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MH 78 14.47% (mh78-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 78 14.47% (mh78-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.16 at α=11.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh78-il-1000000-n5.txt
Download as CSV file: xf-mh78-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 78  14.47%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0895   0.08194   0.07908   0.0131   1.0000   0.0066
 -15.500  -1.1359   0.06780   0.06468   0.0032   1.0000   0.0066
 -15.250  -1.1658   0.05741   0.05407  -0.0047   1.0000   0.0066
 -15.000  -1.1847   0.05042   0.04690  -0.0095   1.0000   0.0066
 -14.750  -1.1955   0.04574   0.04208  -0.0118   1.0000   0.0066
 -14.500  -1.2137   0.04107   0.03723  -0.0129   1.0000   0.0066
 -14.250  -1.2225   0.03799   0.03402  -0.0124   1.0000   0.0066
 -14.000  -1.2276   0.03555   0.03146  -0.0111   1.0000   0.0066
 -13.750  -1.2324   0.03335   0.02912  -0.0092   1.0000   0.0066
 -13.500  -1.2276   0.03198   0.02768  -0.0073   1.0000   0.0066
 -13.250  -1.2287   0.03028   0.02586  -0.0047   1.0000   0.0066
 -13.000  -1.2286   0.02874   0.02420  -0.0017   1.0000   0.0066
 -12.750  -1.2225   0.02765   0.02303   0.0010   1.0000   0.0066
 -12.500  -1.2181   0.02645   0.02172   0.0042   1.0000   0.0067
 -12.250  -1.2063   0.02548   0.02068   0.0064   1.0000   0.0067
 -12.000  -1.1928   0.02445   0.01956   0.0083   1.0000   0.0068
 -11.750  -1.1766   0.02355   0.01859   0.0100   1.0000   0.0068
 -11.500  -1.1596   0.02271   0.01760   0.0116   0.9074   0.0068
 -11.250  -1.1470   0.02222   0.01680   0.0144   0.8177   0.0069
 -11.000  -1.1284   0.02159   0.01598   0.0159   0.7740   0.0069
 -10.750  -1.1084   0.02096   0.01520   0.0173   0.7399   0.0070
 -10.500  -1.0875   0.02036   0.01445   0.0185   0.7097   0.0070
 -10.250  -1.0659   0.01976   0.01373   0.0196   0.6850   0.0071
 -10.000  -1.0436   0.01921   0.01305   0.0207   0.6614   0.0071
  -9.750  -1.0207   0.01869   0.01243   0.0217   0.6396   0.0072
  -9.500  -0.9974   0.01817   0.01181   0.0226   0.6199   0.0072
  -9.250  -0.9737   0.01768   0.01122   0.0235   0.6012   0.0073
  -9.000  -0.9496   0.01722   0.01067   0.0244   0.5838   0.0073
  -8.750  -0.9251   0.01679   0.01014   0.0252   0.5658   0.0074
  -8.500  -0.9004   0.01635   0.00962   0.0259   0.5493   0.0075
  -8.250  -0.8753   0.01595   0.00914   0.0267   0.5342   0.0076
  -8.000  -0.8500   0.01556   0.00867   0.0274   0.5199   0.0078
  -7.500  -0.7987   0.01484   0.00780   0.0287   0.4916   0.0080
  -7.250  -0.7726   0.01450   0.00740   0.0293   0.4785   0.0081
  -6.750  -0.7199   0.01389   0.00665   0.0305   0.4535   0.0084
  -6.500  -0.6933   0.01362   0.00632   0.0310   0.4423   0.0085
  -6.250  -0.6665   0.01335   0.00600   0.0315   0.4302   0.0086
  -6.000  -0.6401   0.01301   0.00560   0.0321   0.4195   0.0089
  -5.750  -0.6131   0.01275   0.00529   0.0326   0.4091   0.0091
  -5.500  -0.5860   0.01251   0.00501   0.0330   0.4006   0.0093
  -5.250  -0.5587   0.01229   0.00475   0.0335   0.3903   0.0096
  -5.000  -0.5312   0.01210   0.00452   0.0339   0.3806   0.0099
  -4.750  -0.5037   0.01191   0.00429   0.0343   0.3706   0.0102
  -4.500  -0.4759   0.01174   0.00408   0.0346   0.3629   0.0106
  -4.250  -0.4482   0.01157   0.00387   0.0350   0.3546   0.0109
  -4.000  -0.4205   0.01139   0.00366   0.0354   0.3470   0.0116
  -3.750  -0.3927   0.01123   0.00348   0.0357   0.3389   0.0124
  -3.500  -0.3647   0.01111   0.00331   0.0360   0.3301   0.0132
  -3.250  -0.3368   0.01096   0.00315   0.0364   0.3235   0.0145
  -3.000  -0.3087   0.01084   0.00301   0.0367   0.3162   0.0162
  -2.750  -0.2806   0.01071   0.00287   0.0369   0.3103   0.0189
  -2.500  -0.2526   0.01057   0.00275   0.0372   0.3040   0.0235
  -2.250  -0.2245   0.01046   0.00263   0.0375   0.2963   0.0299
  -2.000  -0.1965   0.01032   0.00252   0.0378   0.2909   0.0393
  -1.750  -0.1687   0.01016   0.00240   0.0381   0.2853   0.0552
  -1.500  -0.1411   0.00998   0.00230   0.0384   0.2795   0.0789
  -1.250  -0.1137   0.00975   0.00220   0.0387   0.2753   0.1139
  -1.000  -0.0866   0.00951   0.00211   0.0390   0.2703   0.1595
  -0.750  -0.0596   0.00928   0.00204   0.0393   0.2646   0.2094
  -0.250  -0.0055   0.00882   0.00193   0.0400   0.2567   0.3194
   0.000   0.0199   0.00841   0.00187   0.0406   0.2528   0.4221
   0.250   0.0447   0.00801   0.00182   0.0412   0.2485   0.5302
   0.500   0.0703   0.00773   0.00179   0.0419   0.2445   0.6114
   0.750   0.0960   0.00747   0.00177   0.0425   0.2414   0.6840
   1.000   0.1213   0.00725   0.00179   0.0434   0.2382   0.7580
   1.250   0.1475   0.00716   0.00185   0.0441   0.2348   0.8118
   1.500   0.1752   0.00720   0.00193   0.0445   0.2311   0.8387
   1.750   0.2036   0.00725   0.00200   0.0448   0.2282   0.8558
   2.000   0.2322   0.00732   0.00206   0.0450   0.2254   0.8686
   2.250   0.2606   0.00739   0.00213   0.0452   0.2224   0.8783
   2.500   0.2891   0.00749   0.00220   0.0454   0.2195   0.8888
   2.750   0.3168   0.00760   0.00231   0.0458   0.2164   0.8995
   3.000   0.3448   0.00770   0.00240   0.0461   0.2138   0.9093
   3.250   0.3723   0.00780   0.00251   0.0465   0.2118   0.9177
   3.500   0.4000   0.00791   0.00260   0.0468   0.2091   0.9254
   3.750   0.4272   0.00802   0.00271   0.0473   0.2066   0.9316
   4.000   0.4545   0.00814   0.00281   0.0477   0.2040   0.9372
   4.250   0.4824   0.00828   0.00291   0.0479   0.2012   0.9410
   4.500   0.5109   0.00838   0.00300   0.0480   0.1992   0.9433
   4.750   0.5395   0.00847   0.00309   0.0480   0.1972   0.9453
   5.000   0.5678   0.00858   0.00319   0.0481   0.1948   0.9474
   5.250   0.5961   0.00869   0.00329   0.0481   0.1925   0.9496
   5.500   0.6244   0.00883   0.00341   0.0482   0.1901   0.9517
   5.750   0.6523   0.00898   0.00353   0.0482   0.1876   0.9542
   6.000   0.6803   0.00911   0.00366   0.0483   0.1857   0.9565
   6.250   0.7088   0.00922   0.00377   0.0483   0.1840   0.9583
   6.500   0.7374   0.00934   0.00390   0.0482   0.1818   0.9600
   6.750   0.7658   0.00948   0.00403   0.0481   0.1795   0.9619
   7.000   0.7939   0.00964   0.00418   0.0481   0.1773   0.9641
   7.250   0.8217   0.00982   0.00435   0.0481   0.1750   0.9666
   7.500   0.8492   0.00999   0.00452   0.0482   0.1730   0.9692
   7.750   0.8773   0.01012   0.00467   0.0481   0.1716   0.9713
   8.000   0.9071   0.01028   0.00484   0.0477   0.1696   0.9727
   8.250   0.9367   0.01046   0.00502   0.0472   0.1674   0.9743
   8.500   0.9659   0.01066   0.00521   0.0468   0.1652   0.9761
   8.750   0.9948   0.01088   0.00543   0.0464   0.1630   0.9782
   9.000   1.0233   0.01110   0.00566   0.0461   0.1609   0.9806
   9.250   1.0518   0.01128   0.00586   0.0459   0.1597   0.9830
   9.500   1.0831   0.01148   0.00608   0.0450   0.1579   0.9840
   9.750   1.1140   0.01171   0.00632   0.0441   0.1558   0.9851
  10.000   1.1446   0.01196   0.00658   0.0433   0.1538   0.9863
  10.250   1.1747   0.01224   0.00686   0.0425   0.1517   0.9877
  10.500   1.2045   0.01255   0.00718   0.0417   0.1493   0.9892
  10.750   1.2345   0.01278   0.00744   0.0410   0.1481   0.9907
  11.000   1.2639   0.01303   0.00772   0.0403   0.1464   0.9924
  11.250   1.2932   0.01331   0.00803   0.0396   0.1444   0.9940
  11.500   1.3234   0.01363   0.00836   0.0386   0.1422   0.9955
  11.750   1.3530   0.01401   0.00874   0.0377   0.1397   0.9974
  12.000   1.3824   0.01438   0.00913   0.0368   0.1377   0.9992
  12.250   1.4069   0.01467   0.00946   0.0369   0.1362   1.0000
  12.500   1.4259   0.01498   0.00980   0.0381   0.1344   1.0000
  12.750   1.4452   0.01533   0.01018   0.0391   0.1323   1.0000
  13.000   1.4643   0.01575   0.01061   0.0400   0.1302   1.0000
  13.250   1.4831   0.01623   0.01110   0.0409   0.1281   1.0000
  13.500   1.5030   0.01664   0.01155   0.0416   0.1267   1.0000
  13.750   1.5226   0.01705   0.01202   0.0422   0.1252   1.0000
  14.000   1.5410   0.01753   0.01254   0.0430   0.1235   1.0000
  14.250   1.5574   0.01809   0.01313   0.0439   0.1216   1.0000
  14.500   1.5695   0.01878   0.01385   0.0452   0.1197   1.0000
  14.750   1.5724   0.01971   0.01483   0.0473   0.1181   1.0000
  15.000   1.5780   0.02084   0.01602   0.0484   0.1168   1.0000
  15.250   1.5853   0.02213   0.01737   0.0488   0.1154   1.0000
  15.500   1.5915   0.02370   0.01901   0.0488   0.1137   1.0000
  15.750   1.5956   0.02563   0.02100   0.0485   0.1121   1.0000
  16.000   1.5962   0.02802   0.02346   0.0479   0.1102   1.0000
  16.250   1.5927   0.03093   0.02643   0.0470   0.1085   1.0000
  16.500   1.5905   0.03376   0.02935   0.0461   0.1071   1.0000
  16.750   1.5865   0.03681   0.03248   0.0451   0.1057   1.0000
  17.000   1.5789   0.04027   0.03603   0.0439   0.1043   1.0000
  17.250   1.5652   0.04446   0.04029   0.0424   0.1027   1.0000
  17.500   1.5458   0.04930   0.04521   0.0405   0.1009   1.0000
  17.750   1.5196   0.05507   0.05107   0.0382   0.0994   1.0000
  18.000   1.5031   0.05989   0.05599   0.0362   0.0981   1.0000
  18.250   1.4856   0.06498   0.06117   0.0340   0.0964   1.0000
  18.500   1.4658   0.07050   0.06677   0.0316   0.0945   1.0000
  18.750   1.4442   0.07638   0.07273   0.0289   0.0929   1.0000
  19.000   1.4137   0.08363   0.08005   0.0254   0.0906   1.0000
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