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MH 108 11.98% (mh108-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 108 11.98% (mh108-il)
Reynolds number: 200,000
Max Cl/Cd: 58.51 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh108-il-200000-n5.txt
Download as CSV file: xf-mh108-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7603   0.12627   0.12257   0.0238   1.0000   0.0094
 -14.250  -0.7928   0.11305   0.10927   0.0167   1.0000   0.0092
 -14.000  -0.8208   0.10198   0.09810   0.0104   1.0000   0.0088
 -13.750  -0.8529   0.09047   0.08644   0.0035   1.0000   0.0084
 -13.500  -0.8755   0.08124   0.07706  -0.0024   1.0000   0.0084
 -13.250  -0.8963   0.07268   0.06834  -0.0084   1.0000   0.0086
 -13.000  -0.9184   0.06453   0.06000  -0.0137   1.0000   0.0081
 -12.750  -0.9348   0.05786   0.05314  -0.0182   1.0000   0.0080
 -12.500  -0.9452   0.05280   0.04789  -0.0217   1.0000   0.0083
 -12.250  -0.9584   0.04801   0.04290  -0.0238   1.0000   0.0082
 -12.000  -0.9670   0.04446   0.03916  -0.0247   1.0000   0.0083
 -11.750  -0.9727   0.04164   0.03612  -0.0245   1.0000   0.0086
 -11.500  -0.9779   0.03909   0.03338  -0.0232   1.0000   0.0087
 -11.250  -0.9796   0.03705   0.03114  -0.0213   1.0000   0.0090
 -11.000  -0.9793   0.03521   0.02910  -0.0190   1.0000   0.0092
 -10.750  -0.9772   0.03350   0.02721  -0.0164   1.0000   0.0094
 -10.500  -0.9722   0.03174   0.02530  -0.0141   1.0000   0.0097
 -10.250  -0.9642   0.03011   0.02354  -0.0121   1.0000   0.0099
 -10.000  -0.9535   0.02865   0.02197  -0.0103   1.0000   0.0103
  -9.750  -0.9400   0.02735   0.02056  -0.0087   1.0000   0.0106
  -9.500  -0.9253   0.02610   0.01918  -0.0071   1.0000   0.0112
  -9.250  -0.9095   0.02490   0.01784  -0.0056   1.0000   0.0118
  -9.000  -0.8926   0.02378   0.01655  -0.0042   1.0000   0.0125
  -8.750  -0.8756   0.02262   0.01527  -0.0027   1.0000   0.0134
  -8.500  -0.8571   0.02161   0.01418  -0.0014   1.0000   0.0146
  -8.250  -0.8367   0.02079   0.01326  -0.0003   1.0000   0.0167
  -8.000  -0.8170   0.01985   0.01229   0.0008   1.0000   0.0195
  -7.750  -0.7958   0.01907   0.01142   0.0019   1.0000   0.0232
  -7.500  -0.7751   0.01822   0.01057   0.0030   1.0000   0.0287
  -7.250  -0.7536   0.01749   0.00984   0.0040   1.0000   0.0368
  -7.000  -0.7314   0.01684   0.00921   0.0049   1.0000   0.0465
  -6.750  -0.7088   0.01627   0.00867   0.0058   1.0000   0.0573
  -6.500  -0.6860   0.01574   0.00818   0.0066   1.0000   0.0694
  -6.250  -0.6630   0.01525   0.00772   0.0075   1.0000   0.0825
  -6.000  -0.6400   0.01480   0.00729   0.0083   1.0000   0.0960
  -5.750  -0.6170   0.01437   0.00689   0.0092   1.0000   0.1097
  -5.500  -0.5941   0.01396   0.00653   0.0101   1.0000   0.1235
  -5.000  -0.5161   0.01313   0.00574   0.0053   0.9094   0.1651
  -4.750  -0.4832   0.01286   0.00538   0.0045   0.8597   0.1858
  -4.500  -0.4576   0.01264   0.00509   0.0052   0.8182   0.2064
  -4.250  -0.4333   0.01245   0.00483   0.0062   0.7833   0.2277
  -4.000  -0.4094   0.01225   0.00458   0.0072   0.7530   0.2508
  -3.750  -0.3851   0.01208   0.00433   0.0081   0.7254   0.2748
  -3.500  -0.3607   0.01190   0.00412   0.0089   0.7005   0.3011
  -3.250  -0.3362   0.01171   0.00392   0.0097   0.6774   0.3295
  -3.000  -0.3115   0.01154   0.00374   0.0105   0.6560   0.3602
  -2.750  -0.2867   0.01136   0.00356   0.0112   0.6355   0.3914
  -2.500  -0.2620   0.01120   0.00341   0.0120   0.6161   0.4244
  -2.250  -0.2373   0.01104   0.00328   0.0128   0.5981   0.4594
  -2.000  -0.2124   0.01088   0.00315   0.0136   0.5808   0.4953
  -1.750  -0.1878   0.01071   0.00306   0.0144   0.5640   0.5335
  -1.500  -0.1633   0.01055   0.00297   0.0153   0.5477   0.5744
  -1.250  -0.1388   0.01040   0.00291   0.0162   0.5325   0.6177
  -1.000  -0.1140   0.01027   0.00287   0.0171   0.5184   0.6623
  -0.750  -0.0888   0.01016   0.00286   0.0180   0.5045   0.7073
  -0.500  -0.0627   0.01009   0.00286   0.0188   0.4907   0.7513
  -0.250  -0.0347   0.01006   0.00289   0.0192   0.4775   0.7932
   0.000  -0.0034   0.01010   0.00295   0.0189   0.4649   0.8311
   0.250   0.0314   0.01020   0.00302   0.0179   0.4522   0.8630
   0.500   0.0688   0.01033   0.00311   0.0163   0.4396   0.8877
   0.750   0.1056   0.01047   0.00319   0.0148   0.4276   0.9076
   1.000   0.1419   0.01063   0.00328   0.0133   0.4170   0.9232
   1.250   0.1787   0.01080   0.00336   0.0117   0.4070   0.9358
   1.500   0.2155   0.01095   0.00346   0.0100   0.3968   0.9465
   1.750   0.2501   0.01111   0.00355   0.0087   0.3877   0.9568
   2.000   0.2860   0.01127   0.00364   0.0072   0.3791   0.9657
   2.250   0.3230   0.01141   0.00374   0.0053   0.3707   0.9730
   2.500   0.3581   0.01157   0.00383   0.0038   0.3628   0.9809
   2.750   0.3967   0.01167   0.00391   0.0016   0.3547   0.9865
   3.000   0.4335   0.01182   0.00400  -0.0004   0.3476   0.9926
   3.250   0.4722   0.01189   0.00408  -0.0027   0.3395   0.9978
   3.500   0.5023   0.01203   0.00418  -0.0033   0.3332   1.0000
   3.750   0.5259   0.01214   0.00431  -0.0025   0.3267   1.0000
   4.000   0.5493   0.01228   0.00443  -0.0017   0.3206   1.0000
   4.250   0.5729   0.01244   0.00459  -0.0009   0.3146   1.0000
   4.500   0.5965   0.01259   0.00476  -0.0002   0.3083   1.0000
   4.750   0.6199   0.01278   0.00493   0.0006   0.3027   1.0000
   5.000   0.6438   0.01293   0.00514   0.0014   0.2961   1.0000
   5.250   0.6673   0.01314   0.00534   0.0022   0.2901   1.0000
   5.500   0.6911   0.01332   0.00558   0.0029   0.2838   1.0000
   5.750   0.7147   0.01352   0.00580   0.0037   0.2772   1.0000
   6.000   0.7384   0.01374   0.00606   0.0045   0.2708   1.0000
   6.250   0.7620   0.01395   0.00633   0.0053   0.2637   1.0000
   6.500   0.7854   0.01419   0.00660   0.0061   0.2568   1.0000
   6.750   0.8089   0.01441   0.00688   0.0068   0.2490   1.0000
   7.000   0.8323   0.01466   0.00719   0.0076   0.2413   1.0000
   7.250   0.8554   0.01493   0.00749   0.0084   0.2328   1.0000
   7.500   0.8787   0.01519   0.00785   0.0092   0.2238   1.0000
   7.750   0.9014   0.01549   0.00819   0.0101   0.2144   1.0000
   8.000   0.9238   0.01582   0.00855   0.0109   0.2039   1.0000
   8.250   0.9461   0.01617   0.00896   0.0118   0.1928   1.0000
   8.500   0.9679   0.01657   0.00939   0.0127   0.1811   1.0000
   8.750   0.9890   0.01703   0.00990   0.0136   0.1693   1.0000
   9.000   1.0093   0.01755   0.01043   0.0146   0.1574   1.0000
   9.250   1.0289   0.01813   0.01102   0.0157   0.1459   1.0000
   9.500   1.0476   0.01878   0.01168   0.0168   0.1344   1.0000
   9.750   1.0661   0.01943   0.01237   0.0180   0.1232   1.0000
  10.000   1.0841   0.02011   0.01310   0.0191   0.1128   1.0000
  10.250   1.1011   0.02086   0.01391   0.0204   0.1033   1.0000
  10.500   1.1164   0.02171   0.01478   0.0217   0.0940   1.0000
  10.750   1.1311   0.02258   0.01568   0.0231   0.0844   1.0000
  11.000   1.1446   0.02349   0.01665   0.0246   0.0753   1.0000
  11.250   1.1555   0.02453   0.01772   0.0262   0.0670   1.0000
  11.500   1.1630   0.02574   0.01894   0.0280   0.0593   1.0000
  11.750   1.1690   0.02690   0.02017   0.0301   0.0523   1.0000
  12.000   1.1668   0.02837   0.02167   0.0327   0.0476   1.0000
  12.250   1.1664   0.02999   0.02340   0.0343   0.0430   1.0000
  12.500   1.1618   0.03236   0.02584   0.0349   0.0392   1.0000
  12.750   1.1586   0.03503   0.02863   0.0347   0.0361   1.0000
  13.000   1.1543   0.03816   0.03185   0.0338   0.0331   1.0000
  13.250   1.1464   0.04195   0.03573   0.0324   0.0308   1.0000
  13.500   1.1367   0.04616   0.04003   0.0307   0.0291   1.0000
  13.750   1.1297   0.05013   0.04414   0.0291   0.0275   1.0000
  14.000   1.1198   0.05455   0.04867   0.0272   0.0258   1.0000
  14.250   1.1075   0.05939   0.05359   0.0251   0.0242   1.0000
  14.500   1.0946   0.06438   0.05869   0.0229   0.0236   1.0000
  14.750   1.0799   0.06974   0.06414   0.0205   0.0228   1.0000
  15.000   1.0662   0.07508   0.06956   0.0181   0.0220   1.0000
  15.250   1.0559   0.08015   0.07475   0.0157   0.0212   1.0000
  15.500   1.0450   0.08546   0.08017   0.0133   0.0202   1.0000
  15.750   1.0338   0.09095   0.08578   0.0107   0.0196   1.0000
  16.000   1.0217   0.09680   0.09171   0.0079   0.0185   1.0000
  16.250   1.0089   0.10284   0.09783   0.0050   0.0179   1.0000
  16.500   0.9980   0.10869   0.10376   0.0021   0.0175   1.0000
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