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WORTMANN FX 057-816 (fx057816-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 057-816 (fx057816-il)
Reynolds number: 500,000
Max Cl/Cd: 113.83 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx057816-il-500000.txt
Download as CSV file: xf-fx057816-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.5768   0.05402   0.05010  -0.0824   0.6068   0.0198
 -12.250  -0.6347   0.04547   0.04131  -0.0856   0.6066   0.0195
 -12.000  -0.6742   0.04022   0.03574  -0.0839   0.6063   0.0196
 -11.750  -0.7019   0.03659   0.03181  -0.0801   0.6059   0.0196
 -11.500  -0.7119   0.03435   0.02927  -0.0768   0.6054   0.0198
 -11.250  -0.7214   0.03109   0.02566  -0.0739   0.6049   0.0202
 -11.000  -0.7114   0.02963   0.02407  -0.0723   0.6043   0.0205
 -10.750  -0.6944   0.02891   0.02330  -0.0713   0.6037   0.0210
 -10.500  -0.6780   0.02791   0.02216  -0.0703   0.6030   0.0215
 -10.250  -0.6606   0.02689   0.02097  -0.0693   0.6024   0.0222
 -10.000  -0.6431   0.02569   0.01954  -0.0683   0.6017   0.0228
  -9.750  -0.6240   0.02468   0.01829  -0.0675   0.6010   0.0235
  -9.500  -0.6056   0.02334   0.01678  -0.0666   0.6004   0.0243
  -9.250  -0.5827   0.02282   0.01626  -0.0662   0.5999   0.0252
  -9.000  -0.5583   0.02252   0.01593  -0.0659   0.5993   0.0262
  -8.750  -0.5343   0.02195   0.01524  -0.0655   0.5986   0.0274
  -8.500  -0.5112   0.02107   0.01421  -0.0650   0.5978   0.0286
  -8.250  -0.4864   0.02076   0.01392  -0.0647   0.5970   0.0298
  -8.000  -0.4606   0.02058   0.01372  -0.0645   0.5962   0.0311
  -7.750  -0.4351   0.02016   0.01318  -0.0643   0.5955   0.0328
  -7.500  -0.4100   0.01976   0.01275  -0.0641   0.5948   0.0345
  -7.250  -0.3829   0.01996   0.01299  -0.0641   0.5940   0.0360
  -7.000  -0.3563   0.01988   0.01283  -0.0640   0.5933   0.0382
  -6.750  -0.3304   0.01952   0.01240  -0.0638   0.5926   0.0403
  -6.500  -0.3032   0.01972   0.01262  -0.0638   0.5919   0.0418
  -6.250  -0.2761   0.01979   0.01265  -0.0638   0.5912   0.0441
  -6.000  -0.2495   0.01957   0.01230  -0.0637   0.5906   0.0466
  -5.750  -0.2226   0.01957   0.01234  -0.0638   0.5899   0.0483
  -5.500  -0.1954   0.01963   0.01238  -0.0638   0.5893   0.0504
  -5.250  -0.1680   0.01962   0.01228  -0.0638   0.5886   0.0529
  -5.000  -0.1413   0.01916   0.01174  -0.0638   0.5879   0.0554
  -4.750  -0.1143   0.01899   0.01159  -0.0639   0.5873   0.0573
  -4.500  -0.0871   0.01896   0.01153  -0.0639   0.5867   0.0596
  -4.250  -0.0598   0.01893   0.01145  -0.0639   0.5861   0.0620
  -4.000  -0.0324   0.01918   0.01162  -0.0640   0.5855   0.0637
  -3.750  -0.0070   0.01847   0.01094  -0.0639   0.5847   0.0663
  -3.500   0.0200   0.01824   0.01076  -0.0640   0.5842   0.0685
  -3.250   0.0471   0.01806   0.01061  -0.0640   0.5836   0.0704
  -3.000   0.0742   0.01793   0.01049  -0.0641   0.5829   0.0725
  -2.750   0.1013   0.01787   0.01044  -0.0641   0.5821   0.0741
  -2.500   0.1283   0.01784   0.01042  -0.0642   0.5812   0.0752
  -2.250   0.1540   0.01747   0.01007  -0.0641   0.5801   0.0769
  -2.000   0.1799   0.01720   0.00985  -0.0640   0.5791   0.0793
  -1.750   0.2066   0.01711   0.00979  -0.0641   0.5782   0.0811
  -1.500   0.2334   0.01708   0.00977  -0.0642   0.5774   0.0830
  -1.250   0.2605   0.01707   0.00977  -0.0643   0.5766   0.0849
  -1.000   0.2877   0.01709   0.00980  -0.0644   0.5759   0.0871
  -0.750   0.3152   0.01713   0.00983  -0.0646   0.5752   0.0886
  -0.500   0.3423   0.01705   0.00976  -0.0647   0.5746   0.0917
  -0.250   0.3698   0.01703   0.00977  -0.0649   0.5740   0.0953
   0.000   0.3976   0.01707   0.00981  -0.0651   0.5735   0.0991
   0.250   0.4254   0.01712   0.00986  -0.0653   0.5729   0.1037
   0.500   0.4532   0.01709   0.00988  -0.0656   0.5722   0.1186
   0.750   0.4733   0.01521   0.01004  -0.0656   0.5717   0.7510
   1.000   0.4989   0.01556   0.01047  -0.0649   0.5711   0.8087
   1.250   0.5241   0.01596   0.01089  -0.0642   0.5706   0.8281
   1.500   0.5481   0.01643   0.01137  -0.0633   0.5700   0.8428
   1.750   0.5719   0.01706   0.01201  -0.0627   0.5692   0.8536
   2.000   0.5913   0.01767   0.01278  -0.0616   0.5674   0.8611
   2.250   0.6131   0.01848   0.01367  -0.0613   0.5651   0.8683
   2.500   0.6330   0.01895   0.01423  -0.0601   0.5631   0.8738
   2.750   0.6550   0.01945   0.01477  -0.0594   0.5618   0.8813
   3.000   0.6773   0.01981   0.01518  -0.0586   0.5607   0.8869
   3.250   0.6981   0.02014   0.01554  -0.0574   0.5598   0.8935
   3.500   0.7239   0.02040   0.01580  -0.0573   0.5590   0.8990
   3.750   0.7507   0.02024   0.01566  -0.0570   0.5583   0.9018
   4.000   0.7776   0.01998   0.01539  -0.0565   0.5576   0.9056
   4.250   0.8049   0.01975   0.01514  -0.0560   0.5570   0.9109
   4.500   0.8346   0.01964   0.01503  -0.0564   0.5564   0.9141
   4.750   0.8656   0.01948   0.01485  -0.0571   0.5557   0.9152
   5.000   0.8955   0.01940   0.01477  -0.0577   0.5551   0.9159
   5.250   0.9169   0.01997   0.01542  -0.0573   0.5530   0.9174
   5.500   0.9247   0.02143   0.01709  -0.0559   0.5468   0.9197
   5.750   0.9598   0.02072   0.01636  -0.0569   0.5459   0.9202
   6.000   0.9923   0.02032   0.01597  -0.0576   0.5450   0.9210
   6.250   1.0284   0.01953   0.01517  -0.0587   0.5442   0.9216
   6.500   1.0653   0.01863   0.01423  -0.0598   0.5431   0.9222
   6.750   1.0991   0.01809   0.01370  -0.0608   0.5423   0.9230
   7.000   1.1324   0.01765   0.01326  -0.0617   0.5415   0.9238
   7.250   1.1672   0.01706   0.01265  -0.0628   0.5405   0.9246
   7.500   1.1957   0.01694   0.01260  -0.0632   0.5383   0.9259
   7.750   1.2190   0.01694   0.01275  -0.0630   0.5336   0.9277
   8.000   1.2583   0.01551   0.01128  -0.0644   0.5297   0.9286
   8.250   1.2973   0.01428   0.00998  -0.0658   0.5264   0.9293
   8.500   1.3225   0.01407   0.00991  -0.0657   0.5209   0.9309
   8.750   1.3529   0.01333   0.00921  -0.0661   0.5137   0.9323
   9.000   1.3785   0.01307   0.00907  -0.0659   0.5038   0.9341
   9.250   1.4052   0.01274   0.00879  -0.0659   0.4877   0.9360
   9.500   1.4274   0.01254   0.00845  -0.0652   0.4489   0.9386
   9.750   1.4122   0.01421   0.00970  -0.0596   0.3758   0.9450
  10.000   1.3759   0.01633   0.01177  -0.0514   0.3469   0.9605
  10.250   1.3400   0.02236   0.01781  -0.0512   0.3228   1.0000
  10.500   1.3099   0.02673   0.02210  -0.0487   0.3037   1.0000
  10.750   1.2848   0.03052   0.02577  -0.0462   0.2839   1.0000
  11.000   1.2682   0.03369   0.02885  -0.0442   0.2658   1.0000
  11.250   1.2591   0.03638   0.03145  -0.0426   0.2488   1.0000
  11.500   1.2530   0.03906   0.03404  -0.0414   0.2303   1.0000
  11.750   1.2516   0.04145   0.03633  -0.0405   0.2085   1.0000
  12.000   1.2448   0.04438   0.03909  -0.0395   0.1785   1.0000
  12.250   1.2363   0.04749   0.04196  -0.0385   0.1437   1.0000
  12.500   1.2317   0.05032   0.04458  -0.0376   0.1160   1.0000
  12.750   1.2338   0.05262   0.04680  -0.0371   0.1013   1.0000
  13.000   1.2383   0.05473   0.04885  -0.0367   0.0902   1.0000
  13.250   1.2460   0.05659   0.05069  -0.0365   0.0816   1.0000
  13.500   1.2536   0.05848   0.05255  -0.0363   0.0724   1.0000
  13.750   1.2589   0.06064   0.05467  -0.0361   0.0606   1.0000
  14.000   1.2614   0.06312   0.05701  -0.0359   0.0442   1.0000
  14.250   1.2640   0.06562   0.05942  -0.0357   0.0345   1.0000
  14.500   1.2686   0.06801   0.06181  -0.0356   0.0304   1.0000
  14.750   1.2714   0.07065   0.06445  -0.0356   0.0275   1.0000
  15.000   1.2779   0.07291   0.06677  -0.0356   0.0260   1.0000
  15.250   1.2837   0.07528   0.06919  -0.0358   0.0243   1.0000
  15.500   1.2864   0.07809   0.07204  -0.0360   0.0232   1.0000
  15.750   1.2869   0.08119   0.07517  -0.0362   0.0223   1.0000
  16.000   1.2930   0.08365   0.07772  -0.0365   0.0216   1.0000
  16.250   1.2979   0.08631   0.08045  -0.0369   0.0209   1.0000
  16.500   1.3025   0.08902   0.08323  -0.0373   0.0201   1.0000
  16.750   1.3051   0.09204   0.08630  -0.0379   0.0194   1.0000
  17.000   1.3037   0.09557   0.08987  -0.0385   0.0187   1.0000
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