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MH 92 15.49% (mh92-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 92 15.49% (mh92-il)
Reynolds number: 1,000,000
Max Cl/Cd: 94.19 at α=10.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh92-il-1000000.txt
Download as CSV file: xf-mh92-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 92  15.49%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.7153   0.12585   0.12412   0.0237   1.0000   0.0084
 -16.000  -0.6999   0.12576   0.12409   0.0235   1.0000   0.0085
 -15.750  -0.9240   0.08958   0.08699  -0.0031   1.0000   0.0077
 -15.500  -0.9627   0.07816   0.07534  -0.0102   1.0000   0.0077
 -15.250  -0.9828   0.07081   0.06783  -0.0146   1.0000   0.0076
 -15.000  -1.0019   0.06420   0.06105  -0.0182   1.0000   0.0076
 -14.750  -1.0217   0.05802   0.05468  -0.0211   1.0000   0.0075
 -14.500  -1.0337   0.05341   0.04992  -0.0227   1.0000   0.0075
 -14.250  -1.0466   0.04897   0.04531  -0.0238   1.0000   0.0075
 -14.000  -1.0544   0.04545   0.04165  -0.0241   1.0000   0.0074
 -13.750  -1.0630   0.04202   0.03804  -0.0239   1.0000   0.0075
 -13.500  -1.0671   0.03925   0.03513  -0.0232   1.0000   0.0074
 -13.250  -1.0693   0.03675   0.03249  -0.0222   1.0000   0.0074
 -13.000  -1.0700   0.03448   0.03009  -0.0208   1.0000   0.0074
 -12.750  -1.0679   0.03254   0.02802  -0.0193   1.0000   0.0074
 -12.500  -1.0641   0.03079   0.02616  -0.0177   1.0000   0.0074
 -12.250  -1.0590   0.02916   0.02442  -0.0160   1.0000   0.0074
 -12.000  -1.0519   0.02776   0.02292  -0.0142   1.0000   0.0074
 -11.750  -1.0437   0.02646   0.02152  -0.0123   1.0000   0.0075
 -11.500  -1.0347   0.02521   0.02018  -0.0104   1.0000   0.0075
 -11.250  -1.0241   0.02413   0.01902  -0.0085   1.0000   0.0076
 -11.000  -1.0124   0.02316   0.01798  -0.0066   1.0000   0.0076
 -10.750  -1.0007   0.02216   0.01691  -0.0047   1.0000   0.0076
 -10.500  -0.9866   0.02139   0.01609  -0.0028   1.0000   0.0077
 -10.250  -0.9732   0.02056   0.01520  -0.0009   1.0000   0.0077
 -10.000  -0.9526   0.01992   0.01450  -0.0001   0.9643   0.0078
  -9.750  -0.9487   0.01873   0.01309   0.0038   0.9028   0.0080
  -9.500  -0.9397   0.01794   0.01215   0.0069   0.8758   0.0082
  -9.250  -0.9236   0.01736   0.01147   0.0089   0.8557   0.0082
  -9.000  -0.9060   0.01680   0.01082   0.0106   0.8384   0.0085
  -8.750  -0.8861   0.01635   0.01030   0.0120   0.8226   0.0088
  -8.500  -0.8655   0.01591   0.00978   0.0132   0.8077   0.0091
  -8.250  -0.8447   0.01542   0.00921   0.0145   0.7935   0.0091
  -8.000  -0.8225   0.01502   0.00874   0.0155   0.7803   0.0095
  -7.750  -0.7999   0.01462   0.00827   0.0165   0.7677   0.0097
  -7.250  -0.7536   0.01386   0.00736   0.0182   0.7423   0.0101
  -7.000  -0.7321   0.01328   0.00672   0.0194   0.7307   0.0107
  -6.500  -0.6829   0.01264   0.00599   0.0207   0.7068   0.0116
  -6.250  -0.6578   0.01235   0.00564   0.0213   0.6955   0.0122
  -6.000  -0.6331   0.01201   0.00524   0.0220   0.6835   0.0132
  -5.750  -0.6077   0.01172   0.00493   0.0225   0.6723   0.0142
  -5.500  -0.5822   0.01144   0.00460   0.0231   0.6610   0.0163
  -5.250  -0.5566   0.01115   0.00430   0.0236   0.6495   0.0197
  -5.000  -0.5312   0.01084   0.00400   0.0241   0.6387   0.0270
  -4.750  -0.5062   0.01050   0.00371   0.0247   0.6275   0.0433
  -4.500  -0.4814   0.01011   0.00343   0.0252   0.6167   0.0686
  -4.250  -0.4577   0.00963   0.00313   0.0259   0.6060   0.1111
  -4.000  -0.4342   0.00912   0.00285   0.0266   0.5956   0.1666
  -3.750  -0.4106   0.00864   0.00260   0.0273   0.5852   0.2275
  -3.500  -0.3865   0.00821   0.00239   0.0279   0.5740   0.2903
  -3.250  -0.3615   0.00785   0.00223   0.0284   0.5639   0.3444
  -3.000  -0.3362   0.00756   0.00208   0.0289   0.5533   0.3940
  -2.750  -0.3108   0.00725   0.00195   0.0294   0.5426   0.4470
  -2.500  -0.2853   0.00699   0.00184   0.0299   0.5321   0.4998
  -2.250  -0.2593   0.00677   0.00175   0.0303   0.5216   0.5438
  -2.000  -0.2331   0.00658   0.00168   0.0307   0.5115   0.5883
  -1.750  -0.2066   0.00644   0.00162   0.0311   0.5003   0.6256
  -1.500  -0.1794   0.00633   0.00158   0.0313   0.4899   0.6545
  -1.250  -0.1517   0.00628   0.00155   0.0315   0.4797   0.6798
  -1.000  -0.1240   0.00624   0.00154   0.0317   0.4686   0.7024
  -0.750  -0.0959   0.00622   0.00153   0.0318   0.4584   0.7226
  -0.500  -0.0678   0.00624   0.00154   0.0319   0.4477   0.7406
  -0.250  -0.0393   0.00625   0.00155   0.0320   0.4377   0.7560
   0.000  -0.0107   0.00630   0.00157   0.0320   0.4273   0.7686
   0.250   0.0178   0.00634   0.00159   0.0320   0.4172   0.7797
   0.500   0.0465   0.00639   0.00162   0.0319   0.4075   0.7890
   0.750   0.0751   0.00647   0.00165   0.0319   0.3970   0.7983
   1.000   0.1040   0.00652   0.00169   0.0319   0.3880   0.8060
   1.250   0.1325   0.00661   0.00174   0.0318   0.3782   0.8140
   1.500   0.1614   0.00668   0.00177   0.0317   0.3692   0.8210
   1.750   0.1898   0.00676   0.00184   0.0317   0.3603   0.8278
   2.000   0.2186   0.00684   0.00189   0.0316   0.3524   0.8344
   2.250   0.2471   0.00694   0.00195   0.0316   0.3438   0.8405
   2.500   0.2756   0.00701   0.00202   0.0316   0.3361   0.8465
   2.750   0.3039   0.00714   0.00210   0.0315   0.3275   0.8530
   3.000   0.3323   0.00721   0.00218   0.0315   0.3212   0.8593
   3.250   0.3602   0.00733   0.00228   0.0316   0.3138   0.8656
   3.500   0.3886   0.00744   0.00237   0.0315   0.3074   0.8714
   3.750   0.4168   0.00753   0.00245   0.0315   0.3005   0.8762
   4.000   0.4446   0.00766   0.00256   0.0315   0.2936   0.8809
   4.250   0.4729   0.00775   0.00266   0.0315   0.2882   0.8856
   4.500   0.5008   0.00790   0.00276   0.0314   0.2818   0.8902
   4.750   0.5286   0.00800   0.00287   0.0315   0.2760   0.8946
   5.000   0.5562   0.00811   0.00298   0.0315   0.2703   0.8989
   5.250   0.5835   0.00827   0.00312   0.0316   0.2640   0.9036
   5.500   0.6113   0.00839   0.00324   0.0316   0.2593   0.9079
   5.750   0.6386   0.00850   0.00336   0.0317   0.2538   0.9123
   6.000   0.6648   0.00869   0.00352   0.0320   0.2473   0.9169
   6.250   0.6918   0.00880   0.00366   0.0321   0.2432   0.9220
   6.500   0.7185   0.00894   0.00379   0.0323   0.2379   0.9269
   6.750   0.7436   0.00913   0.00397   0.0328   0.2317   0.9318
   7.000   0.7698   0.00925   0.00412   0.0331   0.2275   0.9367
   7.250   0.7959   0.00941   0.00426   0.0333   0.2219   0.9414
   7.500   0.8204   0.00962   0.00445   0.0338   0.2154   0.9459
   7.750   0.8461   0.00973   0.00460   0.0342   0.2117   0.9506
   8.000   0.8710   0.00990   0.00477   0.0346   0.2069   0.9558
   8.250   0.8955   0.01014   0.00499   0.0351   0.2010   0.9605
   8.500   0.9213   0.01027   0.00516   0.0353   0.1975   0.9655
   8.750   0.9465   0.01045   0.00535   0.0356   0.1930   0.9709
   9.000   0.9755   0.01074   0.00562   0.0350   0.1872   0.9744
   9.250   1.0053   0.01094   0.00584   0.0343   0.1835   0.9782
   9.500   1.0339   0.01116   0.00608   0.0338   0.1792   0.9826
   9.750   1.0670   0.01151   0.00640   0.0322   0.1733   0.9843
  10.000   1.1003   0.01176   0.00668   0.0307   0.1694   0.9860
  10.250   1.1337   0.01205   0.00697   0.0291   0.1649   0.9876
  10.500   1.1654   0.01245   0.00735   0.0276   0.1589   0.9898
  10.750   1.1972   0.01271   0.00765   0.0263   0.1552   0.9923
  11.000   1.2290   0.01305   0.00799   0.0249   0.1504   0.9944
  11.250   1.2606   0.01350   0.00843   0.0233   0.1446   0.9966
  11.500   1.2931   0.01380   0.00876   0.0218   0.1403   0.9987
  11.750   1.3155   0.01421   0.00916   0.0220   0.1354   1.0000
  12.000   1.3200   0.01454   0.00950   0.0257   0.1315   1.0000
  12.250   1.3333   0.01484   0.00983   0.0278   0.1279   1.0000
  12.500   1.3459   0.01531   0.01028   0.0297   0.1231   1.0000
  12.750   1.3560   0.01580   0.01078   0.0321   0.1186   1.0000
  13.000   1.3649   0.01631   0.01131   0.0345   0.1143   1.0000
  13.250   1.3702   0.01713   0.01211   0.0368   0.1089   1.0000
  13.500   1.3812   0.01782   0.01283   0.0383   0.1052   1.0000
  13.750   1.3887   0.01879   0.01380   0.0398   0.1006   1.0000
  14.000   1.3960   0.01987   0.01492   0.0411   0.0968   1.0000
  14.250   1.4053   0.02092   0.01601   0.0420   0.0935   1.0000
  14.500   1.4105   0.02233   0.01743   0.0429   0.0898   1.0000
  14.750   1.4159   0.02383   0.01896   0.0436   0.0865   1.0000
  15.000   1.4228   0.02529   0.02047   0.0441   0.0836   1.0000
  15.250   1.4255   0.02717   0.02237   0.0444   0.0807   1.0000
  15.500   1.4256   0.02936   0.02460   0.0446   0.0774   1.0000
  15.750   1.4306   0.03122   0.02653   0.0447   0.0757   1.0000
  16.000   1.4320   0.03345   0.02881   0.0446   0.0736   1.0000
  16.250   1.4289   0.03617   0.03157   0.0443   0.0713   1.0000
  16.500   1.4231   0.03926   0.03473   0.0438   0.0694   1.0000
  16.750   1.4226   0.04189   0.03743   0.0433   0.0677   1.0000
  17.000   1.4203   0.04476   0.04038   0.0427   0.0663   1.0000
  17.250   1.4146   0.04811   0.04380   0.0418   0.0647   1.0000
  17.500   1.4055   0.05198   0.04774   0.0406   0.0633   1.0000
  17.750   1.3933   0.05631   0.05213   0.0392   0.0617   1.0000
  18.000   1.3830   0.06052   0.05643   0.0377   0.0603   1.0000
  18.250   1.3771   0.06426   0.06026   0.0364   0.0593   1.0000
  18.500   1.3683   0.06844   0.06451   0.0348   0.0580   1.0000
  18.750   1.3570   0.07302   0.06917   0.0330   0.0568   1.0000
  19.000   1.3429   0.07808   0.07430   0.0309   0.0555   1.0000
  19.250   1.3253   0.08374   0.08002   0.0284   0.0539   1.0000
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