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HSNLF(1)-0213 AIRFOIL (hsnlf213-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HSNLF(1)-0213 AIRFOIL (hsnlf213-il)
Reynolds number: 1,000,000
Max Cl/Cd: 67.4 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hsnlf213-il-1000000-n5.txt
Download as CSV file: xf-hsnlf213-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HSNLF(1)-0213 AIRFOIL                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.2261   0.06246   0.05928  -0.0242   0.7854   0.0044
 -16.500  -1.2482   0.05602   0.05265  -0.0270   0.7831   0.0044
 -16.250  -1.2626   0.05138   0.04784  -0.0282   0.7805   0.0045
 -16.000  -1.2716   0.04773   0.04404  -0.0284   0.7779   0.0045
 -15.750  -1.2772   0.04469   0.04086  -0.0281   0.7753   0.0046
 -15.500  -1.2799   0.04205   0.03808  -0.0275   0.7728   0.0046
 -15.250  -1.2802   0.03973   0.03564  -0.0267   0.7706   0.0047
 -15.000  -1.2784   0.03764   0.03342  -0.0258   0.7682   0.0048
 -14.750  -1.2746   0.03577   0.03142  -0.0248   0.7659   0.0049
 -14.500  -1.2696   0.03402   0.02955  -0.0238   0.7637   0.0050
 -14.250  -1.2626   0.03248   0.02787  -0.0227   0.7616   0.0051
 -14.000  -1.2549   0.03100   0.02627  -0.0216   0.7596   0.0051
 -13.750  -1.2453   0.02969   0.02484  -0.0204   0.7578   0.0053
 -13.500  -1.2352   0.02843   0.02345  -0.0192   0.7563   0.0053
 -13.250  -1.2233   0.02730   0.02222  -0.0180   0.7546   0.0054
 -13.000  -1.2100   0.02628   0.02109  -0.0168   0.7529   0.0055
 -12.750  -1.1961   0.02535   0.02005  -0.0155   0.7512   0.0056
 -12.500  -1.1814   0.02456   0.01916  -0.0141   0.7496   0.0057
 -12.250  -1.1643   0.02367   0.01816  -0.0132   0.7480   0.0058
 -12.000  -1.1472   0.02270   0.01708  -0.0122   0.7464   0.0059
 -11.750  -1.1278   0.02192   0.01621  -0.0115   0.7448   0.0061
 -11.500  -1.1071   0.02125   0.01547  -0.0109   0.7432   0.0063
 -11.250  -1.0855   0.02062   0.01478  -0.0103   0.7419   0.0064
 -11.000  -1.0634   0.02003   0.01413  -0.0099   0.7407   0.0066
 -10.750  -1.0408   0.01945   0.01349  -0.0095   0.7395   0.0068
 -10.500  -1.0179   0.01889   0.01287  -0.0091   0.7382   0.0070
 -10.250  -0.9946   0.01834   0.01225  -0.0087   0.7369   0.0071
 -10.000  -0.9710   0.01782   0.01166  -0.0084   0.7356   0.0073
  -9.750  -0.9471   0.01731   0.01109  -0.0081   0.7344   0.0075
  -9.500  -0.9227   0.01684   0.01055  -0.0078   0.7331   0.0077
  -9.250  -0.8981   0.01639   0.01004  -0.0076   0.7319   0.0078
  -9.000  -0.8739   0.01586   0.00944  -0.0073   0.7307   0.0081
  -8.750  -0.8493   0.01536   0.00890  -0.0070   0.7295   0.0084
  -8.500  -0.8241   0.01496   0.00845  -0.0069   0.7281   0.0086
  -8.250  -0.7985   0.01458   0.00805  -0.0067   0.7269   0.0089
  -8.000  -0.7726   0.01423   0.00767  -0.0067   0.7260   0.0093
  -7.750  -0.7465   0.01390   0.00731  -0.0066   0.7250   0.0097
  -7.500  -0.7202   0.01359   0.00698  -0.0066   0.7240   0.0101
  -7.250  -0.6937   0.01328   0.00663  -0.0066   0.7229   0.0104
  -7.000  -0.6678   0.01287   0.00621  -0.0065   0.7218   0.0110
  -6.750  -0.6413   0.01256   0.00589  -0.0065   0.7207   0.0116
  -6.500  -0.6145   0.01227   0.00557  -0.0065   0.7197   0.0121
  -6.250  -0.5876   0.01199   0.00528  -0.0065   0.7185   0.0127
  -6.000  -0.5605   0.01174   0.00500  -0.0066   0.7174   0.0133
  -5.750  -0.5336   0.01145   0.00469  -0.0066   0.7162   0.0142
  -5.500  -0.5064   0.01120   0.00444  -0.0067   0.7150   0.0151
  -5.250  -0.4789   0.01098   0.00420  -0.0068   0.7140   0.0161
  -5.000  -0.4513   0.01078   0.00398  -0.0069   0.7130   0.0170
  -4.750  -0.4238   0.01055   0.00374  -0.0070   0.7119   0.0184
  -4.500  -0.3960   0.01034   0.00354  -0.0072   0.7111   0.0199
  -4.250  -0.3680   0.01016   0.00336  -0.0074   0.7103   0.0213
  -4.000  -0.3401   0.00995   0.00317  -0.0075   0.7092   0.0236
  -3.750  -0.3119   0.00977   0.00300  -0.0077   0.7081   0.0262
  -3.500  -0.2838   0.00958   0.00284  -0.0080   0.7069   0.0302
  -3.250  -0.2557   0.00939   0.00269  -0.0082   0.7058   0.0368
  -3.000  -0.2276   0.00920   0.00254  -0.0084   0.7048   0.0483
  -2.750  -0.1995   0.00900   0.00241  -0.0086   0.7037   0.0637
  -2.500  -0.1715   0.00876   0.00228  -0.0089   0.7026   0.0888
  -2.000  -0.1172   0.00800   0.00196  -0.0093   0.7002   0.2146
  -1.750  -0.0903   0.00755   0.00180  -0.0095   0.6991   0.3014
  -1.500  -0.0647   0.00683   0.00158  -0.0097   0.6978   0.4448
  -1.000  -0.0118   0.00617   0.00187  -0.0097   0.6956   0.7366
  -0.750   0.0177   0.00639   0.00210  -0.0099   0.6944   0.7482
  -0.500   0.0471   0.00664   0.00235  -0.0100   0.6928   0.7578
  -0.250   0.0763   0.00659   0.00232  -0.0103   0.6907   0.7605
   0.000   0.1059   0.00657   0.00229  -0.0107   0.6877   0.7616
   0.250   0.1354   0.00655   0.00224  -0.0111   0.6842   0.7625
   0.500   0.1649   0.00654   0.00221  -0.0115   0.6810   0.7632
   0.750   0.1947   0.00651   0.00219  -0.0120   0.6778   0.7635
   1.000   0.2245   0.00648   0.00215  -0.0125   0.6736   0.7637
   1.250   0.2540   0.00645   0.00210  -0.0129   0.6684   0.7639
   1.500   0.2837   0.00644   0.00208  -0.0134   0.6631   0.7642
   1.750   0.3133   0.00641   0.00205  -0.0138   0.6549   0.7645
   2.000   0.3428   0.00640   0.00202  -0.0143   0.6434   0.7648
   2.250   0.3721   0.00641   0.00199  -0.0147   0.6270   0.7649
   2.500   0.4012   0.00647   0.00198  -0.0150   0.6040   0.7650
   2.750   0.4281   0.00685   0.00206  -0.0152   0.5306   0.7652
   3.000   0.4532   0.00761   0.00238  -0.0154   0.4271   0.7653
   3.250   0.4801   0.00802   0.00258  -0.0156   0.3748   0.7655
   3.500   0.5065   0.00850   0.00281  -0.0159   0.3169   0.7658
   3.750   0.5314   0.00916   0.00312  -0.0160   0.2385   0.7660
   4.000   0.5574   0.00962   0.00337  -0.0162   0.1894   0.7662
   4.250   0.5840   0.00998   0.00358  -0.0164   0.1569   0.7663
   4.500   0.6106   0.01031   0.00378  -0.0166   0.1310   0.7663
   4.750   0.6372   0.01063   0.00401  -0.0167   0.1093   0.7664
   5.000   0.6638   0.01093   0.00423  -0.0169   0.0909   0.7665
   5.250   0.6903   0.01124   0.00445  -0.0170   0.0756   0.7668
   5.500   0.7168   0.01152   0.00469  -0.0172   0.0645   0.7670
   5.750   0.7432   0.01181   0.00492  -0.0173   0.0555   0.7671
   6.000   0.7696   0.01208   0.00516  -0.0174   0.0493   0.7672
   6.250   0.7959   0.01235   0.00541  -0.0175   0.0445   0.7673
   6.500   0.8220   0.01263   0.00567  -0.0176   0.0405   0.7674
   6.750   0.8478   0.01292   0.00595  -0.0177   0.0368   0.7674
   7.000   0.8737   0.01319   0.00623  -0.0177   0.0342   0.7675
   7.250   0.8989   0.01352   0.00654  -0.0177   0.0316   0.7676
   7.500   0.9241   0.01384   0.00686  -0.0176   0.0297   0.7677
   7.750   0.9493   0.01413   0.00718  -0.0176   0.0287   0.7678
   8.000   0.9740   0.01446   0.00752  -0.0175   0.0275   0.7678
   8.250   0.9982   0.01481   0.00788  -0.0174   0.0264   0.7679
   8.500   1.0219   0.01520   0.00827  -0.0172   0.0253   0.7680
   8.750   1.0445   0.01566   0.00876  -0.0168   0.0240   0.7681
   9.000   1.0679   0.01602   0.00915  -0.0166   0.0236   0.7682
   9.250   1.0907   0.01641   0.00958  -0.0163   0.0231   0.7683
   9.500   1.1128   0.01683   0.01003  -0.0159   0.0226   0.7684
   9.750   1.1342   0.01728   0.01052  -0.0155   0.0221   0.7685
  10.000   1.1529   0.01775   0.01103  -0.0146   0.0216   0.7686
  10.250   1.1711   0.01829   0.01160  -0.0138   0.0211   0.7687
  10.500   1.1900   0.01891   0.01226  -0.0132   0.0206   0.7688
  10.750   1.2082   0.01959   0.01297  -0.0127   0.0201   0.7689
  11.000   1.2250   0.02039   0.01381  -0.0120   0.0194   0.7690
  11.250   1.2411   0.02124   0.01470  -0.0113   0.0189   0.7691
  11.500   1.2588   0.02193   0.01546  -0.0107   0.0187   0.7693
  11.750   1.2760   0.02267   0.01625  -0.0102   0.0185   0.7695
  12.000   1.2927   0.02345   0.01708  -0.0096   0.0182   0.7697
  12.250   1.3092   0.02423   0.01791  -0.0090   0.0179   0.7698
  12.500   1.3254   0.02503   0.01877  -0.0084   0.0175   0.7699
  12.750   1.3417   0.02581   0.01959  -0.0078   0.0169   0.7699
  13.000   1.3574   0.02664   0.02046  -0.0072   0.0164   0.7700
  13.250   1.3721   0.02756   0.02140  -0.0066   0.0159   0.7701
  13.500   1.3850   0.02861   0.02249  -0.0058   0.0153   0.7702
  13.750   1.3955   0.02987   0.02381  -0.0049   0.0148   0.7703
  14.000   1.4090   0.03088   0.02489  -0.0043   0.0147   0.7703
  14.250   1.4212   0.03200   0.02608  -0.0036   0.0145   0.7704
  14.500   1.4325   0.03320   0.02735  -0.0029   0.0142   0.7705
  14.750   1.4429   0.03448   0.02870  -0.0022   0.0140   0.7706
  15.000   1.4529   0.03580   0.03010  -0.0015   0.0138   0.7707
  15.250   1.4621   0.03721   0.03158  -0.0008   0.0135   0.7707
  15.500   1.4706   0.03869   0.03313  -0.0002   0.0132   0.7708
  15.750   1.4785   0.04024   0.03475   0.0004   0.0130   0.7709
  16.000   1.4851   0.04192   0.03651   0.0010   0.0127   0.7710
  16.250   1.4918   0.04365   0.03830   0.0015   0.0124   0.7710
  16.500   1.4974   0.04557   0.04028   0.0019   0.0122   0.7711
  16.750   1.5018   0.04765   0.04243   0.0023   0.0119   0.7712
  17.000   1.5043   0.04999   0.04486   0.0025   0.0116   0.7712
  17.250   1.5070   0.05241   0.04736   0.0026   0.0114   0.7713
  17.500   1.5092   0.05496   0.05001   0.0025   0.0113   0.7714
  17.750   1.5104   0.05769   0.05284   0.0023   0.0112   0.7714
  18.000   1.5100   0.06070   0.05595   0.0020   0.0110   0.7715
  18.250   1.5091   0.06387   0.05923   0.0014   0.0108   0.7716
  18.500   1.5064   0.06737   0.06284   0.0007   0.0107   0.7716
  18.750   1.5025   0.07116   0.06674  -0.0003   0.0105   0.7717
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