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MH 104 15.28% (mh104-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 104 15.28% (mh104-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.82 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh104-il-1000000.txt
Download as CSV file: xf-mh104-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 104  15.28%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7385   0.12999   0.12810   0.0073   1.0000   0.0059
 -16.250  -0.7849   0.11387   0.11177  -0.0019   1.0000   0.0058
 -16.000  -0.8162   0.10236   0.10010  -0.0088   1.0000   0.0057
 -15.750  -0.8767   0.08617   0.08355  -0.0185   1.0000   0.0054
 -15.500  -0.8868   0.08028   0.07759  -0.0221   1.0000   0.0055
 -15.250  -0.9122   0.07210   0.06921  -0.0269   1.0000   0.0054
 -15.000  -0.9156   0.06778   0.06485  -0.0296   1.0000   0.0055
 -14.750  -0.9433   0.06001   0.05684  -0.0338   1.0000   0.0053
 -14.500  -0.9558   0.05471   0.05141  -0.0368   1.0000   0.0053
 -14.250  -0.9618   0.05050   0.04709  -0.0391   1.0000   0.0054
 -14.000  -0.9669   0.04662   0.04310  -0.0410   1.0000   0.0054
 -13.750  -0.9728   0.04291   0.03926  -0.0426   1.0000   0.0054
 -13.500  -0.9878   0.03844   0.03459  -0.0434   1.0000   0.0053
 -13.250  -0.9845   0.03633   0.03243  -0.0438   1.0000   0.0054
 -13.000  -0.9842   0.03411   0.03011  -0.0437   1.0000   0.0055
 -12.750  -0.9876   0.03172   0.02759  -0.0428   1.0000   0.0055
 -12.500  -0.9877   0.02983   0.02560  -0.0414   1.0000   0.0055
 -12.250  -0.9871   0.02816   0.02382  -0.0396   1.0000   0.0055
 -12.000  -0.9871   0.02652   0.02207  -0.0373   1.0000   0.0055
 -11.750  -0.9839   0.02523   0.02068  -0.0348   1.0000   0.0055
 -11.500  -0.9757   0.02435   0.01974  -0.0325   1.0000   0.0056
 -11.250  -0.9714   0.02323   0.01853  -0.0295   1.0000   0.0056
 -11.000  -0.9658   0.02224   0.01746  -0.0264   1.0000   0.0057
 -10.750  -0.9560   0.02132   0.01647  -0.0238   1.0000   0.0057
 -10.500  -0.9424   0.02049   0.01557  -0.0219   1.0000   0.0057
 -10.250  -0.9271   0.01959   0.01460  -0.0203   0.9867   0.0058
 -10.000  -0.8964   0.01874   0.01349  -0.0215   0.8890   0.0059
  -9.750  -0.8835   0.01812   0.01265  -0.0190   0.8471   0.0060
  -9.500  -0.8662   0.01757   0.01196  -0.0172   0.8187   0.0061
  -9.250  -0.8485   0.01695   0.01119  -0.0156   0.7962   0.0061
  -9.000  -0.8282   0.01647   0.01060  -0.0143   0.7766   0.0063
  -8.750  -0.8074   0.01598   0.00999  -0.0131   0.7586   0.0064
  -8.500  -0.7855   0.01556   0.00945  -0.0121   0.7418   0.0066
  -8.250  -0.7657   0.01490   0.00868  -0.0108   0.7260   0.0067
  -8.000  -0.7459   0.01420   0.00785  -0.0094   0.7117   0.0069
  -7.750  -0.7238   0.01367   0.00724  -0.0084   0.6985   0.0073
  -7.500  -0.7002   0.01327   0.00676  -0.0076   0.6857   0.0076
  -7.250  -0.6761   0.01291   0.00631  -0.0069   0.6732   0.0080
  -7.000  -0.6514   0.01259   0.00591  -0.0062   0.6605   0.0086
  -6.750  -0.6274   0.01215   0.00540  -0.0055   0.6484   0.0098
  -6.500  -0.6022   0.01186   0.00505  -0.0049   0.6370   0.0116
  -6.250  -0.5776   0.01148   0.00463  -0.0042   0.6261   0.0157
  -6.000  -0.5527   0.01113   0.00428  -0.0036   0.6154   0.0234
  -5.750  -0.5278   0.01077   0.00395  -0.0031   0.6054   0.0356
  -5.500  -0.5037   0.01035   0.00362  -0.0024   0.5954   0.0578
  -5.250  -0.4800   0.00985   0.00327  -0.0017   0.5853   0.0935
  -5.000  -0.4563   0.00938   0.00297  -0.0010   0.5759   0.1379
  -4.750  -0.4318   0.00901   0.00274  -0.0005   0.5662   0.1785
  -4.500  -0.4061   0.00872   0.00257   0.0000   0.5573   0.2133
  -4.250  -0.3801   0.00851   0.00243   0.0003   0.5485   0.2421
  -4.000  -0.3534   0.00833   0.00231   0.0006   0.5401   0.2661
  -3.750  -0.3265   0.00821   0.00220   0.0008   0.5319   0.2856
  -3.500  -0.2992   0.00809   0.00210   0.0010   0.5236   0.3035
  -3.250  -0.2723   0.00797   0.00202   0.0013   0.5156   0.3264
  -3.000  -0.2452   0.00785   0.00194   0.0015   0.5078   0.3475
  -2.750  -0.2177   0.00778   0.00186   0.0017   0.5005   0.3637
  -2.500  -0.1901   0.00770   0.00180   0.0018   0.4935   0.3792
  -2.250  -0.1627   0.00764   0.00174   0.0020   0.4866   0.3952
  -2.000  -0.1350   0.00756   0.00168   0.0021   0.4806   0.4118
  -1.750  -0.1075   0.00751   0.00164   0.0022   0.4741   0.4292
  -1.500  -0.0799   0.00745   0.00160   0.0024   0.4683   0.4470
  -1.250  -0.0524   0.00738   0.00156   0.0025   0.4623   0.4661
  -1.000  -0.0252   0.00733   0.00154   0.0027   0.4566   0.4865
  -0.750   0.0023   0.00725   0.00152   0.0029   0.4521   0.5088
  -0.500   0.0295   0.00718   0.00150   0.0031   0.4472   0.5332
  -0.250   0.0565   0.00713   0.00149   0.0033   0.4422   0.5594
   0.000   0.0834   0.00705   0.00149   0.0036   0.4379   0.5892
   0.250   0.1101   0.00696   0.00149   0.0039   0.4336   0.6205
   0.500   0.1366   0.00690   0.00151   0.0042   0.4293   0.6517
   0.750   0.1627   0.00685   0.00153   0.0047   0.4249   0.6849
   1.250   0.2154   0.00669   0.00159   0.0055   0.4177   0.7510
   1.500   0.2412   0.00664   0.00163   0.0061   0.4137   0.7845
   1.750   0.2670   0.00662   0.00169   0.0066   0.4096   0.8166
   2.000   0.2938   0.00657   0.00174   0.0070   0.4067   0.8474
   2.250   0.3211   0.00654   0.00181   0.0073   0.4032   0.8772
   2.500   0.3503   0.00656   0.00189   0.0072   0.3995   0.9033
   2.750   0.3813   0.00667   0.00200   0.0067   0.3952   0.9244
   3.000   0.4156   0.00673   0.00210   0.0054   0.3922   0.9397
   3.250   0.4526   0.00683   0.00221   0.0036   0.3887   0.9495
   3.500   0.4868   0.00694   0.00231   0.0023   0.3851   0.9575
   3.750   0.5209   0.00710   0.00243   0.0010   0.3810   0.9639
   4.000   0.5530   0.00721   0.00255   0.0002   0.3777   0.9699
   4.250   0.5913   0.00730   0.00265  -0.0020   0.3742   0.9722
   4.500   0.6278   0.00741   0.00275  -0.0039   0.3701   0.9752
   4.750   0.6610   0.00757   0.00288  -0.0050   0.3658   0.9794
   5.000   0.6946   0.00768   0.00300  -0.0063   0.3621   0.9827
   5.250   0.7330   0.00775   0.00308  -0.0085   0.3578   0.9843
   5.500   0.7702   0.00786   0.00318  -0.0106   0.3531   0.9863
   5.750   0.8064   0.00799   0.00330  -0.0125   0.3482   0.9887
   6.000   0.8419   0.00805   0.00340  -0.0141   0.3438   0.9913
   6.250   0.8765   0.00817   0.00351  -0.0157   0.3383   0.9937
   6.500   0.9151   0.00827   0.00361  -0.0181   0.3326   0.9954
   6.750   0.9545   0.00833   0.00369  -0.0207   0.3263   0.9976
   7.000   0.9928   0.00847   0.00381  -0.0231   0.3193   0.9996
   7.250   1.0205   0.00854   0.00391  -0.0232   0.3127   1.0000
   7.750   1.0668   0.00883   0.00419  -0.0217   0.2969   1.0000
   8.000   1.0895   0.00902   0.00437  -0.0209   0.2877   1.0000
   8.250   1.1115   0.00926   0.00457  -0.0200   0.2759   1.0000
   8.500   1.1335   0.00950   0.00479  -0.0190   0.2635   1.0000
   8.750   1.1546   0.00981   0.00506  -0.0180   0.2499   1.0000
   9.000   1.1749   0.01017   0.00537  -0.0169   0.2352   1.0000
   9.250   1.1944   0.01057   0.00571  -0.0156   0.2204   1.0000
   9.500   1.2133   0.01100   0.00608  -0.0143   0.2052   1.0000
   9.750   1.2313   0.01148   0.00649  -0.0129   0.1894   1.0000
  10.000   1.2487   0.01196   0.00692  -0.0113   0.1746   1.0000
  10.250   1.2657   0.01245   0.00736  -0.0097   0.1617   1.0000
  10.500   1.2815   0.01298   0.00784  -0.0080   0.1484   1.0000
  10.750   1.2971   0.01349   0.00831  -0.0062   0.1372   1.0000
  11.000   1.3114   0.01404   0.00883  -0.0043   0.1259   1.0000
  11.250   1.3248   0.01460   0.00936  -0.0023   0.1161   1.0000
  11.500   1.3351   0.01526   0.00997   0.0002   0.1051   1.0000
  11.750   1.3426   0.01599   0.01066   0.0030   0.0943   1.0000
  12.000   1.3427   0.01675   0.01138   0.0071   0.0853   1.0000
  12.250   1.3435   0.01756   0.01219   0.0106   0.0776   1.0000
  12.500   1.3439   0.01869   0.01330   0.0134   0.0696   1.0000
  12.750   1.3450   0.02009   0.01470   0.0153   0.0628   1.0000
  13.000   1.3483   0.02163   0.01626   0.0165   0.0564   1.0000
  13.250   1.3499   0.02350   0.01814   0.0173   0.0510   1.0000
  13.500   1.3515   0.02557   0.02023   0.0178   0.0457   1.0000
  13.750   1.3497   0.02808   0.02275   0.0181   0.0397   1.0000
  14.000   1.3491   0.03058   0.02528   0.0182   0.0363   1.0000
  14.250   1.3465   0.03336   0.02809   0.0181   0.0321   1.0000
  14.500   1.3437   0.03621   0.03098   0.0180   0.0296   1.0000
  14.750   1.3392   0.03926   0.03408   0.0177   0.0266   1.0000
  15.000   1.3357   0.04225   0.03713   0.0175   0.0247   1.0000
  15.250   1.3292   0.04560   0.04052   0.0171   0.0227   1.0000
  15.500   1.3252   0.04872   0.04370   0.0166   0.0213   1.0000
  15.750   1.3196   0.05215   0.04719   0.0160   0.0197   1.0000
  16.000   1.3122   0.05588   0.05097   0.0153   0.0181   1.0000
  16.250   1.3083   0.05924   0.05440   0.0145   0.0170   1.0000
  16.500   1.3035   0.06278   0.05801   0.0137   0.0159   1.0000
  16.750   1.2982   0.06643   0.06171   0.0128   0.0151   1.0000
  17.000   1.2910   0.07037   0.06570   0.0118   0.0139   1.0000
  17.250   1.2872   0.07395   0.06936   0.0108   0.0133   1.0000
  17.500   1.2819   0.07778   0.07325   0.0098   0.0126   1.0000
  17.750   1.2763   0.08161   0.07715   0.0087   0.0120   1.0000
  18.000   1.2686   0.08585   0.08143   0.0074   0.0113   1.0000
  18.250   1.2620   0.09000   0.08565   0.0061   0.0106   1.0000
  18.500   1.2579   0.09378   0.08951   0.0049   0.0101   1.0000
  18.750   1.2510   0.09803   0.09382   0.0034   0.0094   1.0000
  19.000   1.2439   0.10238   0.09824   0.0019   0.0092   1.0000
  19.250   1.2352   0.10700   0.10292   0.0003   0.0087   1.0000
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