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ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: ONERA HOR12 AIRFOIL (hor12-il)
Reynolds number: 500,000
Max Cl/Cd: 97.88 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hor12-il-500000-n5.txt
Download as CSV file: xf-hor12-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.8410   0.09722   0.09429  -0.0155   1.0005   0.0200
 -14.250  -0.8771   0.08640   0.08332  -0.0223   1.0005   0.0201
 -14.000  -0.9060   0.07744   0.07424  -0.0283   1.0005   0.0202
 -13.750  -0.9340   0.06904   0.06573  -0.0342   1.0005   0.0202
 -13.500  -0.9610   0.06096   0.05754  -0.0402   1.0005   0.0203
 -13.250  -0.9897   0.05280   0.04926  -0.0466   1.0005   0.0203
 -13.000  -1.0076   0.04368   0.03996  -0.0572   1.0005   0.0204
 -12.750  -0.9989   0.03478   0.03079  -0.0716   1.0005   0.0206
 -12.500  -0.9752   0.03049   0.02629  -0.0793   1.0005   0.0209
 -12.250  -0.9511   0.02855   0.02423  -0.0822   1.0005   0.0213
 -12.000  -0.9260   0.02704   0.02260  -0.0842   1.0005   0.0217
 -11.750  -0.9003   0.02574   0.02119  -0.0859   1.0005   0.0222
 -11.500  -0.8740   0.02456   0.01989  -0.0873   1.0005   0.0228
 -11.250  -0.8472   0.02347   0.01868  -0.0885   1.0005   0.0234
 -11.000  -0.8199   0.02252   0.01759  -0.0896   1.0005   0.0240
 -10.750  -0.7921   0.02172   0.01665  -0.0905   1.0005   0.0245
 -10.500  -0.7644   0.02075   0.01559  -0.0915   1.0005   0.0250
 -10.250  -0.7365   0.01974   0.01451  -0.0926   1.0005   0.0256
 -10.000  -0.7080   0.01895   0.01367  -0.0935   1.0005   0.0262
  -9.750  -0.6794   0.01824   0.01289  -0.0943   1.0005   0.0268
  -9.500  -0.6505   0.01759   0.01217  -0.0950   1.0005   0.0275
  -9.250  -0.6215   0.01700   0.01150  -0.0957   1.0005   0.0282
  -9.000  -0.5923   0.01649   0.01092  -0.0963   0.9993   0.0290
  -8.750  -0.5576   0.01606   0.01038  -0.0980   0.9770   0.0296
  -8.500  -0.5240   0.01517   0.00944  -0.0999   0.9600   0.0309
  -8.250  -0.4933   0.01462   0.00883  -0.1007   0.9453   0.0318
  -8.000  -0.4647   0.01419   0.00832  -0.1009   0.9299   0.0325
  -7.750  -0.4368   0.01381   0.00784  -0.1010   0.9117   0.0332
  -7.500  -0.4092   0.01347   0.00738  -0.1009   0.8932   0.0338
  -7.250  -0.3811   0.01316   0.00696  -0.1008   0.8739   0.0344
  -7.000  -0.3529   0.01289   0.00656  -0.1008   0.8534   0.0350
  -6.750  -0.3243   0.01257   0.00612  -0.1009   0.8325   0.0361
  -6.250  -0.2662   0.01209   0.00541  -0.1012   0.7946   0.0381
  -6.000  -0.2368   0.01188   0.00511  -0.1014   0.7790   0.0394
  -5.750  -0.2072   0.01170   0.00483  -0.1017   0.7646   0.0408
  -5.500  -0.1774   0.01150   0.00456  -0.1020   0.7514   0.0430
  -5.250  -0.1475   0.01131   0.00431  -0.1023   0.7394   0.0467
  -5.000  -0.1177   0.01112   0.00408  -0.1026   0.7278   0.0525
  -4.750  -0.0877   0.01093   0.00387  -0.1029   0.7164   0.0608
  -4.500  -0.0577   0.01076   0.00369  -0.1033   0.7058   0.0709
  -4.250  -0.0278   0.01063   0.00353  -0.1036   0.6958   0.0799
  -4.000   0.0021   0.01051   0.00338  -0.1039   0.6854   0.0881
  -3.750   0.0320   0.01041   0.00325  -0.1041   0.6754   0.0943
  -3.250   0.0918   0.01024   0.00301  -0.1047   0.6545   0.1089
  -3.000   0.1216   0.01017   0.00291  -0.1049   0.6445   0.1167
  -2.750   0.1515   0.01010   0.00282  -0.1052   0.6342   0.1254
  -2.500   0.1814   0.01004   0.00274  -0.1054   0.6245   0.1343
  -2.250   0.2112   0.00998   0.00267  -0.1057   0.6152   0.1442
  -2.000   0.2411   0.00992   0.00261  -0.1060   0.6057   0.1553
  -1.750   0.2710   0.00987   0.00256  -0.1062   0.5964   0.1680
  -1.500   0.3008   0.00983   0.00252  -0.1065   0.5864   0.1819
  -1.250   0.3306   0.00979   0.00250  -0.1067   0.5770   0.1973
  -1.000   0.3603   0.00978   0.00248  -0.1070   0.5672   0.2130
  -0.750   0.3901   0.00976   0.00247  -0.1072   0.5569   0.2278
  -0.500   0.4198   0.00975   0.00247  -0.1074   0.5473   0.2435
  -0.250   0.4495   0.00973   0.00247  -0.1077   0.5372   0.2619
   0.000   0.4792   0.00970   0.00249  -0.1080   0.5270   0.2815
   0.250   0.5089   0.00969   0.00252  -0.1082   0.5172   0.3081
   0.500   0.5384   0.00970   0.00256  -0.1085   0.5071   0.3344
   0.750   0.5680   0.00972   0.00262  -0.1087   0.4979   0.3577
   1.000   0.5974   0.00977   0.00269  -0.1089   0.4885   0.3839
   1.250   0.6269   0.00980   0.00276  -0.1091   0.4795   0.4051
   1.500   0.6561   0.00988   0.00284  -0.1092   0.4708   0.4224
   1.750   0.6855   0.00994   0.00292  -0.1094   0.4613   0.4394
   2.000   0.7147   0.01002   0.00301  -0.1095   0.4528   0.4554
   2.250   0.7439   0.01010   0.00310  -0.1097   0.4432   0.4703
   2.500   0.7730   0.01018   0.00320  -0.1098   0.4334   0.4849
   2.750   0.8020   0.01029   0.00331  -0.1099   0.4229   0.5007
   3.000   0.8309   0.01039   0.00341  -0.1100   0.4113   0.5152
   3.250   0.8598   0.01049   0.00354  -0.1102   0.4000   0.5305
   3.500   0.8886   0.01060   0.00367  -0.1103   0.3897   0.5492
   3.750   0.9174   0.01070   0.00381  -0.1104   0.3792   0.5725
   4.000   0.9463   0.01075   0.00397  -0.1106   0.3697   0.6156
   4.250   0.9728   0.01051   0.00422  -0.1102   0.3593   0.8035
   4.500   0.9949   0.01031   0.00423  -0.1087   0.3488   0.9995
   4.750   1.0234   0.01051   0.00439  -0.1087   0.3388   0.9995
   5.000   1.0517   0.01075   0.00458  -0.1088   0.3275   0.9995
   5.250   1.0796   0.01103   0.00479  -0.1088   0.3107   0.9995
   5.500   1.1072   0.01134   0.00501  -0.1088   0.2922   0.9995
   5.750   1.1347   0.01166   0.00526  -0.1088   0.2754   0.9995
   6.000   1.1620   0.01200   0.00552  -0.1087   0.2584   0.9995
   6.250   1.1889   0.01237   0.00580  -0.1086   0.2408   0.9995
   6.500   1.2155   0.01279   0.00613  -0.1085   0.2226   0.9995
   6.750   1.2420   0.01319   0.00646  -0.1083   0.2056   0.9995
   7.000   1.2681   0.01363   0.00682  -0.1082   0.1885   0.9995
   7.250   1.2937   0.01412   0.00723  -0.1079   0.1700   0.9995
   7.500   1.3187   0.01466   0.00768  -0.1076   0.1511   0.9995
   7.750   1.3431   0.01525   0.00817  -0.1072   0.1324   0.9995
   8.000   1.3671   0.01586   0.00869  -0.1067   0.1140   0.9995
   8.250   1.3903   0.01654   0.00928  -0.1062   0.0963   0.9995
   8.500   1.4130   0.01723   0.00988  -0.1056   0.0812   0.9995
   8.750   1.4353   0.01792   0.01051  -0.1049   0.0677   0.9995
   9.000   1.4571   0.01863   0.01117  -0.1041   0.0573   0.9995
   9.250   1.4783   0.01934   0.01185  -0.1032   0.0493   0.9995
   9.500   1.4996   0.01999   0.01249  -0.1024   0.0445   0.9995
   9.750   1.5202   0.02066   0.01317  -0.1014   0.0409   0.9995
  10.000   1.5410   0.02126   0.01381  -0.1004   0.0384   0.9995
  10.250   1.5605   0.02194   0.01452  -0.0993   0.0364   0.9995
  10.500   1.5783   0.02270   0.01531  -0.0980   0.0346   0.9995
  10.750   1.5960   0.02339   0.01605  -0.0966   0.0334   0.9995
  11.000   1.6116   0.02416   0.01686  -0.0950   0.0321   0.9995
  11.250   1.6248   0.02502   0.01776  -0.0931   0.0309   0.9995
  11.500   1.6338   0.02599   0.01879  -0.0905   0.0297   0.9995
  11.750   1.6393   0.02719   0.02004  -0.0877   0.0287   0.9995
  12.000   1.6484   0.02830   0.02123  -0.0857   0.0281   0.9995
  12.250   1.6568   0.02957   0.02260  -0.0838   0.0275   0.9995
  12.500   1.6644   0.03102   0.02414  -0.0822   0.0268   0.9995
  12.750   1.6709   0.03268   0.02588  -0.0808   0.0261   0.9995
  13.000   1.6762   0.03458   0.02786  -0.0796   0.0254   0.9995
  13.250   1.6799   0.03676   0.03012  -0.0787   0.0247   0.9995
  13.500   1.6814   0.03931   0.03276  -0.0779   0.0241   0.9995
  13.750   1.6817   0.04210   0.03564  -0.0774   0.0235   0.9995
  14.000   1.6868   0.04442   0.03807  -0.0770   0.0230   0.9995
  14.250   1.6900   0.04698   0.04074  -0.0767   0.0225   0.9995
  14.500   1.6916   0.04980   0.04367  -0.0765   0.0218   0.9995
  14.750   1.6917   0.05286   0.04683  -0.0764   0.0212   0.9995
  15.000   1.6898   0.05617   0.05025  -0.0764   0.0206   0.9995
  15.250   1.6863   0.05976   0.05393  -0.0766   0.0201   0.9995
  15.500   1.6813   0.06360   0.05787  -0.0769   0.0196   0.9995
  15.750   1.6744   0.06777   0.06213  -0.0774   0.0192   0.9995
  16.000   1.6699   0.07172   0.06620  -0.0779   0.0187   0.9995
  16.250   1.6648   0.07585   0.07045  -0.0786   0.0182   0.9995
  16.500   1.6588   0.08017   0.07487  -0.0794   0.0177   0.9995
  16.750   1.6520   0.08466   0.07947  -0.0803   0.0172   0.9995
  17.000   1.6448   0.08932   0.08422  -0.0814   0.0167   0.9995
  17.250   1.6369   0.09412   0.08912  -0.0826   0.0162   0.9995
  17.500   1.6280   0.09912   0.09421  -0.0840   0.0157   0.9995
  17.750   1.6190   0.10420   0.09939  -0.0855   0.0154   0.9995
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