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AS5046 (16%) (as5046-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: AS5046 (16%) (as5046-il)
Reynolds number: 200,000
Max Cl/Cd: 58.09 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-as5046-il-200000.txt
Download as CSV file: xf-as5046-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5046 (16%)                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.4471   0.09529   0.09208  -0.0488   1.0000   0.0717
 -11.750  -0.4853   0.08643   0.08316  -0.0539   1.0000   0.0717
 -11.500  -0.5170   0.07946   0.07614  -0.0569   1.0000   0.0717
 -11.250  -0.5470   0.07341   0.07002  -0.0588   1.0000   0.0716
 -11.000  -0.5751   0.06815   0.06469  -0.0597   1.0000   0.0715
 -10.750  -0.6670   0.07069   0.06700  -0.0551   1.0000   0.0649
 -10.500  -0.6836   0.06709   0.06335  -0.0553   1.0000   0.0657
 -10.250  -0.7023   0.06405   0.06024  -0.0545   1.0000   0.0665
 -10.000  -0.7212   0.06160   0.05772  -0.0522   1.0000   0.0677
  -9.750  -0.7474   0.06080   0.05641  -0.0508   0.9770   0.0716
  -9.500  -0.7288   0.05396   0.04954  -0.0546   0.9431   0.0753
  -9.250  -0.6986   0.05072   0.04615  -0.0584   0.9243   0.0803
  -9.000  -0.6843   0.04695   0.04202  -0.0610   0.9068   0.0885
  -8.750  -0.6626   0.03686   0.03022  -0.0578   0.8953   0.0416
  -8.500  -0.6336   0.03185   0.02459  -0.0573   0.8870   0.0327
  -8.250  -0.6081   0.03018   0.02225  -0.0566   0.8792   0.0302
  -8.000  -0.5785   0.02798   0.01994  -0.0568   0.8728   0.0299
  -7.750  -0.5498   0.02640   0.01819  -0.0567   0.8672   0.0300
  -7.500  -0.5223   0.02516   0.01681  -0.0565   0.8618   0.0302
  -7.250  -0.4947   0.02361   0.01533  -0.0563   0.8573   0.0311
  -7.000  -0.4705   0.02272   0.01448  -0.0560   0.8530   0.0330
  -6.750  -0.4466   0.02195   0.01365  -0.0554   0.8492   0.0346
  -6.500  -0.4243   0.02114   0.01281  -0.0547   0.8452   0.0357
  -6.250  -0.4055   0.02011   0.01181  -0.0538   0.8409   0.0371
  -6.000  -0.3868   0.01922   0.01093  -0.0531   0.8368   0.0393
  -5.750  -0.3656   0.01852   0.01016  -0.0526   0.8335   0.0426
  -5.500  -0.3453   0.01769   0.00931  -0.0523   0.8305   0.0491
  -5.250  -0.3246   0.01676   0.00844  -0.0519   0.8272   0.0654
  -5.000  -0.3264   0.01293   0.00716  -0.0506   0.8232   0.5103
  -4.750  -0.2995   0.01411   0.00850  -0.0490   0.8199   0.6071
  -4.500  -0.2716   0.01536   0.00970  -0.0476   0.8172   0.6327
  -4.250  -0.2445   0.01660   0.01091  -0.0460   0.8147   0.6506
  -4.000  -0.2193   0.01817   0.01254  -0.0432   0.8115   0.6674
  -3.750  -0.1938   0.01908   0.01346  -0.0411   0.8083   0.6752
  -3.500  -0.1666   0.01920   0.01349  -0.0410   0.8051   0.6833
  -3.250  -0.1400   0.01932   0.01351  -0.0406   0.8020   0.6890
  -3.000  -0.1135   0.01961   0.01374  -0.0397   0.7992   0.6932
  -2.750  -0.0853   0.01942   0.01343  -0.0410   0.7961   0.7026
  -2.500  -0.0602   0.01955   0.01356  -0.0399   0.7925   0.7053
  -2.250  -0.0343   0.01967   0.01365  -0.0393   0.7890   0.7089
  -2.000  -0.0069   0.01963   0.01354  -0.0395   0.7855   0.7143
  -1.750   0.0216   0.01948   0.01328  -0.0404   0.7825   0.7201
  -1.500   0.0465   0.01955   0.01336  -0.0397   0.7786   0.7228
  -1.250   0.0725   0.01956   0.01337  -0.0394   0.7743   0.7262
  -1.000   0.1003   0.01948   0.01323  -0.0398   0.7701   0.7307
  -0.750   0.1306   0.01932   0.01295  -0.0412   0.7663   0.7358
  -0.500   0.1551   0.01933   0.01299  -0.0405   0.7616   0.7380
  -0.250   0.1807   0.01932   0.01300  -0.0401   0.7562   0.7408
   0.000   0.2083   0.01927   0.01290  -0.0401   0.7515   0.7441
   0.250   0.2369   0.01922   0.01281  -0.0407   0.7467   0.7479
   0.500   0.2666   0.01910   0.01266  -0.0419   0.7404   0.7517
   0.750   0.2929   0.01898   0.01254  -0.0415   0.7354   0.7538
   1.000   0.3202   0.01896   0.01250  -0.0413   0.7309   0.7558
   1.250   0.3460   0.01892   0.01251  -0.0412   0.7240   0.7582
   1.500   0.3748   0.01879   0.01237  -0.0415   0.7185   0.7609
   1.750   0.4037   0.01871   0.01226  -0.0420   0.7124   0.7636
   2.000   0.4332   0.01851   0.01206  -0.0426   0.7044   0.7661
   2.250   0.4644   0.01824   0.01172  -0.0432   0.6983   0.7686
   2.500   0.4895   0.01804   0.01160  -0.0427   0.6888   0.7705
   2.750   0.5191   0.01777   0.01129  -0.0428   0.6830   0.7723
   3.000   0.5454   0.01762   0.01122  -0.0427   0.6738   0.7743
   3.250   0.5754   0.01733   0.01091  -0.0429   0.6672   0.7765
   3.500   0.6030   0.01715   0.01080  -0.0431   0.6578   0.7792
   3.750   0.6341   0.01682   0.01045  -0.0437   0.6505   0.7816
   4.000   0.6631   0.01658   0.01029  -0.0442   0.6398   0.7836
   4.250   0.6925   0.01619   0.00990  -0.0443   0.6309   0.7854
   4.500   0.7192   0.01585   0.00965  -0.0440   0.6189   0.7873
   4.750   0.7459   0.01555   0.00943  -0.0436   0.6049   0.7896
   5.000   0.7733   0.01525   0.00918  -0.0434   0.5885   0.7919
   5.250   0.8008   0.01499   0.00892  -0.0433   0.5685   0.7941
   5.500   0.8275   0.01484   0.00873  -0.0431   0.5412   0.7963
   5.750   0.8531   0.01484   0.00858  -0.0428   0.5070   0.7986
   6.000   0.8766   0.01509   0.00864  -0.0422   0.4672   0.8010
   6.250   0.8964   0.01545   0.00884  -0.0409   0.4292   0.8033
   6.500   0.9156   0.01595   0.00916  -0.0396   0.3934   0.8056
   6.750   0.9349   0.01650   0.00957  -0.0385   0.3600   0.8079
   7.000   0.9542   0.01708   0.01002  -0.0375   0.3294   0.8104
   7.250   0.9740   0.01767   0.01051  -0.0367   0.3023   0.8130
   7.500   0.9932   0.01833   0.01104  -0.0358   0.2793   0.8158
   7.750   1.0125   0.01888   0.01156  -0.0349   0.2590   0.8185
   8.000   1.0302   0.01945   0.01210  -0.0336   0.2419   0.8214
   8.250   1.0481   0.02005   0.01268  -0.0325   0.2269   0.8243
   8.500   1.0655   0.02071   0.01331  -0.0314   0.2134   0.8274
   8.750   1.0826   0.02141   0.01396  -0.0303   0.2007   0.8306
   9.000   1.1005   0.02203   0.01462  -0.0294   0.1884   0.8339
   9.250   1.1136   0.02265   0.01530  -0.0275   0.1776   0.8371
   9.500   1.1247   0.02345   0.01608  -0.0255   0.1678   0.8412
   9.750   1.1389   0.02422   0.01690  -0.0241   0.1573   0.8459
  10.000   1.1532   0.02509   0.01784  -0.0230   0.1472   0.8506
  10.250   1.1635   0.02611   0.01885  -0.0214   0.1384   0.8554
  10.500   1.1761   0.02705   0.01990  -0.0203   0.1293   0.8609
  10.750   1.1877   0.02822   0.02111  -0.0193   0.1210   0.8670
  11.000   1.1962   0.02942   0.02234  -0.0179   0.1138   0.8739
  11.500   1.2138   0.03193   0.02500  -0.0154   0.1010   0.8941
  11.750   1.2189   0.03310   0.02632  -0.0132   0.0959   0.9144
  12.000   1.2211   0.03416   0.02751  -0.0110   0.0915   1.0000
  12.250   1.2330   0.03593   0.02920  -0.0109   0.0865   1.0000
  12.500   1.2459   0.03753   0.03093  -0.0111   0.0820   1.0000
  12.750   1.2562   0.03926   0.03266  -0.0111   0.0781   1.0000
  13.000   1.2668   0.04104   0.03444  -0.0105   0.0745   1.0000
  13.250   1.2761   0.04284   0.03637  -0.0103   0.0713   1.0000
  13.500   1.2846   0.04465   0.03822  -0.0100   0.0683   1.0000
  13.750   1.2961   0.04640   0.03986  -0.0091   0.0652   1.0000
  14.000   1.3006   0.04857   0.04225  -0.0088   0.0632   1.0000
  14.250   1.3060   0.05070   0.04452  -0.0085   0.0609   1.0000
  14.500   1.3119   0.05275   0.04662  -0.0082   0.0588   1.0000
  14.750   1.3209   0.05464   0.04844  -0.0076   0.0566   1.0000
  15.000   1.3241   0.05718   0.05114  -0.0071   0.0549   1.0000
  15.250   1.3231   0.06000   0.05418  -0.0070   0.0535   1.0000
  15.500   1.3225   0.06284   0.05719  -0.0070   0.0520   1.0000
  15.750   1.3231   0.06559   0.06003  -0.0070   0.0506   1.0000
  16.000   1.3266   0.06804   0.06251  -0.0071   0.0492   1.0000
  16.250   1.3338   0.07050   0.06495  -0.0064   0.0475   1.0000
  16.500   1.3234   0.07462   0.06932  -0.0072   0.0469   1.0000
  16.750   1.3126   0.07906   0.07401  -0.0084   0.0461   1.0000
  17.000   1.3018   0.08377   0.07894  -0.0098   0.0454   1.0000
  17.250   1.2905   0.08875   0.08412  -0.0115   0.0446   1.0000
  17.500   1.2781   0.09405   0.08962  -0.0136   0.0439   1.0000
  17.750   1.2649   0.09969   0.09544  -0.0162   0.0433   1.0000
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