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GOE 601 AIRFOIL (goe601-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 601 AIRFOIL (goe601-il)
Reynolds number: 500,000
Max Cl/Cd: 82.81 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe601-il-500000.txt
Download as CSV file: xf-goe601-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 601 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.7391   0.11949   0.11638  -0.0596   1.0000   0.0267
 -18.500  -0.7974   0.10438   0.10101  -0.0687   1.0000   0.0266
 -18.250  -0.8330   0.09434   0.09078  -0.0749   1.0000   0.0266
 -18.000  -0.8600   0.08636   0.08260  -0.0799   1.0000   0.0267
 -17.750  -0.8821   0.07972   0.07581  -0.0833   1.0000   0.0267
 -17.500  -0.9004   0.07413   0.07010  -0.0858   1.0000   0.0271
 -17.250  -0.9121   0.06962   0.06548  -0.0878   1.0000   0.0272
 -17.000  -0.9155   0.06647   0.06230  -0.0887   1.0000   0.0275
 -16.750  -0.9213   0.06309   0.05886  -0.0899   1.0000   0.0278
 -16.500  -0.9274   0.05982   0.05552  -0.0910   1.0000   0.0280
 -16.250  -0.9345   0.05657   0.05218  -0.0919   1.0000   0.0283
 -16.000  -0.9418   0.05343   0.04895  -0.0925   1.0000   0.0285
 -15.750  -0.9483   0.05053   0.04594  -0.0928   1.0000   0.0287
 -15.500  -0.9525   0.04809   0.04343  -0.0929   1.0000   0.0291
 -15.250  -0.9580   0.04564   0.04088  -0.0926   1.0000   0.0294
 -15.000  -0.9639   0.04334   0.03848  -0.0919   1.0000   0.0297
 -14.750  -0.9702   0.04121   0.03624  -0.0908   1.0000   0.0300
 -14.500  -0.9769   0.03931   0.03423  -0.0894   1.0000   0.0303
 -14.250  -0.9833   0.03761   0.03242  -0.0875   1.0000   0.0306
 -14.000  -0.9918   0.03611   0.03080  -0.0851   1.0000   0.0309
 -13.750  -1.0003   0.03485   0.02942  -0.0822   1.0000   0.0311
 -13.500  -1.0009   0.03302   0.02755  -0.0796   1.0000   0.0315
 -13.250  -1.0027   0.03176   0.02627  -0.0767   1.0000   0.0319
 -13.000  -0.9976   0.03062   0.02511  -0.0750   0.9994   0.0323
 -12.750  -0.9729   0.02933   0.02377  -0.0769   0.9968   0.0329
 -12.500  -0.9472   0.02820   0.02257  -0.0788   0.9941   0.0337
 -12.250  -0.9237   0.02705   0.02133  -0.0800   0.9908   0.0344
 -12.000  -0.8986   0.02609   0.02026  -0.0813   0.9872   0.0352
 -11.750  -0.8701   0.02526   0.01931  -0.0830   0.9843   0.0358
 -11.500  -0.8428   0.02366   0.01768  -0.0847   0.9824   0.0368
 -11.250  -0.8222   0.02261   0.01663  -0.0847   0.9767   0.0375
 -11.000  -0.7945   0.02175   0.01574  -0.0860   0.9732   0.0385
 -10.750  -0.7633   0.02094   0.01488  -0.0877   0.9709   0.0396
 -10.500  -0.7305   0.02010   0.01397  -0.0897   0.9693   0.0405
 -10.250  -0.7102   0.01944   0.01324  -0.0889   0.9618   0.0412
 -10.000  -0.6818   0.01830   0.01207  -0.0902   0.9587   0.0424
  -9.750  -0.6493   0.01737   0.01113  -0.0921   0.9566   0.0438
  -9.500  -0.6264   0.01675   0.01048  -0.0918   0.9495   0.0449
  -9.250  -0.5979   0.01612   0.00980  -0.0924   0.9442   0.0462
  -9.000  -0.5660   0.01553   0.00914  -0.0938   0.9406   0.0475
  -8.750  -0.5514   0.01490   0.00849  -0.0916   0.9295   0.0490
  -8.500  -0.5238   0.01430   0.00786  -0.0920   0.9243   0.0513
  -8.250  -0.5070   0.01393   0.00745  -0.0900   0.9130   0.0534
  -8.000  -0.4834   0.01344   0.00692  -0.0894   0.9057   0.0565
  -7.750  -0.4628   0.01302   0.00650  -0.0881   0.8966   0.0611
  -7.500  -0.4398   0.01257   0.00610  -0.0874   0.8894   0.0720
  -7.250  -0.4158   0.01232   0.00592  -0.0868   0.8815   0.0913
  -7.000  -0.3872   0.01213   0.00571  -0.0870   0.8759   0.1032
  -6.750  -0.3658   0.01188   0.00546  -0.0859   0.8681   0.1104
  -6.500  -0.3390   0.01172   0.00523  -0.0858   0.8621   0.1164
  -6.250  -0.3150   0.01151   0.00497  -0.0851   0.8562   0.1215
  -6.000  -0.2923   0.01128   0.00473  -0.0842   0.8498   0.1269
  -5.750  -0.2658   0.01112   0.00449  -0.0840   0.8446   0.1319
  -5.500  -0.2429   0.01091   0.00429  -0.0831   0.8392   0.1383
  -5.250  -0.2198   0.01070   0.00409  -0.0822   0.8336   0.1459
  -5.000  -0.1956   0.01045   0.00387  -0.0816   0.8286   0.1605
  -4.750  -0.1743   0.01007   0.00367  -0.0806   0.8238   0.2039
  -4.500  -0.1536   0.00974   0.00355  -0.0794   0.8186   0.2565
  -4.250  -0.1297   0.00953   0.00343  -0.0786   0.8139   0.2890
  -4.000  -0.1037   0.00939   0.00332  -0.0783   0.8095   0.3143
  -3.750  -0.0814   0.00921   0.00324  -0.0773   0.8040   0.3405
  -3.500  -0.0585   0.00901   0.00315  -0.0763   0.7984   0.3700
  -3.250  -0.0339   0.00887   0.00309  -0.0756   0.7930   0.4049
  -3.000  -0.0099   0.00879   0.00310  -0.0748   0.7878   0.4367
  -2.750   0.0146   0.00874   0.00308  -0.0740   0.7822   0.4588
  -2.500   0.0409   0.00871   0.00304  -0.0736   0.7773   0.4745
  -2.250   0.0684   0.00872   0.00301  -0.0735   0.7728   0.4880
  -2.000   0.0929   0.00869   0.00299  -0.0727   0.7674   0.5009
  -1.750   0.1183   0.00863   0.00296  -0.0721   0.7621   0.5133
  -1.500   0.1453   0.00859   0.00291  -0.0718   0.7571   0.5258
  -1.250   0.1706   0.00858   0.00289  -0.0712   0.7518   0.5366
  -1.000   0.1956   0.00850   0.00286  -0.0706   0.7463   0.5463
  -0.750   0.2223   0.00847   0.00280  -0.0702   0.7411   0.5563
  -0.500   0.2478   0.00841   0.00279  -0.0697   0.7356   0.5671
  -0.250   0.2722   0.00835   0.00276  -0.0689   0.7292   0.5780
   0.000   0.2983   0.00830   0.00272  -0.0684   0.7234   0.5900
   0.250   0.3230   0.00825   0.00271  -0.0676   0.7173   0.6024
   0.500   0.3468   0.00817   0.00270  -0.0667   0.7099   0.6169
   0.750   0.3718   0.00812   0.00267  -0.0660   0.7032   0.6360
   1.000   0.3942   0.00804   0.00269  -0.0647   0.6953   0.6566
   1.250   0.4185   0.00799   0.00268  -0.0639   0.6888   0.6797
   1.500   0.4411   0.00793   0.00272  -0.0627   0.6811   0.7031
   1.750   0.4637   0.00786   0.00272  -0.0614   0.6728   0.7298
   2.000   0.4854   0.00779   0.00277  -0.0600   0.6638   0.7599
   2.250   0.5072   0.00772   0.00281  -0.0585   0.6548   0.7969
   2.500   0.5296   0.00767   0.00290  -0.0571   0.6448   0.8346
   2.750   0.5549   0.00768   0.00298  -0.0563   0.6339   0.8693
   3.000   0.5839   0.00775   0.00309  -0.0564   0.6205   0.9012
   3.250   0.6209   0.00791   0.00325  -0.0583   0.6039   0.9240
   3.500   0.6591   0.00811   0.00342  -0.0604   0.5846   0.9410
   3.750   0.6931   0.00837   0.00360  -0.0617   0.5583   0.9543
   4.000   0.7250   0.00880   0.00383  -0.0628   0.5167   0.9638
   4.250   0.7530   0.00939   0.00416  -0.0631   0.4616   0.9730
   4.500   0.7779   0.01014   0.00458  -0.0630   0.3992   0.9830
   4.750   0.8095   0.01081   0.00499  -0.0645   0.3569   0.9898
   5.000   0.8432   0.01131   0.00534  -0.0662   0.3351   0.9958
   5.500   0.8835   0.01182   0.00575  -0.0639   0.3127   1.0000
   5.750   0.8848   0.01198   0.00588  -0.0587   0.3060   1.0000
   6.000   0.8900   0.01219   0.00606  -0.0544   0.2999   1.0000
   6.250   0.9007   0.01236   0.00623  -0.0511   0.2930   1.0000
   6.500   0.9103   0.01263   0.00647  -0.0477   0.2868   1.0000
   6.750   0.9234   0.01286   0.00670  -0.0449   0.2810   1.0000
   7.000   0.9379   0.01309   0.00693  -0.0425   0.2744   1.0000
   7.250   0.9495   0.01345   0.00724  -0.0397   0.2676   1.0000
   7.500   0.9672   0.01365   0.00747  -0.0379   0.2602   1.0000
   7.750   0.9813   0.01398   0.00778  -0.0356   0.2532   1.0000
   8.000   0.9979   0.01426   0.00808  -0.0337   0.2468   1.0000
   8.250   1.0136   0.01460   0.00840  -0.0318   0.2381   1.0000
   8.500   1.0296   0.01494   0.00874  -0.0299   0.2283   1.0000
   8.750   1.0440   0.01538   0.00912  -0.0279   0.2156   1.0000
   9.000   1.0567   0.01591   0.00957  -0.0257   0.1955   1.0000
   9.250   1.0652   0.01669   0.01018  -0.0230   0.1665   1.0000
   9.500   1.0586   0.01832   0.01138  -0.0186   0.1037   1.0000
   9.750   1.0507   0.02021   0.01293  -0.0142   0.0553   1.0000
  10.000   1.0602   0.02117   0.01385  -0.0121   0.0473   1.0000
  10.250   1.0710   0.02210   0.01476  -0.0103   0.0437   1.0000
  10.500   1.0837   0.02292   0.01564  -0.0087   0.0420   1.0000
  10.750   1.0953   0.02385   0.01660  -0.0071   0.0404   1.0000
  11.000   1.1059   0.02486   0.01764  -0.0055   0.0391   1.0000
  11.250   1.1138   0.02609   0.01890  -0.0037   0.0379   1.0000
  11.500   1.1237   0.02720   0.02007  -0.0022   0.0371   1.0000
  11.750   1.1338   0.02833   0.02126  -0.0008   0.0365   1.0000
  12.000   1.1429   0.02955   0.02254   0.0006   0.0358   1.0000
  12.250   1.1510   0.03087   0.02392   0.0019   0.0353   1.0000
  12.500   1.1579   0.03233   0.02544   0.0033   0.0347   1.0000
  12.750   1.1634   0.03395   0.02711   0.0046   0.0340   1.0000
  13.000   1.1656   0.03586   0.02907   0.0060   0.0333   1.0000
  13.250   1.1666   0.03795   0.03122   0.0073   0.0329   1.0000
  13.500   1.1633   0.04048   0.03381   0.0086   0.0323   1.0000
  13.750   1.1699   0.04221   0.03562   0.0094   0.0320   1.0000
  14.000   1.1748   0.04415   0.03764   0.0101   0.0317   1.0000
  14.250   1.1791   0.04621   0.03977   0.0108   0.0314   1.0000
  14.500   1.1828   0.04838   0.04201   0.0113   0.0310   1.0000
  14.750   1.1866   0.05058   0.04429   0.0118   0.0305   1.0000
  15.000   1.1899   0.05288   0.04665   0.0121   0.0300   1.0000
  15.250   1.1924   0.05530   0.04913   0.0124   0.0297   1.0000
  15.500   1.1942   0.05786   0.05174   0.0126   0.0292   1.0000
  15.750   1.1963   0.06039   0.05432   0.0127   0.0289   1.0000
  16.000   1.1974   0.06298   0.05695   0.0129   0.0285   1.0000
  16.250   1.1999   0.06543   0.05943   0.0131   0.0282   1.0000
  16.500   1.2029   0.06748   0.06149   0.0141   0.0276   1.0000
  16.750   1.2077   0.06980   0.06388   0.0140   0.0275   1.0000
  17.000   1.2109   0.07244   0.06662   0.0137   0.0272   1.0000
  17.250   1.2132   0.07524   0.06952   0.0133   0.0268   1.0000
  17.500   1.2167   0.07779   0.07215   0.0131   0.0265   1.0000
  17.750   1.2189   0.08061   0.07505   0.0126   0.0261   1.0000
  18.000   1.2217   0.08331   0.07783   0.0122   0.0257   1.0000
  18.250   1.2242   0.08605   0.08063   0.0117   0.0254   1.0000
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