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ONERA HOR20 AIRFOIL (hor20-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: ONERA HOR20 AIRFOIL (hor20-il)
Reynolds number: 200,000
Max Cl/Cd: 63.43 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hor20-il-200000-n5.txt
Download as CSV file: xf-hor20-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8951   0.09553   0.09002  -0.0358   1.0000   0.0763
 -16.000  -0.8926   0.09237   0.08688  -0.0374   1.0000   0.0775
 -15.750  -0.8977   0.08797   0.08245  -0.0399   1.0000   0.0788
 -15.500  -0.9121   0.08217   0.07656  -0.0432   1.0000   0.0803
 -15.250  -0.9310   0.07577   0.07000  -0.0471   1.0000   0.0819
 -15.000  -0.9457   0.07019   0.06427  -0.0504   1.0000   0.0833
 -14.750  -0.9451   0.06711   0.06121  -0.0520   1.0000   0.0844
 -14.500  -0.9509   0.06323   0.05728  -0.0542   1.0000   0.0856
 -14.250  -0.9579   0.05921   0.05319  -0.0565   1.0000   0.0869
 -14.000  -0.9650   0.05520   0.04909  -0.0588   1.0000   0.0882
 -13.750  -0.9717   0.05129   0.04506  -0.0612   1.0000   0.0896
 -13.500  -0.9735   0.04807   0.04180  -0.0630   1.0000   0.0908
 -13.250  -0.9740   0.04503   0.03874  -0.0648   1.0000   0.0919
 -13.000  -0.9749   0.04187   0.03554  -0.0668   1.0000   0.0932
 -12.750  -0.9750   0.03877   0.03238  -0.0689   1.0000   0.0947
 -12.500  -0.9742   0.03573   0.02924  -0.0712   1.0000   0.0963
 -12.250  -0.9747   0.03270   0.02609  -0.0736   1.0000   0.0978
 -12.000  -0.9690   0.03055   0.02393  -0.0751   1.0000   0.0992
 -11.750  -0.9581   0.02913   0.02247  -0.0754   1.0000   0.1011
 -11.500  -0.9343   0.02788   0.02114  -0.0773   0.9801   0.1038
 -11.250  -0.9040   0.02673   0.01989  -0.0799   0.9605   0.1066
 -11.000  -0.8767   0.02575   0.01889  -0.0815   0.9405   0.1092
 -10.750  -0.8521   0.02494   0.01798  -0.0820   0.9187   0.1119
 -10.500  -0.8284   0.02422   0.01712  -0.0821   0.8986   0.1146
 -10.250  -0.8062   0.02352   0.01639  -0.0819   0.8794   0.1169
  -9.750  -0.7593   0.02236   0.01502  -0.0813   0.8441   0.1223
  -9.500  -0.7353   0.02181   0.01438  -0.0810   0.8290   0.1249
  -9.250  -0.7111   0.02132   0.01381  -0.0807   0.8145   0.1276
  -9.000  -0.6855   0.02086   0.01326  -0.0806   0.8011   0.1309
  -8.500  -0.6336   0.02000   0.01226  -0.0804   0.7765   0.1377
  -8.250  -0.6071   0.01965   0.01178  -0.0803   0.7650   0.1417
  -8.000  -0.5797   0.01927   0.01133  -0.0803   0.7536   0.1455
  -7.750  -0.5526   0.01892   0.01094  -0.0803   0.7426   0.1495
  -7.500  -0.5247   0.01861   0.01053  -0.0804   0.7322   0.1541
  -7.250  -0.4969   0.01829   0.01016  -0.0804   0.7210   0.1583
  -7.000  -0.4689   0.01801   0.00982  -0.0804   0.7111   0.1630
  -6.750  -0.4402   0.01775   0.00947  -0.0806   0.7007   0.1681
  -6.500  -0.4120   0.01750   0.00919  -0.0806   0.6909   0.1728
  -6.250  -0.3830   0.01727   0.00891  -0.0808   0.6809   0.1786
  -6.000  -0.3542   0.01706   0.00864  -0.0809   0.6705   0.1840
  -5.750  -0.3253   0.01689   0.00842  -0.0810   0.6613   0.1896
  -5.250  -0.2669   0.01655   0.00797  -0.0812   0.6422   0.2007
  -5.000  -0.2373   0.01641   0.00777  -0.0814   0.6328   0.2065
  -4.750  -0.2078   0.01627   0.00756  -0.0816   0.6234   0.2120
  -4.500  -0.1785   0.01616   0.00741  -0.0817   0.6153   0.2174
  -4.250  -0.1486   0.01604   0.00724  -0.0819   0.6062   0.2234
  -4.000  -0.1191   0.01594   0.00706  -0.0820   0.5975   0.2288
  -3.750  -0.0895   0.01583   0.00694  -0.0821   0.5898   0.2343
  -3.500  -0.0596   0.01575   0.00680  -0.0823   0.5817   0.2404
  -3.250  -0.0299   0.01567   0.00665  -0.0825   0.5741   0.2458
  -3.000  -0.0003   0.01558   0.00655  -0.0826   0.5669   0.2515
  -2.750   0.0296   0.01551   0.00645  -0.0828   0.5592   0.2577
  -2.500   0.0595   0.01546   0.00632  -0.0830   0.5522   0.2634
  -2.250   0.0890   0.01539   0.00624  -0.0831   0.5462   0.2693
  -2.000   0.1190   0.01532   0.00619  -0.0833   0.5393   0.2756
  -1.500   0.1783   0.01526   0.00605  -0.0836   0.5264   0.2879
  -1.250   0.2083   0.01523   0.00603  -0.0838   0.5205   0.2947
  -0.750   0.2677   0.01520   0.00599  -0.0840   0.5080   0.3081
  -0.500   0.2973   0.01524   0.00598  -0.0841   0.5024   0.3156
  -0.250   0.3273   0.01524   0.00599  -0.0843   0.4964   0.3229
   0.000   0.3569   0.01525   0.00604  -0.0844   0.4902   0.3308
   0.250   0.3864   0.01532   0.00605  -0.0845   0.4846   0.3397
   0.500   0.4159   0.01537   0.00611  -0.0846   0.4794   0.3481
   0.750   0.4457   0.01540   0.00620  -0.0847   0.4734   0.3577
   1.000   0.4753   0.01546   0.00626  -0.0848   0.4676   0.3670
   1.250   0.5045   0.01554   0.00634  -0.0848   0.4622   0.3768
   1.500   0.5340   0.01564   0.00641  -0.0849   0.4571   0.3866
   1.750   0.5634   0.01569   0.00655  -0.0850   0.4516   0.3955
   2.000   0.5926   0.01580   0.00663  -0.0850   0.4460   0.4055
   2.250   0.6215   0.01591   0.00672  -0.0850   0.4409   0.4139
   2.500   0.6506   0.01601   0.00686  -0.0850   0.4357   0.4227
   2.750   0.6799   0.01613   0.00697  -0.0851   0.4302   0.4318
   3.000   0.7085   0.01623   0.00711  -0.0850   0.4247   0.4396
   3.250   0.7369   0.01639   0.00722  -0.0849   0.4197   0.4483
   3.500   0.7658   0.01652   0.00737  -0.0849   0.4144   0.4559
   3.750   0.7942   0.01663   0.00755  -0.0849   0.4090   0.4631
   4.000   0.8224   0.01678   0.00770  -0.0847   0.4037   0.4713
   4.250   0.8502   0.01698   0.00782  -0.0846   0.3988   0.4790
   4.500   0.8784   0.01709   0.00804  -0.0845   0.3930   0.4859
   4.750   0.9061   0.01724   0.00822  -0.0843   0.3871   0.4933
   5.000   0.9335   0.01745   0.00837  -0.0841   0.3818   0.5007
   5.250   0.9607   0.01760   0.00859  -0.0839   0.3765   0.5079
   5.500   0.9880   0.01777   0.00882  -0.0836   0.3706   0.5162
   5.750   1.0147   0.01799   0.00901  -0.0834   0.3648   0.5240
   6.000   1.0408   0.01819   0.00923  -0.0830   0.3597   0.5313
   6.250   1.0675   0.01837   0.00951  -0.0827   0.3540   0.5403
   6.500   1.0934   0.01858   0.00977  -0.0823   0.3483   0.5508
   6.750   1.1185   0.01882   0.01003  -0.0817   0.3434   0.5632
   7.000   1.1438   0.01904   0.01034  -0.0813   0.3383   0.5759
   7.250   1.1687   0.01927   0.01065  -0.0807   0.3323   0.5902
   7.500   1.1924   0.01952   0.01096  -0.0800   0.3266   0.6059
   7.750   1.2159   0.01978   0.01130  -0.0793   0.3214   0.6255
   8.000   1.2391   0.02001   0.01169  -0.0785   0.3157   0.6559
   8.250   1.2602   0.02018   0.01207  -0.0773   0.3103   0.7238
   8.500   1.2774   0.02014   0.01233  -0.0751   0.3057   1.0000
   8.750   1.3002   0.02054   0.01277  -0.0744   0.3005   1.0000
   9.000   1.3213   0.02099   0.01322  -0.0734   0.2952   1.0000
   9.250   1.3403   0.02151   0.01368  -0.0721   0.2904   1.0000
   9.500   1.3594   0.02201   0.01420  -0.0709   0.2853   1.0000
   9.750   1.3765   0.02254   0.01475  -0.0694   0.2799   1.0000
  10.000   1.3896   0.02316   0.01535  -0.0673   0.2751   1.0000
  10.250   1.4032   0.02386   0.01603  -0.0655   0.2707   1.0000
  10.500   1.4181   0.02456   0.01679  -0.0640   0.2658   1.0000
  10.750   1.4311   0.02538   0.01763  -0.0624   0.2611   1.0000
  11.000   1.4425   0.02634   0.01855  -0.0608   0.2569   1.0000
  11.250   1.4560   0.02726   0.01953  -0.0595   0.2527   1.0000
  11.500   1.4682   0.02830   0.02062  -0.0583   0.2481   1.0000
  11.750   1.4784   0.02949   0.02182  -0.0570   0.2437   1.0000
  12.000   1.4876   0.03082   0.02313  -0.0558   0.2397   1.0000
  12.250   1.4986   0.03210   0.02450  -0.0548   0.2352   1.0000
  12.500   1.5073   0.03358   0.02603  -0.0539   0.2306   1.0000
  12.750   1.5140   0.03524   0.02768  -0.0529   0.2265   1.0000
  13.000   1.5216   0.03691   0.02941  -0.0521   0.2224   1.0000
  13.250   1.5285   0.03870   0.03127  -0.0514   0.2179   1.0000
  13.500   1.5335   0.04066   0.03327  -0.0507   0.2138   1.0000
  13.750   1.5372   0.04274   0.03533  -0.0500   0.2103   1.0000
  14.000   1.5423   0.04482   0.03753  -0.0495   0.2062   1.0000
  14.250   1.5451   0.04713   0.03991  -0.0491   0.2021   1.0000
  14.500   1.5462   0.04960   0.04239  -0.0486   0.1983   1.0000
  14.750   1.5478   0.05208   0.04492  -0.0483   0.1948   1.0000
  15.000   1.5491   0.05475   0.04768  -0.0481   0.1908   1.0000
  15.250   1.5488   0.05760   0.05059  -0.0480   0.1869   1.0000
  15.500   1.5475   0.06054   0.05352  -0.0480   0.1834   1.0000
  15.750   1.5467   0.06364   0.05672  -0.0481   0.1795   1.0000
  16.000   1.5442   0.06696   0.06012  -0.0484   0.1753   1.0000
  16.250   1.5408   0.07037   0.06354  -0.0487   0.1715   1.0000
  16.500   1.5377   0.07386   0.06710  -0.0491   0.1678   1.0000
  16.750   1.5338   0.07752   0.07085  -0.0497   0.1638   1.0000
  17.000   1.5303   0.08110   0.07446  -0.0502   0.1604   1.0000
  17.250   1.5273   0.08461   0.07799  -0.0507   0.1573   1.0000
  17.500   1.5227   0.08850   0.08200  -0.0515   0.1537   1.0000
  17.750   1.5173   0.09250   0.08606  -0.0524   0.1502   1.0000
  18.000   1.5142   0.09610   0.08966  -0.0531   0.1470   1.0000
  18.250   1.5081   0.10032   0.09400  -0.0542   0.1437   1.0000
  18.500   1.5024   0.10447   0.09823  -0.0553   0.1404   1.0000
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