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ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: ONERA HOR12 AIRFOIL (hor12-il)
Reynolds number: 500,000
Max Cl/Cd: 103.72 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hor12-il-500000.txt
Download as CSV file: xf-hor12-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: ONERA HOR12 AIRFOIL                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.8414   0.06273   0.05982  -0.0412   1.0005   0.0270
 -12.250  -0.8911   0.04954   0.04637  -0.0539   1.0005   0.0267
 -12.000  -0.8932   0.04022   0.03678  -0.0691   1.0005   0.0269
 -11.750  -0.8751   0.03506   0.03134  -0.0786   1.0005   0.0275
 -11.500  -0.8554   0.03221   0.02825  -0.0824   1.0005   0.0282
 -11.250  -0.8329   0.03002   0.02583  -0.0851   1.0005   0.0289
 -11.000  -0.8079   0.02851   0.02410  -0.0870   1.0005   0.0294
 -10.750  -0.7868   0.02526   0.02058  -0.0895   1.0005   0.0304
 -10.500  -0.7613   0.02379   0.01906  -0.0907   1.0005   0.0313
 -10.250  -0.7344   0.02268   0.01788  -0.0917   1.0005   0.0321
 -10.000  -0.7068   0.02163   0.01672  -0.0927   1.0005   0.0330
  -9.750  -0.6789   0.02064   0.01561  -0.0936   1.0005   0.0339
  -9.500  -0.6504   0.01981   0.01465  -0.0943   1.0005   0.0347
  -9.250  -0.6222   0.01840   0.01311  -0.0954   1.0005   0.0357
  -9.000  -0.5937   0.01737   0.01204  -0.0963   1.0005   0.0369
  -8.750  -0.5648   0.01677   0.01141  -0.0970   1.0005   0.0381
  -8.500  -0.5357   0.01622   0.01082  -0.0976   1.0005   0.0394
  -8.250  -0.5067   0.01574   0.01026  -0.0980   1.0005   0.0406
  -8.000  -0.4779   0.01516   0.00961  -0.0985   1.0005   0.0417
  -7.750  -0.4494   0.01429   0.00873  -0.0992   1.0005   0.0432
  -7.500  -0.4206   0.01380   0.00823  -0.0997   0.9992   0.0444
  -7.250  -0.3826   0.01329   0.00767  -0.1020   0.9914   0.0458
  -7.000  -0.3450   0.01283   0.00715  -0.1041   0.9808   0.0471
  -6.750  -0.3096   0.01249   0.00673  -0.1056   0.9663   0.0484
  -6.500  -0.2782   0.01202   0.00620  -0.1063   0.9495   0.0503
  -6.250  -0.2506   0.01170   0.00582  -0.1060   0.9309   0.0523
  -6.000  -0.2236   0.01146   0.00551  -0.1055   0.9111   0.0544
  -5.750  -0.1964   0.01125   0.00521  -0.1051   0.8915   0.0570
  -5.500  -0.1682   0.01092   0.00483  -0.1050   0.8718   0.0624
  -5.250  -0.1396   0.01065   0.00452  -0.1049   0.8526   0.0719
  -5.000  -0.1108   0.01044   0.00429  -0.1049   0.8341   0.0860
  -4.750  -0.0818   0.01031   0.00409  -0.1050   0.8169   0.0973
  -4.500  -0.0527   0.01023   0.00393  -0.1050   0.8010   0.1063
  -4.250  -0.0233   0.01013   0.00379  -0.1051   0.7866   0.1155
  -4.000   0.0062   0.01005   0.00364  -0.1053   0.7731   0.1234
  -3.750   0.0356   0.00999   0.00352  -0.1054   0.7605   0.1315
  -3.500   0.0653   0.00990   0.00339  -0.1056   0.7482   0.1401
  -3.250   0.0950   0.00984   0.00329  -0.1058   0.7359   0.1497
  -3.000   0.1248   0.00975   0.00319  -0.1060   0.7246   0.1609
  -2.750   0.1545   0.00969   0.00310  -0.1062   0.7138   0.1730
  -2.500   0.1844   0.00961   0.00302  -0.1065   0.7027   0.1863
  -2.250   0.2142   0.00956   0.00296  -0.1067   0.6925   0.2003
  -2.000   0.2438   0.00954   0.00291  -0.1069   0.6824   0.2153
  -1.750   0.2737   0.00948   0.00287  -0.1072   0.6718   0.2307
  -1.500   0.3034   0.00945   0.00283  -0.1074   0.6619   0.2461
  -1.250   0.3332   0.00941   0.00279  -0.1076   0.6515   0.2622
  -1.000   0.3630   0.00935   0.00276  -0.1079   0.6412   0.2804
  -0.750   0.3927   0.00932   0.00275  -0.1081   0.6312   0.3018
  -0.500   0.4225   0.00928   0.00276  -0.1083   0.6207   0.3284
  -0.250   0.4522   0.00925   0.00279  -0.1086   0.6105   0.3589
   0.000   0.4817   0.00927   0.00283  -0.1088   0.6004   0.3888
   0.250   0.5114   0.00926   0.00289  -0.1090   0.5897   0.4159
   0.500   0.5409   0.00931   0.00293  -0.1091   0.5796   0.4382
   0.750   0.5702   0.00936   0.00298  -0.1092   0.5693   0.4574
   1.000   0.5997   0.00939   0.00303  -0.1094   0.5587   0.4761
   1.250   0.6291   0.00945   0.00309  -0.1095   0.5488   0.4932
   1.500   0.6584   0.00950   0.00314  -0.1097   0.5383   0.5090
   1.750   0.6877   0.00954   0.00321  -0.1098   0.5280   0.5259
   2.000   0.7169   0.00959   0.00328  -0.1099   0.5182   0.5442
   2.250   0.7462   0.00963   0.00335  -0.1101   0.5077   0.5656
   2.500   0.7754   0.00964   0.00345  -0.1103   0.4973   0.5946
   2.750   0.8043   0.00962   0.00357  -0.1104   0.4869   0.6531
   3.000   0.8273   0.00916   0.00370  -0.1090   0.4764   0.8670
   3.250   0.8531   0.00908   0.00366  -0.1083   0.4659   0.9995
   3.500   0.8821   0.00926   0.00377  -0.1084   0.4554   0.9995
   3.750   0.9113   0.00940   0.00388  -0.1086   0.4447   0.9995
   4.000   0.9402   0.00957   0.00400  -0.1087   0.4349   0.9995
   4.250   0.9688   0.00978   0.00414  -0.1088   0.4243   0.9995
   4.500   0.9977   0.00993   0.00429  -0.1089   0.4137   0.9995
   4.750   1.0263   0.01013   0.00444  -0.1089   0.4039   0.9995
   5.000   1.0546   0.01036   0.00462  -0.1090   0.3930   0.9995
   5.250   1.0829   0.01055   0.00478  -0.1090   0.3795   0.9995
   5.500   1.1111   0.01077   0.00496  -0.1090   0.3657   0.9995
   5.750   1.1391   0.01100   0.00516  -0.1090   0.3529   0.9995
   6.000   1.1669   0.01125   0.00537  -0.1090   0.3403   0.9995
   6.250   1.1945   0.01152   0.00560  -0.1090   0.3271   0.9995
   6.500   1.2219   0.01182   0.00585  -0.1089   0.3137   0.9995
   6.750   1.2492   0.01210   0.00611  -0.1088   0.3005   0.9995
   7.000   1.2764   0.01240   0.00639  -0.1087   0.2869   0.9995
   7.250   1.3031   0.01274   0.00669  -0.1086   0.2717   0.9995
   7.500   1.3294   0.01312   0.00702  -0.1084   0.2556   0.9995
   7.750   1.3552   0.01356   0.00739  -0.1081   0.2383   0.9995
   8.000   1.3806   0.01402   0.00779  -0.1078   0.2196   0.9995
   8.250   1.4053   0.01456   0.00825  -0.1074   0.1983   0.9995
   8.500   1.4289   0.01522   0.00878  -0.1069   0.1755   0.9995
   8.750   1.4511   0.01600   0.00941  -0.1063   0.1487   0.9995
   9.000   1.4715   0.01696   0.01018  -0.1054   0.1179   0.9995
   9.250   1.4897   0.01811   0.01112  -0.1043   0.0869   0.9995
   9.500   1.5074   0.01921   0.01208  -0.1030   0.0672   0.9995
   9.750   1.5260   0.02014   0.01296  -0.1018   0.0579   0.9995
  10.000   1.5449   0.02096   0.01378  -0.1006   0.0532   0.9995
  10.250   1.5615   0.02192   0.01476  -0.0991   0.0497   0.9995
  10.500   1.5800   0.02262   0.01553  -0.0978   0.0478   0.9995
  10.750   1.5961   0.02344   0.01640  -0.0962   0.0457   0.9995
  11.000   1.6084   0.02442   0.01741  -0.0941   0.0437   0.9995
  11.250   1.6134   0.02577   0.01881  -0.0911   0.0418   0.9995
  11.500   1.6237   0.02661   0.01974  -0.0887   0.0409   0.9995
  11.750   1.6327   0.02766   0.02088  -0.0865   0.0397   0.9995
  12.000   1.6407   0.02890   0.02220  -0.0845   0.0385   0.9995
  12.250   1.6475   0.03037   0.02374  -0.0827   0.0374   0.9995
  12.500   1.6516   0.03220   0.02563  -0.0810   0.0363   0.9995
  12.750   1.6507   0.03467   0.02817  -0.0795   0.0352   0.9995
  13.000   1.6511   0.03721   0.03083  -0.0784   0.0343   0.9995
  13.250   1.6575   0.03925   0.03298  -0.0777   0.0335   0.9995
  13.500   1.6614   0.04164   0.03547  -0.0772   0.0327   0.9995
  13.750   1.6641   0.04423   0.03815  -0.0768   0.0318   0.9995
  14.000   1.6646   0.04714   0.04114  -0.0765   0.0310   0.9995
  14.250   1.6614   0.05055   0.04462  -0.0764   0.0302   0.9995
  14.500   1.6529   0.05465   0.04881  -0.0764   0.0294   0.9995
  14.750   1.6388   0.05948   0.05373  -0.0765   0.0287   0.9995
  15.000   1.6379   0.06279   0.05717  -0.0766   0.0282   0.9995
  15.250   1.6352   0.06637   0.06086  -0.0769   0.0277   0.9995
  15.500   1.6314   0.07020   0.06481  -0.0773   0.0270   0.9995
  15.750   1.6264   0.07427   0.06899  -0.0779   0.0264   0.9995
  16.000   1.6205   0.07855   0.07336  -0.0787   0.0258   0.9995
  16.250   1.6138   0.08300   0.07790  -0.0796   0.0253   0.9995
  16.500   1.6057   0.08773   0.08270  -0.0806   0.0248   0.9995
  16.750   1.5953   0.09279   0.08783  -0.0818   0.0243   0.9995
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