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MH 91 14.98% (mh91-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 91 14.98% (mh91-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.65 at α=10.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh91-il-1000000.txt
Download as CSV file: xf-mh91-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 91  14.98%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.9142   0.08405   0.08150  -0.0070   1.0000   0.0080
 -15.000  -0.9294   0.07694   0.07425  -0.0119   1.0000   0.0080
 -14.750  -0.9406   0.07106   0.06825  -0.0157   1.0000   0.0080
 -14.500  -0.9456   0.06668   0.06378  -0.0184   1.0000   0.0080
 -14.250  -0.9563   0.06175   0.05873  -0.0211   1.0000   0.0079
 -14.000  -0.9648   0.05753   0.05439  -0.0232   1.0000   0.0079
 -13.750  -0.9930   0.05070   0.04736  -0.0249   1.0000   0.0078
 -13.500  -1.0076   0.04639   0.04288  -0.0256   1.0000   0.0077
 -13.250  -1.0180   0.04285   0.03919  -0.0254   1.0000   0.0076
 -13.000  -1.0299   0.03936   0.03550  -0.0245   1.0000   0.0076
 -12.750  -1.0325   0.03699   0.03301  -0.0234   1.0000   0.0076
 -12.500  -1.0385   0.03431   0.03014  -0.0216   1.0000   0.0075
 -12.250  -1.0398   0.03213   0.02780  -0.0197   1.0000   0.0075
 -12.000  -1.0381   0.03023   0.02575  -0.0176   1.0000   0.0075
 -11.750  -1.0328   0.02872   0.02413  -0.0156   1.0000   0.0075
 -11.500  -1.0272   0.02714   0.02241  -0.0134   1.0000   0.0075
 -11.250  -1.0189   0.02583   0.02100  -0.0113   1.0000   0.0075
 -11.000  -1.0094   0.02460   0.01968  -0.0091   1.0000   0.0075
 -10.750  -0.9989   0.02346   0.01844  -0.0069   1.0000   0.0075
 -10.500  -0.9872   0.02244   0.01734  -0.0048   1.0000   0.0075
 -10.250  -0.9743   0.02149   0.01632  -0.0027   1.0000   0.0076
 -10.000  -0.9591   0.02061   0.01537  -0.0009   1.0000   0.0076
  -9.750  -0.9416   0.01975   0.01444   0.0005   1.0000   0.0077
  -9.500  -0.9183   0.01897   0.01352   0.0009   0.9259   0.0077
  -9.250  -0.9040   0.01843   0.01284   0.0034   0.8954   0.0078
  -9.000  -0.8854   0.01797   0.01226   0.0050   0.8737   0.0079
  -8.750  -0.8709   0.01700   0.01115   0.0072   0.8549   0.0080
  -8.500  -0.8552   0.01609   0.01012   0.0092   0.8382   0.0082
  -8.250  -0.8352   0.01552   0.00947   0.0105   0.8232   0.0084
  -8.000  -0.8138   0.01503   0.00891   0.0117   0.8087   0.0087
  -7.750  -0.7910   0.01462   0.00844   0.0126   0.7946   0.0090
  -7.500  -0.7680   0.01418   0.00794   0.0135   0.7812   0.0092
  -7.250  -0.7441   0.01383   0.00751   0.0143   0.7686   0.0096
  -7.000  -0.7202   0.01347   0.00706   0.0151   0.7556   0.0099
  -6.750  -0.6953   0.01315   0.00669   0.0157   0.7427   0.0101
  -6.500  -0.6725   0.01260   0.00607   0.0167   0.7306   0.0107
  -6.250  -0.6477   0.01227   0.00569   0.0173   0.7184   0.0112
  -6.000  -0.6221   0.01198   0.00535   0.0178   0.7060   0.0118
  -5.750  -0.5961   0.01172   0.00504   0.0183   0.6941   0.0126
  -5.500  -0.5709   0.01138   0.00465   0.0188   0.6821   0.0138
  -5.250  -0.5446   0.01115   0.00437   0.0193   0.6698   0.0154
  -5.000  -0.5186   0.01085   0.00405   0.0197   0.6582   0.0187
  -4.750  -0.4929   0.01055   0.00375   0.0202   0.6464   0.0258
  -4.500  -0.4674   0.01020   0.00347   0.0207   0.6346   0.0419
  -4.250  -0.4424   0.00980   0.00319   0.0212   0.6236   0.0709
  -4.000  -0.4183   0.00932   0.00290   0.0218   0.6117   0.1192
  -3.750  -0.3944   0.00879   0.00263   0.0225   0.6004   0.1814
  -3.500  -0.3703   0.00831   0.00239   0.0231   0.5896   0.2473
  -3.250  -0.3456   0.00792   0.00220   0.0236   0.5776   0.3093
  -3.000  -0.3201   0.00758   0.00205   0.0240   0.5661   0.3641
  -2.750  -0.2943   0.00730   0.00192   0.0244   0.5552   0.4142
  -2.500  -0.2685   0.00702   0.00181   0.0248   0.5434   0.4700
  -2.250  -0.2425   0.00678   0.00172   0.0252   0.5320   0.5218
  -2.000  -0.2161   0.00659   0.00164   0.0256   0.5207   0.5645
  -1.750  -0.1896   0.00642   0.00158   0.0259   0.5091   0.6084
  -1.500  -0.1624   0.00631   0.00153   0.0262   0.4976   0.6405
  -1.250  -0.1349   0.00625   0.00150   0.0264   0.4861   0.6674
  -1.000  -0.1071   0.00620   0.00148   0.0266   0.4746   0.6924
  -0.750  -0.0790   0.00619   0.00148   0.0267   0.4633   0.7143
  -0.500  -0.0509   0.00620   0.00148   0.0268   0.4517   0.7339
  -0.250  -0.0227   0.00621   0.00149   0.0269   0.4407   0.7513
   0.000   0.0057   0.00624   0.00151   0.0269   0.4298   0.7662
   0.250   0.0340   0.00629   0.00154   0.0270   0.4183   0.7781
   0.500   0.0628   0.00633   0.00156   0.0270   0.4079   0.7888
   0.750   0.0913   0.00640   0.00159   0.0270   0.3974   0.7989
   1.000   0.1198   0.00647   0.00163   0.0270   0.3865   0.8076
   1.250   0.1485   0.00653   0.00167   0.0269   0.3773   0.8163
   1.500   0.1770   0.00663   0.00172   0.0269   0.3673   0.8240
   1.750   0.2056   0.00669   0.00177   0.0269   0.3581   0.8314
   2.250   0.2625   0.00686   0.00190   0.0268   0.3408   0.8452
   2.500   0.2909   0.00697   0.00197   0.0268   0.3327   0.8521
   2.750   0.3194   0.00705   0.00203   0.0268   0.3250   0.8585
   3.000   0.3472   0.00717   0.00213   0.0269   0.3168   0.8655
   3.250   0.3755   0.00727   0.00222   0.0269   0.3098   0.8727
   3.500   0.4032   0.00739   0.00232   0.0270   0.3022   0.8788
   3.750   0.4313   0.00747   0.00241   0.0270   0.2965   0.8844
   4.000   0.4593   0.00760   0.00250   0.0270   0.2895   0.8899
   4.250   0.4871   0.00771   0.00261   0.0270   0.2828   0.8948
   4.500   0.5148   0.00781   0.00271   0.0272   0.2770   0.8997
   4.750   0.5422   0.00797   0.00283   0.0272   0.2704   0.9049
   5.000   0.5702   0.00808   0.00294   0.0272   0.2653   0.9097
   5.250   0.5972   0.00819   0.00306   0.0274   0.2592   0.9144
   5.500   0.6238   0.00836   0.00321   0.0276   0.2527   0.9194
   5.750   0.6513   0.00846   0.00332   0.0277   0.2482   0.9245
   6.000   0.6778   0.00860   0.00345   0.0280   0.2425   0.9294
   6.250   0.7034   0.00877   0.00362   0.0284   0.2364   0.9348
   6.500   0.7296   0.00889   0.00375   0.0287   0.2318   0.9409
   6.750   0.7548   0.00904   0.00390   0.0293   0.2258   0.9463
   7.000   0.7797   0.00921   0.00406   0.0298   0.2202   0.9521
   7.250   0.8052   0.00934   0.00420   0.0302   0.2152   0.9576
   7.500   0.8310   0.00953   0.00438   0.0305   0.2096   0.9625
   7.750   0.8568   0.00970   0.00456   0.0308   0.2049   0.9682
   8.000   0.8850   0.00986   0.00473   0.0306   0.2001   0.9726
   8.250   0.9149   0.01011   0.00496   0.0299   0.1943   0.9761
   8.500   0.9452   0.01031   0.00517   0.0291   0.1898   0.9801
   8.750   0.9760   0.01052   0.00538   0.0282   0.1853   0.9834
   9.000   1.0095   0.01082   0.00567   0.0266   0.1794   0.9851
   9.250   1.0436   0.01105   0.00591   0.0250   0.1751   0.9866
   9.500   1.0772   0.01130   0.00617   0.0234   0.1703   0.9883
   9.750   1.1094   0.01167   0.00651   0.0220   0.1645   0.9906
  10.000   1.1413   0.01188   0.00676   0.0208   0.1606   0.9930
  10.250   1.1742   0.01218   0.00706   0.0193   0.1556   0.9948
  10.500   1.2069   0.01258   0.00743   0.0177   0.1500   0.9969
  10.750   1.2400   0.01283   0.00772   0.0161   0.1457   0.9988
  11.000   1.2649   0.01320   0.00807   0.0160   0.1404   1.0000
  11.250   1.2749   0.01349   0.00838   0.0189   0.1365   1.0000
  11.500   1.2904   0.01375   0.00866   0.0208   0.1328   1.0000
  11.750   1.3062   0.01414   0.00903   0.0225   0.1279   1.0000
  12.000   1.3236   0.01454   0.00944   0.0238   0.1230   1.0000
  12.250   1.3413   0.01495   0.00986   0.0250   0.1180   1.0000
  12.500   1.3564   0.01549   0.01038   0.0264   0.1121   1.0000
  12.750   1.3717   0.01596   0.01086   0.0279   0.1073   1.0000
  13.000   1.3785   0.01661   0.01150   0.0306   0.1024   1.0000
  13.250   1.3888   0.01720   0.01212   0.0325   0.0987   1.0000
  13.500   1.3973   0.01798   0.01292   0.0344   0.0949   1.0000
  13.750   1.4035   0.01899   0.01394   0.0361   0.0908   1.0000
  14.000   1.4140   0.01986   0.01486   0.0372   0.0877   1.0000
  14.250   1.4212   0.02103   0.01604   0.0383   0.0845   1.0000
  14.500   1.4253   0.02250   0.01753   0.0393   0.0808   1.0000
  14.750   1.4347   0.02369   0.01878   0.0400   0.0786   1.0000
  15.000   1.4406   0.02521   0.02035   0.0405   0.0763   1.0000
  15.250   1.4429   0.02711   0.02228   0.0409   0.0736   1.0000
  15.500   1.4455   0.02910   0.02432   0.0412   0.0710   1.0000
  15.750   1.4506   0.03093   0.02622   0.0412   0.0693   1.0000
  16.000   1.4520   0.03317   0.02852   0.0411   0.0674   1.0000
  16.250   1.4494   0.03588   0.03128   0.0408   0.0655   1.0000
  16.500   1.4436   0.03901   0.03446   0.0403   0.0635   1.0000
  16.750   1.4432   0.04166   0.03720   0.0398   0.0622   1.0000
  17.000   1.4413   0.04453   0.04015   0.0391   0.0609   1.0000
  17.250   1.4355   0.04791   0.04360   0.0382   0.0593   1.0000
  17.500   1.4270   0.05177   0.04753   0.0370   0.0581   1.0000
  17.750   1.4143   0.05620   0.05203   0.0355   0.0565   1.0000
  18.000   1.4011   0.06085   0.05677   0.0338   0.0552   1.0000
  18.250   1.3963   0.06453   0.06053   0.0324   0.0541   1.0000
  18.500   1.3862   0.06897   0.06506   0.0306   0.0530   1.0000
  18.750   1.3729   0.07392   0.07010   0.0286   0.0517   1.0000
  19.000   1.3579   0.07923   0.07548   0.0263   0.0506   1.0000
  19.250   1.3412   0.08488   0.08121   0.0237   0.0494   1.0000
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