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WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=50,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 75-141 (fx75141-il)
Reynolds number: 50,000
Max Cl/Cd: 30.28 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx75141-il-50000.txt
Download as CSV file: xf-fx75141-il-50000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.000  -0.4180   0.11283   0.10677  -0.0137   1.0000   0.3412
  -7.750  -0.3934   0.10825   0.10216  -0.0123   1.0000   0.3499
  -7.500  -0.4109   0.10697   0.10098  -0.0099   1.0000   0.3602
  -7.250  -0.4291   0.10635   0.10044  -0.0070   1.0000   0.3734
  -7.000  -0.4116   0.10273   0.09680  -0.0053   1.0000   0.3862
  -6.750  -0.4127   0.10034   0.09445  -0.0032   1.0000   0.3969
  -6.500  -0.5893   0.08050   0.07487  -0.0292   1.0000   0.1972
  -6.250  -0.6062   0.06757   0.06140  -0.0397   1.0000   0.1590
  -6.000  -0.6020   0.05846   0.05130  -0.0469   1.0000   0.1464
  -5.750  -0.5865   0.05417   0.04669  -0.0481   1.0000   0.1453
  -5.500  -0.5675   0.04999   0.04207  -0.0496   1.0000   0.1440
  -5.250  -0.5449   0.04635   0.03776  -0.0514   1.0000   0.1456
  -5.000  -0.5228   0.04343   0.03446  -0.0522   1.0000   0.1492
  -4.750  -0.5012   0.04125   0.03208  -0.0522   1.0000   0.1533
  -4.500  -0.4772   0.03930   0.02967  -0.0526   1.0000   0.1601
  -4.250  -0.4547   0.03755   0.02772  -0.0525   1.0000   0.1678
  -4.000  -0.4312   0.03618   0.02602  -0.0523   1.0000   0.1774
  -3.750  -0.4100   0.03497   0.02482  -0.0518   1.0000   0.1902
  -3.500  -0.3884   0.03388   0.02369  -0.0510   1.0000   0.2055
  -3.250  -0.3667   0.03299   0.02274  -0.0503   1.0000   0.2270
  -3.000  -0.3470   0.03206   0.02207  -0.0492   1.0000   0.2563
  -2.750  -0.3257   0.03095   0.02138  -0.0486   1.0000   0.3109
  -2.500  -0.3096   0.02973   0.02200  -0.0457   1.0000   0.5153
  -2.250  -0.3146   0.03111   0.02385  -0.0363   1.0000   0.6445
  -2.000  -0.3154   0.03229   0.02498  -0.0289   1.0000   0.7064
  -1.750  -0.3157   0.03293   0.02556  -0.0220   1.0000   0.7522
  -1.500  -0.3153   0.03319   0.02572  -0.0157   1.0000   0.7931
  -1.250  -0.3171   0.03310   0.02558  -0.0090   1.0000   0.8301
  -1.000  -0.3173   0.03281   0.02519  -0.0030   1.0000   0.8693
  -0.750  -0.3121   0.03238   0.02470   0.0018   1.0000   0.9118
  -0.500  -0.2261   0.03365   0.02570  -0.0089   1.0000   0.9817
  -0.250  -0.1906   0.03399   0.02579  -0.0136   1.0000   1.0000
   0.000  -0.1894   0.03344   0.02513  -0.0120   1.0000   1.0000
   0.250  -0.1791   0.03330   0.02483  -0.0120   1.0000   1.0000
   0.500  -0.1619   0.03353   0.02489  -0.0130   1.0000   1.0000
   0.750  -0.1411   0.03400   0.02518  -0.0146   1.0000   1.0000
   1.000  -0.1183   0.03465   0.02566  -0.0165   1.0000   1.0000
   1.250  -0.0947   0.03542   0.02627  -0.0184   1.0000   1.0000
   1.500  -0.0709   0.03629   0.02699  -0.0203   1.0000   1.0000
   1.750  -0.0472   0.03723   0.02779  -0.0221   1.0000   1.0000
   2.000  -0.0238   0.03824   0.02868  -0.0239   1.0000   1.0000
   2.250  -0.0007   0.03931   0.02964  -0.0256   1.0000   1.0000
   2.500   0.0219   0.04044   0.03066  -0.0272   1.0000   1.0000
   2.750   0.0440   0.04162   0.03175  -0.0288   1.0000   1.0000
   3.000   0.0657   0.04284   0.03290  -0.0302   1.0000   1.0000
   3.250   0.0868   0.04412   0.03410  -0.0316   1.0000   1.0000
   3.500   0.1075   0.04545   0.03537  -0.0329   1.0000   1.0000
   3.750   0.1277   0.04683   0.03670  -0.0342   1.0000   1.0000
   4.000   0.1502   0.04843   0.03826  -0.0360   0.9986   1.0000
   4.250   0.1921   0.05145   0.04123  -0.0413   0.9884   1.0000
   4.500   0.2263   0.05377   0.04354  -0.0454   0.9739   1.0000
   4.750   0.2634   0.05634   0.04611  -0.0497   0.9572   1.0000
   5.000   0.3008   0.05909   0.04887  -0.0539   0.9407   1.0000
   5.250   0.3380   0.06202   0.05181  -0.0579   0.9235   1.0000
   5.500   0.3588   0.06342   0.05327  -0.0592   0.9041   1.0000
   5.750   0.3871   0.06542   0.05531  -0.0614   0.8822   1.0000
   6.000   0.4265   0.06828   0.05823  -0.0652   0.8607   1.0000
   6.250   0.4473   0.07000   0.06001  -0.0660   0.8383   1.0000
   6.500   0.5622   0.06883   0.05895  -0.0712   0.7283   1.0000
   6.750   0.5900   0.06970   0.05990  -0.0716   0.7057   1.0000
   7.000   0.6360   0.07031   0.06063  -0.0733   0.6844   1.0000
   7.250   0.6519   0.07130   0.06173  -0.0727   0.6638   1.0000
   7.500   0.6874   0.07181   0.06237  -0.0733   0.6438   1.0000
   7.750   0.7362   0.07161   0.06234  -0.0744   0.6252   1.0000
   8.000   0.7461   0.07290   0.06376  -0.0733   0.6043   1.0000
   8.250   0.7763   0.07316   0.06417  -0.0731   0.5840   1.0000
   8.500   0.8193   0.07234   0.06356  -0.0729   0.5648   1.0000
   8.750   0.8629   0.07099   0.06245  -0.0723   0.5456   1.0000
   9.000   0.8729   0.07215   0.06374  -0.0707   0.5221   1.0000
   9.250   0.9286   0.06870   0.06061  -0.0692   0.5022   1.0000
   9.500   1.1040   0.04881   0.04145  -0.0659   0.4825   1.0000
   9.750   1.1829   0.04077   0.03351  -0.0632   0.4325   1.0000
  10.000   1.2029   0.03973   0.03219  -0.0597   0.3820   1.0000
  10.250   1.2127   0.04035   0.03236  -0.0563   0.3328   1.0000
  10.500   1.2193   0.04199   0.03352  -0.0534   0.2873   1.0000
  10.750   1.2338   0.04404   0.03507  -0.0515   0.2458   1.0000
  11.000   1.2523   0.04639   0.03717  -0.0502   0.2136   1.0000
  11.250   1.2862   0.04883   0.03931  -0.0505   0.1862   1.0000
  11.500   1.3071   0.05150   0.04204  -0.0499   0.1696   1.0000
  11.750   1.3354   0.05448   0.04506  -0.0501   0.1558   1.0000
  12.000   1.3407   0.05727   0.04818  -0.0481   0.1480   1.0000
  12.250   1.3574   0.06063   0.05167  -0.0475   0.1404   1.0000
  12.500   1.3511   0.06401   0.05544  -0.0449   0.1367   1.0000
  12.750   1.3826   0.06762   0.05896  -0.0458   0.1285   1.0000
  13.000   1.3622   0.07111   0.06285  -0.0425   0.1274   1.0000
  13.250   1.3396   0.07508   0.06719  -0.0399   0.1266   1.0000
  13.500   1.3149   0.07958   0.07202  -0.0380   0.1262   1.0000
  13.750   1.2875   0.08468   0.07741  -0.0368   0.1262   1.0000
  14.000   1.2571   0.09047   0.08347  -0.0365   0.1265   1.0000
  14.250   1.2255   0.09702   0.09024  -0.0371   0.1272   1.0000
  14.500   1.1938   0.10435   0.09776  -0.0389   0.1280   1.0000
  14.750   1.1636   0.11245   0.10599  -0.0416   0.1288   1.0000
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