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WORTMANN FX 057-816 (fx057816-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 057-816 (fx057816-il)
Reynolds number: 1,000,000
Max Cl/Cd: 155.81 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx057816-il-1000000.txt
Download as CSV file: xf-fx057816-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.8643   0.04544   0.04152  -0.0879   0.5915   0.0119
 -15.000  -0.8898   0.04041   0.03632  -0.0896   0.5911   0.0119
 -14.750  -0.9058   0.03707   0.03282  -0.0892   0.5906   0.0119
 -14.500  -0.9144   0.03463   0.03025  -0.0879   0.5901   0.0120
 -14.250  -0.9157   0.03286   0.02837  -0.0865   0.5895   0.0122
 -14.000  -0.9163   0.03123   0.02661  -0.0847   0.5889   0.0124
 -13.750  -0.9164   0.02969   0.02495  -0.0826   0.5882   0.0125
 -13.500  -0.9132   0.02843   0.02357  -0.0804   0.5875   0.0127
 -13.250  -0.9096   0.02733   0.02235  -0.0778   0.5868   0.0128
 -13.000  -0.9056   0.02637   0.02126  -0.0751   0.5858   0.0130
 -12.750  -0.8934   0.02550   0.02027  -0.0735   0.5848   0.0131
 -12.500  -0.8772   0.02473   0.01940  -0.0722   0.5845   0.0132
 -12.250  -0.8677   0.02332   0.01782  -0.0704   0.5842   0.0135
 -12.000  -0.8545   0.02214   0.01654  -0.0689   0.5837   0.0139
 -11.750  -0.8363   0.02133   0.01565  -0.0678   0.5832   0.0142
 -11.500  -0.8158   0.02068   0.01494  -0.0671   0.5826   0.0146
 -11.250  -0.7944   0.02007   0.01426  -0.0664   0.5821   0.0150
 -11.000  -0.7726   0.01947   0.01357  -0.0657   0.5815   0.0153
 -10.750  -0.7493   0.01898   0.01301  -0.0652   0.5809   0.0158
 -10.500  -0.7257   0.01850   0.01244  -0.0648   0.5803   0.0162
 -10.250  -0.7042   0.01774   0.01159  -0.0641   0.5797   0.0167
 -10.000  -0.6817   0.01707   0.01086  -0.0635   0.5791   0.0174
  -9.750  -0.6574   0.01661   0.01035  -0.0631   0.5784   0.0180
  -9.500  -0.6324   0.01620   0.00989  -0.0628   0.5778   0.0187
  -9.250  -0.6073   0.01579   0.00942  -0.0625   0.5772   0.0194
  -9.000  -0.5820   0.01539   0.00894  -0.0622   0.5766   0.0200
  -8.750  -0.5576   0.01485   0.00837  -0.0618   0.5760   0.0212
  -8.500  -0.5317   0.01451   0.00800  -0.0616   0.5754   0.0222
  -8.250  -0.5053   0.01423   0.00767  -0.0615   0.5749   0.0233
  -8.000  -0.4796   0.01384   0.00725  -0.0612   0.5743   0.0249
  -7.750  -0.4530   0.01357   0.00698  -0.0611   0.5737   0.0266
  -7.500  -0.4260   0.01337   0.00671  -0.0610   0.5730   0.0281
  -7.250  -0.3994   0.01309   0.00646  -0.0609   0.5723   0.0307
  -7.000  -0.3718   0.01298   0.00631  -0.0610   0.5716   0.0328
  -6.750  -0.3445   0.01285   0.00619  -0.0610   0.5709   0.0354
  -6.500  -0.3163   0.01292   0.00626  -0.0611   0.5699   0.0378
  -6.250  -0.2885   0.01290   0.00624  -0.0612   0.5692   0.0399
  -6.000  -0.2600   0.01287   0.00624  -0.0613   0.5689   0.0420
  -5.750  -0.2311   0.01290   0.00627  -0.0616   0.5686   0.0439
  -5.500  -0.2022   0.01292   0.00627  -0.0618   0.5683   0.0454
  -5.250  -0.1746   0.01273   0.00606  -0.0618   0.5679   0.0473
  -5.000  -0.1461   0.01269   0.00605  -0.0620   0.5675   0.0489
  -4.750  -0.1174   0.01269   0.00606  -0.0622   0.5670   0.0504
  -4.500  -0.0887   0.01270   0.00606  -0.0625   0.5665   0.0520
  -4.250  -0.0601   0.01267   0.00602  -0.0627   0.5660   0.0533
  -4.000  -0.0311   0.01273   0.00606  -0.0629   0.5654   0.0541
  -3.750  -0.0049   0.01221   0.00555  -0.0628   0.5648   0.0565
  -3.500   0.0235   0.01213   0.00549  -0.0630   0.5642   0.0581
  -3.250   0.0519   0.01205   0.00541  -0.0632   0.5635   0.0596
  -3.000   0.0802   0.01195   0.00531  -0.0634   0.5629   0.0610
  -2.750   0.1086   0.01186   0.00522  -0.0636   0.5624   0.0624
  -2.500   0.1371   0.01177   0.00513  -0.0638   0.5618   0.0633
  -2.250   0.1657   0.01172   0.00506  -0.0641   0.5613   0.0639
  -2.000   0.1928   0.01135   0.00469  -0.0642   0.5608   0.0662
  -1.750   0.2210   0.01121   0.00454  -0.0644   0.5602   0.0679
  -1.500   0.2496   0.01111   0.00445  -0.0647   0.5598   0.0694
  -1.250   0.2782   0.01103   0.00438  -0.0649   0.5593   0.0709
  -1.000   0.3070   0.01097   0.00431  -0.0652   0.5588   0.0725
  -0.750   0.3358   0.01093   0.00427  -0.0656   0.5583   0.0741
  -0.500   0.3647   0.01090   0.00424  -0.0659   0.5578   0.0752
  -0.250   0.3934   0.01082   0.00415  -0.0662   0.5572   0.0771
   0.000   0.4222   0.01076   0.00409  -0.0665   0.5566   0.0803
   0.250   0.4510   0.01076   0.00410  -0.0669   0.5560   0.0833
   0.500   0.4796   0.01083   0.00418  -0.0672   0.5552   0.0863
   0.750   0.5076   0.01105   0.00443  -0.0675   0.5542   0.0902
   1.000   0.5365   0.01099   0.00444  -0.0679   0.5539   0.1032
   1.250   0.5626   0.00928   0.00435  -0.0692   0.5536   0.6667
   1.500   0.5898   0.00924   0.00466  -0.0691   0.5532   0.7945
   1.750   0.6185   0.00938   0.00483  -0.0693   0.5528   0.8090
   2.000   0.6473   0.00954   0.00500  -0.0696   0.5523   0.8193
   2.250   0.6752   0.00966   0.00517  -0.0696   0.5518   0.8268
   2.500   0.7038   0.00978   0.00531  -0.0698   0.5510   0.8332
   2.750   0.7324   0.00984   0.00539  -0.0700   0.5501   0.8385
   3.000   0.7607   0.00984   0.00543  -0.0701   0.5489   0.8424
   3.250   0.7893   0.00987   0.00548  -0.0704   0.5478   0.8464
   3.500   0.8181   0.00993   0.00556  -0.0707   0.5469   0.8505
   3.750   0.8464   0.00997   0.00562  -0.0709   0.5461   0.8550
   4.000   0.8742   0.00999   0.00567  -0.0709   0.5452   0.8589
   4.250   0.9035   0.00990   0.00558  -0.0713   0.5439   0.8616
   4.500   0.9333   0.00981   0.00548  -0.0717   0.5426   0.8638
   4.750   0.9625   0.00987   0.00553  -0.0722   0.5417   0.8666
   5.000   0.9919   0.00996   0.00561  -0.0727   0.5403   0.8675
   5.250   1.0209   0.00990   0.00560  -0.0732   0.5383   0.8681
   5.500   1.0500   0.00978   0.00553  -0.0737   0.5367   0.8691
   5.750   1.0790   0.00976   0.00555  -0.0742   0.5353   0.8699
   6.000   1.1079   0.00974   0.00558  -0.0747   0.5340   0.8707
   6.250   1.1371   0.00968   0.00555  -0.0752   0.5324   0.8714
   6.500   1.1668   0.00953   0.00542  -0.0757   0.5303   0.8722
   6.750   1.1965   0.00935   0.00524  -0.0763   0.5279   0.8729
   7.000   1.2255   0.00922   0.00513  -0.0767   0.5241   0.8737
   7.250   1.2542   0.00908   0.00508  -0.0771   0.5199   0.8746
   7.500   1.2835   0.00890   0.00492  -0.0776   0.5146   0.8755
   7.750   1.3121   0.00884   0.00489  -0.0780   0.5094   0.8764
   8.000   1.3406   0.00878   0.00489  -0.0785   0.5003   0.8774
   8.250   1.3680   0.00878   0.00487  -0.0787   0.4836   0.8786
   8.500   1.3859   0.00945   0.00528  -0.0776   0.4258   0.8801
   8.750   1.3689   0.01240   0.00761  -0.0721   0.3097   0.8825
   9.000   1.3650   0.01408   0.00910  -0.0683   0.2690   0.8844
   9.250   1.3576   0.01545   0.01043  -0.0640   0.2491   0.8875
   9.500   1.3348   0.01837   0.01344  -0.0598   0.2400   0.8919
   9.750   1.3119   0.02200   0.01712  -0.0568   0.2320   0.8963
  10.000   1.2921   0.02494   0.02005  -0.0533   0.2207   0.9007
  10.250   1.2766   0.02752   0.02263  -0.0502   0.2089   0.9054
  10.500   1.2616   0.03013   0.02520  -0.0474   0.1918   0.9102
  10.750   1.2457   0.03293   0.02791  -0.0447   0.1712   0.9153
  11.000   1.2316   0.03559   0.03045  -0.0422   0.1440   0.9223
  11.250   1.2196   0.03840   0.03313  -0.0401   0.1165   0.9316
  11.500   1.2210   0.04033   0.03504  -0.0390   0.1002   0.9506
  11.750   1.2331   0.04226   0.03694  -0.0401   0.0872   1.0000
  12.000   1.2400   0.04406   0.03869  -0.0396   0.0796   1.0000
  12.250   1.2506   0.04554   0.04018  -0.0394   0.0741   1.0000
  12.500   1.2589   0.04721   0.04181  -0.0390   0.0668   1.0000
  12.750   1.2688   0.04876   0.04333  -0.0387   0.0589   1.0000
  13.000   1.2742   0.05073   0.04520  -0.0383   0.0456   1.0000
  13.250   1.2751   0.05316   0.04751  -0.0378   0.0309   1.0000
  13.500   1.2811   0.05516   0.04947  -0.0375   0.0252   1.0000
  13.750   1.2883   0.05707   0.05137  -0.0372   0.0223   1.0000
  14.000   1.2982   0.05877   0.05310  -0.0371   0.0207   1.0000
  14.250   1.3052   0.06080   0.05514  -0.0370   0.0194   1.0000
  14.500   1.3119   0.06287   0.05725  -0.0369   0.0182   1.0000
  14.750   1.3222   0.06460   0.05902  -0.0369   0.0175   1.0000
  15.000   1.3319   0.06639   0.06085  -0.0370   0.0166   1.0000
  15.250   1.3385   0.06858   0.06307  -0.0370   0.0159   1.0000
  15.500   1.3430   0.07102   0.06555  -0.0371   0.0151   1.0000
  15.750   1.3495   0.07326   0.06784  -0.0372   0.0147   1.0000
  16.000   1.3585   0.07527   0.06991  -0.0374   0.0143   1.0000
  16.250   1.3658   0.07751   0.07220  -0.0377   0.0138   1.0000
  16.500   1.3730   0.07975   0.07449  -0.0380   0.0134   1.0000
  16.750   1.3797   0.08207   0.07686  -0.0383   0.0130   1.0000
  17.000   1.3826   0.08495   0.07978  -0.0388   0.0125   1.0000
  17.250   1.3843   0.08802   0.08291  -0.0393   0.0121   1.0000
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