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MH 91 14.98% (mh91-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 91 14.98% (mh91-il)
Reynolds number: 1,000,000
Max Cl/Cd: 91.45 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh91-il-1000000-n5.txt
Download as CSV file: xf-mh91-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.9810   0.12898   0.12646   0.0225   1.0000   0.0044
 -18.000  -1.0159   0.11646   0.11376   0.0149   1.0000   0.0044
 -17.750  -1.0448   0.10573   0.10285   0.0084   1.0000   0.0043
 -17.500  -1.0765   0.09484   0.09179   0.0018   1.0000   0.0044
 -17.250  -1.1022   0.08561   0.08239  -0.0038   1.0000   0.0043
 -17.000  -1.1168   0.07872   0.07536  -0.0079   1.0000   0.0043
 -16.750  -1.1342   0.07162   0.06812  -0.0121   1.0000   0.0043
 -16.500  -1.1517   0.06488   0.06123  -0.0159   1.0000   0.0043
 -16.250  -1.1621   0.05961   0.05584  -0.0186   1.0000   0.0043
 -16.000  -1.1716   0.05478   0.05088  -0.0209   1.0000   0.0043
 -15.750  -1.1812   0.05024   0.04621  -0.0227   1.0000   0.0043
 -15.500  -1.1854   0.04668   0.04254  -0.0238   1.0000   0.0043
 -15.250  -1.1909   0.04320   0.03894  -0.0245   1.0000   0.0043
 -15.000  -1.1949   0.04012   0.03576  -0.0247   1.0000   0.0044
 -14.750  -1.1973   0.03742   0.03295  -0.0245   1.0000   0.0044
 -14.500  -1.1944   0.03537   0.03081  -0.0240   1.0000   0.0043
 -14.250  -1.1930   0.03332   0.02866  -0.0231   1.0000   0.0044
 -14.000  -1.1911   0.03141   0.02666  -0.0220   1.0000   0.0044
 -13.750  -1.1866   0.02979   0.02497  -0.0207   1.0000   0.0045
 -13.500  -1.1810   0.02834   0.02343  -0.0192   1.0000   0.0045
 -13.250  -1.1741   0.02705   0.02206  -0.0177   1.0000   0.0045
 -13.000  -1.1660   0.02588   0.02083  -0.0160   1.0000   0.0046
 -12.750  -1.1579   0.02476   0.01964  -0.0142   1.0000   0.0045
 -12.500  -1.1480   0.02378   0.01860  -0.0124   1.0000   0.0046
 -12.250  -1.1361   0.02295   0.01771  -0.0106   1.0000   0.0047
 -12.000  -1.1245   0.02213   0.01684  -0.0087   1.0000   0.0048
 -11.750  -1.1127   0.02133   0.01599  -0.0067   1.0000   0.0048
 -11.500  -1.0991   0.02066   0.01527  -0.0048   1.0000   0.0049
 -11.250  -1.0870   0.01996   0.01451  -0.0026   0.9931   0.0049
 -11.000  -1.0688   0.01943   0.01382  -0.0012   0.9073   0.0049
 -10.750  -1.0570   0.01901   0.01327   0.0015   0.8774   0.0050
 -10.500  -1.0414   0.01847   0.01261   0.0035   0.8555   0.0050
 -10.250  -1.0231   0.01800   0.01205   0.0051   0.8370   0.0051
 -10.000  -1.0041   0.01751   0.01146   0.0065   0.8205   0.0053
  -9.750  -0.9842   0.01704   0.01090   0.0078   0.8054   0.0054
  -9.500  -0.9636   0.01658   0.01035   0.0090   0.7908   0.0054
  -9.250  -0.9420   0.01615   0.00985   0.0100   0.7770   0.0055
  -9.000  -0.9196   0.01577   0.00939   0.0110   0.7636   0.0056
  -8.750  -0.8970   0.01537   0.00892   0.0119   0.7510   0.0057
  -8.500  -0.8737   0.01502   0.00849   0.0127   0.7381   0.0058
  -8.250  -0.8505   0.01462   0.00803   0.0135   0.7257   0.0059
  -8.000  -0.8276   0.01417   0.00751   0.0144   0.7139   0.0062
  -7.750  -0.8035   0.01383   0.00712   0.0151   0.7016   0.0064
  -7.500  -0.7789   0.01350   0.00674   0.0157   0.6892   0.0066
  -7.250  -0.7539   0.01322   0.00641   0.0163   0.6778   0.0068
  -7.000  -0.7287   0.01294   0.00607   0.0168   0.6654   0.0070
  -6.750  -0.7032   0.01268   0.00576   0.0173   0.6531   0.0073
  -6.500  -0.6775   0.01243   0.00546   0.0178   0.6414   0.0076
  -6.250  -0.6515   0.01221   0.00517   0.0182   0.6293   0.0079
  -6.000  -0.6257   0.01193   0.00487   0.0186   0.6174   0.0085
  -5.750  -0.5995   0.01171   0.00461   0.0190   0.6060   0.0092
  -5.500  -0.5730   0.01152   0.00436   0.0194   0.5936   0.0099
  -5.250  -0.5464   0.01131   0.00413   0.0197   0.5817   0.0110
  -5.000  -0.5197   0.01112   0.00391   0.0200   0.5703   0.0125
  -4.750  -0.4930   0.01094   0.00369   0.0203   0.5583   0.0148
  -4.500  -0.4661   0.01075   0.00349   0.0206   0.5472   0.0185
  -4.250  -0.4394   0.01054   0.00329   0.0208   0.5366   0.0250
  -4.000  -0.4128   0.01034   0.00309   0.0211   0.5244   0.0353
  -3.750  -0.3862   0.01010   0.00290   0.0214   0.5137   0.0499
  -3.500  -0.3599   0.00985   0.00271   0.0217   0.5033   0.0718
  -3.250  -0.3345   0.00950   0.00250   0.0221   0.4917   0.1111
  -3.000  -0.3098   0.00907   0.00228   0.0226   0.4810   0.1690
  -2.750  -0.2849   0.00868   0.00209   0.0231   0.4709   0.2288
  -2.500  -0.2601   0.00826   0.00193   0.0236   0.4604   0.2976
  -2.250  -0.2344   0.00796   0.00180   0.0239   0.4499   0.3522
  -2.000  -0.2085   0.00770   0.00169   0.0243   0.4391   0.4041
  -1.750  -0.1825   0.00744   0.00161   0.0246   0.4297   0.4591
  -1.500  -0.1553   0.00732   0.00155   0.0248   0.4185   0.4927
  -1.250  -0.1276   0.00723   0.00150   0.0249   0.4083   0.5195
  -1.000  -0.0998   0.00717   0.00146   0.0250   0.3990   0.5432
  -0.750  -0.0720   0.00711   0.00143   0.0251   0.3882   0.5673
  -0.500  -0.0442   0.00705   0.00141   0.0252   0.3789   0.5926
  -0.250  -0.0166   0.00699   0.00140   0.0253   0.3696   0.6189
   0.000   0.0113   0.00695   0.00139   0.0254   0.3607   0.6439
   0.250   0.0391   0.00694   0.00140   0.0255   0.3508   0.6653
   0.500   0.0673   0.00692   0.00142   0.0255   0.3431   0.6856
   0.750   0.0954   0.00695   0.00145   0.0256   0.3340   0.7035
   1.000   0.1237   0.00696   0.00148   0.0256   0.3260   0.7200
   1.250   0.1521   0.00702   0.00152   0.0256   0.3182   0.7344
   1.500   0.1806   0.00705   0.00156   0.0255   0.3117   0.7479
   1.750   0.2089   0.00711   0.00161   0.0255   0.3035   0.7592
   2.000   0.2375   0.00717   0.00167   0.0255   0.2970   0.7701
   2.250   0.2659   0.00723   0.00173   0.0254   0.2907   0.7803
   2.500   0.2943   0.00731   0.00180   0.0254   0.2845   0.7895
   2.750   0.3228   0.00737   0.00187   0.0253   0.2791   0.7994
   3.000   0.3510   0.00746   0.00195   0.0253   0.2721   0.8093
   3.250   0.3793   0.00755   0.00204   0.0253   0.2664   0.8194
   3.500   0.4076   0.00763   0.00212   0.0253   0.2613   0.8274
   3.750   0.4358   0.00774   0.00222   0.0252   0.2555   0.8345
   4.000   0.4642   0.00784   0.00231   0.0251   0.2504   0.8403
   4.250   0.4923   0.00794   0.00241   0.0251   0.2444   0.8462
   4.500   0.5203   0.00807   0.00252   0.0251   0.2388   0.8521
   4.750   0.5487   0.00818   0.00263   0.0250   0.2347   0.8572
   5.000   0.5765   0.00828   0.00275   0.0250   0.2296   0.8625
   5.250   0.6041   0.00843   0.00288   0.0250   0.2234   0.8681
   5.500   0.6322   0.00856   0.00301   0.0249   0.2192   0.8733
   5.750   0.6598   0.00868   0.00314   0.0249   0.2144   0.8783
   6.000   0.6869   0.00884   0.00329   0.0250   0.2090   0.8841
   6.250   0.7144   0.00898   0.00344   0.0250   0.2043   0.8902
   6.500   0.7414   0.00912   0.00360   0.0251   0.1994   0.8960
   6.750   0.7677   0.00932   0.00378   0.0253   0.1931   0.9022
   7.000   0.7947   0.00948   0.00394   0.0254   0.1882   0.9077
   7.250   0.8213   0.00965   0.00412   0.0255   0.1829   0.9122
   7.500   0.8471   0.00986   0.00432   0.0258   0.1779   0.9172
   7.750   0.8737   0.01002   0.00450   0.0259   0.1741   0.9222
   8.000   0.9000   0.01021   0.00469   0.0260   0.1696   0.9268
   8.250   0.9250   0.01044   0.00492   0.0264   0.1646   0.9317
   8.500   0.9507   0.01062   0.00513   0.0266   0.1609   0.9370
   8.750   0.9762   0.01082   0.00534   0.0269   0.1569   0.9421
   9.000   1.0007   0.01107   0.00559   0.0273   0.1523   0.9475
   9.250   1.0255   0.01129   0.00583   0.0276   0.1485   0.9536
   9.500   1.0507   0.01152   0.00608   0.0279   0.1442   0.9592
   9.750   1.0765   0.01180   0.00637   0.0279   0.1397   0.9651
  10.000   1.1028   0.01208   0.00666   0.0278   0.1356   0.9713
  10.250   1.1321   0.01238   0.00697   0.0270   0.1306   0.9761
  10.500   1.1603   0.01277   0.00734   0.0263   0.1252   0.9815
  10.750   1.1908   0.01309   0.00768   0.0253   0.1210   0.9852
  11.000   1.2206   0.01353   0.00810   0.0241   0.1148   0.9895
  11.250   1.2500   0.01393   0.00852   0.0231   0.1100   0.9947
  11.500   1.2776   0.01440   0.00897   0.0223   0.1046   1.0000
  11.750   1.2937   0.01482   0.00939   0.0238   0.1004   1.0000
  12.000   1.3103   0.01526   0.00984   0.0252   0.0956   1.0000
  12.250   1.3250   0.01581   0.01038   0.0267   0.0909   1.0000
  12.500   1.3392   0.01630   0.01088   0.0283   0.0867   1.0000
  12.750   1.3460   0.01695   0.01152   0.0310   0.0824   1.0000
  13.000   1.3551   0.01760   0.01220   0.0330   0.0793   1.0000
  13.250   1.3640   0.01838   0.01301   0.0348   0.0758   1.0000
  13.500   1.3721   0.01931   0.01395   0.0363   0.0731   1.0000
  13.750   1.3814   0.02027   0.01495   0.0374   0.0706   1.0000
  14.000   1.3908   0.02131   0.01603   0.0384   0.0684   1.0000
  14.250   1.3981   0.02256   0.01732   0.0393   0.0660   1.0000
  14.500   1.4026   0.02413   0.01890   0.0400   0.0630   1.0000
  14.750   1.4106   0.02551   0.02034   0.0405   0.0612   1.0000
  15.000   1.4173   0.02706   0.02195   0.0409   0.0598   1.0000
  15.250   1.4199   0.02904   0.02397   0.0411   0.0574   1.0000
  15.500   1.4207   0.03128   0.02624   0.0411   0.0549   1.0000
  15.750   1.4240   0.03336   0.02839   0.0410   0.0534   1.0000
  16.000   1.4254   0.03570   0.03080   0.0408   0.0521   1.0000
  16.250   1.4239   0.03838   0.03355   0.0403   0.0507   1.0000
  16.500   1.4186   0.04156   0.03678   0.0397   0.0490   1.0000
  16.750   1.4148   0.04465   0.03995   0.0389   0.0477   1.0000
  17.000   1.4110   0.04782   0.04321   0.0381   0.0467   1.0000
  17.250   1.4034   0.05159   0.04705   0.0369   0.0452   1.0000
  17.500   1.3958   0.05544   0.05098   0.0356   0.0443   1.0000
  17.750   1.3828   0.06005   0.05566   0.0339   0.0429   1.0000
  18.000   1.3708   0.06468   0.06038   0.0321   0.0418   1.0000
  18.250   1.3601   0.06921   0.06500   0.0303   0.0407   1.0000
  18.500   1.3483   0.07403   0.06990   0.0283   0.0397   1.0000
  18.750   1.3341   0.07924   0.07520   0.0261   0.0386   1.0000
  19.000   1.3201   0.08455   0.08060   0.0237   0.0379   1.0000
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