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GOE 741 AIRFOIL (goe741-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 741 AIRFOIL (goe741-il)
Reynolds number: 200,000
Max Cl/Cd: 61.58 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe741-il-200000.txt
Download as CSV file: xf-goe741-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 741 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.2893   0.10729   0.10271  -0.0069   0.6501   0.0730
  -9.500  -0.2923   0.10397   0.09941  -0.0097   0.6466   0.0759
  -9.250  -0.3234   0.09847   0.09400  -0.0169   0.6449   0.0775
  -9.000  -0.2995   0.09600   0.09149  -0.0150   0.6393   0.0782
  -8.750  -0.2853   0.09356   0.08902  -0.0146   0.6349   0.0790
  -8.500  -0.2766   0.09097   0.08639  -0.0150   0.6313   0.0802
  -8.250  -0.2726   0.08810   0.08352  -0.0162   0.6277   0.0819
  -8.000  -0.2794   0.08447   0.07995  -0.0192   0.6241   0.0844
  -7.750  -0.3580   0.07715   0.07257  -0.0283   0.6242   0.0867
  -7.500  -0.3362   0.07438   0.06984  -0.0269   0.6193   0.0872
  -7.250  -0.3203   0.07218   0.06763  -0.0258   0.6154   0.0880
  -7.000  -0.3094   0.06992   0.06533  -0.0253   0.6122   0.0889
  -6.750  -0.3009   0.06754   0.06289  -0.0252   0.6092   0.0903
  -6.500  -0.2954   0.06460   0.05994  -0.0259   0.6058   0.0926
  -6.250  -0.3136   0.05810   0.05304  -0.0283   0.6038   0.0980
  -6.000  -0.3501   0.04007   0.03385  -0.0259   0.6040   0.0696
  -5.750  -0.3275   0.03905   0.03288  -0.0255   0.5998   0.0705
  -5.500  -0.3208   0.03365   0.02684  -0.0229   0.5970   0.0654
  -5.250  -0.3108   0.02898   0.02131  -0.0201   0.5944   0.0632
  -5.000  -0.2895   0.02724   0.01919  -0.0189   0.5913   0.0634
  -4.750  -0.2651   0.02596   0.01774  -0.0182   0.5876   0.0640
  -4.500  -0.2397   0.02499   0.01663  -0.0177   0.5837   0.0651
  -4.250  -0.2140   0.02409   0.01553  -0.0171   0.5801   0.0667
  -4.000  -0.1878   0.02319   0.01435  -0.0164   0.5769   0.0681
  -3.750  -0.1610   0.02226   0.01319  -0.0158   0.5739   0.0694
  -3.500  -0.1338   0.02162   0.01255  -0.0156   0.5706   0.0710
  -3.250  -0.1059   0.02113   0.01208  -0.0155   0.5667   0.0731
  -3.000  -0.0780   0.02065   0.01153  -0.0152   0.5631   0.0759
  -2.750  -0.0504   0.02012   0.01100  -0.0150   0.5598   0.0791
  -2.500  -0.0231   0.01983   0.01069  -0.0146   0.5568   0.0837
  -2.250   0.0041   0.01940   0.01020  -0.0142   0.5540   0.0888
  -2.000   0.0313   0.01920   0.01001  -0.0139   0.5507   0.0958
  -1.750   0.0580   0.01883   0.00978  -0.0137   0.5470   0.1057
  -1.500   0.0842   0.01849   0.00953  -0.0133   0.5435   0.1203
  -1.250   0.1101   0.01816   0.00930  -0.0128   0.5404   0.1387
  -1.000   0.1364   0.01800   0.00922  -0.0123   0.5375   0.1583
  -0.750   0.1633   0.01801   0.00922  -0.0119   0.5348   0.1788
  -0.500   0.1898   0.01812   0.00939  -0.0116   0.5315   0.2007
  -0.250   0.2158   0.01812   0.00954  -0.0113   0.5278   0.2250
   0.000   0.2413   0.01803   0.00958  -0.0109   0.5242   0.2535
   0.250   0.2666   0.01786   0.00951  -0.0103   0.5209   0.2843
   0.750   0.3143   0.01740   0.00933  -0.0085   0.5156   0.3714
   1.000   0.5010   0.01692   0.01047  -0.0377   0.5076   0.9862
   1.250   0.5687   0.01671   0.01010  -0.0455   0.5024   1.0000
   1.500   0.5939   0.01668   0.00993  -0.0448   0.4990   1.0000
   1.750   0.6190   0.01682   0.00989  -0.0441   0.4958   1.0000
   2.000   0.6442   0.01700   0.01014  -0.0439   0.4911   1.0000
   2.250   0.6694   0.01716   0.01029  -0.0435   0.4870   1.0000
   2.500   0.6946   0.01723   0.01030  -0.0429   0.4835   1.0000
   2.750   0.7199   0.01727   0.01024  -0.0423   0.4805   1.0000
   3.000   0.7452   0.01739   0.01022  -0.0417   0.4777   1.0000
   3.250   0.7696   0.01767   0.01060  -0.0414   0.4730   1.0000
   3.500   0.7941   0.01785   0.01080  -0.0409   0.4686   1.0000
   3.750   0.8191   0.01793   0.01084  -0.0404   0.4651   1.0000
   4.000   0.8444   0.01795   0.01078  -0.0397   0.4622   1.0000
   4.250   0.8697   0.01809   0.01079  -0.0391   0.4594   1.0000
   4.500   0.8925   0.01846   0.01132  -0.0387   0.4543   1.0000
   4.750   0.9165   0.01864   0.01152  -0.0382   0.4498   1.0000
   5.000   0.9414   0.01864   0.01147  -0.0375   0.4462   1.0000
   5.250   0.9670   0.01860   0.01132  -0.0368   0.4432   1.0000
   5.500   0.9897   0.01892   0.01171  -0.0362   0.4384   1.0000
   5.750   1.0125   0.01913   0.01199  -0.0356   0.4332   1.0000
   6.000   1.0369   0.01914   0.01196  -0.0349   0.4292   1.0000
   6.250   1.0625   0.01909   0.01182  -0.0342   0.4260   1.0000
   6.500   1.0839   0.01946   0.01228  -0.0335   0.4210   1.0000
   6.750   1.1056   0.01970   0.01259  -0.0327   0.4156   1.0000
   7.000   1.1299   0.01969   0.01254  -0.0320   0.4116   1.0000
   7.250   1.1556   0.01967   0.01240  -0.0313   0.4081   1.0000
   7.500   1.1733   0.02019   0.01310  -0.0302   0.4019   1.0000
   7.750   1.1955   0.02028   0.01321  -0.0294   0.3967   1.0000
   8.000   1.2205   0.02021   0.01303  -0.0286   0.3926   1.0000
   8.250   1.2382   0.02062   0.01355  -0.0274   0.3864   1.0000
   8.500   1.2583   0.02081   0.01377  -0.0263   0.3807   1.0000
   8.750   1.2821   0.02082   0.01370  -0.0255   0.3763   1.0000
   9.000   1.2982   0.02132   0.01429  -0.0241   0.3705   1.0000
   9.250   1.3156   0.02164   0.01466  -0.0227   0.3649   1.0000
   9.500   1.3380   0.02173   0.01467  -0.0218   0.3603   1.0000
   9.750   1.3520   0.02229   0.01532  -0.0201   0.3549   1.0000
  10.000   1.3657   0.02273   0.01582  -0.0183   0.3493   1.0000
  10.250   1.3860   0.02288   0.01590  -0.0172   0.3444   1.0000
  10.500   1.3974   0.02349   0.01657  -0.0151   0.3394   1.0000
  10.750   1.4059   0.02412   0.01729  -0.0128   0.3344   1.0000
  11.000   1.4212   0.02449   0.01764  -0.0112   0.3300   1.0000
  11.250   1.4411   0.02487   0.01796  -0.0101   0.3260   1.0000
  11.500   1.4368   0.02590   0.01915  -0.0065   0.3215   1.0000
  11.750   1.4357   0.02663   0.01992  -0.0030   0.3173   1.0000
  12.000   1.4491   0.02702   0.02026  -0.0013   0.3132   1.0000
  12.250   1.4548   0.02785   0.02111   0.0009   0.3091   1.0000
  12.500   1.4435   0.02948   0.02288   0.0038   0.3048   1.0000
  12.750   1.4490   0.03051   0.02394   0.0053   0.3005   1.0000
  13.000   1.4725   0.03064   0.02399   0.0059   0.2964   1.0000
  13.250   1.4657   0.03253   0.02600   0.0077   0.2924   1.0000
  13.500   1.4585   0.03460   0.02820   0.0092   0.2880   1.0000
  13.750   1.4683   0.03557   0.02918   0.0100   0.2837   1.0000
  14.000   1.4949   0.03549   0.02900   0.0106   0.2794   1.0000
  14.250   1.4714   0.03897   0.03269   0.0118   0.2752   1.0000
  14.500   1.4683   0.04108   0.03488   0.0126   0.2705   1.0000
  14.750   1.4881   0.04132   0.03507   0.0132   0.2663   1.0000
  15.000   1.4864   0.04346   0.03730   0.0138   0.2620   1.0000
  15.250   1.4666   0.04725   0.04124   0.0141   0.2572   1.0000
  15.500   1.4766   0.04833   0.04232   0.0146   0.2524   1.0000
  15.750   1.4944   0.04876   0.04271   0.0152   0.2479   1.0000
  16.000   1.4604   0.05429   0.04847   0.0148   0.2428   1.0000
  16.250   1.4651   0.05606   0.05026   0.0149   0.2379   1.0000
  16.500   1.4880   0.05586   0.04998   0.0156   0.2330   1.0000
  16.750   1.4476   0.06275   0.05712   0.0143   0.2273   1.0000
  17.000   1.4562   0.06414   0.05848   0.0143   0.2218   1.0000
  17.250   1.4523   0.06706   0.06144   0.0140   0.2161   1.0000
  17.500   1.4287   0.07256   0.06709   0.0127   0.2104   1.0000
  17.750   1.4603   0.07106   0.06542   0.0135   0.2045   1.0000
  18.000   1.4148   0.07965   0.07427   0.0112   0.1989   1.0000
  18.250   1.4125   0.08267   0.07732   0.0104   0.1931   1.0000
  18.500   1.4097   0.08581   0.08048   0.0097   0.1876   1.0000
  18.750   1.3824   0.09250   0.08732   0.0077   0.1816   1.0000
  19.000   1.4085   0.09157   0.08628   0.0082   0.1764   1.0000
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