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MH 92 15.49% (mh92-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 92 15.49% (mh92-il)
Reynolds number: 500,000
Max Cl/Cd: 76.64 at α=9.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh92-il-500000.txt
Download as CSV file: xf-mh92-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.7675   0.08448   0.08178  -0.0168   1.0000   0.0255
 -12.750  -0.7914   0.07858   0.07575  -0.0203   1.0000   0.0254
 -12.500  -0.9798   0.04553   0.04103  -0.0225   1.0000   0.0127
 -12.250  -0.9844   0.04378   0.03910  -0.0207   1.0000   0.0126
 -11.750  -0.9847   0.03879   0.03381  -0.0171   1.0000   0.0125
 -11.500  -0.9811   0.03631   0.03119  -0.0153   1.0000   0.0123
 -11.250  -0.9792   0.03415   0.02883  -0.0129   1.0000   0.0123
 -11.000  -0.9720   0.03228   0.02679  -0.0108   1.0000   0.0123
 -10.750  -0.9619   0.03050   0.02486  -0.0090   1.0000   0.0123
 -10.500  -0.9518   0.02898   0.02314  -0.0069   1.0000   0.0124
 -10.250  -0.9370   0.02754   0.02158  -0.0054   1.0000   0.0124
 -10.000  -0.9228   0.02644   0.02033  -0.0036   1.0000   0.0125
  -9.750  -0.9024   0.02463   0.01843  -0.0029   1.0000   0.0127
  -9.500  -0.8829   0.02321   0.01700  -0.0021   1.0000   0.0130
  -9.250  -0.8639   0.02219   0.01594  -0.0011   1.0000   0.0130
  -9.000  -0.8434   0.02129   0.01505  -0.0004   0.9802   0.0134
  -8.750  -0.8158   0.02050   0.01416  -0.0007   0.9284   0.0138
  -8.500  -0.8026   0.01993   0.01345   0.0020   0.8972   0.0141
  -8.250  -0.7873   0.01929   0.01270   0.0043   0.8752   0.0142
  -8.000  -0.7702   0.01869   0.01199   0.0062   0.8566   0.0147
  -7.750  -0.7518   0.01812   0.01131   0.0079   0.8399   0.0150
  -7.500  -0.7333   0.01752   0.01059   0.0096   0.8247   0.0154
  -7.250  -0.7164   0.01674   0.00975   0.0115   0.8100   0.0158
  -7.000  -0.6965   0.01617   0.00913   0.0128   0.7960   0.0165
  -6.750  -0.6751   0.01569   0.00860   0.0140   0.7828   0.0172
  -6.500  -0.6528   0.01529   0.00809   0.0151   0.7703   0.0181
  -6.250  -0.6320   0.01470   0.00746   0.0164   0.7574   0.0195
  -6.000  -0.6084   0.01433   0.00703   0.0172   0.7450   0.0214
  -5.750  -0.5861   0.01383   0.00648   0.0183   0.7331   0.0235
  -5.500  -0.5629   0.01338   0.00599   0.0193   0.7210   0.0275
  -5.250  -0.5398   0.01288   0.00550   0.0202   0.7091   0.0362
  -5.000  -0.5182   0.01226   0.00500   0.0213   0.6979   0.0628
  -4.750  -0.4977   0.01150   0.00453   0.0225   0.6861   0.1207
  -4.500  -0.4775   0.01075   0.00413   0.0236   0.6750   0.1971
  -4.250  -0.4569   0.01008   0.00379   0.0247   0.6639   0.2792
  -4.000  -0.4341   0.00960   0.00355   0.0256   0.6524   0.3437
  -3.750  -0.4109   0.00920   0.00333   0.0264   0.6417   0.3988
  -3.500  -0.3873   0.00884   0.00315   0.0273   0.6303   0.4526
  -3.250  -0.3634   0.00853   0.00300   0.0281   0.6194   0.5050
  -2.750  -0.3141   0.00805   0.00277   0.0296   0.5972   0.5947
  -2.500  -0.2892   0.00786   0.00269   0.0304   0.5865   0.6379
  -2.250  -0.2636   0.00774   0.00265   0.0311   0.5754   0.6757
  -2.000  -0.2367   0.00767   0.00263   0.0315   0.5644   0.7021
  -1.750  -0.2096   0.00767   0.00261   0.0319   0.5532   0.7239
  -1.500  -0.1819   0.00766   0.00260   0.0323   0.5419   0.7430
  -1.250  -0.1542   0.00769   0.00260   0.0326   0.5313   0.7598
  -1.000  -0.1265   0.00774   0.00261   0.0328   0.5199   0.7748
  -0.750  -0.0985   0.00778   0.00263   0.0331   0.5086   0.7882
  -0.500  -0.0707   0.00786   0.00264   0.0333   0.4981   0.8003
  -0.250  -0.0425   0.00792   0.00268   0.0335   0.4867   0.8098
   0.000  -0.0146   0.00799   0.00269   0.0337   0.4758   0.8200
   0.250   0.0134   0.00810   0.00275   0.0339   0.4652   0.8279
   0.500   0.0413   0.00817   0.00278   0.0340   0.4544   0.8370
   0.750   0.0694   0.00826   0.00284   0.0342   0.4439   0.8437
   1.000   0.0971   0.00837   0.00290   0.0344   0.4333   0.8516
   1.250   0.1249   0.00846   0.00295   0.0346   0.4234   0.8584
   1.750   0.1800   0.00869   0.00310   0.0351   0.4035   0.8721
   2.000   0.2072   0.00883   0.00319   0.0354   0.3943   0.8779
   2.250   0.2344   0.00895   0.00330   0.0357   0.3848   0.8846
   2.500   0.2609   0.00909   0.00339   0.0361   0.3761   0.8919
   2.750   0.2880   0.00921   0.00350   0.0365   0.3675   0.8970
   3.000   0.3147   0.00936   0.00361   0.0368   0.3596   0.9027
   3.250   0.3412   0.00946   0.00369   0.0372   0.3513   0.9088
   3.500   0.3678   0.00962   0.00381   0.0375   0.3435   0.9130
   3.750   0.3949   0.00973   0.00392   0.0378   0.3361   0.9178
   4.000   0.4203   0.00990   0.00403   0.0383   0.3290   0.9237
   4.250   0.4471   0.00999   0.00414   0.0386   0.3224   0.9282
   4.500   0.4741   0.01014   0.00427   0.0388   0.3153   0.9325
   4.750   0.4998   0.01030   0.00440   0.0392   0.3088   0.9378
   5.000   0.5256   0.01041   0.00452   0.0397   0.3024   0.9431
   5.250   0.5540   0.01062   0.00468   0.0395   0.2959   0.9469
   5.500   0.5822   0.01075   0.00484   0.0395   0.2900   0.9517
   5.750   0.6078   0.01090   0.00498   0.0398   0.2838   0.9575
   6.000   0.6408   0.01115   0.00519   0.0386   0.2773   0.9602
   6.250   0.6741   0.01131   0.00538   0.0374   0.2715   0.9632
   6.500   0.7048   0.01153   0.00557   0.0366   0.2653   0.9669
   6.750   0.7341   0.01174   0.00578   0.0361   0.2596   0.9710
   7.000   0.7705   0.01193   0.00599   0.0341   0.2535   0.9723
   7.250   0.8062   0.01225   0.00626   0.0320   0.2469   0.9738
   7.500   0.8422   0.01242   0.00648   0.0302   0.2414   0.9755
   7.750   0.8757   0.01265   0.00670   0.0286   0.2351   0.9779
   8.000   0.9055   0.01294   0.00698   0.0278   0.2294   0.9816
   8.250   0.9399   0.01312   0.00720   0.0261   0.2237   0.9836
   8.500   0.9746   0.01344   0.00749   0.0242   0.2179   0.9852
   8.750   1.0086   0.01371   0.00779   0.0225   0.2127   0.9872
   9.000   1.0420   0.01395   0.00806   0.0209   0.2073   0.9897
   9.250   1.0729   0.01434   0.00842   0.0196   0.2019   0.9928
   9.500   1.1069   0.01459   0.00874   0.0179   0.1969   0.9948
   9.750   1.1404   0.01488   0.00906   0.0161   0.1917   0.9970
  10.000   1.1720   0.01538   0.00952   0.0145   0.1861   0.9995
  10.250   1.1916   0.01557   0.00980   0.0155   0.1824   1.0000
  10.500   1.2016   0.01583   0.01010   0.0183   0.1787   1.0000
  10.750   1.2077   0.01617   0.01043   0.0216   0.1751   1.0000
  11.000   1.2109   0.01657   0.01083   0.0254   0.1716   1.0000
  11.250   1.2220   0.01681   0.01114   0.0279   0.1682   1.0000
  11.500   1.2327   0.01717   0.01154   0.0303   0.1643   1.0000
  11.750   1.2402   0.01769   0.01204   0.0331   0.1603   1.0000
  12.000   1.2477   0.01822   0.01261   0.0357   0.1568   1.0000
  12.250   1.2597   0.01873   0.01319   0.0374   0.1529   1.0000
  12.500   1.2688   0.01946   0.01393   0.0390   0.1486   1.0000
  12.750   1.2753   0.02046   0.01493   0.0407   0.1445   1.0000
  13.000   1.2890   0.02117   0.01573   0.0415   0.1406   1.0000
  13.250   1.2978   0.02222   0.01681   0.0425   0.1361   1.0000
  13.500   1.3021   0.02364   0.01823   0.0435   0.1319   1.0000
  13.750   1.3142   0.02464   0.01932   0.0441   0.1278   1.0000
  14.000   1.3201   0.02614   0.02084   0.0446   0.1235   1.0000
  14.250   1.3220   0.02802   0.02274   0.0451   0.1196   1.0000
  14.500   1.3307   0.02946   0.02426   0.0453   0.1154   1.0000
  14.750   1.3324   0.03154   0.02637   0.0454   0.1115   1.0000
  15.000   1.3309   0.03397   0.02883   0.0454   0.1079   1.0000
  15.250   1.3359   0.03590   0.03085   0.0453   0.1046   1.0000
  15.500   1.3348   0.03846   0.03346   0.0450   0.1014   1.0000
  15.750   1.3285   0.04160   0.03662   0.0445   0.0985   1.0000
  16.000   1.3275   0.04428   0.03938   0.0440   0.0959   1.0000
  16.250   1.3264   0.04705   0.04224   0.0433   0.0933   1.0000
  16.500   1.3215   0.05035   0.04560   0.0424   0.0909   1.0000
  16.750   1.3121   0.05426   0.04954   0.0412   0.0886   1.0000
  17.000   1.3066   0.05781   0.05316   0.0400   0.0864   1.0000
  17.250   1.3044   0.06110   0.05655   0.0388   0.0843   1.0000
  17.500   1.2983   0.06492   0.06044   0.0373   0.0820   1.0000
  17.750   1.2897   0.06911   0.06468   0.0357   0.0801   1.0000
  18.000   1.2793   0.07354   0.06912   0.0339   0.0779   1.0000
  18.250   1.2750   0.07740   0.07309   0.0322   0.0761   1.0000
  18.500   1.2697   0.08142   0.07721   0.0304   0.0743   1.0000
  18.750   1.2623   0.08581   0.08166   0.0284   0.0724   1.0000
  19.000   1.2537   0.09038   0.08626   0.0263   0.0706   1.0000
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