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MH 108 11.98% (mh108-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 108 11.98% (mh108-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.75 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh108-il-1000000-n5.txt
Download as CSV file: xf-mh108-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 108  11.98%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.0306   0.10163   0.09895   0.0089   1.0000   0.0020
 -16.250  -1.0691   0.09020   0.08737   0.0024   1.0000   0.0019
 -16.000  -1.1170   0.07729   0.07428  -0.0051   1.0000   0.0019
 -15.750  -1.1459   0.06795   0.06479  -0.0106   1.0000   0.0018
 -15.500  -1.1610   0.06112   0.05784  -0.0147   1.0000   0.0018
 -15.250  -1.1913   0.05177   0.04828  -0.0210   1.0000   0.0018
 -15.000  -1.2111   0.04500   0.04134  -0.0254   1.0000   0.0018
 -14.750  -1.2200   0.04070   0.03691  -0.0275   1.0000   0.0018
 -14.500  -1.2341   0.03657   0.03262  -0.0286   1.0000   0.0018
 -14.250  -1.2472   0.03329   0.02918  -0.0280   1.0000   0.0018
 -14.000  -1.2534   0.03103   0.02680  -0.0264   1.0000   0.0018
 -13.750  -1.2549   0.02935   0.02501  -0.0243   1.0000   0.0018
 -13.500  -1.2590   0.02765   0.02318  -0.0214   1.0000   0.0019
 -13.250  -1.2584   0.02634   0.02177  -0.0183   1.0000   0.0020
 -13.000  -1.2534   0.02534   0.02068  -0.0153   1.0000   0.0020
 -12.750  -1.2448   0.02437   0.01962  -0.0129   1.0000   0.0020
 -12.500  -1.2325   0.02340   0.01857  -0.0110   1.0000   0.0021
 -12.250  -1.2183   0.02250   0.01757  -0.0092   1.0000   0.0021
 -12.000  -1.2022   0.02167   0.01667  -0.0077   1.0000   0.0022
 -11.750  -1.1850   0.02090   0.01583  -0.0063   1.0000   0.0023
 -11.500  -1.1670   0.02014   0.01498  -0.0050   1.0000   0.0023
 -11.250  -1.1479   0.01944   0.01422  -0.0038   1.0000   0.0024
 -11.000  -1.1280   0.01878   0.01350  -0.0027   1.0000   0.0025
 -10.750  -1.1078   0.01811   0.01275  -0.0015   1.0000   0.0025
 -10.500  -1.0868   0.01750   0.01209  -0.0005   1.0000   0.0027
 -10.250  -1.0652   0.01693   0.01145   0.0005   1.0000   0.0027
 -10.000  -1.0431   0.01639   0.01086   0.0014   1.0000   0.0028
  -9.750  -1.0207   0.01587   0.01028   0.0023   1.0000   0.0029
  -9.500  -0.9977   0.01539   0.00975   0.0031   1.0000   0.0030
  -9.250  -0.9754   0.01482   0.00913   0.0040   1.0000   0.0032
  -9.000  -0.9524   0.01432   0.00859   0.0049   1.0000   0.0034
  -8.750  -0.9289   0.01387   0.00811   0.0057   1.0000   0.0036
  -8.500  -0.9051   0.01346   0.00766   0.0064   1.0000   0.0039
  -8.250  -0.8811   0.01307   0.00724   0.0072   1.0000   0.0042
  -8.000  -0.8568   0.01271   0.00685   0.0079   1.0000   0.0046
  -7.750  -0.8240   0.01228   0.00640   0.0067   0.9718   0.0052
  -7.500  -0.7900   0.01204   0.00595   0.0056   0.8729   0.0062
  -7.250  -0.7675   0.01191   0.00561   0.0068   0.8194   0.0069
  -7.000  -0.7438   0.01168   0.00525   0.0077   0.7787   0.0087
  -6.750  -0.7192   0.01146   0.00492   0.0084   0.7450   0.0110
  -6.500  -0.6944   0.01120   0.00458   0.0091   0.7152   0.0151
  -6.000  -0.6441   0.01065   0.00396   0.0102   0.6640   0.0294
  -5.750  -0.6186   0.01041   0.00367   0.0107   0.6422   0.0383
  -5.500  -0.5928   0.01016   0.00343   0.0112   0.6228   0.0487
  -5.250  -0.5668   0.00994   0.00320   0.0116   0.6040   0.0599
  -5.000  -0.5407   0.00973   0.00298   0.0120   0.5855   0.0723
  -4.750  -0.5145   0.00952   0.00277   0.0124   0.5686   0.0871
  -4.250  -0.4614   0.00918   0.00243   0.0131   0.5385   0.1134
  -4.000  -0.4346   0.00904   0.00227   0.0134   0.5225   0.1255
  -3.750  -0.4077   0.00890   0.00213   0.0137   0.5079   0.1405
  -3.500  -0.3809   0.00876   0.00200   0.0140   0.4945   0.1568
  -3.250  -0.3537   0.00864   0.00188   0.0142   0.4819   0.1704
  -3.000  -0.3267   0.00852   0.00177   0.0145   0.4690   0.1871
  -2.750  -0.2997   0.00840   0.00166   0.0148   0.4562   0.2043
  -2.500  -0.2726   0.00829   0.00157   0.0150   0.4439   0.2233
  -2.250  -0.2454   0.00820   0.00149   0.0153   0.4331   0.2420
  -2.000  -0.2181   0.00811   0.00141   0.0155   0.4224   0.2592
  -1.750  -0.1910   0.00799   0.00134   0.0157   0.4122   0.2835
  -1.500  -0.1639   0.00789   0.00128   0.0160   0.4019   0.3082
  -1.000  -0.1095   0.00772   0.00119   0.0164   0.3822   0.3561
  -0.750  -0.0823   0.00763   0.00115   0.0167   0.3741   0.3830
  -0.500  -0.0551   0.00755   0.00112   0.0169   0.3658   0.4103
  -0.250  -0.0279   0.00747   0.00110   0.0171   0.3579   0.4374
   0.000  -0.0007   0.00741   0.00109   0.0174   0.3493   0.4654
   0.250   0.0264   0.00733   0.00108   0.0176   0.3423   0.4957
   0.500   0.0533   0.00725   0.00108   0.0179   0.3355   0.5284
   0.750   0.0801   0.00716   0.00109   0.0182   0.3297   0.5629
   1.000   0.1068   0.00708   0.00110   0.0186   0.3230   0.6003
   1.250   0.1332   0.00700   0.00112   0.0190   0.3167   0.6395
   1.500   0.1596   0.00691   0.00115   0.0194   0.3115   0.6784
   1.750   0.1856   0.00684   0.00119   0.0199   0.3054   0.7180
   2.000   0.2115   0.00676   0.00123   0.0205   0.3002   0.7579
   2.250   0.2373   0.00670   0.00128   0.0211   0.2946   0.7962
   2.500   0.2630   0.00666   0.00134   0.0217   0.2890   0.8337
   2.750   0.2895   0.00662   0.00142   0.0223   0.2845   0.8680
   3.000   0.3173   0.00663   0.00150   0.0225   0.2790   0.8988
   3.250   0.3481   0.00670   0.00161   0.0221   0.2736   0.9236
   3.500   0.3821   0.00678   0.00172   0.0209   0.2686   0.9404
   3.750   0.4172   0.00691   0.00183   0.0195   0.2628   0.9514
   4.000   0.4517   0.00703   0.00194   0.0181   0.2579   0.9587
   4.250   0.4835   0.00714   0.00205   0.0174   0.2525   0.9656
   4.500   0.5154   0.00728   0.00216   0.0166   0.2463   0.9705
   4.750   0.5491   0.00739   0.00228   0.0154   0.2412   0.9740
   5.000   0.5801   0.00753   0.00240   0.0148   0.2345   0.9782
   5.250   0.6096   0.00767   0.00253   0.0145   0.2284   0.9823
   5.500   0.6460   0.00782   0.00266   0.0127   0.2208   0.9845
   5.750   0.6815   0.00798   0.00280   0.0110   0.2125   0.9872
   6.000   0.7147   0.00817   0.00296   0.0098   0.2036   0.9899
   6.250   0.7458   0.00835   0.00312   0.0091   0.1932   0.9921
   6.500   0.7766   0.00856   0.00330   0.0084   0.1826   0.9938
   6.750   0.8093   0.00879   0.00349   0.0072   0.1702   0.9951
   7.000   0.8414   0.00906   0.00371   0.0061   0.1572   0.9965
   7.250   0.8732   0.00934   0.00396   0.0051   0.1451   0.9980
   7.500   0.9047   0.00965   0.00422   0.0041   0.1333   0.9992
   7.750   0.9335   0.01000   0.00452   0.0036   0.1197   1.0000
   8.000   0.9559   0.01036   0.00482   0.0045   0.1080   1.0000
   8.250   0.9789   0.01065   0.00510   0.0053   0.1005   1.0000
   8.500   1.0014   0.01099   0.00543   0.0062   0.0920   1.0000
   8.750   1.0231   0.01141   0.00580   0.0072   0.0809   1.0000
   9.000   1.0442   0.01187   0.00620   0.0082   0.0693   1.0000
   9.250   1.0650   0.01236   0.00664   0.0093   0.0587   1.0000
   9.500   1.0849   0.01292   0.00714   0.0104   0.0468   1.0000
   9.750   1.1045   0.01350   0.00766   0.0116   0.0371   1.0000
  10.000   1.1235   0.01411   0.00823   0.0128   0.0285   1.0000
  10.250   1.1429   0.01466   0.00877   0.0140   0.0233   1.0000
  10.500   1.1623   0.01518   0.00930   0.0152   0.0194   1.0000
  10.750   1.1811   0.01574   0.00987   0.0164   0.0162   1.0000
  11.000   1.2000   0.01628   0.01042   0.0176   0.0139   1.0000
  11.250   1.2174   0.01691   0.01107   0.0190   0.0112   1.0000
  11.500   1.2345   0.01753   0.01172   0.0204   0.0094   1.0000
  11.750   1.2513   0.01815   0.01238   0.0217   0.0080   1.0000
  12.000   1.2662   0.01887   0.01312   0.0233   0.0066   1.0000
  12.250   1.2807   0.01957   0.01387   0.0249   0.0056   1.0000
  12.500   1.2937   0.02031   0.01466   0.0266   0.0049   1.0000
  12.750   1.3039   0.02117   0.01556   0.0286   0.0042   1.0000
  13.000   1.3106   0.02194   0.01640   0.0312   0.0041   1.0000
  13.250   1.3137   0.02288   0.01741   0.0339   0.0038   1.0000
  13.500   1.3160   0.02416   0.01876   0.0357   0.0034   1.0000
  13.750   1.3184   0.02582   0.02050   0.0366   0.0033   1.0000
  14.000   1.3189   0.02807   0.02285   0.0365   0.0029   1.0000
  14.250   1.3197   0.03069   0.02557   0.0357   0.0027   1.0000
  14.500   1.3200   0.03362   0.02860   0.0345   0.0026   1.0000
  14.750   1.3184   0.03694   0.03203   0.0330   0.0025   1.0000
  15.000   1.3142   0.04065   0.03584   0.0314   0.0026   1.0000
  15.250   1.3071   0.04475   0.04005   0.0295   0.0024   1.0000
  15.500   1.2971   0.04925   0.04466   0.0276   0.0024   1.0000
  15.750   1.2846   0.05408   0.04959   0.0255   0.0022   1.0000
  16.000   1.2691   0.05933   0.05495   0.0233   0.0021   1.0000
  16.250   1.2548   0.06446   0.06018   0.0212   0.0021   1.0000
  16.500   1.2406   0.06962   0.06545   0.0190   0.0022   1.0000
  16.750   1.2239   0.07539   0.07132   0.0165   0.0021   1.0000
  17.000   1.2122   0.08051   0.07653   0.0143   0.0022   1.0000
  17.250   1.1962   0.08640   0.08252   0.0117   0.0021   1.0000
  17.500   1.1795   0.09247   0.08867   0.0090   0.0019   1.0000
  17.750   1.1671   0.09799   0.09429   0.0066   0.0020   1.0000
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