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WORTMANN FX 057-816 (fx057816-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 057-816 (fx057816-il)
Reynolds number: 1,000,000
Max Cl/Cd: 152.99 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx057816-il-1000000-n5.txt
Download as CSV file: xf-fx057816-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 057-816                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.8607   0.04783   0.04377  -0.0908   0.5731   0.0067
 -15.250  -0.9029   0.04106   0.03678  -0.0925   0.5728   0.0066
 -15.000  -0.9196   0.03743   0.03298  -0.0918   0.5724   0.0067
 -14.750  -0.9303   0.03476   0.03016  -0.0903   0.5718   0.0067
 -14.500  -0.9368   0.03261   0.02787  -0.0884   0.5712   0.0068
 -14.250  -0.9374   0.03093   0.02606  -0.0864   0.5705   0.0068
 -14.000  -0.9378   0.02943   0.02444  -0.0840   0.5702   0.0069
 -13.750  -0.9353   0.02826   0.02317  -0.0813   0.5698   0.0069
 -13.500  -0.9325   0.02690   0.02168  -0.0788   0.5694   0.0070
 -13.250  -0.9231   0.02560   0.02027  -0.0771   0.5690   0.0072
 -13.000  -0.9094   0.02453   0.01910  -0.0758   0.5686   0.0073
 -12.750  -0.8939   0.02352   0.01798  -0.0746   0.5681   0.0075
 -12.500  -0.8764   0.02263   0.01700  -0.0736   0.5675   0.0077
 -12.250  -0.8577   0.02181   0.01609  -0.0727   0.5670   0.0078
 -12.000  -0.8376   0.02107   0.01527  -0.0720   0.5664   0.0080
 -11.750  -0.8168   0.02037   0.01448  -0.0712   0.5658   0.0082
 -11.500  -0.7952   0.01971   0.01374  -0.0706   0.5651   0.0084
 -11.250  -0.7730   0.01909   0.01304  -0.0701   0.5644   0.0086
 -11.000  -0.7500   0.01852   0.01237  -0.0696   0.5637   0.0088
 -10.750  -0.7266   0.01798   0.01175  -0.0691   0.5631   0.0090
 -10.500  -0.7028   0.01746   0.01116  -0.0687   0.5625   0.0092
 -10.250  -0.6794   0.01685   0.01048  -0.0682   0.5619   0.0096
 -10.000  -0.6551   0.01633   0.00990  -0.0679   0.5614   0.0099
  -9.750  -0.6304   0.01585   0.00937  -0.0676   0.5608   0.0103
  -9.500  -0.6052   0.01543   0.00890  -0.0673   0.5603   0.0108
  -9.250  -0.5797   0.01506   0.00847  -0.0671   0.5597   0.0113
  -9.000  -0.5538   0.01471   0.00807  -0.0669   0.5592   0.0117
  -8.750  -0.5280   0.01432   0.00761  -0.0667   0.5586   0.0122
  -8.500  -0.5023   0.01392   0.00718  -0.0665   0.5580   0.0130
  -8.250  -0.4761   0.01358   0.00680  -0.0663   0.5573   0.0137
  -8.000  -0.4497   0.01328   0.00646  -0.0662   0.5567   0.0145
  -7.750  -0.4229   0.01301   0.00615  -0.0662   0.5563   0.0152
  -7.500  -0.3963   0.01268   0.00580  -0.0661   0.5560   0.0166
  -7.250  -0.3696   0.01236   0.00548  -0.0660   0.5556   0.0182
  -7.000  -0.3425   0.01210   0.00520  -0.0660   0.5552   0.0198
  -6.750  -0.3155   0.01181   0.00492  -0.0660   0.5547   0.0230
  -6.500  -0.2882   0.01157   0.00470  -0.0660   0.5542   0.0262
  -6.250  -0.2604   0.01141   0.00458  -0.0661   0.5536   0.0322
  -6.000  -0.2323   0.01128   0.00446  -0.0662   0.5531   0.0363
  -5.750  -0.2041   0.01115   0.00433  -0.0663   0.5526   0.0381
  -5.500  -0.1760   0.01102   0.00418  -0.0665   0.5521   0.0401
  -5.250  -0.1474   0.01094   0.00412  -0.0667   0.5516   0.0430
  -5.000  -0.1187   0.01090   0.00408  -0.0669   0.5511   0.0455
  -4.750  -0.0900   0.01084   0.00402  -0.0671   0.5506   0.0476
  -4.500  -0.0613   0.01079   0.00395  -0.0673   0.5501   0.0493
  -4.250  -0.0325   0.01073   0.00388  -0.0676   0.5496   0.0504
  -4.000  -0.0036   0.01073   0.00386  -0.0678   0.5491   0.0513
  -3.750   0.0257   0.01076   0.00390  -0.0681   0.5486   0.0518
  -3.500   0.0537   0.01058   0.00369  -0.0683   0.5482   0.0530
  -3.250   0.0818   0.01037   0.00346  -0.0685   0.5477   0.0542
  -3.000   0.1102   0.01022   0.00329  -0.0687   0.5472   0.0552
  -2.750   0.1387   0.01010   0.00316  -0.0689   0.5467   0.0561
  -2.500   0.1674   0.01000   0.00305  -0.0692   0.5461   0.0569
  -2.250   0.1961   0.00990   0.00294  -0.0695   0.5455   0.0576
  -2.000   0.2248   0.00983   0.00285  -0.0698   0.5449   0.0583
  -1.750   0.2536   0.00976   0.00277  -0.0701   0.5444   0.0591
  -1.500   0.2824   0.00970   0.00271  -0.0704   0.5439   0.0601
  -1.250   0.3113   0.00966   0.00267  -0.0707   0.5433   0.0610
  -1.000   0.3402   0.00963   0.00263  -0.0710   0.5427   0.0622
  -0.750   0.3692   0.00959   0.00260  -0.0714   0.5424   0.0636
  -0.500   0.3982   0.00955   0.00258  -0.0718   0.5421   0.0650
  -0.250   0.4273   0.00953   0.00258  -0.0721   0.5417   0.0660
   0.000   0.4564   0.00951   0.00257  -0.0725   0.5414   0.0665
   0.250   0.4854   0.00945   0.00254  -0.0729   0.5409   0.0690
   0.500   0.5145   0.00942   0.00253  -0.0733   0.5405   0.0713
   0.750   0.5435   0.00939   0.00254  -0.0737   0.5399   0.0732
   1.000   0.5726   0.00937   0.00255  -0.0742   0.5393   0.0751
   1.250   0.6017   0.00936   0.00256  -0.0746   0.5387   0.0769
   1.500   0.6308   0.00935   0.00258  -0.0750   0.5381   0.0804
   1.750   0.6599   0.00934   0.00261  -0.0755   0.5376   0.0866
   2.000   0.6884   0.00885   0.00265  -0.0762   0.5371   0.3004
   2.250   0.7174   0.00855   0.00269  -0.0770   0.5365   0.4238
   2.500   0.7456   0.00769   0.00283  -0.0778   0.5359   0.7754
   2.750   0.7747   0.00774   0.00290  -0.0782   0.5350   0.7908
   3.000   0.8041   0.00778   0.00295  -0.0787   0.5339   0.8011
   3.250   0.8330   0.00781   0.00302  -0.0790   0.5328   0.8094
   3.500   0.8624   0.00787   0.00306  -0.0795   0.5317   0.8157
   3.750   0.8910   0.00791   0.00312  -0.0798   0.5303   0.8201
   4.000   0.9197   0.00796   0.00320  -0.0801   0.5285   0.8249
   4.250   0.9489   0.00800   0.00328  -0.0806   0.5271   0.8273
   4.500   0.9781   0.00803   0.00335  -0.0811   0.5257   0.8290
   4.750   1.0073   0.00808   0.00342  -0.0816   0.5243   0.8303
   5.000   1.0364   0.00812   0.00349  -0.0821   0.5227   0.8321
   5.250   1.0648   0.00814   0.00357  -0.0824   0.5211   0.8357
   5.500   1.0936   0.00816   0.00362  -0.0828   0.5192   0.8377
   5.750   1.1224   0.00817   0.00363  -0.0833   0.5164   0.8385
   6.000   1.1512   0.00821   0.00372  -0.0838   0.5139   0.8394
   6.250   1.1800   0.00826   0.00383  -0.0843   0.5117   0.8403
   6.500   1.2089   0.00830   0.00392  -0.0848   0.5080   0.8411
   6.750   1.2374   0.00832   0.00395  -0.0852   0.5036   0.8418
   7.000   1.2659   0.00836   0.00404  -0.0857   0.4971   0.8426
   7.250   1.2928   0.00845   0.00408  -0.0859   0.4770   0.8434
   7.500   1.2978   0.01017   0.00526  -0.0831   0.3745   0.8447
   7.750   1.2897   0.01259   0.00722  -0.0787   0.2863   0.8464
   8.000   1.2974   0.01373   0.00824  -0.0765   0.2585   0.8475
   8.250   1.3024   0.01482   0.00928  -0.0739   0.2382   0.8492
   8.500   1.2957   0.01611   0.01056  -0.0696   0.2231   0.8514
   8.750   1.2726   0.01980   0.01435  -0.0666   0.2139   0.8549
   9.000   1.2509   0.02310   0.01766  -0.0631   0.2039   0.8578
   9.250   1.2338   0.02591   0.02044  -0.0599   0.1912   0.8603
   9.500   1.2149   0.02884   0.02330  -0.0567   0.1736   0.8625
   9.750   1.2029   0.03135   0.02574  -0.0541   0.1544   0.8647
  10.000   1.1824   0.03449   0.02874  -0.0511   0.1249   0.8672
  10.250   1.1756   0.03688   0.03102  -0.0493   0.1049   0.8693
  10.500   1.1797   0.03864   0.03275  -0.0483   0.0949   0.8713
  10.750   1.1869   0.04020   0.03428  -0.0475   0.0868   0.8732
  11.000   1.1963   0.04162   0.03569  -0.0468   0.0802   0.8751
  11.250   1.2049   0.04316   0.03721  -0.0463   0.0732   0.8772
  11.750   1.2254   0.04600   0.04007  -0.0453   0.0624   0.8818
  12.000   1.2341   0.04755   0.04159  -0.0448   0.0530   0.8846
  12.250   1.2329   0.04999   0.04387  -0.0439   0.0303   0.8875
  12.500   1.2389   0.05190   0.04576  -0.0434   0.0220   0.8905
  12.750   1.2481   0.05354   0.04741  -0.0431   0.0191   0.8937
  13.000   1.2583   0.05507   0.04898  -0.0428   0.0166   0.8977
  13.250   1.2690   0.05655   0.05050  -0.0425   0.0152   0.9029
  13.500   1.2780   0.05822   0.05221  -0.0422   0.0138   0.9091
  13.750   1.2861   0.05993   0.05398  -0.0418   0.0128   0.9197
  14.000   1.2971   0.06143   0.05561  -0.0417   0.0120   0.9475
  15.000   1.3395   0.06877   0.06308  -0.0429   0.0094   1.0000
  15.250   1.3492   0.07061   0.06496  -0.0430   0.0089   1.0000
  15.500   1.3587   0.07247   0.06685  -0.0431   0.0085   1.0000
  15.750   1.3669   0.07453   0.06894  -0.0433   0.0081   1.0000
  16.000   1.3739   0.07679   0.07124  -0.0435   0.0077   1.0000
  16.250   1.3813   0.07897   0.07346  -0.0437   0.0074   1.0000
  16.500   1.3901   0.08101   0.07555  -0.0440   0.0072   1.0000
  16.750   1.3972   0.08331   0.07790  -0.0444   0.0070   1.0000
  17.000   1.4044   0.08561   0.08025  -0.0448   0.0066   1.0000
  17.250   1.4113   0.08795   0.08266  -0.0452   0.0063   1.0000
  17.500   1.4172   0.09047   0.08522  -0.0457   0.0061   1.0000
  17.750   1.4218   0.09319   0.08799  -0.0463   0.0059   1.0000
  18.000   1.4262   0.09594   0.09080  -0.0469   0.0057   1.0000
  18.250   1.4299   0.09883   0.09375  -0.0476   0.0056   1.0000
  18.500   1.4348   0.10158   0.09657  -0.0483   0.0054   1.0000
  18.750   1.4395   0.10437   0.09942  -0.0491   0.0053   1.0000
  19.000   1.4427   0.10744   0.10256  -0.0500   0.0052   1.0000
  19.250   1.4460   0.11047   0.10566  -0.0509   0.0050   1.0000
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