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AS5046 (16%) (as5046-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: AS5046 (16%) (as5046-il)
Reynolds number: 500,000
Max Cl/Cd: 77.7 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-as5046-il-500000.txt
Download as CSV file: xf-as5046-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.3638   0.14905   0.14686  -0.0203   1.0000   0.0190
 -15.500  -0.3635   0.14624   0.14406  -0.0216   1.0000   0.0196
 -15.250  -0.5521   0.16094   0.15849  -0.0057   1.0000   0.0178
 -12.750  -0.4559   0.08608   0.08334  -0.0541   0.8196   0.0237
 -12.500  -0.5002   0.07479   0.07191  -0.0600   0.8176   0.0230
 -12.250  -0.5428   0.06570   0.06264  -0.0638   0.8142   0.0225
 -12.000  -0.5746   0.05908   0.05585  -0.0657   0.8096   0.0224
 -11.750  -0.6013   0.05366   0.05026  -0.0665   0.8047   0.0224
 -11.500  -0.6239   0.04911   0.04552  -0.0667   0.8001   0.0224
 -11.250  -0.6420   0.04530   0.04156  -0.0664   0.7960   0.0225
 -11.000  -0.6580   0.04190   0.03801  -0.0658   0.7918   0.0226
 -10.750  -0.6712   0.03899   0.03493  -0.0648   0.7876   0.0229
 -10.500  -0.6825   0.03640   0.03214  -0.0635   0.7837   0.0234
  -9.500  -0.7440   0.03188   0.02552  -0.0521   0.7761   0.0176
  -9.250  -0.7169   0.02951   0.02318  -0.0521   0.7735   0.0162
  -9.000  -0.6954   0.02731   0.02076  -0.0515   0.7710   0.0157
  -8.750  -0.6724   0.02555   0.01879  -0.0510   0.7685   0.0156
  -8.500  -0.6474   0.02370   0.01672  -0.0504   0.7661   0.0151
  -8.250  -0.6227   0.02224   0.01510  -0.0497   0.7638   0.0148
  -8.000  -0.5991   0.02120   0.01402  -0.0492   0.7615   0.0149
  -7.750  -0.5764   0.02030   0.01308  -0.0486   0.7593   0.0151
  -7.500  -0.5543   0.01948   0.01224  -0.0481   0.7571   0.0154
  -7.250  -0.5325   0.01871   0.01143  -0.0475   0.7550   0.0158
  -7.000  -0.5106   0.01800   0.01067  -0.0470   0.7530   0.0162
  -6.750  -0.4883   0.01734   0.00995  -0.0466   0.7510   0.0167
  -6.500  -0.4649   0.01683   0.00937  -0.0463   0.7488   0.0172
  -6.250  -0.4445   0.01588   0.00841  -0.0459   0.7469   0.0180
  -6.000  -0.4206   0.01529   0.00783  -0.0458   0.7450   0.0189
  -5.750  -0.3953   0.01484   0.00735  -0.0458   0.7431   0.0203
  -5.500  -0.3706   0.01426   0.00676  -0.0458   0.7412   0.0223
  -5.250  -0.3443   0.01386   0.00633  -0.0459   0.7393   0.0249
  -5.000  -0.3183   0.01337   0.00582  -0.0460   0.7373   0.0297
  -4.750  -0.2936   0.01255   0.00519  -0.0461   0.7353   0.0693
  -4.500  -0.2757   0.00987   0.00396  -0.0473   0.7334   0.3932
  -4.250  -0.2489   0.00911   0.00391  -0.0480   0.7317   0.5618
  -4.000  -0.2192   0.00928   0.00412  -0.0482   0.7299   0.5978
  -3.750  -0.1895   0.00953   0.00435  -0.0484   0.7277   0.6163
  -3.500  -0.1602   0.00988   0.00471  -0.0484   0.7256   0.6298
  -3.250  -0.1310   0.01020   0.00501  -0.0484   0.7233   0.6403
  -3.000  -0.1018   0.01045   0.00524  -0.0484   0.7211   0.6469
  -2.750  -0.0715   0.01061   0.00528  -0.0489   0.7189   0.6526
  -2.500  -0.0427   0.01068   0.00534  -0.0490   0.7168   0.6558
  -2.250  -0.0136   0.01081   0.00546  -0.0492   0.7146   0.6589
  -2.000   0.0158   0.01085   0.00550  -0.0495   0.7120   0.6622
  -1.750   0.0454   0.01087   0.00549  -0.0499   0.7091   0.6657
  -1.500   0.0754   0.01089   0.00545  -0.0505   0.7060   0.6688
  -1.250   0.1047   0.01083   0.00535  -0.0508   0.7029   0.6711
  -1.000   0.1339   0.01086   0.00535  -0.0510   0.6998   0.6731
  -0.750   0.1629   0.01086   0.00536  -0.0513   0.6964   0.6751
  -0.500   0.1921   0.01084   0.00535  -0.0515   0.6926   0.6775
  -0.250   0.2216   0.01083   0.00532  -0.0519   0.6891   0.6802
   0.000   0.2514   0.01083   0.00527  -0.0523   0.6859   0.6828
   0.250   0.2815   0.01086   0.00524  -0.0529   0.6829   0.6848
   0.500   0.3111   0.01081   0.00519  -0.0534   0.6792   0.6865
   0.750   0.3400   0.01068   0.00510  -0.0536   0.6746   0.6881
   1.000   0.3691   0.01056   0.00497  -0.0538   0.6694   0.6896
   1.250   0.3983   0.01051   0.00489  -0.0541   0.6643   0.6910
   1.500   0.4272   0.01040   0.00483  -0.0543   0.6584   0.6927
   1.750   0.4565   0.01032   0.00475  -0.0546   0.6533   0.6944
   2.000   0.4861   0.01028   0.00467  -0.0550   0.6487   0.6962
   2.250   0.5152   0.01019   0.00464  -0.0553   0.6425   0.6978
   2.500   0.5446   0.01011   0.00456  -0.0557   0.6367   0.6995
   2.750   0.5740   0.01005   0.00450  -0.0560   0.6305   0.7012
   3.000   0.6033   0.00998   0.00446  -0.0563   0.6218   0.7027
   3.250   0.6320   0.00985   0.00435  -0.0565   0.6139   0.7041
   3.500   0.6605   0.00976   0.00430  -0.0567   0.6031   0.7054
   3.750   0.6889   0.00970   0.00427  -0.0568   0.5894   0.7068
   4.000   0.7168   0.00969   0.00424  -0.0568   0.5725   0.7083
   4.250   0.7440   0.00974   0.00426  -0.0568   0.5493   0.7100
   4.500   0.7698   0.00991   0.00430  -0.0565   0.5160   0.7117
   4.750   0.7941   0.01022   0.00444  -0.0559   0.4763   0.7134
   5.000   0.8183   0.01059   0.00465  -0.0555   0.4388   0.7150
   5.250   0.8426   0.01097   0.00489  -0.0551   0.4050   0.7165
   5.500   0.8666   0.01139   0.00516  -0.0547   0.3720   0.7180
   5.750   0.8904   0.01179   0.00543  -0.0542   0.3415   0.7196
   6.000   0.9137   0.01218   0.00571  -0.0537   0.3127   0.7213
   6.250   0.9369   0.01258   0.00602  -0.0531   0.2841   0.7228
   6.500   0.9599   0.01301   0.00636  -0.0526   0.2592   0.7244
   6.750   0.9832   0.01341   0.00669  -0.0521   0.2380   0.7260
   7.000   1.0062   0.01383   0.00703  -0.0515   0.2198   0.7277
   7.250   1.0294   0.01423   0.00739  -0.0510   0.2044   0.7294
   7.500   1.0526   0.01462   0.00775  -0.0505   0.1914   0.7314
   7.750   1.0755   0.01504   0.00813  -0.0500   0.1796   0.7333
   8.000   1.0976   0.01550   0.00854  -0.0493   0.1686   0.7351
   8.250   1.1201   0.01584   0.00891  -0.0487   0.1584   0.7369
   8.500   1.1420   0.01622   0.00931  -0.0480   0.1488   0.7387
   8.750   1.1623   0.01671   0.00977  -0.0471   0.1390   0.7406
   9.000   1.1833   0.01713   0.01021  -0.0463   0.1294   0.7425
   9.250   1.2034   0.01759   0.01068  -0.0454   0.1202   0.7446
   9.500   1.2214   0.01816   0.01122  -0.0442   0.1108   0.7468
   9.750   1.2388   0.01872   0.01177  -0.0429   0.1018   0.7490
  10.000   1.2527   0.01928   0.01235  -0.0410   0.0944   0.7512
  10.250   1.2649   0.02001   0.01307  -0.0390   0.0869   0.7538
  10.500   1.2802   0.02067   0.01378  -0.0376   0.0806   0.7564
  10.750   1.2921   0.02159   0.01471  -0.0359   0.0747   0.7589
  11.000   1.3058   0.02243   0.01560  -0.0346   0.0699   0.7617
  11.250   1.3144   0.02369   0.01687  -0.0331   0.0652   0.7645
  11.500   1.3293   0.02460   0.01786  -0.0323   0.0617   0.7673
  11.750   1.3400   0.02587   0.01916  -0.0314   0.0582   0.7703
  12.000   1.3485   0.02738   0.02075  -0.0305   0.0551   0.7735
  12.250   1.3617   0.02856   0.02203  -0.0299   0.0526   0.7771
  12.500   1.3717   0.03003   0.02354  -0.0293   0.0500   0.7809
  12.750   1.3747   0.03212   0.02566  -0.0284   0.0475   0.7847
  13.000   1.3869   0.03339   0.02708  -0.0279   0.0458   0.7891
  13.250   1.3963   0.03492   0.02871  -0.0273   0.0440   0.7945
  13.500   1.4026   0.03674   0.03059  -0.0267   0.0423   0.8005
  13.750   1.4015   0.03920   0.03313  -0.0257   0.0405   0.8074
  14.000   1.4082   0.04099   0.03506  -0.0252   0.0393   0.8163
  14.250   1.4146   0.04279   0.03704  -0.0246   0.0380   0.8287
  14.500   1.4189   0.04473   0.03914  -0.0240   0.0368   0.8506
  14.750   1.4093   0.04626   0.04095  -0.0205   0.0361   1.0000
  15.000   1.4085   0.04897   0.04369  -0.0202   0.0350   1.0000
  15.250   1.4009   0.05242   0.04720  -0.0199   0.0339   1.0000
  15.500   1.4064   0.05472   0.04961  -0.0200   0.0331   1.0000
  15.750   1.4093   0.05733   0.05232  -0.0201   0.0322   1.0000
  16.000   1.4106   0.06022   0.05530  -0.0204   0.0313   1.0000
  16.250   1.4107   0.06332   0.05848  -0.0209   0.0305   1.0000
  16.500   1.4088   0.06676   0.06199  -0.0216   0.0297   1.0000
  16.750   1.4028   0.07074   0.06604  -0.0223   0.0290   1.0000
  17.000   1.3929   0.07520   0.07056  -0.0231   0.0283   1.0000
  17.250   1.3922   0.07882   0.07432  -0.0242   0.0278   1.0000
  17.500   1.3896   0.08272   0.07834  -0.0254   0.0272   1.0000
  17.750   1.3849   0.08692   0.08266  -0.0267   0.0266   1.0000
  18.000   1.3797   0.09128   0.08712  -0.0283   0.0261   1.0000
  18.250   1.3736   0.09582   0.09175  -0.0299   0.0256   1.0000
  18.500   1.3669   0.10052   0.09654  -0.0318   0.0251   1.0000
  18.750   1.3593   0.10537   0.10147  -0.0337   0.0247   1.0000
  19.000   1.3507   0.11030   0.10646  -0.0357   0.0242   1.0000
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