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ONERA HOR12 AIRFOIL (hor12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: ONERA HOR12 AIRFOIL (hor12-il)
Reynolds number: 1,000,000
Max Cl/Cd: 121.35 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hor12-il-1000000.txt
Download as CSV file: xf-hor12-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.9782   0.08594   0.08346  -0.0227   1.0005   0.0185
 -15.000  -1.0050   0.07767   0.07510  -0.0282   1.0005   0.0185
 -14.750  -1.0396   0.06864   0.06596  -0.0345   1.0005   0.0185
 -14.500  -1.0860   0.05803   0.05522  -0.0424   1.0005   0.0184
 -14.250  -1.1500   0.04188   0.03880  -0.0591   1.0005   0.0181
 -14.000  -1.1415   0.03082   0.02744  -0.0772   1.0005   0.0184
 -13.750  -1.1172   0.02860   0.02511  -0.0807   1.0005   0.0188
 -13.500  -1.0926   0.02711   0.02353  -0.0828   1.0005   0.0192
 -13.250  -1.0673   0.02586   0.02218  -0.0844   1.0005   0.0197
 -13.000  -1.0415   0.02477   0.02099  -0.0857   1.0005   0.0202
 -12.750  -1.0150   0.02391   0.02003  -0.0867   1.0005   0.0205
 -12.500  -0.9896   0.02239   0.01843  -0.0885   1.0005   0.0211
 -12.250  -0.9622   0.02174   0.01775  -0.0893   1.0005   0.0216
 -12.000  -0.9345   0.02123   0.01721  -0.0899   1.0005   0.0221
 -11.750  -0.9066   0.02077   0.01671  -0.0904   1.0005   0.0227
 -11.500  -0.8785   0.02025   0.01613  -0.0910   1.0005   0.0234
 -11.250  -0.8503   0.01976   0.01557  -0.0916   1.0005   0.0240
 -11.000  -0.8218   0.01932   0.01506  -0.0921   1.0005   0.0244
 -10.750  -0.7931   0.01902   0.01468  -0.0926   1.0005   0.0247
 -10.500  -0.7655   0.01731   0.01288  -0.0942   1.0005   0.0257
 -10.250  -0.7368   0.01662   0.01217  -0.0950   1.0005   0.0264
 -10.000  -0.7078   0.01606   0.01158  -0.0956   1.0005   0.0270
  -9.750  -0.6786   0.01553   0.01099  -0.0963   1.0005   0.0277
  -9.500  -0.6492   0.01504   0.01046  -0.0968   1.0005   0.0284
  -9.250  -0.6198   0.01460   0.00996  -0.0974   1.0005   0.0290
  -9.000  -0.5903   0.01428   0.00960  -0.0978   1.0005   0.0294
  -8.750  -0.5603   0.01342   0.00865  -0.0988   1.0005   0.0303
  -8.500  -0.5302   0.01268   0.00787  -0.0997   1.0005   0.0313
  -8.250  -0.4957   0.01218   0.00734  -0.1013   0.9862   0.0323
  -7.750  -0.4335   0.01151   0.00654  -0.1026   0.9506   0.0339
  -7.500  -0.4062   0.01126   0.00620  -0.1024   0.9345   0.0344
  -7.250  -0.3784   0.01102   0.00587  -0.1022   0.9161   0.0349
  -7.000  -0.3504   0.01073   0.00547  -0.1021   0.8963   0.0355
  -6.750  -0.3219   0.01043   0.00506  -0.1021   0.8761   0.0366
  -6.500  -0.2929   0.01020   0.00474  -0.1022   0.8546   0.0378
  -6.250  -0.2638   0.01002   0.00447  -0.1023   0.8333   0.0390
  -6.000  -0.2345   0.00988   0.00422  -0.1024   0.8131   0.0402
  -5.750  -0.2049   0.00976   0.00400  -0.1026   0.7953   0.0411
  -5.500  -0.1751   0.00961   0.00376  -0.1028   0.7796   0.0424
  -5.250  -0.1451   0.00945   0.00355  -0.1031   0.7656   0.0450
  -5.000  -0.1151   0.00931   0.00336  -0.1034   0.7527   0.0481
  -4.750  -0.0850   0.00914   0.00317  -0.1037   0.7407   0.0553
  -4.500  -0.0549   0.00897   0.00300  -0.1041   0.7292   0.0676
  -4.250  -0.0248   0.00882   0.00287  -0.1044   0.7174   0.0799
  -4.000   0.0053   0.00871   0.00275  -0.1047   0.7062   0.0898
  -3.750   0.0353   0.00861   0.00264  -0.1050   0.6956   0.0991
  -3.500   0.0652   0.00855   0.00255  -0.1052   0.6851   0.1066
  -3.250   0.0953   0.00846   0.00246  -0.1055   0.6754   0.1155
  -2.750   0.1552   0.00834   0.00231  -0.1060   0.6560   0.1334
  -2.500   0.1852   0.00827   0.00225  -0.1063   0.6463   0.1444
  -2.250   0.2152   0.00822   0.00219  -0.1066   0.6364   0.1554
  -2.000   0.2451   0.00817   0.00214  -0.1068   0.6271   0.1677
  -1.500   0.3050   0.00808   0.00208  -0.1074   0.6075   0.1980
  -1.250   0.3349   0.00806   0.00207  -0.1076   0.5979   0.2140
  -1.000   0.3647   0.00804   0.00206  -0.1079   0.5877   0.2295
  -0.500   0.4244   0.00802   0.00204  -0.1084   0.5676   0.2583
  -0.250   0.4542   0.00799   0.00204  -0.1086   0.5575   0.2738
   0.000   0.4840   0.00798   0.00205  -0.1089   0.5476   0.2933
   0.250   0.5138   0.00796   0.00208  -0.1091   0.5370   0.3237
   0.500   0.5437   0.00793   0.00211  -0.1094   0.5272   0.3544
   0.750   0.5733   0.00794   0.00217  -0.1097   0.5171   0.3861
   1.000   0.6029   0.00797   0.00223  -0.1099   0.5067   0.4138
   1.250   0.6325   0.00800   0.00229  -0.1101   0.4975   0.4330
   1.500   0.6619   0.00808   0.00235  -0.1102   0.4877   0.4502
   1.750   0.6914   0.00814   0.00242  -0.1104   0.4763   0.4657
   2.000   0.7207   0.00822   0.00248  -0.1106   0.4636   0.4784
   2.250   0.7500   0.00830   0.00255  -0.1107   0.4530   0.4918
   2.500   0.7794   0.00837   0.00263  -0.1109   0.4434   0.5058
   2.750   0.8087   0.00844   0.00271  -0.1111   0.4343   0.5205
   3.250   0.8672   0.00857   0.00289  -0.1114   0.4145   0.5591
   3.500   0.8965   0.00861   0.00301  -0.1116   0.4046   0.5953
   3.750   0.9257   0.00856   0.00317  -0.1119   0.3936   0.6917
   4.000   0.9479   0.00802   0.00322  -0.1104   0.3846   0.9995
   4.250   0.9769   0.00820   0.00333  -0.1105   0.3732   0.9995
   4.500   1.0056   0.00839   0.00346  -0.1107   0.3598   0.9995
   5.000   1.0629   0.00879   0.00374  -0.1109   0.3327   0.9995
   5.250   1.0914   0.00901   0.00389  -0.1109   0.3188   0.9995
   5.500   1.1197   0.00923   0.00406  -0.1110   0.3060   0.9995
   5.750   1.1480   0.00946   0.00424  -0.1110   0.2931   0.9995
   6.000   1.1760   0.00972   0.00443  -0.1111   0.2797   0.9995
   6.250   1.2039   0.00999   0.00464  -0.1111   0.2655   0.9995
   6.500   1.2315   0.01028   0.00488  -0.1111   0.2507   0.9995
   6.750   1.2589   0.01060   0.00512  -0.1110   0.2348   0.9995
   7.000   1.2859   0.01096   0.00540  -0.1109   0.2173   0.9995
   7.250   1.3125   0.01137   0.00572  -0.1108   0.1972   0.9995
   7.500   1.3385   0.01186   0.00608  -0.1106   0.1770   0.9995
   7.750   1.3642   0.01234   0.00646  -0.1104   0.1563   0.9995
   8.000   1.3889   0.01297   0.00694  -0.1101   0.1319   0.9995
   8.250   1.4125   0.01370   0.00750  -0.1096   0.1052   0.9995
   8.500   1.4351   0.01452   0.00813  -0.1090   0.0786   0.9995
   8.750   1.4575   0.01532   0.00879  -0.1083   0.0589   0.9995
   9.000   1.4807   0.01595   0.00935  -0.1077   0.0489   0.9995
   9.250   1.5039   0.01654   0.00991  -0.1070   0.0435   0.9995
   9.500   1.5278   0.01700   0.01038  -0.1065   0.0405   0.9995
   9.750   1.5513   0.01747   0.01086  -0.1059   0.0382   0.9995
  10.000   1.5736   0.01803   0.01142  -0.1051   0.0360   0.9995
  10.250   1.5957   0.01858   0.01200  -0.1043   0.0343   0.9995
  10.500   1.6180   0.01906   0.01251  -0.1035   0.0334   0.9995
  10.750   1.6393   0.01960   0.01308  -0.1026   0.0324   0.9995
  11.000   1.6594   0.02021   0.01371  -0.1016   0.0314   0.9995
  11.250   1.6779   0.02090   0.01442  -0.1003   0.0303   0.9995
  11.500   1.6940   0.02170   0.01526  -0.0986   0.0291   0.9995
  11.750   1.7101   0.02240   0.01602  -0.0970   0.0284   0.9995
  12.000   1.7262   0.02303   0.01671  -0.0954   0.0279   0.9995
  12.250   1.7401   0.02375   0.01749  -0.0935   0.0273   0.9995
  12.500   1.7490   0.02458   0.01837  -0.0908   0.0265   0.9995
  12.750   1.7563   0.02561   0.01946  -0.0882   0.0258   0.9995
  13.000   1.7621   0.02692   0.02081  -0.0858   0.0249   0.9995
  13.250   1.7643   0.02866   0.02262  -0.0835   0.0240   0.9995
  13.500   1.7713   0.03018   0.02422  -0.0820   0.0234   0.9995
  13.750   1.7832   0.03135   0.02545  -0.0809   0.0229   0.9995
  14.000   1.7930   0.03279   0.02697  -0.0799   0.0223   0.9995
  14.250   1.8015   0.03443   0.02868  -0.0790   0.0215   0.9995
  14.500   1.8081   0.03634   0.03064  -0.0782   0.0207   0.9995
  14.750   1.8123   0.03858   0.03294  -0.0776   0.0200   0.9995
  15.000   1.8124   0.04137   0.03579  -0.0770   0.0193   0.9995
  15.250   1.8171   0.04368   0.03818  -0.0766   0.0188   0.9995
  15.500   1.8209   0.04611   0.04070  -0.0763   0.0182   0.9995
  15.750   1.8224   0.04889   0.04354  -0.0760   0.0175   0.9995
  16.000   1.8218   0.05193   0.04666  -0.0759   0.0168   0.9995
  16.250   1.8185   0.05533   0.05012  -0.0758   0.0161   0.9995
  16.500   1.8119   0.05924   0.05410  -0.0760   0.0155   0.9995
  16.750   1.8069   0.06302   0.05799  -0.0762   0.0151   0.9995
  17.000   1.8004   0.06708   0.06214  -0.0766   0.0147   0.9995
  17.250   1.7926   0.07142   0.06657  -0.0772   0.0142   0.9995
  17.500   1.7838   0.07602   0.07125  -0.0780   0.0137   0.9995
  17.750   1.7735   0.08086   0.07618  -0.0789   0.0133   0.9995
  18.000   1.7609   0.08615   0.08156  -0.0801   0.0128   0.9995
  18.250   1.7469   0.09176   0.08727  -0.0815   0.0124   0.9995
  18.500   1.7361   0.09693   0.09255  -0.0828   0.0122   0.9995
  18.750   1.7242   0.10230   0.09803  -0.0843   0.0119   0.9995
  19.000   1.7117   0.10784   0.10367  -0.0860   0.0116   0.9995
  19.250   1.6989   0.11353   0.10946  -0.0879   0.0113   0.9995
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