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MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 94 16.03% (mh94-il)
Reynolds number: 1,000,000
Max Cl/Cd: 76.69 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh94-il-1000000.txt
Download as CSV file: xf-mh94-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 94  16.03%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.8186   0.12754   0.12479  -0.0432   1.0000   0.0087
 -19.250  -0.8599   0.11578   0.11276  -0.0492   1.0000   0.0084
 -19.000  -0.8733   0.10964   0.10654  -0.0522   1.0000   0.0085
 -18.750  -0.8891   0.10323   0.10001  -0.0553   1.0000   0.0086
 -18.500  -0.9107   0.09613   0.09272  -0.0584   1.0000   0.0084
 -18.250  -0.9180   0.09154   0.08807  -0.0605   1.0000   0.0085
 -18.000  -0.9303   0.08630   0.08273  -0.0626   1.0000   0.0085
 -17.750  -0.9426   0.08125   0.07754  -0.0645   1.0000   0.0084
 -17.500  -0.9460   0.07749   0.07376  -0.0661   1.0000   0.0086
 -17.250  -0.9551   0.07318   0.06935  -0.0675   1.0000   0.0086
 -17.000  -0.9623   0.06927   0.06534  -0.0686   1.0000   0.0086
 -16.750  -0.9696   0.06548   0.06145  -0.0695   1.0000   0.0086
 -16.500  -0.9723   0.06231   0.05823  -0.0703   1.0000   0.0088
 -16.250  -0.9775   0.05901   0.05485  -0.0709   1.0000   0.0089
 -16.000  -0.9818   0.05599   0.05175  -0.0711   1.0000   0.0088
 -15.750  -0.9879   0.05292   0.04858  -0.0710   1.0000   0.0088
 -15.500  -0.9889   0.05046   0.04606  -0.0710   1.0000   0.0089
 -15.250  -0.9951   0.04763   0.04314  -0.0704   1.0000   0.0088
 -15.000  -0.9980   0.04525   0.04069  -0.0698   1.0000   0.0089
 -14.750  -0.9989   0.04316   0.03854  -0.0691   1.0000   0.0090
 -14.500  -1.0013   0.04105   0.03636  -0.0681   1.0000   0.0091
 -14.250  -1.0017   0.03920   0.03445  -0.0669   1.0000   0.0092
 -14.000  -1.0049   0.03723   0.03241  -0.0654   1.0000   0.0091
 -13.750  -1.0043   0.03565   0.03077  -0.0640   1.0000   0.0093
 -13.500  -1.0089   0.03376   0.02881  -0.0620   1.0000   0.0092
 -13.250  -1.0078   0.03241   0.02740  -0.0601   1.0000   0.0094
 -13.000  -1.0122   0.03075   0.02568  -0.0577   1.0000   0.0093
 -12.750  -1.0124   0.02951   0.02439  -0.0554   1.0000   0.0094
 -12.500  -1.0111   0.02826   0.02308  -0.0533   0.9999   0.0095
 -12.250  -0.9942   0.02673   0.02149  -0.0543   0.9985   0.0095
 -12.000  -0.9746   0.02548   0.02018  -0.0554   0.9968   0.0097
 -11.750  -0.9541   0.02429   0.01892  -0.0565   0.9952   0.0098
 -11.500  -0.9319   0.02321   0.01779  -0.0578   0.9938   0.0098
 -11.250  -0.9125   0.02220   0.01673  -0.0582   0.9916   0.0100
 -11.000  -0.8925   0.02134   0.01582  -0.0585   0.9889   0.0100
 -10.750  -0.8685   0.02060   0.01504  -0.0593   0.9868   0.0101
 -10.500  -0.8501   0.01921   0.01358  -0.0600   0.9844   0.0103
 -10.250  -0.8250   0.01831   0.01262  -0.0612   0.9830   0.0105
 -10.000  -0.8148   0.01762   0.01189  -0.0588   0.9774   0.0108
  -9.750  -0.7897   0.01702   0.01127  -0.0591   0.9749   0.0109
  -9.500  -0.7607   0.01641   0.01065  -0.0601   0.9733   0.0112
  -9.250  -0.7301   0.01581   0.01002  -0.0613   0.9721   0.0116
  -9.000  -0.6979   0.01528   0.00946  -0.0628   0.9712   0.0121
  -8.750  -0.6777   0.01484   0.00900  -0.0617   0.9674   0.0124
  -8.500  -0.6550   0.01434   0.00847  -0.0611   0.9636   0.0128
  -8.250  -0.6256   0.01380   0.00793  -0.0619   0.9618   0.0138
  -8.000  -0.5929   0.01337   0.00749  -0.0632   0.9607   0.0149
  -7.750  -0.5598   0.01286   0.00699  -0.0647   0.9598   0.0167
  -7.500  -0.5270   0.01239   0.00653  -0.0660   0.9588   0.0194
  -7.250  -0.4947   0.01192   0.00610  -0.0672   0.9578   0.0246
  -7.000  -0.4777   0.01155   0.00577  -0.0652   0.9522   0.0312
  -6.750  -0.4519   0.01111   0.00539  -0.0650   0.9487   0.0419
  -6.500  -0.4241   0.01060   0.00498  -0.0652   0.9462   0.0597
  -6.250  -0.3955   0.01004   0.00456  -0.0657   0.9440   0.0858
  -6.000  -0.3760   0.00951   0.00420  -0.0643   0.9390   0.1209
  -5.750  -0.3555   0.00893   0.00384  -0.0630   0.9335   0.1664
  -5.500  -0.3295   0.00837   0.00347  -0.0629   0.9299   0.2121
  -5.250  -0.3052   0.00786   0.00317  -0.0624   0.9254   0.2591
  -5.000  -0.2835   0.00747   0.00294  -0.0612   0.9186   0.3013
  -4.750  -0.2564   0.00706   0.00269  -0.0612   0.9136   0.3439
  -4.500  -0.2315   0.00675   0.00251  -0.0606   0.9070   0.3826
  -4.250  -0.2054   0.00649   0.00235  -0.0602   0.8997   0.4154
  -4.000  -0.1763   0.00631   0.00222  -0.0604   0.8931   0.4380
  -3.750  -0.1499   0.00617   0.00212  -0.0600   0.8840   0.4608
  -3.500  -0.1216   0.00602   0.00202  -0.0599   0.8755   0.4838
  -3.250  -0.0940   0.00594   0.00194  -0.0597   0.8648   0.5004
  -3.000  -0.0663   0.00587   0.00186  -0.0595   0.8538   0.5127
  -2.750  -0.0382   0.00583   0.00179  -0.0594   0.8418   0.5225
  -2.500  -0.0108   0.00581   0.00173  -0.0591   0.8278   0.5325
  -2.250   0.0162   0.00579   0.00168  -0.0588   0.8131   0.5416
  -2.000   0.0432   0.00579   0.00164  -0.0584   0.7978   0.5509
  -1.750   0.0698   0.00580   0.00161  -0.0580   0.7816   0.5597
  -1.500   0.0962   0.00583   0.00158  -0.0575   0.7647   0.5685
  -1.250   0.1224   0.00586   0.00157  -0.0570   0.7473   0.5768
  -1.000   0.1481   0.00591   0.00156  -0.0564   0.7285   0.5862
  -0.750   0.1739   0.00597   0.00156  -0.0559   0.7096   0.5945
  -0.500   0.1993   0.00603   0.00157  -0.0552   0.6898   0.6031
  -0.250   0.2249   0.00612   0.00159  -0.0546   0.6696   0.6106
   0.000   0.2498   0.00619   0.00161  -0.0539   0.6481   0.6186
   0.250   0.2739   0.00632   0.00164  -0.0530   0.6223   0.6263
   0.500   0.2976   0.00646   0.00168  -0.0520   0.5905   0.6336
   0.750   0.3211   0.00662   0.00173  -0.0510   0.5589   0.6412
   1.000   0.3453   0.00680   0.00178  -0.0502   0.5305   0.6483
   1.250   0.3698   0.00692   0.00185  -0.0495   0.5053   0.6559
   1.500   0.3946   0.00708   0.00192  -0.0488   0.4797   0.6634
   1.750   0.4189   0.00726   0.00200  -0.0480   0.4537   0.6704
   2.000   0.4435   0.00742   0.00209  -0.0473   0.4272   0.6777
   2.250   0.4677   0.00764   0.00219  -0.0466   0.4001   0.6849
   2.500   0.4921   0.00781   0.00229  -0.0459   0.3756   0.6920
   2.750   0.5166   0.00800   0.00241  -0.0452   0.3518   0.6994
   3.000   0.5410   0.00823   0.00252  -0.0445   0.3284   0.7062
   3.250   0.5648   0.00842   0.00266  -0.0437   0.3061   0.7137
   3.500   0.5892   0.00863   0.00279  -0.0430   0.2855   0.7210
   3.750   0.6135   0.00884   0.00292  -0.0423   0.2666   0.7277
   4.000   0.6375   0.00903   0.00307  -0.0416   0.2494   0.7349
   4.250   0.6616   0.00925   0.00323  -0.0409   0.2329   0.7420
   4.500   0.6854   0.00947   0.00338  -0.0401   0.2171   0.7487
   4.750   0.7087   0.00969   0.00356  -0.0392   0.2013   0.7560
   5.000   0.7321   0.00993   0.00373  -0.0384   0.1864   0.7629
   5.500   0.7776   0.01040   0.00411  -0.0365   0.1590   0.7774
   5.750   0.7999   0.01065   0.00431  -0.0355   0.1470   0.7843
   6.000   0.8210   0.01087   0.00451  -0.0342   0.1364   0.7917
   6.250   0.8418   0.01112   0.00473  -0.0329   0.1267   0.7998
   6.500   0.8623   0.01139   0.00496  -0.0315   0.1184   0.8072
   6.750   0.8835   0.01160   0.00520  -0.0303   0.1129   0.8152
   7.250   0.9246   0.01212   0.00572  -0.0276   0.1035   0.8317
   7.500   0.9459   0.01235   0.00596  -0.0264   0.1007   0.8405
   7.750   0.9656   0.01260   0.00624  -0.0249   0.0976   0.8495
   8.000   0.9844   0.01294   0.00658  -0.0234   0.0940   0.8595
   8.250   1.0044   0.01314   0.00685  -0.0219   0.0926   0.8698
   8.500   1.0246   0.01336   0.00711  -0.0206   0.0907   0.8806
   8.750   1.0431   0.01361   0.00741  -0.0190   0.0888   0.8935
   9.000   1.0602   0.01388   0.00772  -0.0171   0.0870   0.9086
   9.500   1.0945   0.01449   0.00848  -0.0134   0.0833   0.9632
   9.750   1.1244   0.01479   0.00883  -0.0144   0.0823   1.0000
  10.000   1.1451   0.01512   0.00916  -0.0135   0.0811   1.0000
  10.250   1.1646   0.01547   0.00954  -0.0123   0.0799   1.0000
  10.500   1.1833   0.01587   0.00993  -0.0111   0.0785   1.0000
  10.750   1.2008   0.01633   0.01038  -0.0097   0.0771   1.0000
  11.000   1.2153   0.01691   0.01098  -0.0080   0.0757   1.0000
  11.250   1.2297   0.01751   0.01162  -0.0062   0.0746   1.0000
  11.500   1.2482   0.01791   0.01205  -0.0051   0.0740   1.0000
  11.750   1.2656   0.01837   0.01254  -0.0038   0.0734   1.0000
  12.000   1.2824   0.01885   0.01307  -0.0025   0.0726   1.0000
  12.250   1.2987   0.01937   0.01362  -0.0012   0.0717   1.0000
  12.500   1.3142   0.01995   0.01422   0.0001   0.0709   1.0000
  12.750   1.3291   0.02056   0.01486   0.0015   0.0701   1.0000
  13.000   1.3430   0.02124   0.01556   0.0029   0.0692   1.0000
  13.250   1.3542   0.02208   0.01643   0.0046   0.0683   1.0000
  13.500   1.3614   0.02318   0.01757   0.0066   0.0673   1.0000
  13.750   1.3695   0.02427   0.01871   0.0083   0.0665   1.0000
  14.000   1.3849   0.02494   0.01944   0.0093   0.0661   1.0000
  14.250   1.3983   0.02576   0.02031   0.0104   0.0656   1.0000
  14.500   1.4106   0.02667   0.02127   0.0115   0.0651   1.0000
  14.750   1.4221   0.02765   0.02230   0.0126   0.0645   1.0000
  15.000   1.4339   0.02864   0.02334   0.0136   0.0637   1.0000
  15.250   1.4433   0.02984   0.02460   0.0146   0.0633   1.0000
  15.500   1.4533   0.03103   0.02583   0.0155   0.0626   1.0000
  15.750   1.4624   0.03232   0.02716   0.0163   0.0620   1.0000
  16.000   1.4696   0.03382   0.02871   0.0171   0.0614   1.0000
  16.250   1.4737   0.03562   0.03056   0.0180   0.0607   1.0000
  16.500   1.4742   0.03781   0.03281   0.0187   0.0599   1.0000
  16.750   1.4746   0.04009   0.03516   0.0194   0.0593   1.0000
  17.000   1.4835   0.04168   0.03683   0.0195   0.0590   1.0000
  17.250   1.4907   0.04350   0.03872   0.0197   0.0586   1.0000
  17.500   1.4975   0.04540   0.04069   0.0197   0.0581   1.0000
  17.750   1.5033   0.04744   0.04282   0.0196   0.0576   1.0000
  18.000   1.5075   0.04971   0.04515   0.0194   0.0571   1.0000
  18.250   1.5106   0.05216   0.04767   0.0190   0.0566   1.0000
  18.500   1.5134   0.05471   0.05030   0.0186   0.0561   1.0000
  18.750   1.5150   0.05747   0.05313   0.0179   0.0556   1.0000
  19.000   1.5157   0.06039   0.05611   0.0171   0.0551   1.0000
  19.250   1.5146   0.06361   0.05939   0.0161   0.0545   1.0000
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