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MH 106 13.07% (mh106-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 106 13.07% (mh106-il)
Reynolds number: 200,000
Max Cl/Cd: 60.63 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh106-il-200000-n5.txt
Download as CSV file: xf-mh106-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 106  13.07%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6491   0.13878   0.13517   0.0210   1.0000   0.0095
 -13.750  -0.6577   0.13054   0.12696   0.0174   1.0000   0.0094
 -13.250  -0.8060   0.08122   0.07694  -0.0105   1.0000   0.0073
 -12.750  -0.8363   0.06806   0.06349  -0.0192   1.0000   0.0072
 -12.250  -0.8631   0.05719   0.05226  -0.0256   1.0000   0.0072
 -12.000  -0.8763   0.05254   0.04738  -0.0277   1.0000   0.0072
 -11.750  -0.8895   0.04842   0.04306  -0.0288   1.0000   0.0074
 -11.500  -0.8955   0.04551   0.04001  -0.0288   1.0000   0.0075
 -11.250  -0.8971   0.04349   0.03792  -0.0283   1.0000   0.0077
 -11.000  -0.8994   0.04149   0.03580  -0.0270   1.0000   0.0080
 -10.750  -0.9015   0.03938   0.03352  -0.0251   1.0000   0.0081
 -10.500  -0.9016   0.03750   0.03145  -0.0227   1.0000   0.0082
 -10.250  -0.8984   0.03597   0.02978  -0.0203   1.0000   0.0085
 -10.000  -0.8924   0.03427   0.02786  -0.0181   1.0000   0.0088
  -9.750  -0.8829   0.03251   0.02589  -0.0162   1.0000   0.0091
  -9.500  -0.8712   0.03076   0.02395  -0.0144   1.0000   0.0092
  -9.250  -0.8576   0.02914   0.02215  -0.0128   1.0000   0.0094
  -9.000  -0.8431   0.02758   0.02044  -0.0111   1.0000   0.0096
  -8.750  -0.8278   0.02619   0.01891  -0.0095   1.0000   0.0098
  -8.500  -0.8118   0.02492   0.01753  -0.0079   1.0000   0.0100
  -8.250  -0.7964   0.02367   0.01619  -0.0062   1.0000   0.0103
  -8.000  -0.7816   0.02243   0.01488  -0.0045   1.0000   0.0107
  -7.750  -0.7648   0.02142   0.01382  -0.0029   1.0000   0.0112
  -7.500  -0.7470   0.02051   0.01284  -0.0015   1.0000   0.0118
  -7.250  -0.7288   0.01965   0.01190   0.0000   1.0000   0.0126
  -7.000  -0.7098   0.01885   0.01100   0.0015   1.0000   0.0137
  -6.750  -0.6911   0.01804   0.01016   0.0029   1.0000   0.0155
  -6.500  -0.6708   0.01742   0.00949   0.0041   1.0000   0.0182
  -6.250  -0.6439   0.01659   0.00860   0.0039   0.9788   0.0228
  -6.000  -0.6065   0.01565   0.00765   0.0016   0.9244   0.0369
  -5.750  -0.5754   0.01460   0.00678   0.0005   0.8769   0.0812
  -5.250  -0.5329   0.01309   0.00579   0.0025   0.8046   0.2234
  -5.000  -0.5102   0.01279   0.00550   0.0036   0.7761   0.2641
  -4.750  -0.4866   0.01259   0.00525   0.0045   0.7505   0.2932
  -4.500  -0.4629   0.01240   0.00503   0.0054   0.7274   0.3229
  -4.250  -0.4386   0.01225   0.00482   0.0063   0.7066   0.3487
  -4.000  -0.4137   0.01210   0.00458   0.0070   0.6870   0.3666
  -3.750  -0.3884   0.01197   0.00437   0.0076   0.6681   0.3828
  -3.500  -0.3630   0.01185   0.00416   0.0082   0.6503   0.3989
  -3.250  -0.3374   0.01173   0.00397   0.0088   0.6339   0.4152
  -3.000  -0.3116   0.01162   0.00379   0.0093   0.6189   0.4323
  -2.750  -0.2858   0.01151   0.00363   0.0098   0.6044   0.4501
  -2.500  -0.2601   0.01140   0.00348   0.0104   0.5905   0.4687
  -2.250  -0.2344   0.01129   0.00335   0.0109   0.5772   0.4887
  -2.000  -0.2086   0.01120   0.00323   0.0114   0.5649   0.5105
  -1.750  -0.1831   0.01109   0.00314   0.0120   0.5538   0.5333
  -1.500  -0.1574   0.01100   0.00306   0.0126   0.5431   0.5584
  -1.250  -0.1318   0.01090   0.00299   0.0132   0.5327   0.5856
  -1.000  -0.1063   0.01082   0.00294   0.0138   0.5231   0.6144
  -0.500  -0.0549   0.01066   0.00290   0.0151   0.5053   0.6753
  -0.250  -0.0291   0.01061   0.00291   0.0157   0.4978   0.7071
   0.000  -0.0025   0.01056   0.00294   0.0162   0.4899   0.7389
   0.250   0.0245   0.01055   0.00297   0.0167   0.4829   0.7706
   0.500   0.0531   0.01055   0.00305   0.0168   0.4754   0.8016
   0.750   0.0834   0.01061   0.00312   0.0166   0.4691   0.8303
   1.000   0.1163   0.01068   0.00323   0.0158   0.4624   0.8562
   1.250   0.1507   0.01080   0.00333   0.0147   0.4558   0.8785
   1.500   0.1860   0.01093   0.00345   0.0134   0.4498   0.8970
   1.750   0.2220   0.01106   0.00358   0.0119   0.4435   0.9122
   2.000   0.2569   0.01123   0.00369   0.0106   0.4382   0.9257
   2.250   0.2938   0.01136   0.00383   0.0088   0.4318   0.9364
   2.500   0.3301   0.01151   0.00396   0.0072   0.4260   0.9458
   2.750   0.3636   0.01166   0.00410   0.0060   0.4204   0.9558
   3.000   0.4007   0.01180   0.00425   0.0041   0.4141   0.9631
   3.250   0.4354   0.01196   0.00436   0.0027   0.4088   0.9711
   3.500   0.4723   0.01207   0.00453   0.0008   0.4021   0.9781
   3.750   0.5090   0.01221   0.00465  -0.0011   0.3960   0.9846
   4.000   0.5473   0.01231   0.00480  -0.0034   0.3891   0.9908
   4.250   0.5858   0.01241   0.00490  -0.0058   0.3819   0.9966
   4.500   0.6197   0.01249   0.00505  -0.0072   0.3745   1.0000
   4.750   0.6425   0.01261   0.00518  -0.0064   0.3678   1.0000
   5.000   0.6655   0.01273   0.00534  -0.0055   0.3609   1.0000
   5.250   0.6884   0.01286   0.00551  -0.0047   0.3533   1.0000
   5.500   0.7115   0.01300   0.00570  -0.0038   0.3455   1.0000
   5.750   0.7344   0.01315   0.00587  -0.0029   0.3373   1.0000
   6.000   0.7575   0.01329   0.00609  -0.0021   0.3279   1.0000
   6.250   0.7804   0.01346   0.00632  -0.0013   0.3183   1.0000
   6.500   0.8031   0.01364   0.00653  -0.0004   0.3070   1.0000
   6.750   0.8258   0.01384   0.00678   0.0005   0.2942   1.0000
   7.000   0.8480   0.01407   0.00704   0.0014   0.2789   1.0000
   7.250   0.8700   0.01435   0.00734   0.0024   0.2612   1.0000
   7.500   0.8910   0.01471   0.00769   0.0034   0.2412   1.0000
   7.750   0.9111   0.01516   0.00810   0.0045   0.2212   1.0000
   8.000   0.9305   0.01569   0.00859   0.0057   0.2002   1.0000
   8.250   0.9488   0.01631   0.00915   0.0070   0.1806   1.0000
   8.500   0.9672   0.01692   0.00974   0.0083   0.1628   1.0000
   8.750   0.9846   0.01759   0.01041   0.0096   0.1461   1.0000
   9.000   1.0015   0.01829   0.01110   0.0110   0.1314   1.0000
   9.250   1.0175   0.01903   0.01183   0.0125   0.1179   1.0000
   9.500   1.0329   0.01978   0.01259   0.0141   0.1061   1.0000
   9.750   1.0474   0.02057   0.01340   0.0157   0.0957   1.0000
  10.000   1.0603   0.02144   0.01427   0.0174   0.0865   1.0000
  10.250   1.0731   0.02227   0.01514   0.0192   0.0777   1.0000
  10.500   1.0841   0.02318   0.01612   0.0211   0.0700   1.0000
  10.750   1.0912   0.02426   0.01720   0.0232   0.0630   1.0000
  11.000   1.0982   0.02520   0.01822   0.0255   0.0571   1.0000
  11.250   1.0977   0.02644   0.01948   0.0284   0.0523   1.0000
  11.500   1.0999   0.02777   0.02090   0.0303   0.0481   1.0000
  11.750   1.1006   0.02947   0.02267   0.0315   0.0441   1.0000
  12.000   1.0986   0.03171   0.02494   0.0321   0.0406   1.0000
  12.250   1.1008   0.03382   0.02718   0.0323   0.0376   1.0000
  12.500   1.1002   0.03636   0.02981   0.0321   0.0346   1.0000
  12.750   1.0958   0.03947   0.03296   0.0315   0.0320   1.0000
  13.000   1.0952   0.04226   0.03586   0.0310   0.0297   1.0000
  13.250   1.0934   0.04526   0.03896   0.0303   0.0274   1.0000
  13.500   1.0883   0.04871   0.04247   0.0293   0.0256   1.0000
  13.750   1.0798   0.05264   0.04645   0.0280   0.0241   1.0000
  14.000   1.0770   0.05593   0.04989   0.0271   0.0227   1.0000
  14.250   1.0726   0.05947   0.05354   0.0260   0.0213   1.0000
  14.500   1.0657   0.06342   0.05759   0.0246   0.0199   1.0000
  14.750   1.0584   0.06753   0.06178   0.0231   0.0191   1.0000
  15.000   1.0480   0.07228   0.06660   0.0212   0.0183   1.0000
  15.250   1.0418   0.07658   0.07100   0.0194   0.0173   1.0000
  15.500   1.0355   0.08097   0.07552   0.0176   0.0166   1.0000
  15.750   1.0289   0.08558   0.08023   0.0156   0.0155   1.0000
  16.000   1.0203   0.09061   0.08537   0.0134   0.0149   1.0000
  16.250   1.0130   0.09555   0.09041   0.0112   0.0146   1.0000
  16.500   1.0024   0.10119   0.09613   0.0085   0.0140   1.0000
  16.750   0.9913   0.10707   0.10208   0.0056   0.0134   1.0000
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