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ONERA HOR07 AIRFOIL (hor07-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: ONERA HOR07 AIRFOIL (hor07-il)
Reynolds number: 100,000
Max Cl/Cd: 59.53 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hor07-il-100000-n5.txt
Download as CSV file: xf-hor07-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: ONERA HOR07 AIRFOIL                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.4260   0.11376   0.10886  -0.0030   1.0000   0.0487
  -8.500  -0.4256   0.11158   0.10674  -0.0071   1.0000   0.0494
  -8.250  -0.4237   0.10902   0.10424  -0.0108   1.0000   0.0497
  -8.000  -0.4180   0.10597   0.10124  -0.0149   1.0000   0.0499
  -7.750  -0.4069   0.10012   0.09542  -0.0110   1.0000   0.0514
  -7.500  -0.3948   0.09670   0.09202  -0.0103   1.0000   0.0531
  -7.250  -0.3868   0.09358   0.08894  -0.0117   1.0000   0.0542
  -7.000  -0.3771   0.09024   0.08563  -0.0143   1.0000   0.0551
  -6.750  -0.3660   0.08676   0.08219  -0.0174   1.0000   0.0559
  -6.250  -0.3278   0.07428   0.06965  -0.0363   1.0000   0.0380
  -6.000  -0.3167   0.07124   0.06665  -0.0356   1.0000   0.0364
  -5.750  -0.2982   0.06708   0.06250  -0.0396   1.0000   0.0347
  -5.500  -0.2750   0.06207   0.05744  -0.0456   1.0000   0.0330
  -5.000  -0.1927   0.04273   0.03756  -0.0704   1.0000   0.0287
  -4.750  -0.1418   0.03411   0.02826  -0.0815   0.9885   0.0285
  -4.500  -0.0942   0.02824   0.02160  -0.0892   0.9743   0.0296
  -4.250  -0.0549   0.02624   0.01935  -0.0929   0.9566   0.0321
  -4.000  -0.0137   0.02340   0.01588  -0.0965   0.9389   0.0339
  -3.750   0.0238   0.02117   0.01308  -0.0987   0.9192   0.0354
  -3.500   0.0573   0.01964   0.01107  -0.0996   0.8982   0.0374
  -3.250   0.0880   0.01838   0.00955  -0.0999   0.8794   0.0402
  -3.000   0.1167   0.01768   0.00869  -0.0999   0.8624   0.0465
  -2.750   0.1451   0.01699   0.00786  -0.0998   0.8471   0.0567
  -2.500   0.1735   0.01640   0.00716  -0.0996   0.8326   0.0710
  -2.250   0.2017   0.01598   0.00673  -0.0995   0.8188   0.0930
  -2.000   0.2297   0.01568   0.00643  -0.0993   0.8058   0.1255
  -1.750   0.2576   0.01557   0.00625  -0.0991   0.7933   0.1596
  -1.500   0.2852   0.01547   0.00609  -0.0988   0.7811   0.1826
  -1.250   0.3126   0.01543   0.00597  -0.0984   0.7688   0.2083
  -0.750   0.3671   0.01525   0.00568  -0.0977   0.7431   0.2550
  -0.500   0.3947   0.01513   0.00552  -0.0974   0.7304   0.2753
  -0.250   0.4224   0.01504   0.00538  -0.0971   0.7188   0.2991
   0.000   0.4501   0.01494   0.00524  -0.0969   0.7087   0.3284
   0.500   0.5058   0.01441   0.00522  -0.0968   0.6881   0.4829
   0.750   0.5269   0.01338   0.00497  -0.0947   0.6788   1.0000
   1.000   0.5554   0.01352   0.00499  -0.0947   0.6678   1.0000
   1.250   0.5836   0.01367   0.00501  -0.0946   0.6573   1.0000
   1.500   0.6116   0.01383   0.00504  -0.0944   0.6473   1.0000
   1.750   0.6398   0.01398   0.00514  -0.0944   0.6359   1.0000
   2.000   0.6678   0.01414   0.00524  -0.0943   0.6250   1.0000
   2.250   0.6956   0.01431   0.00534  -0.0941   0.6149   1.0000
   2.500   0.7235   0.01449   0.00548  -0.0940   0.6042   1.0000
   2.750   0.7515   0.01468   0.00567  -0.0939   0.5931   1.0000
   3.000   0.7792   0.01488   0.00585  -0.0937   0.5826   1.0000
   3.250   0.8068   0.01509   0.00604  -0.0936   0.5723   1.0000
   3.500   0.8346   0.01532   0.00630  -0.0935   0.5610   1.0000
   3.750   0.8622   0.01555   0.00660  -0.0934   0.5504   1.0000
   4.000   0.8896   0.01579   0.00685  -0.0932   0.5402   1.0000
   4.250   0.9171   0.01604   0.00718  -0.0930   0.5286   1.0000
   4.500   0.9442   0.01628   0.00745  -0.0928   0.5137   1.0000
   4.750   0.9703   0.01648   0.00767  -0.0923   0.4893   1.0000
   5.000   0.9955   0.01674   0.00781  -0.0917   0.4547   1.0000
   5.250   1.0203   0.01714   0.00807  -0.0911   0.4173   1.0000
   5.500   1.0453   0.01760   0.00847  -0.0906   0.3775   1.0000
   5.750   1.0684   0.01834   0.00897  -0.0900   0.3141   1.0000
   6.000   1.0842   0.02054   0.01014  -0.0893   0.1434   1.0000
   6.250   1.1028   0.02238   0.01157  -0.0885   0.0847   1.0000
   6.500   1.1238   0.02364   0.01284  -0.0878   0.0710   1.0000
   6.750   1.1446   0.02482   0.01411  -0.0870   0.0644   1.0000
   7.000   1.1650   0.02592   0.01540  -0.0861   0.0600   1.0000
   7.250   1.1834   0.02719   0.01676  -0.0850   0.0564   1.0000
   7.500   1.2002   0.02857   0.01821  -0.0837   0.0536   1.0000
   7.750   1.2185   0.02970   0.01950  -0.0825   0.0510   1.0000
   8.000   1.2354   0.03100   0.02091  -0.0811   0.0491   1.0000
   8.250   1.2521   0.03238   0.02241  -0.0796   0.0476   1.0000
   8.500   1.2690   0.03384   0.02394  -0.0782   0.0463   1.0000
   8.750   1.2864   0.03542   0.02557  -0.0769   0.0450   1.0000
   9.000   1.3050   0.03722   0.02741  -0.0758   0.0439   1.0000
   9.250   1.3265   0.03966   0.02988  -0.0750   0.0427   1.0000
   9.500   1.3457   0.04133   0.03184  -0.0738   0.0415   1.0000
   9.750   1.3630   0.04310   0.03392  -0.0725   0.0396   1.0000
  10.000   1.3784   0.04501   0.03610  -0.0712   0.0374   1.0000
  10.250   1.3890   0.04654   0.03780  -0.0697   0.0348   1.0000
  10.500   1.4001   0.04879   0.04003  -0.0686   0.0324   1.0000
  10.750   1.4059   0.05109   0.04275  -0.0664   0.0307   1.0000
  11.000   1.4095   0.05391   0.04597  -0.0641   0.0293   1.0000
  11.250   1.4080   0.05674   0.04913  -0.0614   0.0280   1.0000
  11.500   1.4035   0.05944   0.05210  -0.0589   0.0269   1.0000
  11.750   1.3978   0.06217   0.05507  -0.0570   0.0260   1.0000
  12.000   1.3922   0.06497   0.05803  -0.0558   0.0251   1.0000
  12.250   1.3866   0.06810   0.06128  -0.0550   0.0243   1.0000
  12.500   1.3768   0.07245   0.06576  -0.0545   0.0237   1.0000
  12.750   1.3593   0.07733   0.07100  -0.0549   0.0234   1.0000
  13.000   1.3403   0.08286   0.07686  -0.0560   0.0231   1.0000
  13.250   1.3205   0.08896   0.08325  -0.0579   0.0229   1.0000
  13.500   1.2997   0.09561   0.09016  -0.0605   0.0229   1.0000
  13.750   1.2784   0.10281   0.09760  -0.0639   0.0229   1.0000
  14.000   1.2569   0.11055   0.10554  -0.0681   0.0229   1.0000
  14.250   1.2353   0.11893   0.11410  -0.0731   0.0231   1.0000
  14.500   1.2144   0.12803   0.12331  -0.0789   0.0233   1.0000
  14.750   1.1949   0.13768   0.13308  -0.0851   0.0235   1.0000
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