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HSNLF(1)-0213 AIRFOIL (hsnlf213-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HSNLF(1)-0213 AIRFOIL (hsnlf213-il)
Reynolds number: 1,000,000
Max Cl/Cd: 78.37 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hsnlf213-il-1000000.txt
Download as CSV file: xf-hsnlf213-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9820   0.06588   0.06337  -0.0220   0.7966   0.0068
 -14.000  -1.0368   0.05430   0.05144  -0.0277   0.7949   0.0067
 -13.750  -1.0567   0.04927   0.04619  -0.0283   0.7927   0.0068
 -13.500  -1.0750   0.04482   0.04151  -0.0279   0.7904   0.0069
 -13.250  -1.0832   0.04164   0.03814  -0.0271   0.7882   0.0070
 -13.000  -1.0875   0.03894   0.03527  -0.0260   0.7863   0.0071
 -12.750  -1.0898   0.03649   0.03263  -0.0247   0.7843   0.0073
 -12.500  -1.0877   0.03448   0.03044  -0.0233   0.7821   0.0075
 -12.250  -1.0833   0.03269   0.02847  -0.0217   0.7799   0.0076
 -12.000  -1.0749   0.03132   0.02692  -0.0201   0.7778   0.0078
 -11.750  -1.0644   0.03031   0.02577  -0.0184   0.7758   0.0079
 -11.500  -1.0666   0.02696   0.02203  -0.0159   0.7737   0.0082
 -11.250  -1.0503   0.02591   0.02089  -0.0149   0.7723   0.0084
 -11.000  -1.0307   0.02521   0.02014  -0.0143   0.7709   0.0086
 -10.750  -1.0102   0.02457   0.01943  -0.0138   0.7694   0.0088
 -10.500  -0.9894   0.02386   0.01864  -0.0132   0.7679   0.0091
 -10.250  -0.9683   0.02306   0.01773  -0.0127   0.7664   0.0094
 -10.000  -0.9469   0.02222   0.01678  -0.0121   0.7650   0.0096
  -9.750  -0.9249   0.02139   0.01582  -0.0116   0.7636   0.0099
  -9.500  -0.9021   0.02065   0.01496  -0.0112   0.7621   0.0102
  -9.250  -0.8784   0.02006   0.01425  -0.0109   0.7605   0.0104
  -9.000  -0.8580   0.01865   0.01267  -0.0101   0.7588   0.0107
  -8.750  -0.8352   0.01781   0.01178  -0.0097   0.7575   0.0112
  -8.500  -0.8101   0.01737   0.01131  -0.0096   0.7566   0.0115
  -8.250  -0.7849   0.01693   0.01084  -0.0095   0.7555   0.0119
  -8.000  -0.7597   0.01643   0.01029  -0.0093   0.7543   0.0123
  -7.750  -0.7341   0.01599   0.00980  -0.0091   0.7531   0.0128
  -7.500  -0.7078   0.01567   0.00943  -0.0091   0.7519   0.0132
  -7.250  -0.6817   0.01528   0.00898  -0.0090   0.7506   0.0136
  -7.000  -0.6589   0.01434   0.00799  -0.0085   0.7494   0.0143
  -6.750  -0.6328   0.01398   0.00763  -0.0085   0.7481   0.0149
  -6.500  -0.6066   0.01360   0.00722  -0.0084   0.7468   0.0155
  -6.250  -0.5805   0.01322   0.00679  -0.0083   0.7457   0.0162
  -6.000  -0.5540   0.01290   0.00643  -0.0082   0.7445   0.0168
  -5.750  -0.5287   0.01240   0.00588  -0.0080   0.7432   0.0177
  -5.500  -0.5022   0.01203   0.00551  -0.0080   0.7422   0.0189
  -5.250  -0.4750   0.01175   0.00524  -0.0081   0.7414   0.0202
  -5.000  -0.4474   0.01151   0.00499  -0.0082   0.7404   0.0213
  -4.750  -0.4212   0.01105   0.00452  -0.0081   0.7392   0.0233
  -4.500  -0.3936   0.01081   0.00427  -0.0082   0.7380   0.0253
  -4.250  -0.3658   0.01060   0.00404  -0.0084   0.7368   0.0271
  -4.000  -0.3385   0.01029   0.00376  -0.0084   0.7357   0.0308
  -3.750  -0.3106   0.01009   0.00354  -0.0086   0.7346   0.0348
  -3.500  -0.2828   0.00985   0.00335  -0.0087   0.7335   0.0424
  -3.250  -0.2554   0.00955   0.00315  -0.0089   0.7323   0.0642
  -3.000  -0.2285   0.00917   0.00296  -0.0090   0.7312   0.1078
  -2.750  -0.2032   0.00855   0.00273  -0.0090   0.7300   0.2126
  -2.500  -0.1798   0.00757   0.00243  -0.0090   0.7289   0.3949
  -2.250  -0.1593   0.00625   0.00220  -0.0085   0.7274   0.6758
  -2.000  -0.1294   0.00656   0.00254  -0.0087   0.7264   0.7294
  -1.750  -0.0996   0.00674   0.00271  -0.0090   0.7254   0.7389
  -1.500  -0.0700   0.00689   0.00284  -0.0094   0.7243   0.7463
  -1.250  -0.0408   0.00711   0.00307  -0.0095   0.7230   0.7554
  -1.000  -0.0123   0.00730   0.00330  -0.0094   0.7215   0.7652
  -0.750   0.0159   0.00748   0.00353  -0.0091   0.7200   0.7759
  -0.500   0.0445   0.00782   0.00388  -0.0089   0.7183   0.7861
  -0.250   0.0726   0.00767   0.00374  -0.0089   0.7163   0.7902
   0.000   0.1017   0.00766   0.00370  -0.0092   0.7140   0.7920
   0.250   0.1309   0.00767   0.00370  -0.0095   0.7113   0.7935
   0.500   0.1606   0.00761   0.00365  -0.0100   0.7089   0.7947
   0.750   0.1902   0.00756   0.00359  -0.0104   0.7062   0.7956
   1.000   0.2199   0.00749   0.00350  -0.0109   0.7031   0.7962
   1.250   0.2495   0.00741   0.00339  -0.0113   0.6996   0.7966
   1.500   0.2790   0.00738   0.00334  -0.0117   0.6960   0.7969
   1.750   0.3088   0.00727   0.00325  -0.0122   0.6915   0.7971
   2.000   0.3384   0.00716   0.00313  -0.0127   0.6858   0.7974
   2.250   0.3679   0.00710   0.00305  -0.0131   0.6802   0.7979
   2.500   0.3976   0.00703   0.00300  -0.0136   0.6744   0.7982
   2.750   0.4271   0.00696   0.00290  -0.0140   0.6668   0.7983
   3.000   0.4568   0.00688   0.00285  -0.0144   0.6560   0.7985
   3.250   0.4863   0.00685   0.00283  -0.0149   0.6473   0.7986
   3.500   0.5157   0.00683   0.00279  -0.0154   0.6313   0.7987
   3.750   0.5439   0.00694   0.00275  -0.0156   0.5852   0.7989
   4.000   0.5692   0.00752   0.00295  -0.0156   0.4959   0.7992
   4.250   0.5941   0.00821   0.00328  -0.0157   0.4119   0.7994
   4.500   0.6190   0.00885   0.00359  -0.0159   0.3366   0.7996
   4.750   0.6437   0.00947   0.00391  -0.0160   0.2685   0.7996
   5.000   0.6683   0.01007   0.00422  -0.0160   0.2081   0.7997
   5.250   0.6930   0.01061   0.00453  -0.0161   0.1595   0.7998
   5.500   0.7182   0.01107   0.00482  -0.0161   0.1256   0.7998
   5.750   0.7437   0.01147   0.00510  -0.0162   0.1004   0.7998
   6.000   0.7690   0.01187   0.00539  -0.0163   0.0802   0.8000
   6.250   0.7946   0.01224   0.00568  -0.0163   0.0661   0.8002
   6.500   0.8199   0.01260   0.00599  -0.0163   0.0555   0.8003
   6.750   0.8450   0.01298   0.00631  -0.0163   0.0480   0.8003
   7.000   0.8707   0.01328   0.00663  -0.0163   0.0438   0.8003
   7.250   0.8954   0.01367   0.00698  -0.0163   0.0399   0.8003
   7.500   0.9195   0.01410   0.00743  -0.0161   0.0369   0.8003
   7.750   0.9446   0.01440   0.00775  -0.0160   0.0356   0.8003
   8.000   0.9690   0.01475   0.00813  -0.0159   0.0341   0.8004
   8.250   0.9926   0.01516   0.00854  -0.0157   0.0326   0.8004
   8.500   1.0140   0.01575   0.00914  -0.0152   0.0307   0.8006
   8.750   1.0354   0.01630   0.00975  -0.0147   0.0298   0.8007
   9.000   1.0582   0.01670   0.01019  -0.0144   0.0292   0.8007
   9.250   1.0800   0.01715   0.01068  -0.0140   0.0286   0.8007
   9.500   1.1008   0.01764   0.01121  -0.0135   0.0279   0.8007
   9.750   1.1183   0.01816   0.01177  -0.0125   0.0272   0.8007
  10.000   1.1364   0.01876   0.01241  -0.0118   0.0266   0.8007
  10.250   1.1547   0.01945   0.01313  -0.0112   0.0260   0.8008
  10.500   1.1710   0.02031   0.01402  -0.0105   0.0252   0.8008
  10.750   1.1812   0.02165   0.01543  -0.0092   0.0242   0.8008
  11.000   1.1948   0.02272   0.01657  -0.0082   0.0238   0.8009
  11.250   1.2124   0.02344   0.01735  -0.0077   0.0236   0.8009
  11.500   1.2289   0.02425   0.01822  -0.0070   0.0233   0.8010
  11.750   1.2446   0.02512   0.01915  -0.0063   0.0229   0.8010
  12.000   1.2597   0.02605   0.02014  -0.0056   0.0226   0.8011
  12.250   1.2745   0.02698   0.02113  -0.0049   0.0221   0.8011
  12.500   1.2892   0.02791   0.02212  -0.0043   0.0216   0.8012
  12.750   1.3051   0.02874   0.02298  -0.0038   0.0211   0.8013
  13.000   1.3206   0.02959   0.02385  -0.0034   0.0205   0.8013
  13.250   1.3321   0.03078   0.02507  -0.0027   0.0199   0.8014
  13.500   1.3336   0.03284   0.02722  -0.0011   0.0192   0.8015
  13.750   1.3422   0.03430   0.02877  -0.0002   0.0188   0.8017
  14.000   1.3558   0.03534   0.02988   0.0003   0.0186   0.8018
  14.250   1.3676   0.03652   0.03113   0.0008   0.0184   0.8020
  14.500   1.3772   0.03792   0.03262   0.0014   0.0181   0.8023
  14.750   1.3860   0.03941   0.03419   0.0020   0.0179   0.8027
  15.000   1.3936   0.04102   0.03589   0.0026   0.0176   0.8029
  15.250   1.4008   0.04267   0.03763   0.0032   0.0173   0.8031
  15.500   1.4072   0.04445   0.03948   0.0037   0.0170   0.8032
  15.750   1.4136   0.04629   0.04140   0.0040   0.0168   0.8034
  16.000   1.4198   0.04820   0.04338   0.0042   0.0165   0.8036
  16.250   1.4259   0.05019   0.04543   0.0043   0.0162   0.8037
  16.500   1.4305   0.05242   0.04774   0.0042   0.0159   0.8039
  16.750   1.4324   0.05504   0.05043   0.0041   0.0157   0.8041
  17.000   1.4300   0.05821   0.05369   0.0039   0.0154   0.8043
  17.250   1.4226   0.06209   0.05768   0.0035   0.0152   0.8044
  17.500   1.4088   0.06698   0.06272   0.0027   0.0149   0.8045
  17.750   1.4036   0.07098   0.06683   0.0017   0.0148   0.8047
  18.000   1.4005   0.07483   0.07080   0.0004   0.0147   0.8049
  18.250   1.3980   0.07874   0.07483  -0.0010   0.0146   0.8051
  18.500   1.3918   0.08329   0.07949  -0.0027   0.0145   0.8052
  18.750   1.3842   0.08819   0.08452  -0.0048   0.0144   0.8054
  19.000   1.3737   0.09363   0.09009  -0.0072   0.0143   0.8056
  19.250   1.3621   0.09941   0.09599  -0.0098   0.0142   0.8057
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