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MH 106 13.07% (mh106-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 106 13.07% (mh106-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.52 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh106-il-1000000-n5.txt
Download as CSV file: xf-mh106-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 106  13.07%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9275   0.11156   0.10913   0.0100   1.0000   0.0018
 -16.250  -0.9616   0.10001   0.09741   0.0035   1.0000   0.0018
 -16.000  -0.9967   0.08900   0.08623  -0.0028   1.0000   0.0018
 -15.750  -1.0234   0.08017   0.07726  -0.0077   1.0000   0.0018
 -15.500  -1.0240   0.07606   0.07311  -0.0099   1.0000   0.0018
 -15.250  -1.0486   0.06809   0.06499  -0.0144   1.0000   0.0018
 -15.000  -1.0870   0.05823   0.05489  -0.0200   1.0000   0.0018
 -14.750  -1.0742   0.05645   0.05310  -0.0210   1.0000   0.0018
 -14.500  -1.0868   0.05090   0.04741  -0.0241   1.0000   0.0018
 -14.000  -1.1046   0.04182   0.03806  -0.0285   1.0000   0.0018
 -13.750  -1.1149   0.03778   0.03388  -0.0297   1.0000   0.0018
 -13.500  -1.1402   0.03292   0.02876  -0.0298   1.0000   0.0019
 -13.250  -1.1311   0.03165   0.02745  -0.0292   1.0000   0.0018
 -13.000  -1.1484   0.02856   0.02415  -0.0268   1.0000   0.0019
 -12.750  -1.1427   0.02736   0.02288  -0.0251   1.0000   0.0019
 -12.500  -1.1477   0.02560   0.02098  -0.0219   1.0000   0.0020
 -12.250  -1.1420   0.02459   0.01988  -0.0194   1.0000   0.0019
 -12.000  -1.1386   0.02351   0.01871  -0.0162   1.0000   0.0020
 -11.750  -1.1319   0.02259   0.01772  -0.0133   1.0000   0.0021
 -11.500  -1.1187   0.02183   0.01689  -0.0114   1.0000   0.0021
 -11.250  -1.1028   0.02115   0.01615  -0.0098   1.0000   0.0022
 -11.000  -1.0867   0.02042   0.01535  -0.0082   1.0000   0.0023
 -10.750  -1.0703   0.01966   0.01452  -0.0066   1.0000   0.0023
 -10.500  -1.0532   0.01892   0.01370  -0.0052   1.0000   0.0024
 -10.250  -1.0343   0.01828   0.01301  -0.0039   1.0000   0.0025
 -10.000  -1.0151   0.01764   0.01231  -0.0026   1.0000   0.0026
  -9.750  -0.9955   0.01701   0.01162  -0.0014   1.0000   0.0026
  -9.500  -0.9750   0.01644   0.01099  -0.0002   1.0000   0.0027
  -9.250  -0.9542   0.01587   0.01037   0.0009   1.0000   0.0027
  -9.000  -0.9331   0.01533   0.00977   0.0020   1.0000   0.0028
  -8.750  -0.8910   0.01469   0.00903  -0.0014   0.9305   0.0029
  -8.500  -0.8710   0.01447   0.00854   0.0002   0.8511   0.0030
  -8.250  -0.8496   0.01419   0.00808   0.0014   0.8088   0.0031
  -8.000  -0.8273   0.01385   0.00758   0.0024   0.7772   0.0031
  -7.500  -0.7813   0.01310   0.00656   0.0042   0.7229   0.0034
  -7.250  -0.7572   0.01278   0.00614   0.0049   0.7013   0.0036
  -7.000  -0.7327   0.01248   0.00575   0.0055   0.6819   0.0039
  -6.750  -0.7077   0.01222   0.00540   0.0061   0.6629   0.0042
  -6.500  -0.6823   0.01198   0.00507   0.0066   0.6448   0.0046
  -6.250  -0.6567   0.01176   0.00477   0.0070   0.6270   0.0050
  -6.000  -0.6314   0.01148   0.00443   0.0075   0.6112   0.0062
  -5.750  -0.6056   0.01126   0.00414   0.0079   0.5968   0.0075
  -5.500  -0.5798   0.01101   0.00386   0.0084   0.5831   0.0105
  -5.250  -0.5541   0.01076   0.00358   0.0088   0.5697   0.0159
  -5.000  -0.5283   0.01051   0.00332   0.0092   0.5558   0.0243
  -4.750  -0.5026   0.01024   0.00307   0.0096   0.5427   0.0372
  -4.500  -0.4778   0.00986   0.00278   0.0102   0.5306   0.0661
  -4.250  -0.4543   0.00933   0.00246   0.0109   0.5203   0.1190
  -4.000  -0.4303   0.00887   0.00219   0.0115   0.5102   0.1740
  -3.750  -0.4052   0.00853   0.00201   0.0119   0.5001   0.2189
  -3.500  -0.3787   0.00835   0.00189   0.0122   0.4906   0.2433
  -3.250  -0.3523   0.00817   0.00177   0.0125   0.4807   0.2714
  -3.000  -0.3256   0.00803   0.00167   0.0128   0.4709   0.2947
  -2.750  -0.2982   0.00795   0.00158   0.0130   0.4628   0.3090
  -2.500  -0.2707   0.00788   0.00151   0.0131   0.4548   0.3220
  -2.250  -0.2431   0.00781   0.00144   0.0132   0.4480   0.3349
  -2.000  -0.2155   0.00776   0.00137   0.0134   0.4408   0.3478
  -1.750  -0.1879   0.00770   0.00132   0.0135   0.4343   0.3607
  -1.500  -0.1603   0.00764   0.00127   0.0136   0.4272   0.3737
  -1.250  -0.1327   0.00759   0.00123   0.0138   0.4213   0.3873
  -1.000  -0.1050   0.00754   0.00120   0.0139   0.4158   0.4013
  -0.750  -0.0774   0.00750   0.00117   0.0140   0.4104   0.4162
  -0.500  -0.0496   0.00745   0.00114   0.0141   0.4056   0.4312
  -0.250  -0.0220   0.00740   0.00112   0.0142   0.4003   0.4483
   0.000   0.0055   0.00737   0.00111   0.0143   0.3955   0.4656
   0.250   0.0331   0.00731   0.00111   0.0145   0.3913   0.4839
   0.500   0.0606   0.00725   0.00111   0.0146   0.3869   0.5055
   0.750   0.0880   0.00721   0.00111   0.0148   0.3824   0.5265
   1.000   0.1152   0.00716   0.00112   0.0149   0.3784   0.5505
   1.250   0.1425   0.00709   0.00114   0.0151   0.3743   0.5769
   1.500   0.1696   0.00704   0.00116   0.0153   0.3697   0.6031
   1.750   0.1964   0.00701   0.00119   0.0156   0.3652   0.6316
   2.000   0.2235   0.00695   0.00123   0.0158   0.3613   0.6593
   2.250   0.2503   0.00690   0.00127   0.0161   0.3569   0.6882
   2.750   0.3032   0.00681   0.00137   0.0169   0.3485   0.7484
   3.000   0.3295   0.00676   0.00143   0.0173   0.3439   0.7790
   3.250   0.3557   0.00674   0.00149   0.0177   0.3385   0.8087
   3.500   0.3820   0.00671   0.00157   0.0182   0.3337   0.8384
   3.750   0.4086   0.00670   0.00165   0.0186   0.3278   0.8672
   4.000   0.4360   0.00673   0.00175   0.0188   0.3216   0.8938
   4.250   0.4659   0.00677   0.00186   0.0185   0.3150   0.9164
   4.500   0.4986   0.00688   0.00198   0.0175   0.3075   0.9343
   4.750   0.5333   0.00699   0.00211   0.0161   0.2987   0.9463
   5.000   0.5665   0.00713   0.00224   0.0149   0.2889   0.9556
   5.250   0.6011   0.00730   0.00238   0.0134   0.2763   0.9617
   5.500   0.6308   0.00749   0.00253   0.0130   0.2620   0.9689
   5.750   0.6651   0.00775   0.00272   0.0114   0.2422   0.9725
   6.000   0.6961   0.00805   0.00294   0.0106   0.2217   0.9775
   6.250   0.7255   0.00835   0.00317   0.0101   0.2033   0.9826
   6.500   0.7605   0.00873   0.00346   0.0083   0.1816   0.9853
   6.750   0.7938   0.00907   0.00373   0.0068   0.1625   0.9882
   7.000   0.8248   0.00944   0.00403   0.0059   0.1442   0.9910
   7.250   0.8541   0.00980   0.00432   0.0053   0.1295   0.9934
   7.500   0.8857   0.01021   0.00466   0.0041   0.1119   0.9949
   7.750   0.9173   0.01059   0.00498   0.0029   0.0984   0.9966
   8.250   0.9798   0.01139   0.00569   0.0007   0.0751   0.9997
   8.500   1.0036   0.01180   0.00607   0.0011   0.0650   1.0000
   8.750   1.0244   0.01217   0.00642   0.0022   0.0576   1.0000
   9.000   1.0444   0.01261   0.00683   0.0034   0.0497   1.0000
   9.250   1.0639   0.01307   0.00726   0.0047   0.0425   1.0000
   9.500   1.0837   0.01349   0.00767   0.0059   0.0367   1.0000
   9.750   1.1022   0.01401   0.00816   0.0073   0.0303   1.0000
  10.000   1.1201   0.01455   0.00868   0.0087   0.0247   1.0000
  10.250   1.1378   0.01509   0.00922   0.0102   0.0200   1.0000
  10.500   1.1555   0.01560   0.00974   0.0116   0.0170   1.0000
  10.750   1.1725   0.01616   0.01031   0.0131   0.0144   1.0000
  11.000   1.1890   0.01672   0.01088   0.0146   0.0123   1.0000
  11.250   1.2043   0.01733   0.01151   0.0163   0.0101   1.0000
  11.500   1.2192   0.01794   0.01215   0.0180   0.0087   1.0000
  11.750   1.2318   0.01864   0.01288   0.0199   0.0072   1.0000
  12.000   1.2439   0.01933   0.01361   0.0219   0.0062   1.0000
  12.250   1.2521   0.02005   0.01438   0.0244   0.0054   1.0000
  12.500   1.2544   0.02089   0.01526   0.0277   0.0047   1.0000
  12.750   1.2598   0.02182   0.01625   0.0299   0.0045   1.0000
  13.000   1.2646   0.02303   0.01753   0.0314   0.0039   1.0000
  13.250   1.2694   0.02454   0.01911   0.0323   0.0036   1.0000
  13.500   1.2741   0.02634   0.02098   0.0326   0.0033   1.0000
  13.750   1.2773   0.02851   0.02323   0.0324   0.0029   1.0000
  14.000   1.2818   0.03072   0.02552   0.0319   0.0028   1.0000
  14.250   1.2849   0.03318   0.02806   0.0313   0.0027   1.0000
  14.500   1.2862   0.03591   0.03088   0.0305   0.0025   1.0000
  14.750   1.2858   0.03887   0.03393   0.0296   0.0024   1.0000
  15.000   1.2826   0.04218   0.03733   0.0286   0.0021   1.0000
  15.250   1.2788   0.04558   0.04081   0.0275   0.0021   1.0000
  15.500   1.2738   0.04914   0.04446   0.0264   0.0020   1.0000
  15.750   1.2673   0.05291   0.04832   0.0251   0.0019   1.0000
  16.000   1.2590   0.05693   0.05243   0.0238   0.0018   1.0000
  16.250   1.2522   0.06082   0.05641   0.0225   0.0017   1.0000
  16.500   1.2438   0.06510   0.06078   0.0209   0.0017   1.0000
  16.750   1.2350   0.06953   0.06530   0.0192   0.0016   1.0000
  17.000   1.2262   0.07404   0.06990   0.0175   0.0016   1.0000
  17.250   1.2180   0.07855   0.07450   0.0157   0.0016   1.0000
  17.500   1.2069   0.08356   0.07961   0.0137   0.0014   1.0000
  17.750   1.1997   0.08806   0.08419   0.0119   0.0016   1.0000
  18.000   1.1865   0.09358   0.08981   0.0095   0.0015   1.0000
  18.250   1.1762   0.09869   0.09501   0.0074   0.0015   1.0000
  18.500   1.1632   0.10434   0.10076   0.0050   0.0014   1.0000
  18.750   1.1532   0.10961   0.10612   0.0027   0.0015   1.0000
  19.000   1.1400   0.11546   0.11206   0.0001   0.0014   1.0000
  19.250   1.1278   0.12125   0.11795  -0.0025   0.0015   1.0000
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