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MH 108 11.98% (mh108-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 108 11.98% (mh108-il)
Reynolds number: 500,000
Max Cl/Cd: 82.73 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh108-il-500000.txt
Download as CSV file: xf-mh108-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 108  11.98%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8581   0.10440   0.10168   0.0109   1.0000   0.0071
 -14.500  -0.8759   0.09557   0.09272   0.0054   1.0000   0.0070
 -14.250  -0.8956   0.08686   0.08387  -0.0002   1.0000   0.0069
 -14.000  -0.9072   0.08006   0.07697  -0.0047   1.0000   0.0069
 -13.750  -0.9127   0.07460   0.07142  -0.0084   1.0000   0.0068
 -13.500  -0.9356   0.06620   0.06283  -0.0143   1.0000   0.0069
 -13.250  -0.9652   0.05734   0.05373  -0.0204   1.0000   0.0069
 -13.000  -0.9604   0.05458   0.05091  -0.0222   1.0000   0.0068
 -12.750  -0.9752   0.04929   0.04545  -0.0251   1.0000   0.0068
 -12.250  -0.9987   0.04146   0.03726  -0.0270   1.0000   0.0068
 -12.000  -1.0076   0.03858   0.03419  -0.0262   1.0000   0.0068
 -11.750  -1.0202   0.03561   0.03099  -0.0240   1.0000   0.0069
 -11.500  -1.0188   0.03408   0.02934  -0.0218   1.0000   0.0068
 -11.250  -1.0299   0.03124   0.02627  -0.0179   1.0000   0.0069
 -11.000  -1.0334   0.02889   0.02373  -0.0145   1.0000   0.0071
 -10.750  -1.0250   0.02732   0.02200  -0.0123   1.0000   0.0071
 -10.500  -1.0160   0.02569   0.02027  -0.0102   1.0000   0.0074
 -10.250  -1.0027   0.02444   0.01892  -0.0084   1.0000   0.0076
 -10.000  -0.9871   0.02337   0.01777  -0.0069   1.0000   0.0079
  -9.750  -0.9709   0.02226   0.01655  -0.0053   1.0000   0.0081
  -9.500  -0.9533   0.02126   0.01546  -0.0039   1.0000   0.0085
  -9.250  -0.9349   0.02030   0.01439  -0.0025   1.0000   0.0089
  -9.000  -0.9156   0.01943   0.01342  -0.0012   1.0000   0.0092
  -8.750  -0.8952   0.01865   0.01254   0.0000   1.0000   0.0095
  -8.500  -0.8798   0.01727   0.01107   0.0019   1.0000   0.0102
  -8.250  -0.8594   0.01647   0.01022   0.0031   1.0000   0.0109
  -8.000  -0.8369   0.01590   0.00960   0.0040   1.0000   0.0122
  -7.750  -0.8162   0.01508   0.00870   0.0053   1.0000   0.0138
  -7.500  -0.7938   0.01446   0.00808   0.0063   1.0000   0.0165
  -7.250  -0.7726   0.01367   0.00727   0.0076   1.0000   0.0216
  -7.000  -0.7513   0.01294   0.00657   0.0088   1.0000   0.0324
  -6.750  -0.7288   0.01238   0.00612   0.0098   1.0000   0.0452
  -6.500  -0.7056   0.01196   0.00575   0.0107   1.0000   0.0571
  -6.250  -0.6822   0.01158   0.00542   0.0116   1.0000   0.0690
  -6.000  -0.6590   0.01122   0.00512   0.0125   1.0000   0.0816
  -5.750  -0.6361   0.01088   0.00483   0.0135   1.0000   0.0948
  -5.500  -0.6127   0.01055   0.00458   0.0144   0.9995   0.1100
  -5.250  -0.5704   0.01016   0.00428   0.0112   0.9775   0.1328
  -5.000  -0.5253   0.00980   0.00398   0.0075   0.9326   0.1573
  -4.750  -0.4951   0.00959   0.00371   0.0074   0.8764   0.1786
  -4.500  -0.4718   0.00948   0.00350   0.0086   0.8321   0.1987
  -4.250  -0.4481   0.00933   0.00330   0.0096   0.7956   0.2212
  -4.000  -0.4236   0.00919   0.00311   0.0105   0.7640   0.2454
  -3.750  -0.3986   0.00904   0.00292   0.0112   0.7359   0.2705
  -3.500  -0.3734   0.00887   0.00275   0.0119   0.7106   0.2989
  -3.250  -0.3481   0.00872   0.00260   0.0125   0.6868   0.3285
  -2.750  -0.2971   0.00841   0.00233   0.0137   0.6425   0.3936
  -2.500  -0.2714   0.00826   0.00222   0.0142   0.6226   0.4279
  -2.000  -0.2205   0.00796   0.00202   0.0154   0.5852   0.5036
  -1.750  -0.1951   0.00782   0.00195   0.0161   0.5675   0.5429
  -1.500  -0.1701   0.00767   0.00188   0.0168   0.5505   0.5866
  -1.250  -0.1453   0.00751   0.00183   0.0176   0.5347   0.6333
  -1.000  -0.1206   0.00737   0.00180   0.0185   0.5196   0.6798
  -0.750  -0.0958   0.00725   0.00178   0.0194   0.5047   0.7261
  -0.500  -0.0709   0.00715   0.00178   0.0203   0.4901   0.7709
  -0.250  -0.0453   0.00709   0.00180   0.0211   0.4763   0.8127
   0.000  -0.0185   0.00708   0.00183   0.0217   0.4633   0.8513
   0.250   0.0110   0.00712   0.00190   0.0218   0.4505   0.8837
   0.500   0.0433   0.00721   0.00198   0.0212   0.4376   0.9094
   0.750   0.0788   0.00735   0.00207   0.0199   0.4249   0.9275
   1.000   0.1140   0.00751   0.00217   0.0186   0.4133   0.9413
   1.250   0.1502   0.00770   0.00229   0.0171   0.4027   0.9517
   1.500   0.1886   0.00789   0.00240   0.0151   0.3920   0.9584
   1.750   0.2264   0.00805   0.00252   0.0133   0.3821   0.9651
   2.000   0.2641   0.00823   0.00262   0.0113   0.3732   0.9708
   2.250   0.3044   0.00838   0.00272   0.0088   0.3641   0.9752
   2.500   0.3393   0.00854   0.00284   0.0075   0.3562   0.9818
   2.750   0.3809   0.00867   0.00290   0.0046   0.3481   0.9847
   3.000   0.4211   0.00875   0.00297   0.0020   0.3404   0.9886
   3.250   0.4587   0.00892   0.00307   0.0000   0.3332   0.9929
   3.500   0.4990   0.00894   0.00311  -0.0026   0.3260   0.9961
   3.750   0.5385   0.00905   0.00316  -0.0052   0.3191   0.9994
   4.000   0.5656   0.00910   0.00323  -0.0051   0.3136   1.0000
   4.250   0.5893   0.00917   0.00330  -0.0043   0.3077   1.0000
   4.500   0.6130   0.00930   0.00340  -0.0035   0.3024   1.0000
   4.750   0.6371   0.00936   0.00350  -0.0028   0.2967   1.0000
   5.000   0.6609   0.00949   0.00361  -0.0020   0.2911   1.0000
   5.250   0.6849   0.00961   0.00375  -0.0013   0.2857   1.0000
   5.500   0.7090   0.00971   0.00387  -0.0005   0.2796   1.0000
   5.750   0.7326   0.00991   0.00404   0.0003   0.2739   1.0000
   6.000   0.7571   0.00998   0.00418   0.0010   0.2675   1.0000
   6.250   0.7808   0.01017   0.00435   0.0017   0.2610   1.0000
   6.500   0.8052   0.01028   0.00452   0.0024   0.2545   1.0000
   6.750   0.8290   0.01047   0.00469   0.0032   0.2470   1.0000
   7.000   0.8533   0.01060   0.00488   0.0039   0.2394   1.0000
   7.250   0.8769   0.01082   0.00509   0.0047   0.2309   1.0000
   7.500   0.9011   0.01098   0.00529   0.0054   0.2212   1.0000
   7.750   0.9248   0.01120   0.00552   0.0061   0.2108   1.0000
   8.000   0.9481   0.01146   0.00578   0.0069   0.1994   1.0000
   8.250   0.9710   0.01176   0.00607   0.0077   0.1865   1.0000
   8.500   0.9934   0.01212   0.00641   0.0086   0.1726   1.0000
   8.750   1.0154   0.01253   0.00679   0.0095   0.1595   1.0000
   9.000   1.0368   0.01298   0.00721   0.0104   0.1473   1.0000
   9.500   1.0787   0.01396   0.00814   0.0124   0.1229   1.0000
   9.750   1.0993   0.01446   0.00864   0.0134   0.1113   1.0000
  10.000   1.1195   0.01499   0.00918   0.0145   0.1007   1.0000
  10.250   1.1390   0.01557   0.00975   0.0156   0.0899   1.0000
  10.500   1.1577   0.01620   0.01036   0.0167   0.0798   1.0000
  10.750   1.1752   0.01691   0.01103   0.0180   0.0693   1.0000
  11.250   1.2071   0.01847   0.01255   0.0209   0.0496   1.0000
  11.500   1.2215   0.01930   0.01338   0.0224   0.0416   1.0000
  11.750   1.2340   0.02024   0.01434   0.0242   0.0347   1.0000
  12.000   1.2433   0.02133   0.01543   0.0262   0.0286   1.0000
  12.250   1.2505   0.02245   0.01656   0.0283   0.0238   1.0000
  12.500   1.2531   0.02357   0.01775   0.0311   0.0206   1.0000
  12.750   1.2491   0.02502   0.01924   0.0341   0.0180   1.0000
  13.000   1.2430   0.02711   0.02142   0.0358   0.0162   1.0000
  13.250   1.2415   0.02940   0.02383   0.0360   0.0148   1.0000
  13.500   1.2373   0.03242   0.02694   0.0353   0.0136   1.0000
  13.750   1.2265   0.03664   0.03128   0.0336   0.0126   1.0000
  14.000   1.2173   0.04092   0.03568   0.0318   0.0118   1.0000
  14.250   1.2092   0.04512   0.04001   0.0300   0.0109   1.0000
  14.500   1.1989   0.04965   0.04465   0.0280   0.0106   1.0000
  14.750   1.1862   0.05452   0.04963   0.0260   0.0103   1.0000
  15.000   1.1710   0.05975   0.05498   0.0238   0.0102   1.0000
  15.250   1.1567   0.06493   0.06025   0.0216   0.0099   1.0000
  15.500   1.1398   0.07053   0.06595   0.0192   0.0096   1.0000
  15.750   1.1248   0.07612   0.07163   0.0167   0.0093   1.0000
  16.000   1.1002   0.08336   0.07897   0.0134   0.0089   1.0000
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