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WORTMANN FX 057-816 (fx057816-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 057-816 (fx057816-il)
Reynolds number: 500,000
Max Cl/Cd: 113.34 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx057816-il-500000-n5.txt
Download as CSV file: xf-fx057816-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.7199   0.04967   0.04516  -0.0860   0.5845   0.0095
 -13.750  -0.7601   0.04245   0.03766  -0.0892   0.5843   0.0094
 -13.500  -0.7783   0.03889   0.03394  -0.0887   0.5840   0.0095
 -13.250  -0.7888   0.03627   0.03118  -0.0873   0.5836   0.0096
 -13.000  -0.7939   0.03422   0.02900  -0.0854   0.5831   0.0097
 -12.750  -0.7961   0.03252   0.02717  -0.0831   0.5826   0.0098
 -12.500  -0.7968   0.03117   0.02570  -0.0804   0.5820   0.0100
 -12.250  -0.7903   0.02979   0.02416  -0.0786   0.5815   0.0101
 -12.000  -0.7792   0.02856   0.02280  -0.0772   0.5808   0.0103
 -11.750  -0.7665   0.02737   0.02147  -0.0758   0.5802   0.0105
 -11.500  -0.7514   0.02629   0.02024  -0.0747   0.5794   0.0108
 -11.250  -0.7346   0.02528   0.01908  -0.0737   0.5786   0.0111
 -11.000  -0.7164   0.02435   0.01801  -0.0728   0.5779   0.0114
 -10.750  -0.6968   0.02348   0.01699  -0.0721   0.5772   0.0117
 -10.500  -0.6773   0.02259   0.01598  -0.0713   0.5765   0.0121
 -10.250  -0.6570   0.02176   0.01505  -0.0706   0.5759   0.0126
 -10.000  -0.6350   0.02105   0.01425  -0.0701   0.5753   0.0130
  -9.750  -0.6122   0.02039   0.01350  -0.0696   0.5747   0.0135
  -9.500  -0.5888   0.01977   0.01277  -0.0692   0.5742   0.0140
  -9.250  -0.5650   0.01919   0.01208  -0.0688   0.5736   0.0146
  -9.000  -0.5406   0.01866   0.01144  -0.0685   0.5731   0.0151
  -8.750  -0.5165   0.01807   0.01076  -0.0681   0.5726   0.0160
  -8.500  -0.4918   0.01757   0.01020  -0.0678   0.5720   0.0170
  -8.250  -0.4665   0.01713   0.00970  -0.0676   0.5715   0.0181
  -8.000  -0.4410   0.01674   0.00922  -0.0674   0.5710   0.0193
  -7.750  -0.4154   0.01634   0.00877  -0.0672   0.5704   0.0207
  -7.500  -0.3894   0.01596   0.00839  -0.0670   0.5700   0.0229
  -7.250  -0.3632   0.01563   0.00804  -0.0669   0.5695   0.0252
  -7.000  -0.3365   0.01536   0.00774  -0.0668   0.5689   0.0286
  -6.750  -0.3088   0.01527   0.00770  -0.0669   0.5682   0.0331
  -6.500  -0.2813   0.01515   0.00756  -0.0670   0.5675   0.0366
  -6.250  -0.2539   0.01499   0.00734  -0.0670   0.5668   0.0385
  -6.000  -0.2259   0.01494   0.00730  -0.0671   0.5662   0.0415
  -5.750  -0.1975   0.01500   0.00735  -0.0673   0.5656   0.0440
  -5.500  -0.1694   0.01497   0.00729  -0.0674   0.5650   0.0464
  -5.250  -0.1413   0.01493   0.00720  -0.0675   0.5644   0.0487
  -5.000  -0.1134   0.01485   0.00708  -0.0676   0.5638   0.0503
  -4.750  -0.0851   0.01484   0.00701  -0.0678   0.5632   0.0514
  -4.500  -0.0574   0.01469   0.00683  -0.0679   0.5627   0.0525
  -4.250  -0.0306   0.01437   0.00650  -0.0679   0.5621   0.0551
  -4.000  -0.0027   0.01428   0.00640  -0.0680   0.5616   0.0570
  -3.750   0.0252   0.01416   0.00626  -0.0682   0.5611   0.0588
  -3.500   0.0529   0.01400   0.00607  -0.0683   0.5606   0.0603
  -3.250   0.0806   0.01383   0.00587  -0.0684   0.5601   0.0614
  -3.000   0.1084   0.01367   0.00567  -0.0685   0.5595   0.0625
  -2.750   0.1363   0.01351   0.00548  -0.0686   0.5590   0.0633
  -2.500   0.1642   0.01338   0.00532  -0.0688   0.5584   0.0641
  -2.250   0.1922   0.01326   0.00517  -0.0690   0.5579   0.0648
  -2.000   0.2202   0.01316   0.00506  -0.0691   0.5574   0.0653
  -1.750   0.2483   0.01309   0.00496  -0.0694   0.5570   0.0658
  -1.500   0.2765   0.01304   0.00490  -0.0696   0.5565   0.0663
  -1.250   0.3044   0.01293   0.00482  -0.0698   0.5560   0.0671
  -1.000   0.3323   0.01282   0.00473  -0.0700   0.5555   0.0692
  -0.750   0.3604   0.01277   0.00472  -0.0703   0.5549   0.0715
  -0.500   0.3886   0.01274   0.00472  -0.0706   0.5543   0.0735
  -0.250   0.4169   0.01273   0.00472  -0.0709   0.5537   0.0754
   0.000   0.4452   0.01273   0.00475  -0.0712   0.5531   0.0771
   0.250   0.4735   0.01272   0.00476  -0.0715   0.5524   0.0793
   0.500   0.5019   0.01271   0.00478  -0.0718   0.5516   0.0823
   0.750   0.5303   0.01271   0.00482  -0.0721   0.5508   0.0855
   1.000   0.5587   0.01272   0.00486  -0.0724   0.5501   0.0904
   1.250   0.5871   0.01270   0.00492  -0.0728   0.5495   0.1055
   1.500   0.6139   0.01197   0.00498  -0.0736   0.5489   0.3915
   1.750   0.6378   0.01108   0.00528  -0.0735   0.5484   0.7771
   2.000   0.6662   0.01123   0.00545  -0.0737   0.5478   0.7989
   2.250   0.6941   0.01138   0.00563  -0.0738   0.5473   0.8109
   2.500   0.7218   0.01153   0.00580  -0.0738   0.5467   0.8216
   2.750   0.7500   0.01169   0.00597  -0.0740   0.5462   0.8320
   3.000   0.7771   0.01181   0.00613  -0.0739   0.5457   0.8378
   3.250   0.8052   0.01193   0.00626  -0.0741   0.5452   0.8428
   3.500   0.8343   0.01202   0.00635  -0.0746   0.5446   0.8466
   3.750   0.8626   0.01206   0.00640  -0.0748   0.5438   0.8497
   4.000   0.8913   0.01209   0.00643  -0.0751   0.5428   0.8517
   4.250   0.9181   0.01221   0.00664  -0.0753   0.5413   0.8541
   4.500   0.9449   0.01236   0.00687  -0.0753   0.5399   0.8585
   4.750   0.9727   0.01244   0.00700  -0.0756   0.5380   0.8622
   5.000   1.0014   0.01243   0.00702  -0.0761   0.5360   0.8635
   5.250   1.0302   0.01237   0.00700  -0.0765   0.5343   0.8642
   5.500   1.0591   0.01233   0.00698  -0.0769   0.5328   0.8650
   5.750   1.0880   0.01227   0.00695  -0.0774   0.5315   0.8659
   6.000   1.1168   0.01225   0.00696  -0.0778   0.5303   0.8668
   6.250   1.1452   0.01223   0.00698  -0.0782   0.5286   0.8678
   6.500   1.1715   0.01236   0.00723  -0.0784   0.5256   0.8687
   6.750   1.1989   0.01240   0.00736  -0.0787   0.5227   0.8697
   7.000   1.2272   0.01233   0.00735  -0.0791   0.5197   0.8706
   7.250   1.2559   0.01224   0.00730  -0.0795   0.5172   0.8716
   7.500   1.2837   0.01224   0.00737  -0.0798   0.5144   0.8726
   7.750   1.3098   0.01234   0.00760  -0.0800   0.5076   0.8738
   8.000   1.3376   0.01217   0.00747  -0.0803   0.4956   0.8749
   8.250   1.3646   0.01204   0.00734  -0.0804   0.4770   0.8760
   8.500   1.3816   0.01238   0.00741  -0.0791   0.4276   0.8776
   8.750   1.3493   0.01528   0.00983  -0.0715   0.3390   0.8816
   9.000   1.3159   0.01778   0.01233  -0.0643   0.3162   0.8867
   9.250   1.2772   0.02278   0.01737  -0.0607   0.3016   0.8926
   9.500   1.2494   0.02632   0.02090  -0.0569   0.2881   0.8973
   9.750   1.2249   0.02960   0.02414  -0.0533   0.2722   0.9027
  10.000   1.2116   0.03224   0.02675  -0.0507   0.2576   0.9078
  10.250   1.2035   0.03458   0.02906  -0.0486   0.2438   0.9131
  10.500   1.1992   0.03668   0.03114  -0.0468   0.2293   0.9204
  10.750   1.1967   0.03893   0.03335  -0.0455   0.2111   0.9302
  11.000   1.1943   0.04155   0.03585  -0.0449   0.1834   0.9470
  11.500   1.1869   0.04714   0.04107  -0.0437   0.1210   1.0000
  11.750   1.1883   0.04944   0.04323  -0.0430   0.1016   1.0000
  12.000   1.1948   0.05134   0.04510  -0.0426   0.0914   1.0000
  12.250   1.2031   0.05311   0.04684  -0.0424   0.0832   1.0000
  12.500   1.2123   0.05481   0.04852  -0.0421   0.0762   1.0000
  12.750   1.2220   0.05649   0.05018  -0.0420   0.0692   1.0000
  13.000   1.2317   0.05819   0.05188  -0.0418   0.0608   1.0000
  13.250   1.2372   0.06032   0.05393  -0.0416   0.0460   1.0000
  13.500   1.2369   0.06306   0.05649  -0.0413   0.0272   1.0000
  13.750   1.2446   0.06505   0.05849  -0.0412   0.0221   1.0000
  14.000   1.2524   0.06707   0.06054  -0.0411   0.0197   1.0000
  14.250   1.2593   0.06924   0.06275  -0.0411   0.0173   1.0000
  14.500   1.2687   0.07113   0.06470  -0.0412   0.0162   1.0000
  14.750   1.2777   0.07310   0.06672  -0.0413   0.0150   1.0000
  15.000   1.2850   0.07529   0.06895  -0.0415   0.0142   1.0000
  15.250   1.2911   0.07765   0.07136  -0.0416   0.0134   1.0000
  15.500   1.2975   0.07999   0.07375  -0.0418   0.0127   1.0000
  15.750   1.3055   0.08219   0.07601  -0.0421   0.0121   1.0000
  16.000   1.3120   0.08461   0.07850  -0.0425   0.0115   1.0000
  16.250   1.3184   0.08705   0.08100  -0.0429   0.0110   1.0000
  16.500   1.3239   0.08963   0.08363  -0.0433   0.0105   1.0000
  16.750   1.3272   0.09255   0.08661  -0.0438   0.0101   1.0000
  17.000   1.3306   0.09548   0.08960  -0.0444   0.0097   1.0000
  17.250   1.3356   0.09823   0.09243  -0.0450   0.0094   1.0000
  17.500   1.3393   0.10120   0.09548  -0.0458   0.0091   1.0000
  17.750   1.3433   0.10414   0.09850  -0.0465   0.0088   1.0000
  18.000   1.3458   0.10735   0.10183  -0.0474   0.0086   1.0000
  18.250   1.3482   0.11057   0.10512  -0.0484   0.0084   1.0000
  18.500   1.3498   0.11394   0.10856  -0.0494   0.0081   1.0000
  18.750   1.3512   0.11738   0.11208  -0.0506   0.0079   1.0000
  19.000   1.3503   0.12121   0.11598  -0.0519   0.0077   1.0000
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