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MH 93 15.98% (mh93-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: MH 93 15.98% (mh93-il)
Reynolds number: 100,000
Max Cl/Cd: 39.75 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh93-il-100000-n5.txt
Download as CSV file: xf-mh93-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 93  15.98%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.6983   0.09981   0.09460  -0.0032   1.0000   0.0233
 -13.250  -0.7524   0.08505   0.07950  -0.0138   1.0000   0.0226
 -13.000  -0.7922   0.07552   0.06964  -0.0198   1.0000   0.0223
 -12.750  -0.8193   0.06905   0.06289  -0.0227   1.0000   0.0222
 -12.500  -0.8408   0.06390   0.05744  -0.0241   1.0000   0.0221
 -12.250  -0.8562   0.05976   0.05304  -0.0244   1.0000   0.0221
 -12.000  -0.8659   0.05636   0.04942  -0.0239   1.0000   0.0221
 -11.750  -0.8724   0.05332   0.04616  -0.0230   1.0000   0.0222
 -11.500  -0.8753   0.05062   0.04325  -0.0218   1.0000   0.0223
 -11.250  -0.8750   0.04816   0.04059  -0.0204   1.0000   0.0225
 -11.000  -0.8719   0.04584   0.03807  -0.0189   1.0000   0.0227
 -10.750  -0.8657   0.04366   0.03570  -0.0175   1.0000   0.0229
 -10.500  -0.8567   0.04160   0.03345  -0.0161   1.0000   0.0233
 -10.250  -0.8443   0.03964   0.03130  -0.0148   1.0000   0.0237
 -10.000  -0.8290   0.03775   0.02921  -0.0138   1.0000   0.0242
  -9.750  -0.8111   0.03596   0.02724  -0.0129   1.0000   0.0247
  -9.500  -0.7916   0.03433   0.02546  -0.0122   1.0000   0.0253
  -9.250  -0.7745   0.03302   0.02418  -0.0114   1.0000   0.0261
  -9.000  -0.7572   0.03184   0.02297  -0.0105   1.0000   0.0273
  -8.750  -0.7384   0.03063   0.02164  -0.0095   1.0000   0.0291
  -8.500  -0.7216   0.02946   0.02053  -0.0086   1.0000   0.0305
  -8.250  -0.7046   0.02841   0.01948  -0.0075   1.0000   0.0319
  -8.000  -0.6879   0.02737   0.01839  -0.0064   1.0000   0.0334
  -7.500  -0.6399   0.02530   0.01620  -0.0069   0.9234   0.0387
  -7.250  -0.6222   0.02447   0.01534  -0.0055   0.8967   0.0428
  -7.000  -0.6081   0.02372   0.01450  -0.0033   0.8746   0.0471
  -6.750  -0.5944   0.02299   0.01371  -0.0009   0.8553   0.0533
  -6.500  -0.5805   0.02222   0.01294   0.0015   0.8382   0.0631
  -6.250  -0.5667   0.02138   0.01215   0.0039   0.8228   0.0806
  -6.000  -0.5533   0.02042   0.01140   0.0062   0.8083   0.1156
  -5.750  -0.5408   0.01935   0.01074   0.0084   0.7938   0.1837
  -5.500  -0.5284   0.01840   0.01023   0.0108   0.7803   0.2672
  -5.250  -0.5141   0.01772   0.00984   0.0132   0.7679   0.3399
  -5.000  -0.4983   0.01716   0.00954   0.0154   0.7553   0.4034
  -4.750  -0.4804   0.01674   0.00933   0.0175   0.7426   0.4623
  -4.500  -0.4612   0.01642   0.00916   0.0196   0.7311   0.5149
  -4.250  -0.4399   0.01620   0.00908   0.0214   0.7190   0.5627
  -4.000  -0.4162   0.01609   0.00904   0.0228   0.7068   0.6034
  -3.750  -0.3906   0.01607   0.00901   0.0240   0.6959   0.6350
  -3.500  -0.3643   0.01609   0.00898   0.0250   0.6834   0.6613
  -3.250  -0.3364   0.01618   0.00902   0.0257   0.6717   0.6838
  -3.000  -0.3092   0.01628   0.00901   0.0266   0.6609   0.7044
  -2.750  -0.2814   0.01640   0.00904   0.0272   0.6483   0.7231
  -2.500  -0.2537   0.01653   0.00904   0.0279   0.6372   0.7393
  -2.250  -0.2262   0.01664   0.00904   0.0285   0.6258   0.7538
  -2.000  -0.1997   0.01674   0.00903   0.0293   0.6140   0.7680
  -1.750  -0.1733   0.01685   0.00898   0.0301   0.6037   0.7811
  -1.500  -0.1424   0.01704   0.00908   0.0300   0.5914   0.7908
  -1.250  -0.1170   0.01712   0.00904   0.0309   0.5805   0.8029
  -1.000  -0.0862   0.01730   0.00909   0.0309   0.5696   0.8118
  -0.750  -0.0593   0.01741   0.00911   0.0314   0.5581   0.8221
  -0.500  -0.0292   0.01758   0.00915   0.0315   0.5476   0.8307
  -0.250  -0.0016   0.01770   0.00918   0.0318   0.5362   0.8401
   0.000   0.0300   0.01787   0.00926   0.0315   0.5253   0.8479
   0.250   0.0565   0.01798   0.00925   0.0321   0.5153   0.8574
   0.500   0.0907   0.01817   0.00937   0.0312   0.5036   0.8638
   0.750   0.1138   0.01824   0.00932   0.0322   0.4945   0.8739
   1.000   0.1504   0.01840   0.00943   0.0308   0.4827   0.8785
   1.250   0.1804   0.01852   0.00946   0.0305   0.4725   0.8855
   1.500   0.2072   0.01861   0.00946   0.0307   0.4630   0.8930
   1.750   0.2428   0.01875   0.00955   0.0293   0.4521   0.8974
   2.000   0.2715   0.01885   0.00954   0.0291   0.4433   0.9042
   2.250   0.2999   0.01896   0.00964   0.0289   0.4331   0.9106
   2.500   0.3363   0.01908   0.00965   0.0272   0.4239   0.9145
   2.750   0.3673   0.01921   0.00977   0.0264   0.4139   0.9202
   3.000   0.3936   0.01932   0.00981   0.0266   0.4060   0.9268
   3.250   0.4303   0.01946   0.00995   0.0246   0.3960   0.9304
   3.500   0.4623   0.01961   0.01002   0.0236   0.3879   0.9354
   3.750   0.4876   0.01976   0.01019   0.0238   0.3794   0.9421
   4.000   0.5236   0.01991   0.01027   0.0220   0.3717   0.9455
   4.250   0.5563   0.02009   0.01047   0.0207   0.3627   0.9502
   4.500   0.5817   0.02027   0.01059   0.0209   0.3563   0.9564
   4.750   0.6173   0.02047   0.01085   0.0189   0.3476   0.9597
   5.000   0.6496   0.02065   0.01098   0.0177   0.3405   0.9640
   5.250   0.6773   0.02091   0.01128   0.0173   0.3335   0.9693
   5.500   0.7102   0.02112   0.01151   0.0158   0.3262   0.9729
   5.750   0.7421   0.02136   0.01174   0.0145   0.3199   0.9768
   6.000   0.7708   0.02166   0.01211   0.0138   0.3127   0.9815
   6.250   0.8026   0.02190   0.01231   0.0125   0.3067   0.9850
   6.500   0.8338   0.02223   0.01274   0.0111   0.3001   0.9889
   6.750   0.8635   0.02256   0.01311   0.0101   0.2936   0.9930
   7.000   0.8945   0.02286   0.01337   0.0089   0.2882   0.9965
   7.250   0.9237   0.02328   0.01396   0.0078   0.2815   1.0000
   7.500   0.9401   0.02365   0.01436   0.0093   0.2766   1.0000
   8.000   0.9705   0.02453   0.01534   0.0125   0.2671   1.0000
   8.250   0.9845   0.02497   0.01585   0.0144   0.2622   1.0000
   8.500   0.9989   0.02537   0.01624   0.0162   0.2581   1.0000
   8.750   1.0111   0.02589   0.01683   0.0182   0.2537   1.0000
   9.000   1.0213   0.02644   0.01750   0.0205   0.2488   1.0000
   9.250   1.0323   0.02690   0.01800   0.0228   0.2445   1.0000
   9.500   1.0449   0.02732   0.01836   0.0249   0.2409   1.0000
   9.750   1.0502   0.02800   0.01922   0.0278   0.2363   1.0000
  10.000   1.0569   0.02859   0.01990   0.0305   0.2318   1.0000
  10.250   1.0658   0.02908   0.02039   0.0329   0.2278   1.0000
  10.500   1.0750   0.02964   0.02094   0.0352   0.2241   1.0000
  10.750   1.0766   0.03048   0.02196   0.0382   0.2196   1.0000
  11.000   1.0817   0.03121   0.02275   0.0406   0.2154   1.0000
  11.250   1.0888   0.03181   0.02334   0.0429   0.2117   1.0000
  11.500   1.0914   0.03272   0.02431   0.0453   0.2080   1.0000
  11.750   1.0896   0.03401   0.02575   0.0475   0.2040   1.0000
  12.000   1.0932   0.03516   0.02698   0.0489   0.1999   1.0000
  12.250   1.1031   0.03604   0.02784   0.0499   0.1963   1.0000
  12.500   1.1019   0.03780   0.02973   0.0509   0.1925   1.0000
  12.750   1.0980   0.03989   0.03198   0.0516   0.1884   1.0000
  13.000   1.1010   0.04154   0.03370   0.0521   0.1846   1.0000
  13.250   1.1139   0.04243   0.03453   0.0525   0.1810   1.0000
  13.500   1.0980   0.04599   0.03833   0.0522   0.1772   1.0000
  13.750   1.0878   0.04928   0.04177   0.0517   0.1733   1.0000
  14.000   1.0902   0.05137   0.04390   0.0514   0.1696   1.0000
  14.250   1.0980   0.05295   0.04548   0.0514   0.1663   1.0000
  14.500   1.0620   0.05972   0.05253   0.0488   0.1625   1.0000
  14.750   1.0361   0.06578   0.05874   0.0463   0.1586   1.0000
  15.000   1.0492   0.06679   0.05973   0.0463   0.1551   1.0000
  15.250   1.0200   0.07383   0.06691   0.0431   0.1515   1.0000
  15.500   0.8287   0.10932   0.10263   0.0253   0.1375   1.0000
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