.8072
  -0.500   0.0847   0.03277   0.02275  -0.0598   0.8081   0.8211
  -0.250   0.1018   0.03290   0.02279  -0.0583   0.8009   0.8332
   0.000   0.1329   0.03290   0.02267  -0.0590   0.7967   0.8448
   0.250   0.1459   0.03319   0.02289  -0.0572   0.7887   0.8568
   0.500   0.1713   0.03326   0.02288  -0.0571   0.7830   0.8679
   0.750   0.2052   0.03327   0.02281  -0.0582   0.7795   0.8785
   1.000   0.2137   0.03368   0.02320  -0.0560   0.7698   0.8909
   1.250   0.2461   0.03376   0.02323  -0.0571   0.7654   0.9026
   1.500   0.2645   0.03414   0.02360  -0.0565   0.7575   0.9158
   1.750   0.2956   0.03438   0.02383  -0.0578   0.7515   0.9287
   2.000   0.3384   0.03450   0.02393  -0.0608   0.7479   0.9418
   2.250   0.3616   0.03520   0.02466  -0.0620   0.7382   0.9626
   2.500   0.3997   0.03539   0.02483  -0.0645   0.7334   1.0000
   2.750   0.4150   0.03613   0.02555  -0.0642   0.7243   1.0000
   3.000   0.4462   0.03651   0.02591  -0.0656   0.7187   1.0000
   3.250   0.4674   0.03719   0.02657  -0.0659   0.7107   1.0000
   3.500   0.4949   0.03771   0.02710  -0.0668   0.7041   1.0000
   4.000   0.5443   0.03893   0.02834  -0.0680   0.6893   1.0000
   4.250   0.5817   0.03907   0.02852  -0.0696   0.6851   1.0000
   4.500   0.5941   0.04012   0.02960  -0.0689   0.6741   1.0000
   5.000   0.6450   0.04117   0.03075  -0.0696   0.6585   1.0000
   5.250   0.6650   0.04190   0.03154  -0.0695   0.6490   1.0000
   5.500   0.6976   0.04199   0.03171  -0.0702   0.6424   1.0000
   5.750   0.7146   0.04281   0.03260  -0.0696   0.6314   1.0000
   6.000   0.7532   0.04240   0.03231  -0.0705   0.6258   1.0000
   6.250   0.7695   0.04312   0.03311  -0.0696   0.6133   1.0000
   6.500   0.7916   0.04345   0.03354  -0.0691   0.6019   1.0000
   6.750   0.8324   0.04238   0.03263  -0.0694   0.5950   1.0000
   7.000   0.8505   0.04282   0.03317  -0.0684   0.5817   1.0000
   7.250   0.8722   0.04293   0.03341  -0.0675   0.5691   1.0000
   7.500   0.9165   0.04122   0.03190  -0.0675   0.5626   1.0000
   7.750   0.9353   0.04150   0.03231  -0.0663   0.5484   1.0000
   8.000   0.9562   0.04158   0.03255  -0.0652   0.5341   1.0000
   8.250   0.9792   0.04144   0.03258  -0.0641   0.5193   1.0000
   8.500   1.0038   0.04109   0.03238  -0.0629   0.5033   1.0000
   8.750   1.0306   0.04044   0.03187  -0.0616   0.4853   1.0000
   9.000   1.0470   0.04064   0.03219  -0.0599   0.4627   1.0000
   9.250   1.0694   0.04021   0.03183  -0.0583   0.4364   1.0000
   9.500   1.0837   0.04053   0.03214  -0.0563   0.4047   1.0000
   9.750   1.0947   0.04124   0.03278  -0.0544   0.3697   1.0000
  10.000   1.1045   0.04215   0.03352  -0.0525   0.3333   1.0000
  10.250   1.1115   0.04347   0.03463  -0.0506   0.2988   1.0000
  10.500   1.1149   0.04528   0.03625  -0.0488   0.2681   1.0000
  10.750   1.1170   0.04736   0.03817  -0.0473   0.2413   1.0000
  11.000   1.1182   0.04961   0.04026  -0.0459   0.2183   1.0000
  11.250   1.1196   0.05202   0.04261  -0.0447   0.1963   1.0000
  11.500   1.1207   0.05452   0.04502  -0.0437   0.1773   1.0000
  11.750   1.1226   0.05704   0.04748  -0.0428   0.1607   1.0000
  12.000   1.1254   0.05957   0.04999  -0.0420   0.1460   1.0000
  12.250   1.1298   0.06206   0.05247  -0.0413   0.1331   1.0000
  12.500   1.1350   0.06452   0.05495  -0.0407   0.1221   1.0000
  12.750   1.1406   0.06695   0.05734  -0.0401   0.1132   1.0000
  13.000   1.1487   0.06927   0.05977  -0.0396   0.1050   1.0000
  13.250   1.1573   0.07159   0.06214  -0.0391   0.0982   1.0000
  13.500   1.1657   0.07396   0.06465  -0.0388   0.0920   1.0000
  13.750   1.1771   0.07609   0.06683  -0.0382   0.0869   1.0000
  14.000   1.1841   0.07886   0.06985  -0.0380   0.0819   1.0000
  14.250   1.1940   0.08111   0.07211  -0.0378   0.0779   1.0000
  14.500   1.2027   0.08394   0.07514  -0.0375   0.0745   1.0000
  14.750   1.2027   0.08777   0.07930  -0.0379   0.0717   1.0000
  15.000   1.2023   0.09152   0.08326  -0.0384   0.0690   1.0000
  15.250   1.2060   0.09465   0.08648  -0.0387   0.0666   1.0000
  15.500   1.2089   0.09817   0.09009  -0.0392   0.0646   1.0000
  15.750   1.1946   0.10423   0.09652  -0.0412   0.0637   1.0000
  16.000   1.1763   0.11116   0.10378  -0.0441   0.0631   1.0000
  16.250   1.1533   0.11927   0.11218  -0.0481   0.0627   1.0000
  16.500   1.1256   0.12900   0.12215  -0.0536   0.0627   1.0000
  16.750   1.0907   0.14140   0.13477  -0.0613   0.0631   1.0000
  17.000   1.0500   0.15732   0.15080  -0.0715   0.0637   1.0000
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