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WORTMANN FX 057-816 (fx057816-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 057-816 (fx057816-il)
Reynolds number: 200,000
Max Cl/Cd: 27.11 at α=11.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx057816-il-200000-n5.txt
Download as CSV file: xf-fx057816-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2751   0.10601   0.10074  -0.0526   0.6040   0.0192
 -11.500  -0.2872   0.09872   0.09350  -0.0561   0.6038   0.0197
 -11.250  -0.2942   0.09325   0.08808  -0.0589   0.6034   0.0201
 -11.000  -0.2904   0.09037   0.08520  -0.0606   0.6029   0.0205
 -10.750  -0.2913   0.08645   0.08132  -0.0628   0.6024   0.0209
 -10.500  -0.4623   0.05175   0.04658  -0.0839   0.6033   0.0197
 -10.250  -0.5089   0.04562   0.04015  -0.0812   0.6029   0.0196
 -10.000  -0.5356   0.03987   0.03389  -0.0786   0.6025   0.0199
  -9.750  -0.5290   0.03814   0.03199  -0.0773   0.6019   0.0205
  -9.500  -0.5114   0.03772   0.03149  -0.0767   0.6013   0.0211
  -9.250  -0.4957   0.03676   0.03039  -0.0759   0.6007   0.0217
  -9.000  -0.4826   0.03504   0.02843  -0.0749   0.6002   0.0225
  -8.750  -0.4687   0.03308   0.02618  -0.0739   0.5997   0.0235
  -8.500  -0.4535   0.03099   0.02373  -0.0729   0.5992   0.0248
  -8.250  -0.4357   0.02897   0.02133  -0.0721   0.5985   0.0264
  -8.000  -0.4149   0.02808   0.02036  -0.0716   0.5975   0.0282
  -7.750  -0.3906   0.02801   0.02027  -0.0714   0.5964   0.0297
  -7.500  -0.3664   0.02769   0.01985  -0.0712   0.5953   0.0315
  -7.250  -0.3423   0.02711   0.01911  -0.0709   0.5944   0.0342
  -7.000  -0.3184   0.02595   0.01765  -0.0705   0.5936   0.0377
  -6.750  -0.2939   0.02546   0.01706  -0.0703   0.5928   0.0399
  -6.500  -0.2682   0.02567   0.01726  -0.0702   0.5920   0.0420
  -6.250  -0.2425   0.02567   0.01716  -0.0701   0.5912   0.0451
  -6.000  -0.2167   0.02524   0.01653  -0.0699   0.5904   0.0492
  -5.750  -0.1904   0.02511   0.01616  -0.0697   0.5897   0.0519
  -5.500  -0.1652   0.02451   0.01555  -0.0697   0.5890   0.0546
  -5.250  -0.1392   0.02435   0.01533  -0.0697   0.5884   0.0573
  -5.000  -0.1130   0.02410   0.01495  -0.0697   0.5877   0.0604
  -4.750  -0.0864   0.02379   0.01449  -0.0696   0.5871   0.0635
  -4.500  -0.0595   0.02356   0.01408  -0.0695   0.5864   0.0658
  -4.250  -0.0330   0.02303   0.01347  -0.0694   0.5858   0.0675
  -4.000  -0.0066   0.02261   0.01305  -0.0694   0.5852   0.0697
  -3.750   0.0200   0.02233   0.01272  -0.0694   0.5847   0.0718
  -3.500   0.0458   0.02215   0.01255  -0.0693   0.5837   0.0735
  -3.250   0.0714   0.02204   0.01244  -0.0692   0.5826   0.0750
  -3.000   0.0969   0.02197   0.01237  -0.0692   0.5815   0.0763
  -2.750   0.1225   0.02195   0.01233  -0.0691   0.5804   0.0773
  -2.500   0.1475   0.02182   0.01225  -0.0690   0.5794   0.0785
  -2.250   0.1725   0.02172   0.01220  -0.0689   0.5784   0.0797
  -2.000   0.1978   0.02165   0.01217  -0.0688   0.5774   0.0811
  -1.750   0.2235   0.02160   0.01213  -0.0687   0.5764   0.0831
  -1.500   0.2495   0.02157   0.01210  -0.0687   0.5754   0.0858
  -1.250   0.2755   0.02159   0.01210  -0.0687   0.5746   0.0877
  -1.000   0.3013   0.02155   0.01208  -0.0687   0.5739   0.0897
  -0.750   0.3275   0.02158   0.01210  -0.0688   0.5733   0.0921
  -0.500   0.3540   0.02164   0.01214  -0.0688   0.5727   0.0950
  -0.250   0.3805   0.02170   0.01220  -0.0689   0.5721   0.0983
   0.000   0.4071   0.02176   0.01227  -0.0690   0.5716   0.1034
   0.250   0.4337   0.02182   0.01235  -0.0691   0.5711   0.1125
   0.500   0.4572   0.02118   0.01248  -0.0692   0.5706   0.3359
   0.750   0.4610   0.02121   0.01410  -0.0662   0.5671   0.7132
   1.000   0.4788   0.02206   0.01510  -0.0648   0.5650   0.7983
   1.250   0.4992   0.02273   0.01579  -0.0638   0.5634   0.8204
   1.500   0.5181   0.02332   0.01642  -0.0623   0.5622   0.8412
   1.750   0.5372   0.02380   0.01692  -0.0608   0.5611   0.8556
   2.000   0.5559   0.02422   0.01736  -0.0592   0.5602   0.8687
   2.250   0.5778   0.02452   0.01765  -0.0582   0.5593   0.8794
   2.500   0.5975   0.02472   0.01786  -0.0567   0.5586   0.8868
   2.750   0.6214   0.02493   0.01806  -0.0561   0.5579   0.8945
   3.000   0.6439   0.02512   0.01824  -0.0552   0.5573   0.8986
   3.250   0.6663   0.02536   0.01849  -0.0544   0.5568   0.9042
   4.750   0.6636   0.03575   0.02938  -0.0425   0.5311   0.9481
   5.000   0.6891   0.03604   0.02968  -0.0426   0.5304   0.9522
   5.250   0.7190   0.03600   0.02966  -0.0430   0.5298   0.9541
   5.500   0.7498   0.03583   0.02950  -0.0435   0.5290   0.9561
   6.000   0.7671   0.03923   0.03300  -0.0443   0.5169   0.9737
   6.250   0.8010   0.03900   0.03281  -0.0453   0.5162   0.9800
   6.750   0.8178   0.04180   0.03569  -0.0450   0.5041   1.0000
   7.000   0.8488   0.04150   0.03542  -0.0454   0.5031   1.0000
   7.250   0.8806   0.04112   0.03508  -0.0459   0.5023   1.0000
   7.750   0.8955   0.04414   0.03820  -0.0452   0.4900   1.0000
   8.000   0.9271   0.04370   0.03781  -0.0456   0.4890   1.0000
   8.500   0.9520   0.04564   0.03986  -0.0450   0.4762   1.0000
   8.750   0.9864   0.04475   0.03904  -0.0454   0.4748   1.0000
   9.000   0.9796   0.04746   0.04180  -0.0445   0.4635   1.0000
   9.250   1.0092   0.04700   0.04141  -0.0447   0.4615   1.0000
   9.500   1.0087   0.04918   0.04366  -0.0440   0.4505   1.0000
   9.750   1.0371   0.04871   0.04327  -0.0442   0.4473   1.0000
  10.750   1.0939   0.05227   0.04708  -0.0431   0.4043   1.0000
  11.000   1.1242   0.05149   0.04633  -0.0432   0.3896   1.0000
  11.250   1.2064   0.04464   0.03909  -0.0439   0.3431   1.0000
  11.500   1.2198   0.04499   0.03906  -0.0428   0.3037   1.0000
  11.750   1.2208   0.04697   0.04083  -0.0418   0.2788   1.0000
  12.000   1.2201   0.04930   0.04303  -0.0409   0.2559   1.0000
  12.250   1.2199   0.05170   0.04530  -0.0402   0.2340   1.0000
  12.500   1.2196   0.05423   0.04771  -0.0397   0.2074   1.0000
  12.750   1.2177   0.05700   0.05033  -0.0392   0.1791   1.0000
  13.000   1.2145   0.05995   0.05309  -0.0387   0.1493   1.0000
  13.250   1.2124   0.06288   0.05585  -0.0384   0.1259   1.0000
  13.500   1.2131   0.06557   0.05844  -0.0381   0.1100   1.0000
  13.750   1.2160   0.06809   0.06089  -0.0380   0.0966   1.0000
  14.000   1.2192   0.07063   0.06339  -0.0380   0.0861   1.0000
  14.250   1.2244   0.07301   0.06578  -0.0380   0.0763   1.0000
  14.500   1.2300   0.07539   0.06815  -0.0381   0.0652   1.0000
  14.750   1.2338   0.07799   0.07074  -0.0382   0.0487   1.0000
  15.000   1.2332   0.08116   0.07379  -0.0384   0.0350   1.0000
  15.250   1.2353   0.08408   0.07669  -0.0387   0.0298   1.0000
  15.500   1.2376   0.08704   0.07968  -0.0390   0.0264   1.0000
  15.750   1.2386   0.09023   0.08291  -0.0394   0.0236   1.0000
  16.000   1.2436   0.09293   0.08573  -0.0398   0.0223   1.0000
  16.250   1.2469   0.09589   0.08881  -0.0403   0.0212   1.0000
  16.500   1.2499   0.09894   0.09196  -0.0409   0.0201   1.0000
  16.750   1.2518   0.10217   0.09530  -0.0416   0.0192   1.0000
  17.000   1.2521   0.10567   0.09887  -0.0424   0.0183   1.0000
  17.250   1.2503   0.10950   0.10280  -0.0434   0.0175   1.0000
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