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MH 108 11.98% (mh108-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 108 11.98% (mh108-il)
Reynolds number: 500,000
Max Cl/Cd: 79.76 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh108-il-500000-n5.txt
Download as CSV file: xf-mh108-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.9964   0.08329   0.07989   0.0002   1.0000   0.0034
 -14.750  -1.0240   0.07406   0.07050  -0.0052   1.0000   0.0033
 -14.500  -1.0504   0.06507   0.06135  -0.0107   1.0000   0.0033
 -14.250  -1.0710   0.05720   0.05333  -0.0159   1.0000   0.0033
 -14.000  -1.0868   0.05058   0.04652  -0.0203   1.0000   0.0033
 -13.750  -1.1005   0.04501   0.04078  -0.0237   1.0000   0.0033
 -13.500  -1.1100   0.04084   0.03646  -0.0256   1.0000   0.0034
 -13.250  -1.1166   0.03764   0.03313  -0.0262   1.0000   0.0035
 -13.000  -1.1236   0.03491   0.03024  -0.0255   1.0000   0.0034
 -12.750  -1.1277   0.03277   0.02798  -0.0239   1.0000   0.0034
 -12.500  -1.1271   0.03116   0.02625  -0.0220   1.0000   0.0035
 -12.250  -1.1274   0.02961   0.02457  -0.0193   1.0000   0.0035
 -12.000  -1.1245   0.02834   0.02319  -0.0165   1.0000   0.0036
 -11.750  -1.1187   0.02721   0.02195  -0.0139   1.0000   0.0037
 -11.500  -1.1086   0.02605   0.02068  -0.0118   1.0000   0.0038
 -11.250  -1.0961   0.02498   0.01950  -0.0100   1.0000   0.0039
 -11.000  -1.0819   0.02395   0.01837  -0.0084   1.0000   0.0040
 -10.750  -1.0667   0.02295   0.01725  -0.0068   1.0000   0.0041
 -10.500  -1.0497   0.02204   0.01622  -0.0054   1.0000   0.0043
 -10.250  -1.0317   0.02119   0.01527  -0.0041   1.0000   0.0044
 -10.000  -1.0126   0.02040   0.01439  -0.0028   1.0000   0.0046
  -9.750  -0.9929   0.01964   0.01353  -0.0017   1.0000   0.0047
  -9.500  -0.9738   0.01876   0.01256  -0.0004   1.0000   0.0049
  -9.250  -0.9533   0.01802   0.01175   0.0007   1.0000   0.0053
  -9.000  -0.9317   0.01739   0.01106   0.0016   1.0000   0.0056
  -8.750  -0.9095   0.01679   0.01038   0.0026   1.0000   0.0060
  -8.500  -0.8868   0.01626   0.00979   0.0034   1.0000   0.0065
  -8.250  -0.8643   0.01569   0.00917   0.0044   1.0000   0.0072
  -8.000  -0.8416   0.01513   0.00858   0.0052   1.0000   0.0084
  -7.750  -0.8182   0.01465   0.00805   0.0061   1.0000   0.0095
  -7.500  -0.7955   0.01410   0.00750   0.0070   1.0000   0.0116
  -7.250  -0.7722   0.01362   0.00699   0.0079   1.0000   0.0143
  -7.000  -0.7489   0.01316   0.00654   0.0087   1.0000   0.0186
  -6.750  -0.7225   0.01268   0.00610   0.0089   0.9919   0.0254
  -6.500  -0.6783   0.01216   0.00561   0.0053   0.9260   0.0368
  -6.250  -0.6511   0.01192   0.00524   0.0056   0.8582   0.0470
  -6.000  -0.6286   0.01172   0.00491   0.0069   0.8113   0.0572
  -5.750  -0.6050   0.01151   0.00461   0.0079   0.7747   0.0682
  -5.500  -0.5807   0.01129   0.00433   0.0086   0.7430   0.0816
  -5.250  -0.5559   0.01107   0.00406   0.0093   0.7149   0.0961
  -5.000  -0.5306   0.01087   0.00381   0.0099   0.6894   0.1095
  -4.750  -0.5049   0.01069   0.00357   0.0104   0.6664   0.1227
  -4.500  -0.4790   0.01051   0.00335   0.0109   0.6455   0.1369
  -4.250  -0.4530   0.01034   0.00315   0.0114   0.6255   0.1532
  -4.000  -0.4269   0.01018   0.00296   0.0118   0.6059   0.1703
  -3.750  -0.4005   0.01003   0.00278   0.0122   0.5878   0.1863
  -3.500  -0.3743   0.00986   0.00261   0.0126   0.5715   0.2057
  -3.250  -0.3478   0.00972   0.00246   0.0129   0.5550   0.2253
  -3.000  -0.3214   0.00958   0.00232   0.0133   0.5387   0.2466
  -2.750  -0.2949   0.00945   0.00219   0.0137   0.5233   0.2686
  -2.500  -0.2683   0.00931   0.00208   0.0140   0.5095   0.2918
  -2.250  -0.2418   0.00918   0.00197   0.0143   0.4959   0.3183
  -2.000  -0.2153   0.00905   0.00188   0.0147   0.4821   0.3467
  -1.750  -0.1887   0.00893   0.00180   0.0150   0.4688   0.3739
  -1.500  -0.1622   0.00882   0.00173   0.0154   0.4562   0.4033
  -1.250  -0.1357   0.00870   0.00166   0.0157   0.4450   0.4343
  -0.750  -0.0829   0.00849   0.00157   0.0165   0.4230   0.4971
  -0.500  -0.0567   0.00838   0.00153   0.0170   0.4121   0.5325
  -0.250  -0.0308   0.00827   0.00151   0.0175   0.4022   0.5700
   0.000  -0.0050   0.00816   0.00150   0.0180   0.3930   0.6104
   0.250   0.0205   0.00804   0.00150   0.0186   0.3847   0.6525
   0.500   0.0459   0.00795   0.00151   0.0193   0.3762   0.6938
   0.750   0.0713   0.00785   0.00154   0.0200   0.3677   0.7356
   1.000   0.0969   0.00778   0.00157   0.0207   0.3599   0.7758
   1.250   0.1229   0.00771   0.00163   0.0214   0.3528   0.8155
   1.500   0.1502   0.00770   0.00170   0.0218   0.3460   0.8520
   1.750   0.1803   0.00773   0.00179   0.0216   0.3387   0.8834
   2.000   0.2139   0.00782   0.00190   0.0206   0.3318   0.9083
   2.250   0.2498   0.00793   0.00200   0.0191   0.3249   0.9260
   2.500   0.2859   0.00808   0.00212   0.0175   0.3180   0.9387
   2.750   0.3224   0.00819   0.00222   0.0158   0.3116   0.9475
   3.000   0.3552   0.00834   0.00233   0.0149   0.3050   0.9561
   3.250   0.3900   0.00846   0.00244   0.0136   0.2992   0.9621
   3.500   0.4205   0.00860   0.00256   0.0131   0.2930   0.9693
   3.750   0.4560   0.00874   0.00267   0.0115   0.2872   0.9731
   4.000   0.4892   0.00886   0.00280   0.0105   0.2811   0.9781
   4.250   0.5210   0.00902   0.00293   0.0097   0.2753   0.9826
   4.500   0.5575   0.00913   0.00305   0.0078   0.2694   0.9856
   4.750   0.5936   0.00926   0.00318   0.0061   0.2631   0.9895
   5.000   0.6284   0.00941   0.00333   0.0046   0.2572   0.9933
   5.250   0.6643   0.00952   0.00345   0.0029   0.2503   0.9958
   5.500   0.6987   0.00966   0.00358   0.0014   0.2435   0.9981
   5.750   0.7324   0.00979   0.00372   0.0001   0.2362   1.0000
   6.000   0.7563   0.00995   0.00388   0.0009   0.2293   1.0000
   6.250   0.7803   0.01011   0.00406   0.0016   0.2212   1.0000
   6.500   0.8042   0.01029   0.00424   0.0023   0.2139   1.0000
   6.750   0.8279   0.01051   0.00444   0.0031   0.2042   1.0000
   7.000   0.8516   0.01072   0.00466   0.0039   0.1945   1.0000
   7.250   0.8750   0.01097   0.00491   0.0046   0.1837   1.0000
   7.500   0.8980   0.01127   0.00519   0.0054   0.1719   1.0000
   7.750   0.9207   0.01161   0.00550   0.0063   0.1599   1.0000
   8.000   0.9430   0.01199   0.00584   0.0072   0.1481   1.0000
   8.250   0.9652   0.01237   0.00620   0.0080   0.1362   1.0000
   8.500   0.9871   0.01279   0.00661   0.0090   0.1243   1.0000
   8.750   1.0089   0.01321   0.00702   0.0099   0.1139   1.0000
   9.000   1.0303   0.01365   0.00745   0.0108   0.1048   1.0000
   9.250   1.0510   0.01415   0.00793   0.0118   0.0949   1.0000
   9.500   1.0715   0.01467   0.00843   0.0129   0.0843   1.0000
   9.750   1.0915   0.01522   0.00896   0.0139   0.0740   1.0000
  10.000   1.1110   0.01580   0.00954   0.0151   0.0648   1.0000
  10.250   1.1293   0.01645   0.01017   0.0163   0.0551   1.0000
  10.500   1.1470   0.01715   0.01084   0.0175   0.0468   1.0000
  10.750   1.1633   0.01791   0.01159   0.0189   0.0385   1.0000
  11.000   1.1797   0.01864   0.01232   0.0203   0.0321   1.0000
  11.250   1.1943   0.01946   0.01315   0.0219   0.0263   1.0000
  11.500   1.2075   0.02034   0.01403   0.0235   0.0218   1.0000
  11.750   1.2203   0.02118   0.01494   0.0252   0.0185   1.0000
  12.000   1.2306   0.02214   0.01593   0.0271   0.0156   1.0000
  12.250   1.2377   0.02318   0.01700   0.0292   0.0130   1.0000
  12.500   1.2393   0.02423   0.01811   0.0322   0.0116   1.0000
  12.750   1.2401   0.02552   0.01949   0.0344   0.0102   1.0000
  13.000   1.2403   0.02723   0.02128   0.0356   0.0095   1.0000
  13.250   1.2396   0.02947   0.02361   0.0358   0.0088   1.0000
  13.500   1.2397   0.03200   0.02625   0.0353   0.0081   1.0000
  13.750   1.2382   0.03501   0.02938   0.0342   0.0076   1.0000
  14.000   1.2334   0.03861   0.03308   0.0328   0.0069   1.0000
  14.250   1.2255   0.04273   0.03730   0.0310   0.0064   1.0000
  14.500   1.2173   0.04692   0.04161   0.0292   0.0062   1.0000
  14.750   1.2088   0.05121   0.04601   0.0274   0.0060   1.0000
  15.000   1.1979   0.05582   0.05074   0.0255   0.0060   1.0000
  15.250   1.1868   0.06049   0.05552   0.0236   0.0057   1.0000
  15.500   1.1736   0.06550   0.06063   0.0215   0.0056   1.0000
  15.750   1.1617   0.07040   0.06563   0.0194   0.0054   1.0000
  16.000   1.1471   0.07591   0.07124   0.0170   0.0051   1.0000
  16.250   1.1344   0.08130   0.07675   0.0146   0.0050   1.0000
  16.500   1.1234   0.08652   0.08206   0.0123   0.0050   1.0000
  16.750   1.1100   0.09224   0.08788   0.0097   0.0048   1.0000
  17.000   1.1009   0.09738   0.09312   0.0074   0.0049   1.0000
  17.250   1.0871   0.10340   0.09923   0.0046   0.0047   1.0000
  17.500   1.0745   0.10934   0.10525   0.0018   0.0045   1.0000
  17.750   1.0636   0.11511   0.11111  -0.0010   0.0044   1.0000
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