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MH 117 9.8% (mh117-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 117 9.8% (mh117-il)
Reynolds number: 500,000
Max Cl/Cd: 90.42 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh117-il-500000-n5.txt
Download as CSV file: xf-mh117-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 117  9.8%                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.5846   0.08378   0.08132  -0.0322   1.0000   0.0033
 -11.250  -0.6203   0.07305   0.07059  -0.0380   1.0000   0.0032
 -11.000  -0.6506   0.06375   0.06126  -0.0434   1.0000   0.0030
 -10.750  -0.6889   0.05261   0.05006  -0.0506   1.0000   0.0030
 -10.500  -0.7197   0.04076   0.03803  -0.0623   1.0000   0.0028
 -10.250  -0.7342   0.03574   0.03273  -0.0642   1.0000   0.0028
 -10.000  -0.7391   0.03206   0.02875  -0.0639   1.0000   0.0028
  -9.750  -0.7363   0.02926   0.02568  -0.0628   1.0000   0.0029
  -9.500  -0.7296   0.02692   0.02306  -0.0615   1.0000   0.0030
  -9.250  -0.7081   0.02458   0.02041  -0.0626   0.9973   0.0031
  -9.000  -0.6800   0.02251   0.01804  -0.0646   0.9932   0.0032
  -8.750  -0.6519   0.02102   0.01628  -0.0659   0.9883   0.0034
  -8.500  -0.6221   0.01959   0.01463  -0.0674   0.9839   0.0035
  -8.250  -0.5942   0.01809   0.01293  -0.0684   0.9781   0.0036
  -8.000  -0.5650   0.01682   0.01149  -0.0696   0.9719   0.0039
  -7.750  -0.5348   0.01589   0.01043  -0.0706   0.9655   0.0041
  -7.500  -0.5039   0.01511   0.00954  -0.0716   0.9580   0.0043
  -7.250  -0.4729   0.01438   0.00868  -0.0726   0.9498   0.0045
  -7.000  -0.4407   0.01374   0.00792  -0.0738   0.9413   0.0049
  -6.750  -0.4105   0.01322   0.00729  -0.0744   0.9301   0.0054
  -6.500  -0.3816   0.01257   0.00652  -0.0748   0.9180   0.0061
  -6.250  -0.3539   0.01204   0.00587  -0.0749   0.9050   0.0068
  -6.000  -0.3268   0.01160   0.00531  -0.0747   0.8919   0.0076
  -5.750  -0.3002   0.01117   0.00474  -0.0743   0.8788   0.0092
  -5.500  -0.2739   0.01075   0.00425  -0.0740   0.8664   0.0130
  -5.250  -0.2478   0.01034   0.00382  -0.0737   0.8542   0.0225
  -5.000  -0.2215   0.00999   0.00350  -0.0734   0.8425   0.0372
  -4.750  -0.1950   0.00971   0.00324  -0.0732   0.8312   0.0529
  -4.500  -0.1681   0.00949   0.00302  -0.0729   0.8204   0.0665
  -4.250  -0.1412   0.00930   0.00280  -0.0727   0.8101   0.0802
  -4.000  -0.1142   0.00913   0.00261  -0.0725   0.7998   0.0935
  -3.750  -0.0869   0.00897   0.00242  -0.0724   0.7897   0.1048
  -3.500  -0.0596   0.00882   0.00226  -0.0722   0.7802   0.1189
  -3.000  -0.0049   0.00855   0.00196  -0.0719   0.7613   0.1510
  -2.750   0.0224   0.00842   0.00184  -0.0718   0.7523   0.1706
  -2.500   0.0498   0.00831   0.00174  -0.0716   0.7433   0.1897
  -2.250   0.0774   0.00819   0.00164  -0.0715   0.7342   0.2124
  -2.000   0.1048   0.00807   0.00156  -0.0714   0.7257   0.2388
  -1.750   0.1323   0.00797   0.00149  -0.0713   0.7165   0.2641
  -1.500   0.1597   0.00786   0.00143  -0.0712   0.7075   0.2948
  -1.250   0.1871   0.00777   0.00138  -0.0711   0.6982   0.3250
  -1.000   0.2144   0.00766   0.00134  -0.0709   0.6882   0.3607
  -0.750   0.2417   0.00755   0.00132  -0.0708   0.6783   0.4015
  -0.500   0.2689   0.00745   0.00130  -0.0707   0.6685   0.4443
  -0.250   0.2960   0.00735   0.00130  -0.0705   0.6584   0.4908
   0.000   0.3230   0.00723   0.00131  -0.0703   0.6481   0.5425
   0.250   0.3498   0.00712   0.00134  -0.0701   0.6380   0.5961
   0.500   0.3763   0.00702   0.00137  -0.0697   0.6277   0.6529
   1.000   0.4277   0.00680   0.00148  -0.0685   0.6055   0.7719
   1.250   0.4520   0.00671   0.00154  -0.0675   0.5941   0.8324
   1.500   0.4753   0.00666   0.00160  -0.0662   0.5823   0.8925
   1.750   0.5060   0.00666   0.00163  -0.0665   0.5691   0.9491
   2.000   0.5452   0.00673   0.00166  -0.0689   0.5532   0.9932
   2.250   0.5734   0.00685   0.00171  -0.0690   0.5378   1.0000
   2.500   0.5996   0.00698   0.00178  -0.0686   0.5211   1.0000
   2.750   0.6257   0.00714   0.00186  -0.0683   0.5029   1.0000
   3.000   0.6518   0.00731   0.00197  -0.0679   0.4827   1.0000
   3.250   0.6774   0.00752   0.00208  -0.0675   0.4584   1.0000
   3.750   0.7279   0.00805   0.00239  -0.0666   0.4012   1.0000
   4.000   0.7525   0.00838   0.00258  -0.0660   0.3668   1.0000
   4.250   0.7769   0.00875   0.00279  -0.0655   0.3339   1.0000
   4.500   0.8014   0.00912   0.00303  -0.0650   0.3030   1.0000
   4.750   0.8257   0.00951   0.00329  -0.0644   0.2714   1.0000
   5.000   0.8501   0.00989   0.00356  -0.0639   0.2431   1.0000
   5.500   0.8990   0.01062   0.00411  -0.0629   0.1977   1.0000
   5.750   0.9230   0.01103   0.00443  -0.0624   0.1745   1.0000
   6.000   0.9473   0.01141   0.00475  -0.0619   0.1563   1.0000
   6.250   0.9710   0.01183   0.00510  -0.0613   0.1379   1.0000
   6.500   0.9947   0.01225   0.00545  -0.0607   0.1203   1.0000
   6.750   1.0183   0.01267   0.00582  -0.0601   0.1056   1.0000
   7.000   1.0415   0.01311   0.00622  -0.0594   0.0915   1.0000
   7.250   1.0645   0.01356   0.00665  -0.0588   0.0795   1.0000
   7.500   1.0873   0.01402   0.00708  -0.0580   0.0695   1.0000
   7.750   1.1096   0.01451   0.00754  -0.0573   0.0603   1.0000
   8.000   1.1325   0.01493   0.00799  -0.0566   0.0543   1.0000
   8.250   1.1543   0.01544   0.00850  -0.0557   0.0482   1.0000
   8.500   1.1763   0.01591   0.00899  -0.0549   0.0427   1.0000
   8.750   1.1971   0.01646   0.00956  -0.0540   0.0368   1.0000
   9.000   1.2179   0.01699   0.01010  -0.0530   0.0316   1.0000
   9.250   1.2377   0.01757   0.01068  -0.0519   0.0267   1.0000
   9.500   1.2569   0.01818   0.01129  -0.0508   0.0221   1.0000
   9.750   1.2755   0.01881   0.01194  -0.0496   0.0183   1.0000
  10.000   1.2926   0.01952   0.01265  -0.0482   0.0146   1.0000
  10.250   1.3095   0.02019   0.01338  -0.0467   0.0120   1.0000
  10.500   1.3233   0.02099   0.01419  -0.0449   0.0095   1.0000
  10.750   1.3354   0.02175   0.01502  -0.0427   0.0072   1.0000
  11.000   1.3456   0.02265   0.01597  -0.0403   0.0057   1.0000
  11.250   1.3551   0.02359   0.01697  -0.0380   0.0045   1.0000
  11.500   1.3637   0.02463   0.01807  -0.0357   0.0037   1.0000
  11.750   1.3728   0.02567   0.01922  -0.0337   0.0032   1.0000
  12.000   1.3807   0.02684   0.02047  -0.0318   0.0028   1.0000
  12.250   1.3858   0.02828   0.02202  -0.0298   0.0025   1.0000
  12.500   1.3910   0.02977   0.02362  -0.0280   0.0023   1.0000
  12.750   1.3969   0.03128   0.02524  -0.0265   0.0022   1.0000
  13.000   1.4018   0.03295   0.02703  -0.0252   0.0021   1.0000
  13.250   1.4049   0.03488   0.02909  -0.0239   0.0019   1.0000
  13.500   1.4076   0.03692   0.03128  -0.0230   0.0019   1.0000
  13.750   1.4088   0.03923   0.03373  -0.0222   0.0018   1.0000
  14.000   1.4099   0.04164   0.03626  -0.0217   0.0017   1.0000
  14.250   1.4086   0.04446   0.03921  -0.0214   0.0017   1.0000
  14.500   1.4061   0.04751   0.04241  -0.0214   0.0016   1.0000
  14.750   1.4021   0.05093   0.04597  -0.0217   0.0015   1.0000
  15.000   1.3982   0.05447   0.04964  -0.0223   0.0015   1.0000
  15.250   1.3902   0.05875   0.05407  -0.0234   0.0015   1.0000
  15.500   1.3823   0.06327   0.05875  -0.0248   0.0015   1.0000
  15.750   1.3721   0.06838   0.06401  -0.0268   0.0014   1.0000
  16.000   1.3611   0.07393   0.06970  -0.0291   0.0014   1.0000
  16.250   1.3459   0.08053   0.07647  -0.0322   0.0014   1.0000
  16.500   1.3316   0.08729   0.08340  -0.0356   0.0014   1.0000
  16.750   1.3121   0.09546   0.09174  -0.0400   0.0013   1.0000
  17.000   1.2944   0.10358   0.10002  -0.0444   0.0014   1.0000
  17.250   1.2742   0.11254   0.10914  -0.0494   0.0014   1.0000
  17.500   1.2546   0.12160   0.11836  -0.0545   0.0014   1.0000
  17.750   1.2308   0.13189   0.12880  -0.0604   0.0014   1.0000
  18.000   1.2089   0.14203   0.13909  -0.0663   0.0015   1.0000
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