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MH 93 15.98% (mh93-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 93 15.98% (mh93-il)
Reynolds number: 500,000
Max Cl/Cd: 74.35 at α=10.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh93-il-500000.txt
Download as CSV file: xf-mh93-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 93  15.98%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6561   0.09908   0.09684   0.0011   1.0000   0.0189
 -13.750  -0.9791   0.05603   0.05186  -0.0232   1.0000   0.0126
 -13.500  -0.9886   0.05299   0.04864  -0.0232   1.0000   0.0126
 -13.250  -0.9928   0.05068   0.04621  -0.0227   1.0000   0.0125
 -13.000  -0.9980   0.04697   0.04234  -0.0219   1.0000   0.0124
 -12.750  -1.0074   0.04381   0.03897  -0.0205   1.0000   0.0124
 -12.500  -1.0105   0.04115   0.03613  -0.0190   1.0000   0.0124
 -12.250  -1.0099   0.03874   0.03356  -0.0173   1.0000   0.0124
 -12.000  -1.0065   0.03652   0.03118  -0.0156   1.0000   0.0123
 -11.750  -1.0030   0.03458   0.02905  -0.0137   1.0000   0.0124
 -11.500  -0.9949   0.03287   0.02720  -0.0119   1.0000   0.0124
 -11.250  -0.9860   0.03127   0.02544  -0.0101   1.0000   0.0124
 -11.000  -0.9767   0.03001   0.02402  -0.0082   1.0000   0.0125
 -10.750  -0.9599   0.02820   0.02210  -0.0072   1.0000   0.0126
 -10.500  -0.9412   0.02637   0.02021  -0.0064   1.0000   0.0128
 -10.250  -0.9246   0.02519   0.01901  -0.0053   1.0000   0.0130
 -10.000  -0.9082   0.02419   0.01800  -0.0040   1.0000   0.0132
  -9.750  -0.8911   0.02321   0.01698  -0.0028   1.0000   0.0134
  -9.500  -0.8735   0.02231   0.01606  -0.0016   1.0000   0.0135
  -9.250  -0.8517   0.02146   0.01516  -0.0012   0.9654   0.0139
  -9.000  -0.8316   0.02078   0.01434  -0.0001   0.9119   0.0143
  -8.750  -0.8210   0.02017   0.01359   0.0030   0.8822   0.0146
  -8.000  -0.7787   0.01838   0.01145   0.0102   0.8266   0.0154
  -7.750  -0.7638   0.01760   0.01062   0.0123   0.8115   0.0160
  -7.500  -0.7452   0.01708   0.01004   0.0139   0.7977   0.0164
  -7.250  -0.7258   0.01657   0.00945   0.0154   0.7846   0.0172
  -7.000  -0.7051   0.01614   0.00891   0.0167   0.7720   0.0180
  -6.750  -0.6858   0.01553   0.00827   0.0182   0.7593   0.0190
  -6.500  -0.6639   0.01511   0.00780   0.0193   0.7476   0.0206
  -6.250  -0.6428   0.01461   0.00723   0.0206   0.7358   0.0226
  -6.000  -0.6196   0.01421   0.00679   0.0215   0.7238   0.0251
  -5.750  -0.5976   0.01373   0.00627   0.0226   0.7130   0.0297
  -5.500  -0.5759   0.01318   0.00576   0.0237   0.7014   0.0405
  -5.250  -0.5549   0.01256   0.00528   0.0249   0.6906   0.0678
  -5.000  -0.5354   0.01185   0.00481   0.0262   0.6798   0.1208
  -4.750  -0.5159   0.01108   0.00440   0.0275   0.6690   0.1928
  -4.500  -0.4963   0.01041   0.00405   0.0288   0.6588   0.2707
  -4.250  -0.4746   0.00989   0.00378   0.0298   0.6478   0.3346
  -4.000  -0.4520   0.00948   0.00355   0.0308   0.6377   0.3878
  -3.750  -0.4292   0.00911   0.00335   0.0317   0.6269   0.4399
  -3.500  -0.4059   0.00878   0.00319   0.0327   0.6168   0.4907
  -3.250  -0.3821   0.00851   0.00304   0.0335   0.6064   0.5369
  -3.000  -0.3578   0.00826   0.00292   0.0344   0.5959   0.5795
  -2.750  -0.3334   0.00807   0.00283   0.0352   0.5860   0.6209
  -2.500  -0.3083   0.00789   0.00278   0.0360   0.5754   0.6613
  -2.250  -0.2822   0.00782   0.00275   0.0366   0.5653   0.6916
  -2.000  -0.2551   0.00778   0.00272   0.0370   0.5546   0.7141
  -1.750  -0.2276   0.00778   0.00271   0.0373   0.5447   0.7334
  -1.500  -0.2001   0.00780   0.00270   0.0376   0.5341   0.7503
  -1.250  -0.1722   0.00783   0.00271   0.0379   0.5236   0.7660
  -1.000  -0.1445   0.00790   0.00273   0.0382   0.5136   0.7793
  -0.750  -0.1162   0.00794   0.00277   0.0384   0.5031   0.7904
  -0.500  -0.0884   0.00802   0.00277   0.0386   0.4931   0.8014
  -0.250  -0.0600   0.00809   0.00282   0.0387   0.4824   0.8098
   0.000  -0.0322   0.00816   0.00283   0.0389   0.4727   0.8192
   0.250  -0.0038   0.00826   0.00289   0.0390   0.4623   0.8261
   0.500   0.0242   0.00834   0.00293   0.0392   0.4523   0.8344
   0.750   0.0521   0.00845   0.00298   0.0393   0.4426   0.8408
   1.000   0.0804   0.00854   0.00306   0.0395   0.4329   0.8473
   1.250   0.1078   0.00866   0.00310   0.0396   0.4233   0.8546
   1.500   0.1360   0.00874   0.00318   0.0398   0.4137   0.8598
   1.750   0.1636   0.00888   0.00328   0.0400   0.4048   0.8659
   2.000   0.1908   0.00899   0.00334   0.0402   0.3955   0.8730
   2.250   0.2182   0.00913   0.00346   0.0406   0.3869   0.8782
   2.500   0.2455   0.00927   0.00358   0.0408   0.3783   0.8842
   2.750   0.2721   0.00940   0.00366   0.0411   0.3703   0.8904
   3.000   0.2995   0.00950   0.00375   0.0414   0.3618   0.8945
   3.250   0.3265   0.00967   0.00388   0.0416   0.3543   0.8990
   3.500   0.3535   0.00977   0.00398   0.0419   0.3469   0.9041
   3.750   0.3793   0.00993   0.00407   0.0422   0.3396   0.9092
   4.000   0.4068   0.01002   0.00419   0.0424   0.3327   0.9128
   4.250   0.4333   0.01018   0.00431   0.0428   0.3255   0.9172
   4.500   0.4591   0.01032   0.00444   0.0432   0.3193   0.9223
   4.750   0.4851   0.01043   0.00454   0.0435   0.3130   0.9269
   5.000   0.5116   0.01063   0.00470   0.0438   0.3066   0.9306
   5.250   0.5382   0.01075   0.00484   0.0441   0.3007   0.9352
   5.500   0.5619   0.01088   0.00496   0.0448   0.2946   0.9412
   5.750   0.5895   0.01111   0.00515   0.0448   0.2885   0.9448
   6.000   0.6185   0.01123   0.00532   0.0445   0.2832   0.9487
   6.250   0.6443   0.01139   0.00547   0.0448   0.2774   0.9537
   6.500   0.6711   0.01162   0.00566   0.0448   0.2715   0.9579
   6.750   0.7039   0.01177   0.00585   0.0436   0.2661   0.9601
   7.000   0.7354   0.01200   0.00606   0.0426   0.2603   0.9629
   7.250   0.7651   0.01225   0.00630   0.0419   0.2547   0.9665
   7.500   0.7928   0.01239   0.00649   0.0417   0.2496   0.9705
   7.750   0.8278   0.01267   0.00674   0.0398   0.2438   0.9719
   8.000   0.8633   0.01295   0.00703   0.0379   0.2380   0.9733
   8.250   0.8987   0.01316   0.00727   0.0360   0.2322   0.9749
   8.500   0.9310   0.01352   0.00758   0.0345   0.2260   0.9772
   8.750   0.9622   0.01372   0.00784   0.0334   0.2212   0.9801
   9.000   0.9931   0.01397   0.00812   0.0323   0.2160   0.9830
   9.250   1.0271   0.01440   0.00850   0.0303   0.2104   0.9846
   9.500   1.0618   0.01461   0.00879   0.0285   0.2056   0.9864
   9.750   1.0942   0.01492   0.00912   0.0269   0.2006   0.9887
  10.000   1.1234   0.01541   0.00957   0.0258   0.1952   0.9919
  10.250   1.1563   0.01564   0.00990   0.0242   0.1908   0.9941
  10.500   1.1896   0.01600   0.01028   0.0224   0.1858   0.9964
  10.750   1.2207   0.01654   0.01081   0.0206   0.1804   0.9990
  11.000   1.2413   0.01680   0.01115   0.0213   0.1766   1.0000
  11.250   1.2437   0.01709   0.01147   0.0252   0.1735   1.0000
  11.500   1.2394   0.01741   0.01181   0.0302   0.1707   1.0000
  11.750   1.2296   0.01783   0.01221   0.0359   0.1679   1.0000
  12.000   1.2328   0.01827   0.01270   0.0393   0.1651   1.0000
  12.250   1.2426   0.01878   0.01328   0.0413   0.1614   1.0000
  12.500   1.2509   0.01952   0.01403   0.0430   0.1575   1.0000
  12.750   1.2561   0.02057   0.01506   0.0447   0.1536   1.0000
  13.000   1.2699   0.02126   0.01586   0.0455   0.1500   1.0000
  13.250   1.2798   0.02223   0.01688   0.0464   0.1458   1.0000
  13.500   1.2852   0.02358   0.01821   0.0474   0.1418   1.0000
  13.750   1.2946   0.02474   0.01945   0.0480   0.1381   1.0000
  14.000   1.3033   0.02602   0.02078   0.0485   0.1338   1.0000
  14.250   1.3062   0.02780   0.02256   0.0489   0.1296   1.0000
  14.500   1.3122   0.02941   0.02424   0.0492   0.1258   1.0000
  14.750   1.3176   0.03114   0.02604   0.0494   0.1216   1.0000
  15.000   1.3166   0.03348   0.02838   0.0494   0.1177   1.0000
  15.250   1.3188   0.03561   0.03058   0.0493   0.1140   1.0000
  15.500   1.3208   0.03783   0.03286   0.0491   0.1104   1.0000
  15.750   1.3162   0.04073   0.03579   0.0486   0.1069   1.0000
  16.000   1.3119   0.04368   0.03878   0.0482   0.1040   1.0000
  16.250   1.3123   0.04627   0.04146   0.0476   0.1010   1.0000
  16.500   1.3078   0.04947   0.04472   0.0467   0.0980   1.0000
  16.750   1.2989   0.05325   0.04852   0.0456   0.0953   1.0000
  17.000   1.2947   0.05657   0.05192   0.0446   0.0930   1.0000
  17.250   1.2917   0.05987   0.05531   0.0434   0.0904   1.0000
  17.500   1.2853   0.06365   0.05914   0.0420   0.0881   1.0000
  17.750   1.2749   0.06796   0.06348   0.0404   0.0857   1.0000
  18.000   1.2679   0.07192   0.06749   0.0389   0.0836   1.0000
  18.250   1.2640   0.07563   0.07131   0.0373   0.0814   1.0000
  18.500   1.2581   0.07961   0.07536   0.0356   0.0794   1.0000
  18.750   1.2489   0.08412   0.07991   0.0336   0.0774   1.0000
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