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ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: ONERA HOR12 AIRFOIL (hor12-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.75 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hor12-il-1000000-n5.txt
Download as CSV file: xf-hor12-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -1.0348   0.07782   0.07507  -0.0287   1.0005   0.0145
 -15.000  -1.1037   0.06354   0.06060  -0.0391   1.0005   0.0141
 -14.750  -1.2191   0.03380   0.03030  -0.0725   1.0005   0.0134
 -14.500  -1.1987   0.02831   0.02454  -0.0816   1.0005   0.0136
 -14.250  -1.1763   0.02619   0.02229  -0.0843   1.0005   0.0140
 -14.000  -1.1523   0.02461   0.02063  -0.0862   1.0005   0.0145
 -13.750  -1.1273   0.02337   0.01932  -0.0875   1.0005   0.0150
 -13.500  -1.1015   0.02231   0.01819  -0.0886   1.0005   0.0155
 -13.250  -1.0750   0.02138   0.01717  -0.0896   1.0005   0.0160
 -13.000  -1.0482   0.02052   0.01623  -0.0905   1.0005   0.0164
 -12.750  -1.0209   0.01973   0.01536  -0.0913   1.0005   0.0168
 -12.500  -0.9933   0.01902   0.01461  -0.0920   1.0005   0.0174
 -12.250  -0.9654   0.01845   0.01402  -0.0925   1.0005   0.0181
 -12.000  -0.9372   0.01793   0.01347  -0.0931   1.0005   0.0187
 -11.750  -0.9089   0.01746   0.01296  -0.0936   1.0005   0.0195
 -11.500  -0.8804   0.01697   0.01242  -0.0941   1.0005   0.0201
 -11.250  -0.8517   0.01648   0.01188  -0.0946   1.0005   0.0206
 -11.000  -0.8229   0.01599   0.01137  -0.0952   1.0005   0.0211
 -10.750  -0.7940   0.01558   0.01093  -0.0956   1.0005   0.0216
 -10.500  -0.7649   0.01519   0.01051  -0.0961   1.0005   0.0222
 -10.250  -0.7357   0.01481   0.01009  -0.0966   1.0005   0.0228
 -10.000  -0.7025   0.01445   0.00968  -0.0978   0.9724   0.0234
  -9.750  -0.6728   0.01416   0.00930  -0.0983   0.9517   0.0239
  -9.500  -0.6453   0.01392   0.00898  -0.0982   0.9376   0.0243
  -9.250  -0.6173   0.01366   0.00865  -0.0982   0.9227   0.0246
  -9.000  -0.5895   0.01337   0.00827  -0.0981   0.9046   0.0249
  -8.750  -0.5614   0.01292   0.00770  -0.0983   0.8849   0.0255
  -8.500  -0.5330   0.01260   0.00728  -0.0985   0.8649   0.0262
  -8.250  -0.5043   0.01235   0.00692  -0.0986   0.8443   0.0268
  -8.000  -0.4753   0.01211   0.00657  -0.0988   0.8221   0.0273
  -7.750  -0.4461   0.01189   0.00623  -0.0991   0.8004   0.0278
  -7.500  -0.4166   0.01169   0.00591  -0.0993   0.7814   0.0282
  -7.250  -0.3870   0.01149   0.00561  -0.0996   0.7650   0.0286
  -7.000  -0.3573   0.01130   0.00533  -0.0999   0.7509   0.0289
  -6.750  -0.3275   0.01113   0.00508  -0.1002   0.7386   0.0293
  -6.500  -0.2977   0.01098   0.00485  -0.1005   0.7267   0.0296
  -6.250  -0.2676   0.01073   0.00452  -0.1010   0.7152   0.0306
  -6.000  -0.2376   0.01051   0.00425  -0.1013   0.7043   0.0314
  -5.750  -0.2075   0.01033   0.00401  -0.1017   0.6942   0.0321
  -5.500  -0.1775   0.01016   0.00379  -0.1020   0.6840   0.0328
  -5.250  -0.1474   0.01002   0.00359  -0.1023   0.6748   0.0332
  -5.000  -0.1174   0.00990   0.00341  -0.1026   0.6651   0.0337
  -4.750  -0.0874   0.00977   0.00324  -0.1029   0.6555   0.0342
  -4.500  -0.0573   0.00967   0.00309  -0.1032   0.6461   0.0347
  -4.250  -0.0273   0.00957   0.00295  -0.1035   0.6356   0.0361
  -4.000   0.0027   0.00946   0.00281  -0.1038   0.6254   0.0389
  -3.750   0.0329   0.00930   0.00266  -0.1042   0.6157   0.0493
  -3.500   0.0632   0.00914   0.00253  -0.1046   0.6061   0.0616
  -3.250   0.0932   0.00905   0.00243  -0.1049   0.5973   0.0707
  -3.000   0.1233   0.00897   0.00234  -0.1052   0.5884   0.0786
  -2.750   0.1533   0.00889   0.00227  -0.1055   0.5796   0.0875
  -2.500   0.1832   0.00885   0.00220  -0.1057   0.5695   0.0934
  -2.250   0.2132   0.00879   0.00215  -0.1060   0.5603   0.1014
  -2.000   0.2431   0.00875   0.00210  -0.1063   0.5509   0.1097
  -1.750   0.2730   0.00871   0.00206  -0.1065   0.5408   0.1196
  -1.500   0.3030   0.00867   0.00202  -0.1068   0.5311   0.1320
  -1.000   0.3628   0.00860   0.00198  -0.1074   0.5107   0.1601
  -0.750   0.3926   0.00858   0.00197  -0.1076   0.5013   0.1754
  -0.500   0.4224   0.00858   0.00198  -0.1079   0.4917   0.1904
  -0.250   0.4522   0.00857   0.00199  -0.1082   0.4834   0.2046
   0.000   0.4819   0.00858   0.00200  -0.1084   0.4745   0.2176
   0.250   0.5117   0.00859   0.00203  -0.1086   0.4660   0.2321
   0.500   0.5413   0.00861   0.00205  -0.1089   0.4573   0.2480
   0.750   0.5711   0.00860   0.00208  -0.1091   0.4489   0.2675
   1.000   0.6008   0.00859   0.00213  -0.1094   0.4396   0.2975
   1.250   0.6305   0.00858   0.00219  -0.1097   0.4315   0.3265
   1.500   0.6600   0.00862   0.00225  -0.1099   0.4226   0.3515
   1.750   0.6894   0.00868   0.00233  -0.1101   0.4099   0.3754
   2.000   0.7187   0.00878   0.00241  -0.1103   0.3951   0.3927
   2.250   0.7480   0.00886   0.00250  -0.1105   0.3842   0.4096
   2.500   0.7773   0.00895   0.00259  -0.1107   0.3759   0.4258
   2.750   0.8065   0.00902   0.00268  -0.1108   0.3677   0.4404
   3.000   0.8356   0.00913   0.00278  -0.1110   0.3584   0.4537
   3.250   0.8647   0.00923   0.00289  -0.1111   0.3482   0.4678
   3.500   0.8937   0.00934   0.00300  -0.1112   0.3381   0.4809
   3.750   0.9226   0.00948   0.00312  -0.1114   0.3266   0.4917
   4.000   0.9513   0.00963   0.00326  -0.1115   0.3152   0.5041
   4.250   0.9800   0.00979   0.00340  -0.1116   0.3019   0.5172
   4.500   1.0084   0.01000   0.00357  -0.1117   0.2847   0.5324
   4.750   1.0367   0.01021   0.00376  -0.1118   0.2668   0.5537
   5.000   1.0650   0.01040   0.00397  -0.1120   0.2485   0.5963
   5.250   1.0928   0.01034   0.00430  -0.1122   0.2278   0.7987
   5.500   1.1147   0.01025   0.00444  -0.1107   0.2104   0.9995
   5.750   1.1421   0.01062   0.00470  -0.1107   0.1918   0.9995
   6.000   1.1695   0.01098   0.00497  -0.1107   0.1743   0.9995
   6.250   1.1966   0.01135   0.00525  -0.1106   0.1579   0.9995
   6.500   1.2234   0.01176   0.00557  -0.1105   0.1400   0.9995
   6.750   1.2497   0.01222   0.00592  -0.1104   0.1223   0.9995
   7.000   1.2758   0.01268   0.00628  -0.1102   0.1057   0.9995
   7.250   1.3016   0.01318   0.00668  -0.1099   0.0888   0.9995
   7.500   1.3271   0.01367   0.00709  -0.1096   0.0743   0.9995
   7.750   1.3521   0.01420   0.00754  -0.1093   0.0616   0.9995
   8.000   1.3771   0.01470   0.00797  -0.1089   0.0512   0.9995
   8.250   1.4020   0.01518   0.00841  -0.1085   0.0442   0.9995
   8.500   1.4269   0.01563   0.00883  -0.1081   0.0385   0.9995
   8.750   1.4513   0.01611   0.00928  -0.1077   0.0341   0.9995
   9.000   1.4759   0.01653   0.00970  -0.1072   0.0324   0.9995
   9.250   1.4999   0.01698   0.01016  -0.1067   0.0308   0.9995
   9.500   1.5235   0.01747   0.01064  -0.1061   0.0289   0.9995
   9.750   1.5472   0.01789   0.01108  -0.1055   0.0281   0.9995
  10.000   1.5705   0.01833   0.01155  -0.1049   0.0273   0.9995
  10.250   1.5931   0.01881   0.01206  -0.1042   0.0265   0.9995
  10.500   1.6149   0.01933   0.01260  -0.1033   0.0257   0.9995
  10.750   1.6358   0.01989   0.01319  -0.1024   0.0249   0.9995
  11.000   1.6557   0.02050   0.01382  -0.1013   0.0241   0.9995
  11.250   1.6751   0.02109   0.01446  -0.1001   0.0235   0.9995
  11.500   1.6947   0.02160   0.01501  -0.0990   0.0231   0.9995
  11.750   1.7129   0.02216   0.01561  -0.0976   0.0226   0.9995
  12.000   1.7296   0.02276   0.01626  -0.0961   0.0220   0.9995
  12.250   1.7446   0.02343   0.01698  -0.0943   0.0213   0.9995
  12.500   1.7555   0.02419   0.01778  -0.0919   0.0204   0.9995
  12.750   1.7631   0.02515   0.01877  -0.0892   0.0195   0.9995
  13.000   1.7724   0.02615   0.01983  -0.0871   0.0187   0.9995
  13.250   1.7817   0.02726   0.02100  -0.0852   0.0178   0.9995
  13.500   1.7902   0.02854   0.02232  -0.0835   0.0167   0.9995
  14.000   1.8040   0.03168   0.02555  -0.0806   0.0147   0.9995
  14.250   1.8098   0.03353   0.02745  -0.0795   0.0138   0.9995
  14.500   1.8137   0.03566   0.02964  -0.0785   0.0128   0.9995
  14.750   1.8171   0.03795   0.03200  -0.0778   0.0122   0.9995
  15.000   1.8196   0.04044   0.03456  -0.0772   0.0116   0.9995
  15.250   1.8205   0.04316   0.03736  -0.0767   0.0111   0.9995
  15.500   1.8195   0.04616   0.04044  -0.0764   0.0106   0.9995
  15.750   1.8168   0.04944   0.04380  -0.0762   0.0102   0.9995
  16.000   1.8131   0.05289   0.04733  -0.0760   0.0098   0.9995
  16.250   1.8087   0.05645   0.05099  -0.0761   0.0096   0.9995
  16.500   1.8030   0.06025   0.05489  -0.0762   0.0093   0.9995
  16.750   1.7961   0.06432   0.05906  -0.0765   0.0090   0.9995
  17.000   1.7878   0.06867   0.06351  -0.0770   0.0088   0.9995
  17.250   1.7787   0.07325   0.06819  -0.0777   0.0085   0.9995
  17.500   1.7684   0.07811   0.07315  -0.0786   0.0082   0.9995
  17.750   1.7570   0.08317   0.07831  -0.0797   0.0080   0.9995
  18.000   1.7451   0.08841   0.08365  -0.0809   0.0078   0.9995
  18.250   1.7339   0.09363   0.08897  -0.0822   0.0076   0.9995
  18.500   1.7227   0.09887   0.09432  -0.0836   0.0074   0.9995
  18.750   1.7110   0.10427   0.09982  -0.0852   0.0073   0.9995
  19.000   1.6990   0.10978   0.10544  -0.0869   0.0071   0.9995
  19.250   1.6871   0.11535   0.11111  -0.0888   0.0069   0.9995
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