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ONERA HOR20 AIRFOIL (hor20-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: ONERA HOR20 AIRFOIL (hor20-il)
Reynolds number: 500,000
Max Cl/Cd: 83.87 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hor20-il-500000-n5.txt
Download as CSV file: xf-hor20-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: ONERA HOR20 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.0107   0.10294   0.09867  -0.0278   1.0000   0.0548
 -17.500  -1.0182   0.09829   0.09399  -0.0302   1.0000   0.0557
 -17.250  -1.0275   0.09339   0.08903  -0.0328   1.0000   0.0567
 -17.000  -1.0335   0.08905   0.08463  -0.0351   1.0000   0.0577
 -16.750  -1.0410   0.08453   0.08003  -0.0374   1.0000   0.0586
 -16.500  -1.0478   0.08015   0.07560  -0.0397   1.0000   0.0595
 -16.250  -1.0597   0.07514   0.07054  -0.0423   1.0000   0.0604
 -16.000  -1.0709   0.07024   0.06559  -0.0449   1.0000   0.0613
 -15.750  -1.0810   0.06562   0.06089  -0.0474   1.0000   0.0623
 -15.500  -1.0897   0.06128   0.05648  -0.0497   1.0000   0.0632
 -15.250  -1.0996   0.05700   0.05212  -0.0519   1.0000   0.0641
 -15.000  -1.1115   0.05256   0.04760  -0.0542   1.0000   0.0648
 -14.750  -1.1266   0.04778   0.04275  -0.0568   1.0000   0.0655
 -14.500  -1.1400   0.04321   0.03811  -0.0594   1.0000   0.0663
 -14.250  -1.1516   0.03881   0.03363  -0.0620   1.0000   0.0671
 -14.000  -1.1611   0.03454   0.02928  -0.0647   1.0000   0.0680
 -13.750  -1.1703   0.03005   0.02469  -0.0683   1.0000   0.0688
 -13.500  -1.1616   0.02637   0.02085  -0.0732   1.0000   0.0699
 -13.250  -1.1471   0.02471   0.01913  -0.0743   1.0000   0.0711
 -13.000  -1.1216   0.02343   0.01779  -0.0764   0.9703   0.0726
 -12.750  -1.0944   0.02246   0.01674  -0.0780   0.9480   0.0742
 -12.500  -1.0719   0.02172   0.01591  -0.0781   0.9234   0.0757
 -12.250  -1.0509   0.02103   0.01512  -0.0777   0.8986   0.0770
 -12.000  -1.0296   0.02036   0.01436  -0.0774   0.8761   0.0786
 -11.750  -1.0067   0.01981   0.01370  -0.0771   0.8547   0.0804
 -11.500  -0.9827   0.01934   0.01311  -0.0768   0.8347   0.0822
 -11.250  -0.9580   0.01885   0.01252  -0.0767   0.8172   0.0839
 -11.000  -0.9328   0.01835   0.01195  -0.0767   0.8028   0.0858
 -10.500  -0.8799   0.01757   0.01099  -0.0767   0.7766   0.0897
 -10.250  -0.8533   0.01715   0.01051  -0.0767   0.7649   0.0915
 -10.000  -0.8260   0.01675   0.01006  -0.0768   0.7544   0.0938
  -9.750  -0.7984   0.01643   0.00966  -0.0769   0.7427   0.0963
  -9.500  -0.7706   0.01608   0.00926  -0.0770   0.7326   0.0988
  -9.250  -0.7426   0.01572   0.00887  -0.0772   0.7222   0.1018
  -9.000  -0.7143   0.01545   0.00852  -0.0773   0.7124   0.1045
  -8.750  -0.6856   0.01515   0.00817  -0.0775   0.7022   0.1069
  -8.500  -0.6572   0.01486   0.00783  -0.0776   0.6916   0.1099
  -8.250  -0.6281   0.01460   0.00753  -0.0778   0.6827   0.1130
  -8.000  -0.5991   0.01433   0.00723  -0.0780   0.6730   0.1162
  -7.750  -0.5701   0.01409   0.00694  -0.0782   0.6635   0.1200
  -7.500  -0.5405   0.01388   0.00669  -0.0784   0.6537   0.1237
  -7.250  -0.5114   0.01364   0.00641  -0.0786   0.6433   0.1278
  -7.000  -0.4817   0.01344   0.00618  -0.0788   0.6347   0.1319
  -6.750  -0.4520   0.01324   0.00595  -0.0791   0.6249   0.1358
  -6.500  -0.4224   0.01307   0.00573  -0.0793   0.6153   0.1403
  -6.250  -0.3924   0.01292   0.00554  -0.0795   0.6057   0.1444
  -6.000  -0.3626   0.01274   0.00533  -0.0798   0.5961   0.1489
  -5.750  -0.3325   0.01260   0.00516  -0.0800   0.5877   0.1537
  -5.500  -0.3025   0.01247   0.00499  -0.0803   0.5780   0.1581
  -5.250  -0.2725   0.01234   0.00482  -0.0805   0.5690   0.1632
  -5.000  -0.2422   0.01223   0.00468  -0.0808   0.5610   0.1681
  -4.750  -0.2120   0.01210   0.00454  -0.0810   0.5529   0.1740
  -4.500  -0.1818   0.01202   0.00442  -0.0813   0.5453   0.1805
  -4.250  -0.1515   0.01189   0.00432  -0.0816   0.5376   0.1876
  -4.000  -0.1212   0.01183   0.00422  -0.0818   0.5298   0.1943
  -3.750  -0.0909   0.01176   0.00413  -0.0821   0.5235   0.2002
  -3.500  -0.0604   0.01169   0.00406  -0.0823   0.5179   0.2063
  -3.250  -0.0299   0.01165   0.00399  -0.0826   0.5116   0.2116
  -3.000   0.0003   0.01160   0.00392  -0.0828   0.5053   0.2171
  -2.750   0.0308   0.01157   0.00387  -0.0831   0.5000   0.2225
  -2.500   0.0614   0.01154   0.00382  -0.0833   0.4950   0.2270
  -2.250   0.0918   0.01149   0.00377  -0.0836   0.4896   0.2324
  -2.000   0.1221   0.01148   0.00374  -0.0838   0.4839   0.2378
  -1.750   0.1526   0.01148   0.00371  -0.0840   0.4788   0.2426
  -1.500   0.1832   0.01143   0.00367  -0.0843   0.4733   0.2476
  -1.250   0.2136   0.01140   0.00364  -0.0845   0.4672   0.2532
  -1.000   0.2438   0.01142   0.00362  -0.0847   0.4613   0.2584
  -0.750   0.2743   0.01142   0.00361  -0.0849   0.4565   0.2627
  -0.500   0.3047   0.01137   0.00359  -0.0852   0.4511   0.2688
  -0.250   0.3350   0.01137   0.00359  -0.0854   0.4453   0.2748
   0.250   0.3955   0.01139   0.00360  -0.0858   0.4354   0.2866
   0.500   0.4258   0.01139   0.00362  -0.0860   0.4304   0.2938
   0.750   0.4559   0.01142   0.00364  -0.0862   0.4249   0.3005
   1.000   0.4857   0.01147   0.00368  -0.0864   0.4194   0.3090
   1.250   0.5160   0.01148   0.00373  -0.0866   0.4150   0.3191
   1.500   0.5461   0.01150   0.00379  -0.0867   0.4101   0.3292
   1.750   0.5760   0.01156   0.00385  -0.0869   0.4047   0.3401
   2.000   0.6055   0.01164   0.00393  -0.0870   0.3992   0.3507
   2.250   0.6356   0.01168   0.00400  -0.0872   0.3949   0.3618
   2.500   0.6654   0.01173   0.00409  -0.0873   0.3901   0.3713
   2.750   0.6950   0.01182   0.00418  -0.0874   0.3850   0.3807
   3.000   0.7242   0.01194   0.00429  -0.0875   0.3797   0.3891
   3.250   0.7540   0.01200   0.00439  -0.0876   0.3749   0.3982
   3.500   0.7834   0.01211   0.00450  -0.0876   0.3691   0.4059
   3.750   0.8123   0.01224   0.00462  -0.0877   0.3633   0.4127
   4.000   0.8414   0.01236   0.00475  -0.0877   0.3581   0.4209
   4.250   0.8706   0.01247   0.00487  -0.0877   0.3526   0.4283
   4.500   0.8993   0.01262   0.00501  -0.0877   0.3466   0.4340
   4.750   0.9276   0.01278   0.00517  -0.0876   0.3412   0.4404
   5.000   0.9565   0.01289   0.00531  -0.0876   0.3361   0.4474
   5.250   0.9850   0.01305   0.00547  -0.0876   0.3308   0.4536
   5.500   1.0128   0.01324   0.00565  -0.0874   0.3256   0.4596
   5.750   1.0410   0.01339   0.00583  -0.0873   0.3208   0.4657
   6.000   1.0690   0.01356   0.00601  -0.0872   0.3147   0.4717
   6.250   1.0960   0.01379   0.00621  -0.0870   0.3082   0.4769
   6.500   1.1234   0.01398   0.00642  -0.0868   0.3029   0.4829
   6.750   1.1507   0.01416   0.00663  -0.0866   0.2972   0.4901
   7.000   1.1770   0.01442   0.00687  -0.0862   0.2913   0.4975
   7.250   1.2036   0.01464   0.00711  -0.0859   0.2866   0.5044
   7.500   1.2302   0.01484   0.00736  -0.0856   0.2817   0.5121
   7.750   1.2556   0.01511   0.00763  -0.0852   0.2759   0.5203
   8.000   1.2806   0.01539   0.00793  -0.0847   0.2701   0.5298
   8.250   1.3057   0.01565   0.00822  -0.0842   0.2638   0.5407
   8.500   1.3290   0.01600   0.00856  -0.0834   0.2575   0.5495
   8.750   1.3532   0.01628   0.00889  -0.0828   0.2524   0.5597
   9.000   1.3767   0.01658   0.00923  -0.0821   0.2472   0.5712
   9.250   1.3985   0.01694   0.00963  -0.0812   0.2422   0.5877
   9.500   1.4206   0.01725   0.01003  -0.0803   0.2380   0.6129
   9.750   1.4422   0.01749   0.01045  -0.0793   0.2333   0.6718
  10.000   1.4551   0.01735   0.01088  -0.0765   0.2288   1.0000
  10.250   1.4709   0.01789   0.01139  -0.0747   0.2245   1.0000
  10.500   1.4883   0.01834   0.01187  -0.0731   0.2205   1.0000
  10.750   1.5040   0.01893   0.01246  -0.0714   0.2160   1.0000
  11.000   1.5177   0.01967   0.01320  -0.0697   0.2117   1.0000
  11.250   1.5333   0.02036   0.01391  -0.0683   0.2082   1.0000
  11.500   1.5489   0.02111   0.01468  -0.0670   0.2041   1.0000
  11.750   1.5617   0.02206   0.01564  -0.0656   0.1995   1.0000
  12.000   1.5736   0.02314   0.01672  -0.0643   0.1952   1.0000
  12.250   1.5874   0.02416   0.01776  -0.0632   0.1906   1.0000
  12.500   1.5979   0.02546   0.01907  -0.0621   0.1859   1.0000
  12.750   1.6073   0.02691   0.02054  -0.0611   0.1818   1.0000
  13.000   1.6182   0.02830   0.02195  -0.0602   0.1773   1.0000
  13.250   1.6249   0.03008   0.02375  -0.0593   0.1725   1.0000
  13.500   1.6316   0.03191   0.02560  -0.0585   0.1684   1.0000
  13.750   1.6391   0.03371   0.02744  -0.0578   0.1644   1.0000
  14.000   1.6428   0.03590   0.02966  -0.0571   0.1604   1.0000
  14.250   1.6453   0.03824   0.03203  -0.0565   0.1570   1.0000
  14.500   1.6499   0.04040   0.03423  -0.0559   0.1534   1.0000
  14.750   1.6509   0.04294   0.03681  -0.0554   0.1497   1.0000
  15.000   1.6478   0.04593   0.03983  -0.0549   0.1465   1.0000
  15.250   1.6506   0.04839   0.04236  -0.0545   0.1436   1.0000
  15.500   1.6510   0.05117   0.04519  -0.0543   0.1405   1.0000
  15.750   1.6487   0.05426   0.04833  -0.0541   0.1376   1.0000
  16.000   1.6452   0.05757   0.05169  -0.0540   0.1350   1.0000
  16.250   1.6441   0.06067   0.05486  -0.0540   0.1321   1.0000
  16.500   1.6401   0.06414   0.05837  -0.0541   0.1289   1.0000
  16.750   1.6334   0.06795   0.06222  -0.0543   0.1260   1.0000
  17.000   1.6301   0.07142   0.06575  -0.0545   0.1235   1.0000
  17.250   1.6274   0.07484   0.06923  -0.0548   0.1208   1.0000
  17.500   1.6216   0.07865   0.07309  -0.0552   0.1181   1.0000
  17.750   1.6131   0.08286   0.07735  -0.0557   0.1158   1.0000
  18.000   1.6122   0.08612   0.08068  -0.0561   0.1136   1.0000
  18.250   1.6076   0.08991   0.08453  -0.0567   0.1112   1.0000
  18.500   1.6023   0.09377   0.08844  -0.0573   0.1087   1.0000
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