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MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 102 16.99% (mh102-il)
Reynolds number: 1,000,000
Max Cl/Cd: 118.68 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh102-il-1000000.txt
Download as CSV file: xf-mh102-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 102  16.99%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8456   0.08656   0.08298  -0.0477   1.0000   0.0079
 -16.500  -0.8554   0.08171   0.07807  -0.0500   1.0000   0.0079
 -16.250  -0.8702   0.07622   0.07250  -0.0527   1.0000   0.0079
 -16.000  -0.8860   0.07074   0.06695  -0.0555   1.0000   0.0080
 -15.750  -0.8996   0.06577   0.06190  -0.0579   1.0000   0.0079
 -15.500  -0.9208   0.05988   0.05591  -0.0608   1.0000   0.0080
 -15.250  -0.9313   0.05541   0.05136  -0.0629   1.0000   0.0078
 -15.000  -0.9629   0.04820   0.04402  -0.0666   1.0000   0.0080
 -14.750  -0.9866   0.04184   0.03753  -0.0701   1.0000   0.0080
 -14.500  -0.9933   0.03765   0.03324  -0.0725   1.0000   0.0080
 -14.250  -1.0099   0.03225   0.02769  -0.0759   1.0000   0.0081
 -14.000  -1.0179   0.02868   0.02400  -0.0775   1.0000   0.0082
 -13.750  -1.0267   0.02592   0.02113  -0.0775   1.0000   0.0082
 -13.500  -1.0327   0.02416   0.01930  -0.0757   1.0000   0.0083
 -13.250  -1.0400   0.02296   0.01803  -0.0722   1.0000   0.0084
 -13.000  -1.0498   0.02219   0.01721  -0.0671   1.0000   0.0084
 -12.750  -1.0523   0.02143   0.01641  -0.0628   1.0000   0.0086
 -12.500  -1.0459   0.02070   0.01563  -0.0600   0.9997   0.0087
 -12.250  -1.0134   0.01976   0.01464  -0.0622   0.9970   0.0090
 -12.000  -0.9800   0.01891   0.01373  -0.0643   0.9935   0.0094
 -11.750  -0.9491   0.01817   0.01294  -0.0657   0.9888   0.0097
 -11.500  -0.9185   0.01719   0.01190  -0.0673   0.9834   0.0103
 -11.250  -0.8882   0.01644   0.01112  -0.0685   0.9761   0.0109
 -11.000  -0.8543   0.01579   0.01043  -0.0702   0.9671   0.0115
 -10.750  -0.8197   0.01506   0.00965  -0.0722   0.9526   0.0128
 -10.500  -0.7831   0.01444   0.00896  -0.0743   0.9312   0.0142
 -10.250  -0.7569   0.01391   0.00834  -0.0743   0.9025   0.0164
 -10.000  -0.7355   0.01353   0.00785  -0.0732   0.8772   0.0186
  -9.750  -0.7144   0.01314   0.00739  -0.0720   0.8559   0.0221
  -9.500  -0.6926   0.01277   0.00696  -0.0709   0.8378   0.0265
  -9.250  -0.6706   0.01237   0.00653  -0.0699   0.8217   0.0323
  -9.000  -0.6480   0.01199   0.00611  -0.0690   0.8068   0.0398
  -8.750  -0.6257   0.01156   0.00568  -0.0681   0.7919   0.0505
  -8.500  -0.6031   0.01108   0.00525  -0.0672   0.7781   0.0648
  -8.250  -0.5805   0.01060   0.00482  -0.0664   0.7653   0.0833
  -8.000  -0.5572   0.01019   0.00446  -0.0657   0.7530   0.1030
  -7.750  -0.5322   0.00987   0.00419  -0.0651   0.7411   0.1205
  -7.500  -0.5066   0.00964   0.00397  -0.0646   0.7293   0.1343
  -7.250  -0.4805   0.00947   0.00379  -0.0642   0.7171   0.1453
  -7.000  -0.4539   0.00930   0.00363  -0.0639   0.7059   0.1562
  -6.750  -0.4272   0.00917   0.00348  -0.0635   0.6952   0.1654
  -6.500  -0.3997   0.00908   0.00336  -0.0633   0.6844   0.1734
  -6.250  -0.3727   0.00896   0.00323  -0.0630   0.6741   0.1816
  -6.000  -0.3451   0.00892   0.00314  -0.0628   0.6630   0.1884
  -5.750  -0.3177   0.00881   0.00301  -0.0625   0.6526   0.1948
  -5.250  -0.2621   0.00871   0.00283  -0.0622   0.6325   0.2075
  -5.000  -0.2350   0.00863   0.00273  -0.0619   0.6225   0.2139
  -4.750  -0.2068   0.00857   0.00264  -0.0618   0.6132   0.2187
  -4.500  -0.1789   0.00857   0.00256  -0.0616   0.6031   0.2222
  -4.250  -0.1514   0.00846   0.00245  -0.0614   0.5935   0.2285
  -4.000  -0.1237   0.00842   0.00238  -0.0612   0.5842   0.2336
  -3.750  -0.0954   0.00840   0.00231  -0.0611   0.5753   0.2377
  -3.500  -0.0679   0.00834   0.00223  -0.0608   0.5664   0.2438
  -3.250  -0.0398   0.00828   0.00217  -0.0607   0.5578   0.2496
  -3.000  -0.0120   0.00829   0.00212  -0.0605   0.5486   0.2546
  -2.750   0.0160   0.00823   0.00206  -0.0604   0.5403   0.2617
  -2.500   0.0436   0.00822   0.00202  -0.0602   0.5317   0.2684
  -2.250   0.0721   0.00820   0.00198  -0.0601   0.5244   0.2740
  -2.000   0.0996   0.00817   0.00194  -0.0599   0.5160   0.2829
  -1.750   0.1278   0.00816   0.00192  -0.0598   0.5086   0.2903
  -1.500   0.1556   0.00812   0.00189  -0.0597   0.5010   0.2997
  -1.250   0.1834   0.00814   0.00188  -0.0595   0.4936   0.3081
  -1.000   0.2114   0.00810   0.00187  -0.0594   0.4867   0.3185
  -0.750   0.2391   0.00812   0.00187  -0.0593   0.4793   0.3286
  -0.500   0.2671   0.00809   0.00187  -0.0592   0.4732   0.3408
  -0.250   0.2950   0.00808   0.00187  -0.0590   0.4667   0.3522
   0.000   0.3224   0.00812   0.00189  -0.0588   0.4599   0.3642
   0.250   0.3505   0.00808   0.00190  -0.0588   0.4548   0.3785
   0.500   0.3782   0.00807   0.00192  -0.0586   0.4490   0.3939
   0.750   0.4054   0.00811   0.00196  -0.0584   0.4427   0.4095
   1.000   0.4335   0.00809   0.00199  -0.0583   0.4382   0.4260
   1.250   0.4612   0.00808   0.00202  -0.0582   0.4330   0.4440
   1.500   0.4883   0.00809   0.00207  -0.0580   0.4276   0.4650
   1.750   0.5155   0.00809   0.00213  -0.0577   0.4228   0.4897
   2.000   0.5432   0.00805   0.00217  -0.0576   0.4183   0.5164
   2.250   0.5702   0.00804   0.00223  -0.0574   0.4134   0.5455
   2.500   0.5965   0.00806   0.00232  -0.0570   0.4081   0.5790
   2.750   0.6235   0.00801   0.00239  -0.0567   0.4042   0.6170
   3.000   0.6501   0.00796   0.00246  -0.0564   0.3998   0.6571
   3.250   0.6761   0.00795   0.00255  -0.0560   0.3949   0.6968
   3.500   0.7011   0.00798   0.00267  -0.0553   0.3895   0.7384
   3.750   0.7271   0.00791   0.00276  -0.0548   0.3860   0.7841
   4.000   0.7520   0.00787   0.00286  -0.0540   0.3814   0.8292
   4.250   0.7759   0.00788   0.00298  -0.0530   0.3765   0.8738
   4.500   0.8004   0.00792   0.00311  -0.0521   0.3715   0.9195
   4.750   0.8364   0.00797   0.00323  -0.0536   0.3668   0.9557
   5.000   0.8794   0.00812   0.00336  -0.0568   0.3607   0.9761
   5.250   0.9209   0.00829   0.00350  -0.0598   0.3543   0.9866
   5.500   0.9589   0.00841   0.00361  -0.0619   0.3487   0.9962
   5.750   0.9923   0.00858   0.00374  -0.0632   0.3418   1.0000
   6.000   1.0147   0.00871   0.00385  -0.0621   0.3366   1.0000
   6.250   1.0379   0.00883   0.00397  -0.0612   0.3307   1.0000
   6.500   1.0597   0.00901   0.00411  -0.0600   0.3237   1.0000
   6.750   1.0831   0.00915   0.00424  -0.0591   0.3178   1.0000
   7.000   1.1057   0.00932   0.00439  -0.0581   0.3102   1.0000
   7.250   1.1283   0.00951   0.00456  -0.0572   0.3033   1.0000
   7.500   1.1512   0.00970   0.00472  -0.0562   0.2956   1.0000
   7.750   1.1733   0.00993   0.00492  -0.0552   0.2877   1.0000
   8.000   1.1959   0.01014   0.00511  -0.0543   0.2800   1.0000
   8.250   1.2173   0.01040   0.00534  -0.0532   0.2721   1.0000
   8.500   1.2392   0.01064   0.00556  -0.0522   0.2640   1.0000
   8.750   1.2598   0.01093   0.00582  -0.0510   0.2562   1.0000
   9.000   1.2810   0.01118   0.00606  -0.0499   0.2490   1.0000
   9.250   1.3001   0.01151   0.00635  -0.0484   0.2412   1.0000
   9.500   1.3203   0.01177   0.00661  -0.0472   0.2343   1.0000
   9.750   1.3362   0.01213   0.00694  -0.0452   0.2269   1.0000
  10.000   1.3539   0.01238   0.00720  -0.0434   0.2213   1.0000
  10.250   1.3678   0.01276   0.00755  -0.0411   0.2144   1.0000
  10.500   1.3837   0.01309   0.00789  -0.0392   0.2084   1.0000
  10.750   1.3985   0.01348   0.00827  -0.0372   0.2020   1.0000
  11.000   1.4121   0.01394   0.00871  -0.0351   0.1957   1.0000
  11.250   1.4275   0.01433   0.00912  -0.0333   0.1900   1.0000
  11.500   1.4389   0.01491   0.00967  -0.0311   0.1836   1.0000
  11.750   1.4539   0.01537   0.01015  -0.0294   0.1787   1.0000
  12.000   1.4660   0.01597   0.01075  -0.0275   0.1730   1.0000
  12.250   1.4765   0.01668   0.01146  -0.0255   0.1673   1.0000
  12.500   1.4894   0.01731   0.01211  -0.0239   0.1624   1.0000
  12.750   1.4984   0.01819   0.01299  -0.0220   0.1570   1.0000
  13.000   1.5091   0.01904   0.01386  -0.0205   0.1521   1.0000
  13.250   1.5194   0.01997   0.01480  -0.0190   0.1474   1.0000
  13.500   1.5249   0.02124   0.01607  -0.0174   0.1417   1.0000
  13.750   1.5361   0.02224   0.01711  -0.0163   0.1380   1.0000
  14.000   1.5431   0.02357   0.01845  -0.0151   0.1331   1.0000
  14.250   1.5475   0.02516   0.02005  -0.0139   0.1282   1.0000
  14.500   1.5560   0.02652   0.02145  -0.0131   0.1241   1.0000
  14.750   1.5590   0.02836   0.02331  -0.0121   0.1195   1.0000
  15.000   1.5628   0.03021   0.02519  -0.0114   0.1153   1.0000
  15.250   1.5677   0.03204   0.02706  -0.0108   0.1117   1.0000
  15.500   1.5682   0.03430   0.02934  -0.0103   0.1080   1.0000
  15.750   1.5688   0.03661   0.03169  -0.0098   0.1042   1.0000
  16.000   1.5707   0.03886   0.03400  -0.0095   0.1008   1.0000
  16.250   1.5679   0.04165   0.03681  -0.0093   0.0974   1.0000
  16.500   1.5653   0.04446   0.03967  -0.0091   0.0943   1.0000
  16.750   1.5654   0.04708   0.04234  -0.0091   0.0915   1.0000
  17.000   1.5611   0.05019   0.04550  -0.0092   0.0884   1.0000
  17.250   1.5538   0.05368   0.04903  -0.0094   0.0856   1.0000
  17.500   1.5517   0.05668   0.05209  -0.0097   0.0832   1.0000
  17.750   1.5465   0.06007   0.05553  -0.0100   0.0802   1.0000
  18.000   1.5370   0.06398   0.05948  -0.0105   0.0774   1.0000
  18.250   1.5314   0.06750   0.06306  -0.0111   0.0749   1.0000
  18.500   1.5274   0.07088   0.06650  -0.0116   0.0727   1.0000
  18.750   1.5184   0.07492   0.07059  -0.0124   0.0702   1.0000
  19.000   1.5077   0.07926   0.07497  -0.0134   0.0681   1.0000
  19.250   1.5034   0.08284   0.07862  -0.0142   0.0660   1.0000
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