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MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: MH 102 16.99% (mh102-il)
Reynolds number: 100,000
Max Cl/Cd: 37.8 at α=10.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh102-il-100000.txt
Download as CSV file: xf-mh102-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.5865   0.09527   0.08977  -0.0542   1.0000   0.0567
 -14.000  -0.6242   0.08492   0.07932  -0.0606   1.0000   0.0558
 -13.750  -0.6669   0.07477   0.06898  -0.0675   1.0000   0.0547
 -13.500  -0.7020   0.06671   0.06069  -0.0731   1.0000   0.0540
 -13.250  -0.7287   0.06047   0.05423  -0.0770   1.0000   0.0537
 -13.000  -0.7470   0.05574   0.04930  -0.0794   1.0000   0.0536
 -12.750  -0.7607   0.05188   0.04525  -0.0805   1.0000   0.0542
 -12.500  -0.7715   0.04863   0.04182  -0.0808   1.0000   0.0548
 -12.250  -0.7830   0.04572   0.03871  -0.0802   1.0000   0.0557
 -12.000  -0.7938   0.04330   0.03607  -0.0786   1.0000   0.0564
 -11.750  -0.7839   0.04148   0.03437  -0.0772   1.0000   0.0587
 -11.500  -0.7872   0.03987   0.03274  -0.0747   1.0000   0.0608
 -11.250  -0.7964   0.03834   0.03107  -0.0711   1.0000   0.0626
 -11.000  -0.7947   0.03678   0.02958  -0.0684   1.0000   0.0653
 -10.750  -0.7959   0.03543   0.02826  -0.0653   1.0000   0.0689
 -10.500  -0.7980   0.03397   0.02675  -0.0618   1.0000   0.0722
 -10.250  -0.8005   0.03283   0.02574  -0.0582   1.0000   0.0765
 -10.000  -0.8062   0.03167   0.02455  -0.0541   1.0000   0.0809
  -9.750  -0.8125   0.03075   0.02370  -0.0499   1.0000   0.0863
  -9.500  -0.8183   0.02978   0.02279  -0.0458   1.0000   0.0924
  -9.250  -0.8221   0.02882   0.02186  -0.0421   1.0000   0.1010
  -9.000  -0.8232   0.02800   0.02112  -0.0388   1.0000   0.1126
  -8.750  -0.8167   0.02730   0.02043  -0.0369   0.9987   0.1321
  -8.500  -0.7719   0.02753   0.02084  -0.0414   0.9871   0.1661
  -8.250  -0.7279   0.02813   0.02134  -0.0452   0.9759   0.1921
  -8.000  -0.6798   0.02898   0.02229  -0.0490   0.9661   0.2117
  -7.750  -0.6372   0.02937   0.02265  -0.0519   0.9552   0.2280
  -7.500  -0.5975   0.02947   0.02268  -0.0542   0.9439   0.2427
  -7.250  -0.5505   0.02940   0.02249  -0.0579   0.9361   0.2580
  -7.000  -0.5106   0.02940   0.02248  -0.0599   0.9249   0.2705
  -6.750  -0.4636   0.02907   0.02217  -0.0632   0.9173   0.2817
  -6.500  -0.4264   0.02817   0.02097  -0.0653   0.9071   0.2928
  -6.250  -0.3852   0.02776   0.02060  -0.0674   0.8976   0.3018
  -6.000  -0.3483   0.02677   0.01934  -0.0693   0.8879   0.3113
  -5.750  -0.3151   0.02633   0.01891  -0.0699   0.8760   0.3189
  -5.500  -0.2783   0.02542   0.01766  -0.0715   0.8673   0.3283
  -5.250  -0.2509   0.02500   0.01730  -0.0711   0.8535   0.3348
  -5.000  -0.2224   0.02448   0.01657  -0.0711   0.8418   0.3432
  -4.750  -0.1917   0.02386   0.01585  -0.0712   0.8310   0.3505
  -4.500  -0.1671   0.02356   0.01548  -0.0704   0.8176   0.3583
  -4.250  -0.1394   0.02305   0.01478  -0.0701   0.8070   0.3666
  -4.000  -0.1128   0.02272   0.01444  -0.0695   0.7948   0.3742
  -3.750  -0.0889   0.02245   0.01396  -0.0687   0.7825   0.3837
  -3.500  -0.0593   0.02204   0.01356  -0.0684   0.7731   0.3919
  -3.250  -0.0365   0.02188   0.01324  -0.0675   0.7603   0.4019
  -3.000  -0.0088   0.02157   0.01297  -0.0670   0.7507   0.4111
  -2.750   0.0159   0.02137   0.01264  -0.0663   0.7392   0.4225
  -2.500   0.0417   0.02117   0.01249  -0.0657   0.7289   0.4329
  -2.250   0.0682   0.02095   0.01221  -0.0651   0.7192   0.4453
  -2.000   0.0928   0.02090   0.01209  -0.0644   0.7092   0.4595
  -1.750   0.1197   0.02067   0.01191  -0.0639   0.7001   0.4731
  -1.500   0.1441   0.02060   0.01189  -0.0631   0.6902   0.4881
  -1.250   0.1706   0.02045   0.01174  -0.0625   0.6817   0.5057
  -1.000   0.1951   0.02044   0.01179  -0.0618   0.6730   0.5245
  -0.750   0.2204   0.02035   0.01175  -0.0610   0.6643   0.5455
  -0.500   0.2461   0.02029   0.01175  -0.0603   0.6568   0.5697
  -0.250   0.2692   0.02032   0.01189  -0.0593   0.6477   0.5964
   0.000   0.2967   0.02017   0.01181  -0.0586   0.6418   0.6270
   0.250   0.3164   0.02034   0.01220  -0.0571   0.6323   0.6599
   0.500   0.3419   0.02024   0.01222  -0.0559   0.6256   0.7005
   0.750   0.3639   0.02037   0.01251  -0.0543   0.6184   0.7464
   1.000   0.3856   0.02047   0.01281  -0.0524   0.6106   0.7963
   1.250   0.4162   0.02044   0.01281  -0.0514   0.6051   0.8515
   1.500   0.4502   0.02086   0.01336  -0.0522   0.5959   0.9035
   1.750   0.5103   0.02097   0.01335  -0.0574   0.5885   0.9430
   2.000   0.5755   0.02135   0.01368  -0.0646   0.5790   0.9714
   2.250   0.6471   0.02135   0.01353  -0.0730   0.5707   0.9951
   2.500   0.6684   0.02163   0.01375  -0.0729   0.5640   1.0000
   2.750   0.6768   0.02203   0.01413  -0.0703   0.5569   1.0000
   3.000   0.6966   0.02216   0.01412  -0.0689   0.5515   1.0000
   3.250   0.7089   0.02272   0.01469  -0.0667   0.5447   1.0000
   3.500   0.7253   0.02313   0.01506  -0.0650   0.5377   1.0000
   3.750   0.7517   0.02323   0.01501  -0.0644   0.5325   1.0000
   4.000   0.7629   0.02399   0.01585  -0.0621   0.5248   1.0000
   4.250   0.7843   0.02430   0.01611  -0.0610   0.5182   1.0000
   4.500   0.8150   0.02436   0.01600  -0.0610   0.5133   1.0000
   4.750   0.8228   0.02530   0.01710  -0.0583   0.5046   1.0000
   5.000   0.8495   0.02544   0.01715  -0.0578   0.4985   1.0000
   5.250   0.8699   0.02598   0.01769  -0.0567   0.4919   1.0000
   5.500   0.8871   0.02655   0.01832  -0.0551   0.4840   1.0000
   5.750   0.9197   0.02649   0.01812  -0.0554   0.4786   1.0000
   6.000   0.9296   0.02750   0.01926  -0.0530   0.4702   1.0000
   6.250   0.9561   0.02764   0.01937  -0.0526   0.4635   1.0000
   6.500   0.9805   0.02802   0.01972  -0.0519   0.4571   1.0000
   6.750   0.9943   0.02878   0.02058  -0.0500   0.4487   1.0000
   7.000   1.0299   0.02856   0.02022  -0.0507   0.4430   1.0000
   7.250   1.0363   0.02972   0.02155  -0.0480   0.4343   1.0000
   7.500   1.0654   0.02973   0.02151  -0.0478   0.4276   1.0000
   7.750   1.0836   0.03038   0.02221  -0.0465   0.4203   1.0000
   8.000   1.1013   0.03091   0.02280  -0.0451   0.4124   1.0000
   8.250   1.1409   0.03060   0.02232  -0.0462   0.4066   1.0000
   8.500   1.1384   0.03200   0.02398  -0.0425   0.3975   1.0000
   8.750   1.1757   0.03166   0.02351  -0.0433   0.3911   1.0000
   9.000   1.1782   0.03293   0.02497  -0.0402   0.3829   1.0000
   9.250   1.2065   0.03291   0.02491  -0.0400   0.3757   1.0000
   9.500   1.2226   0.03360   0.02565  -0.0385   0.3685   1.0000
   9.750   1.2350   0.03426   0.02640  -0.0365   0.3607   1.0000
  10.000   1.2705   0.03407   0.02610  -0.0371   0.3539   1.0000
  10.250   1.2628   0.03556   0.02782  -0.0330   0.3460   1.0000
  10.500   1.3128   0.03473   0.02677  -0.0352   0.3391   1.0000
  10.750   1.2918   0.03673   0.02907  -0.0296   0.3318   1.0000
  11.000   1.3244   0.03649   0.02876  -0.0299   0.3246   1.0000
  11.250   1.3247   0.03769   0.03007  -0.0267   0.3180   1.0000
  11.500   1.3242   0.03867   0.03113  -0.0234   0.3112   1.0000
  11.750   1.3619   0.03845   0.03082  -0.0243   0.3040   1.0000
  12.000   1.3306   0.04087   0.03347  -0.0184   0.2984   1.0000
  12.250   1.4010   0.03924   0.03155  -0.0222   0.2897   1.0000
  12.500   1.3534   0.04249   0.03514  -0.0154   0.2854   1.0000
  12.750   1.3446   0.04441   0.03716  -0.0128   0.2794   1.0000
  13.000   1.3871   0.04370   0.03634  -0.0134   0.2719   1.0000
  13.250   1.3374   0.04835   0.04126  -0.0094   0.2675   1.0000
  13.500   1.4268   0.04481   0.03739  -0.0120   0.2580   1.0000
  13.750   1.3653   0.05020   0.04314  -0.0077   0.2549   1.0000
  14.000   0.8085   0.13491   0.12820  -0.0367   0.2302   1.0000
  14.250   0.8758   0.12689   0.12025  -0.0314   0.2273   1.0000
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