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MH 92 15.49% (mh92-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 92 15.49% (mh92-il)
Reynolds number: 200,000
Max Cl/Cd: 54.69 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh92-il-200000-n5.txt
Download as CSV file: xf-mh92-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 92  15.49%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7481   0.11152   0.10759   0.0094   1.0000   0.0124
 -14.500  -0.7791   0.09915   0.09505   0.0013   1.0000   0.0122
 -14.250  -0.8105   0.08788   0.08356  -0.0064   1.0000   0.0121
 -14.000  -0.8319   0.07978   0.07528  -0.0118   1.0000   0.0119
 -13.750  -0.8583   0.07165   0.06689  -0.0170   1.0000   0.0120
 -13.500  -0.8751   0.06581   0.06084  -0.0201   1.0000   0.0119
 -13.250  -0.8917   0.06049   0.05529  -0.0224   1.0000   0.0119
 -13.000  -0.9062   0.05584   0.05040  -0.0237   1.0000   0.0120
 -12.750  -0.9162   0.05203   0.04637  -0.0241   1.0000   0.0120
 -12.500  -0.9235   0.04870   0.04281  -0.0239   1.0000   0.0120
 -12.250  -0.9288   0.04566   0.03954  -0.0232   1.0000   0.0121
 -12.000  -0.9303   0.04307   0.03673  -0.0223   1.0000   0.0122
 -11.750  -0.9299   0.04067   0.03409  -0.0210   1.0000   0.0123
 -11.500  -0.9257   0.03856   0.03178  -0.0196   1.0000   0.0124
 -11.250  -0.9199   0.03661   0.02961  -0.0181   1.0000   0.0126
 -11.000  -0.9103   0.03499   0.02791  -0.0169   1.0000   0.0127
 -10.750  -0.8996   0.03351   0.02635  -0.0156   1.0000   0.0128
 -10.500  -0.8883   0.03227   0.02506  -0.0142   1.0000   0.0131
 -10.250  -0.8754   0.03102   0.02373  -0.0129   1.0000   0.0134
 -10.000  -0.8618   0.02996   0.02260  -0.0115   1.0000   0.0138
  -9.750  -0.8469   0.02884   0.02139  -0.0102   1.0000   0.0143
  -9.500  -0.8310   0.02778   0.02022  -0.0089   1.0000   0.0148
  -9.250  -0.8142   0.02668   0.01901  -0.0077   1.0000   0.0152
  -9.000  -0.7984   0.02562   0.01795  -0.0064   1.0000   0.0156
  -8.750  -0.7818   0.02471   0.01703  -0.0052   0.9788   0.0160
  -8.500  -0.7554   0.02373   0.01597  -0.0057   0.9245   0.0166
  -8.250  -0.7391   0.02302   0.01515  -0.0038   0.8936   0.0170
  -8.000  -0.7246   0.02230   0.01431  -0.0016   0.8700   0.0176
  -7.750  -0.7093   0.02162   0.01349   0.0006   0.8504   0.0182
  -7.500  -0.6942   0.02093   0.01273   0.0027   0.8330   0.0189
  -7.250  -0.6771   0.02033   0.01205   0.0045   0.8172   0.0197
  -7.000  -0.6591   0.01973   0.01134   0.0062   0.8023   0.0210
  -6.750  -0.6404   0.01917   0.01067   0.0078   0.7884   0.0222
  -6.500  -0.6204   0.01866   0.01008   0.0092   0.7747   0.0244
  -6.250  -0.5998   0.01813   0.00950   0.0105   0.7613   0.0274
  -6.000  -0.5790   0.01761   0.00892   0.0117   0.7487   0.0314
  -5.500  -0.5365   0.01655   0.00782   0.0141   0.7237   0.0484
  -5.000  -0.4960   0.01527   0.00678   0.0166   0.7003   0.1099
  -4.750  -0.4771   0.01447   0.00630   0.0179   0.6881   0.1760
  -4.500  -0.4588   0.01370   0.00589   0.0193   0.6769   0.2542
  -4.250  -0.4391   0.01311   0.00556   0.0206   0.6654   0.3248
  -4.000  -0.4185   0.01262   0.00529   0.0219   0.6538   0.3846
  -3.750  -0.3975   0.01221   0.00506   0.0233   0.6428   0.4410
  -3.500  -0.3754   0.01186   0.00489   0.0245   0.6312   0.4946
  -3.250  -0.3528   0.01156   0.00474   0.0257   0.6199   0.5455
  -3.000  -0.3291   0.01135   0.00462   0.0268   0.6089   0.5887
  -2.750  -0.3037   0.01120   0.00454   0.0275   0.5973   0.6206
  -2.500  -0.2777   0.01111   0.00447   0.0282   0.5862   0.6482
  -2.250  -0.2513   0.01106   0.00442   0.0289   0.5749   0.6741
  -2.000  -0.2245   0.01105   0.00439   0.0294   0.5636   0.6980
  -1.750  -0.1975   0.01107   0.00438   0.0300   0.5529   0.7188
  -1.500  -0.1701   0.01110   0.00437   0.0304   0.5413   0.7366
  -1.250  -0.1428   0.01115   0.00436   0.0308   0.5304   0.7523
  -1.000  -0.1158   0.01121   0.00433   0.0313   0.5195   0.7668
  -0.750  -0.0879   0.01128   0.00437   0.0316   0.5084   0.7790
  -0.500  -0.0603   0.01137   0.00438   0.0319   0.4978   0.7902
  -0.250  -0.0335   0.01144   0.00437   0.0323   0.4867   0.8022
   0.000  -0.0052   0.01155   0.00443   0.0326   0.4763   0.8110
   0.250   0.0215   0.01164   0.00443   0.0330   0.4660   0.8213
   0.500   0.0497   0.01176   0.00451   0.0332   0.4551   0.8297
   0.750   0.0762   0.01186   0.00454   0.0336   0.4454   0.8393
   1.000   0.1043   0.01200   0.00463   0.0339   0.4349   0.8471
   1.250   0.1304   0.01212   0.00468   0.0344   0.4254   0.8567
   1.500   0.1588   0.01228   0.00479   0.0345   0.4156   0.8634
   1.750   0.1846   0.01239   0.00486   0.0351   0.4064   0.8721
   2.000   0.2128   0.01255   0.00495   0.0352   0.3970   0.8776
   2.250   0.2409   0.01268   0.00506   0.0352   0.3879   0.8836
   2.500   0.2653   0.01281   0.00510   0.0359   0.3797   0.8914
   2.750   0.2952   0.01296   0.00524   0.0357   0.3707   0.8956
   3.000   0.3233   0.01313   0.00535   0.0357   0.3625   0.9009
   3.250   0.3481   0.01324   0.00545   0.0362   0.3547   0.9080
   3.500   0.3776   0.01342   0.00558   0.0359   0.3467   0.9122
   3.750   0.4073   0.01359   0.00573   0.0356   0.3388   0.9167
   4.000   0.4334   0.01375   0.00586   0.0359   0.3316   0.9230
   4.250   0.4618   0.01393   0.00602   0.0357   0.3250   0.9279
   4.500   0.4933   0.01411   0.00620   0.0349   0.3173   0.9318
   4.750   0.5218   0.01433   0.00636   0.0346   0.3108   0.9371
   5.000   0.5490   0.01449   0.00655   0.0346   0.3041   0.9428
   5.250   0.5821   0.01472   0.00676   0.0334   0.2976   0.9458
   5.500   0.6136   0.01494   0.00698   0.0324   0.2914   0.9495
   5.750   0.6415   0.01514   0.00719   0.0321   0.2847   0.9546
   6.000   0.6714   0.01540   0.00741   0.0314   0.2789   0.9583
   6.250   0.7052   0.01562   0.00769   0.0299   0.2730   0.9609
   6.500   0.7372   0.01587   0.00795   0.0287   0.2667   0.9641
   6.750   0.7659   0.01616   0.00820   0.0281   0.2612   0.9683
   7.000   0.7971   0.01640   0.00852   0.0271   0.2553   0.9716
   7.250   0.8303   0.01670   0.00882   0.0255   0.2494   0.9741
   7.500   0.8615   0.01701   0.00915   0.0243   0.2441   0.9773
   7.750   0.8908   0.01729   0.00950   0.0236   0.2383   0.9813
   8.000   0.9220   0.01764   0.00984   0.0223   0.2329   0.9844
   8.250   0.9539   0.01798   0.01024   0.0209   0.2274   0.9874
   8.500   0.9841   0.01832   0.01064   0.0198   0.2215   0.9911
   8.750   1.0133   0.01873   0.01104   0.0187   0.2162   0.9947
   9.000   1.0446   0.01910   0.01150   0.0173   0.2103   0.9983
   9.250   1.0654   0.01948   0.01192   0.0179   0.2052   1.0000
   9.500   1.0751   0.01987   0.01231   0.0205   0.2015   1.0000
   9.750   1.0856   0.02022   0.01273   0.0230   0.1975   1.0000
  10.000   1.0956   0.02059   0.01317   0.0256   0.1935   1.0000
  10.250   1.1044   0.02101   0.01361   0.0282   0.1894   1.0000
  10.500   1.1122   0.02152   0.01409   0.0309   0.1861   1.0000
  10.750   1.1238   0.02197   0.01464   0.0330   0.1821   1.0000
  11.000   1.1331   0.02249   0.01523   0.0353   0.1780   1.0000
  11.250   1.1390   0.02310   0.01585   0.0378   0.1745   1.0000
  11.500   1.1458   0.02384   0.01661   0.0399   0.1710   1.0000
  11.750   1.1560   0.02459   0.01747   0.0414   0.1668   1.0000
  12.000   1.1645   0.02549   0.01842   0.0427   0.1628   1.0000
  12.250   1.1713   0.02657   0.01952   0.0439   0.1592   1.0000
  12.500   1.1803   0.02765   0.02069   0.0448   0.1554   1.0000
  12.750   1.1886   0.02884   0.02197   0.0455   0.1513   1.0000
  13.000   1.1944   0.03025   0.02344   0.0461   0.1476   1.0000
  13.250   1.1992   0.03183   0.02504   0.0466   0.1442   1.0000
  13.500   1.2062   0.03336   0.02670   0.0469   0.1402   1.0000
  13.750   1.2098   0.03519   0.02860   0.0470   0.1362   1.0000
  14.000   1.2113   0.03727   0.03070   0.0470   0.1330   1.0000
  14.250   1.2147   0.03930   0.03285   0.0469   0.1296   1.0000
  14.500   1.2164   0.04156   0.03521   0.0466   0.1259   1.0000
  14.750   1.2154   0.04413   0.03784   0.0461   0.1226   1.0000
  15.000   1.2128   0.04691   0.04064   0.0455   0.1196   1.0000
  15.250   1.2124   0.04963   0.04350   0.0448   0.1162   1.0000
  15.500   1.2094   0.05269   0.04665   0.0439   0.1131   1.0000
  15.750   1.2048   0.05604   0.05005   0.0428   0.1103   1.0000
  16.000   1.2000   0.05952   0.05358   0.0415   0.1075   1.0000
  16.250   1.1955   0.06314   0.05734   0.0401   0.1044   1.0000
  16.500   1.1892   0.06706   0.06135   0.0385   0.1016   1.0000
  16.750   1.1828   0.07106   0.06539   0.0368   0.0991   1.0000
  17.000   1.1772   0.07498   0.06936   0.0351   0.0968   1.0000
  17.250   1.1691   0.07949   0.07401   0.0330   0.0941   1.0000
  17.500   1.1610   0.08406   0.07868   0.0309   0.0915   1.0000
  17.750   1.1534   0.08857   0.08323   0.0287   0.0891   1.0000
  18.000   1.1485   0.09268   0.08735   0.0267   0.0869   1.0000
  18.250   1.1374   0.09804   0.09286   0.0241   0.0845   1.0000
  18.500   1.1274   0.10325   0.09819   0.0214   0.0822   1.0000
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