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MH 83 13.29% (mh83-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: MH 83 13.29% (mh83-il)
Reynolds number: 200,000
Max Cl/Cd: 59.1 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh83-il-200000.txt
Download as CSV file: xf-mh83-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 83  13.29%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -7.750  -0.2080   0.08998   0.08638  -0.0172   0.7408   0.0512
  -7.500  -0.2066   0.08694   0.08332  -0.0195   0.7279   0.0533
  -7.250  -0.2321   0.08277   0.07917  -0.0294   0.7198   0.0546
  -7.000  -0.2158   0.07972   0.07608  -0.0259   0.7062   0.0552
  -6.750  -0.1994   0.07756   0.07386  -0.0243   0.6926   0.0563
  -6.500  -0.1900   0.07516   0.07140  -0.0249   0.6812   0.0579
  -6.250  -0.1823   0.07203   0.06824  -0.0280   0.6704   0.0601
  -6.000  -0.1789   0.06378   0.05989  -0.0439   0.6642   0.0636
  -5.750  -0.1634   0.06305   0.05915  -0.0396   0.6516   0.0648
  -5.500  -0.1467   0.06083   0.05688  -0.0404   0.6401   0.0675
  -5.250  -0.1283   0.05272   0.04846  -0.0532   0.6335   0.0737
  -5.000  -0.1095   0.05101   0.04675  -0.0524   0.6220   0.0752
  -4.750  -0.0885   0.04843   0.04403  -0.0539   0.6125   0.0783
  -4.500  -0.0556   0.03007   0.02367  -0.0667   0.6107   0.0475
  -4.250  -0.0274   0.02539   0.01827  -0.0673   0.6009   0.0411
  -4.000   0.0000   0.02316   0.01577  -0.0675   0.5909   0.0405
  -3.750   0.0284   0.02143   0.01366  -0.0674   0.5809   0.0402
  -3.500   0.0574   0.02010   0.01200  -0.0673   0.5704   0.0405
  -3.250   0.0854   0.01903   0.01068  -0.0671   0.5612   0.0422
  -3.000   0.1140   0.01827   0.00988  -0.0670   0.5501   0.0441
  -2.750   0.1426   0.01749   0.00891  -0.0666   0.5409   0.0455
  -2.500   0.1715   0.01682   0.00810  -0.0663   0.5309   0.0472
  -2.250   0.1997   0.01611   0.00740  -0.0662   0.5221   0.0501
  -2.000   0.2284   0.01564   0.00686  -0.0660   0.5127   0.0550
  -1.750   0.2571   0.01519   0.00642  -0.0659   0.5038   0.0648
  -1.500   0.2861   0.01449   0.00588  -0.0659   0.4950   0.1044
  -1.250   0.3146   0.01403   0.00570  -0.0660   0.4864   0.1893
  -1.000   0.3429   0.01380   0.00563  -0.0661   0.4781   0.2576
  -0.750   0.3709   0.01360   0.00567  -0.0661   0.4705   0.3439
  -0.500   0.3985   0.01333   0.00569  -0.0659   0.4625   0.4426
  -0.250   0.4248   0.01308   0.00573  -0.0654   0.4557   0.5571
   0.000   0.4481   0.01265   0.00580  -0.0640   0.4480   0.7125
   0.250   0.4783   0.01220   0.00563  -0.0633   0.4413   1.0000
   0.500   0.5075   0.01238   0.00567  -0.0634   0.4340   1.0000
   0.750   0.5364   0.01257   0.00567  -0.0634   0.4277   1.0000
   1.000   0.5651   0.01285   0.00574  -0.0634   0.4221   1.0000
   1.250   0.5939   0.01304   0.00584  -0.0634   0.4154   1.0000
   1.500   0.6225   0.01325   0.00589  -0.0634   0.4098   1.0000
   1.750   0.6509   0.01354   0.00604  -0.0634   0.4043   1.0000
   2.000   0.6794   0.01375   0.00619  -0.0634   0.3985   1.0000
   2.250   0.7078   0.01400   0.00631  -0.0633   0.3937   1.0000
   2.500   0.7360   0.01436   0.00651  -0.0633   0.3894   1.0000
   2.750   0.7642   0.01460   0.00675  -0.0633   0.3842   1.0000
   3.000   0.7924   0.01484   0.00692  -0.0633   0.3793   1.0000
   3.250   0.8204   0.01514   0.00709  -0.0632   0.3752   1.0000
   3.500   0.8483   0.01550   0.00741  -0.0632   0.3710   1.0000
   3.750   0.8761   0.01580   0.00771  -0.0632   0.3666   1.0000
   4.000   0.9039   0.01609   0.00796  -0.0632   0.3627   1.0000
   4.250   0.9318   0.01643   0.00818  -0.0631   0.3592   1.0000
   4.500   0.9592   0.01686   0.00856  -0.0631   0.3555   1.0000
   4.750   0.9864   0.01717   0.00895  -0.0630   0.3513   1.0000
   5.000   1.0138   0.01750   0.00926  -0.0630   0.3476   1.0000
   5.250   1.0413   0.01785   0.00954  -0.0629   0.3444   1.0000
   5.500   1.0688   0.01834   0.00992  -0.0629   0.3415   1.0000
   5.750   1.0952   0.01876   0.01044  -0.0628   0.3380   1.0000
   6.000   1.1216   0.01914   0.01088  -0.0628   0.3342   1.0000
   6.250   1.1484   0.01950   0.01125  -0.0627   0.3308   1.0000
   6.500   1.1754   0.01989   0.01160  -0.0626   0.3280   1.0000
   6.750   1.2026   0.02044   0.01205  -0.0626   0.3254   1.0000
   7.000   1.2278   0.02096   0.01270  -0.0625   0.3222   1.0000
   7.250   1.2530   0.02142   0.01328  -0.0623   0.3186   1.0000
   7.500   1.2788   0.02184   0.01374  -0.0622   0.3154   1.0000
   7.750   1.3052   0.02226   0.01414  -0.0621   0.3127   1.0000
   8.000   1.3320   0.02277   0.01459  -0.0620   0.3102   1.0000
   8.250   1.3567   0.02347   0.01536  -0.0619   0.3074   1.0000
   8.500   1.3796   0.02405   0.01612  -0.0616   0.3041   1.0000
   8.750   1.4035   0.02457   0.01674  -0.0613   0.3008   1.0000
   9.000   1.4286   0.02506   0.01726  -0.0612   0.2981   1.0000
   9.250   1.4548   0.02553   0.01770  -0.0611   0.2957   1.0000
   9.500   1.4810   0.02629   0.01841  -0.0611   0.2930   1.0000
   9.750   1.5004   0.02701   0.01937  -0.0605   0.2899   1.0000
  10.000   1.5210   0.02773   0.02026  -0.0600   0.2867   1.0000
  10.250   1.5434   0.02834   0.02096  -0.0597   0.2838   1.0000
  10.500   1.5681   0.02878   0.02140  -0.0595   0.2812   1.0000
  10.750   1.5952   0.02929   0.02184  -0.0595   0.2787   1.0000
  11.000   1.6131   0.03030   0.02303  -0.0589   0.2758   1.0000
  11.250   1.6282   0.03128   0.02424  -0.0580   0.2726   1.0000
  11.500   1.6460   0.03202   0.02513  -0.0573   0.2694   1.0000
  11.750   1.6683   0.03248   0.02561  -0.0569   0.2666   1.0000
  12.000   1.6954   0.03284   0.02593  -0.0569   0.2641   1.0000
  12.250   1.7131   0.03390   0.02709  -0.0563   0.2613   1.0000
  12.500   1.7179   0.03521   0.02869  -0.0546   0.2580   1.0000
  12.750   1.7277   0.03623   0.02986  -0.0533   0.2548   1.0000
  13.000   1.7452   0.03678   0.03046  -0.0525   0.2520   1.0000
  13.250   1.7749   0.03685   0.03047  -0.0527   0.2493   1.0000
  13.500   1.7864   0.03804   0.03178  -0.0516   0.2464   1.0000
  13.750   1.7679   0.04006   0.03407  -0.0480   0.2437   1.0000
  14.000   1.7535   0.04216   0.03635  -0.0455   0.2409   1.0000
  14.250   1.7561   0.04351   0.03779  -0.0444   0.2381   1.0000
  14.500   1.7895   0.04302   0.03724  -0.0444   0.2352   1.0000
  14.750   1.8047   0.04402   0.03828  -0.0438   0.2323   1.0000
  15.000   1.7542   0.04950   0.04409  -0.0424   0.2297   1.0000
  15.250   1.7010   0.05683   0.05169  -0.0434   0.2265   1.0000
  15.500   1.6924   0.06017   0.05513  -0.0439   0.2234   1.0000
  15.750   1.7643   0.05493   0.04974  -0.0420   0.2206   1.0000
  16.000   1.7478   0.05917   0.05412  -0.0426   0.2177   1.0000
  16.750   1.6188   0.08405   0.07951  -0.0517   0.2062   1.0000
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