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MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 150 23.89% (mh150-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.89 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh150-il-1000000-n5.txt
Download as CSV file: xf-mh150-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 150  23.89%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.7255   0.11528   0.11142  -0.0537   0.8684   0.0136
 -19.000  -0.7304   0.11092   0.10696  -0.0560   0.8589   0.0138
 -18.750  -0.7343   0.10670   0.10266  -0.0584   0.8491   0.0140
 -18.500  -0.7389   0.10244   0.09829  -0.0607   0.8399   0.0142
 -18.250  -0.7412   0.09855   0.09433  -0.0628   0.8318   0.0144
 -18.000  -0.7450   0.09445   0.09014  -0.0651   0.8233   0.0146
 -17.750  -0.7462   0.09077   0.08637  -0.0671   0.8158   0.0149
 -17.500  -0.7490   0.08688   0.08240  -0.0693   0.8082   0.0151
 -17.250  -0.7496   0.08335   0.07878  -0.0712   0.7999   0.0154
 -17.000  -0.7509   0.07972   0.07507  -0.0733   0.7931   0.0156
 -16.750  -0.7512   0.07628   0.07156  -0.0752   0.7863   0.0159
 -16.500  -0.7509   0.07293   0.06812  -0.0771   0.7787   0.0161
 -16.250  -0.7520   0.06944   0.06455  -0.0791   0.7720   0.0165
 -16.000  -0.7538   0.06589   0.06093  -0.0812   0.7655   0.0168
 -15.750  -0.7532   0.06266   0.05762  -0.0831   0.7582   0.0173
 -15.500  -0.7538   0.05930   0.05418  -0.0851   0.7515   0.0177
 -15.250  -0.7514   0.05635   0.05118  -0.0868   0.7457   0.0182
 -15.000  -0.7497   0.05330   0.04805  -0.0887   0.7388   0.0187
 -14.750  -0.7467   0.05045   0.04511  -0.0905   0.7316   0.0191
 -14.500  -0.7445   0.04751   0.04211  -0.0923   0.7261   0.0198
 -14.250  -0.7420   0.04462   0.03917  -0.0942   0.7199   0.0204
 -14.000  -0.7378   0.04194   0.03641  -0.0960   0.7130   0.0212
 -13.750  -0.7312   0.03957   0.03397  -0.0976   0.7067   0.0220
 -13.500  -0.7257   0.03705   0.03140  -0.0993   0.7010   0.0229
 -13.250  -0.7195   0.03466   0.02895  -0.1010   0.6947   0.0239
 -13.000  -0.7111   0.03252   0.02673  -0.1027   0.6882   0.0251
 -12.750  -0.7019   0.03043   0.02461  -0.1043   0.6828   0.0263
 -12.500  -0.6914   0.02848   0.02261  -0.1059   0.6766   0.0279
 -12.250  -0.6790   0.02668   0.02076  -0.1075   0.6700   0.0297
 -12.000  -0.6658   0.02492   0.01895  -0.1092   0.6643   0.0321
 -11.750  -0.6508   0.02327   0.01728  -0.1109   0.6591   0.0348
 -11.500  -0.6357   0.02183   0.01581  -0.1123   0.6526   0.0378
 -11.000  -0.5965   0.01926   0.01318  -0.1162   0.6409   0.0458
 -10.750  -0.5718   0.01810   0.01202  -0.1187   0.6357   0.0508
 -10.500  -0.5450   0.01707   0.01098  -0.1212   0.6295   0.0564
 -10.000  -0.4850   0.01530   0.00920  -0.1267   0.6177   0.0694
  -9.750  -0.4525   0.01454   0.00844  -0.1295   0.6119   0.0770
  -9.500  -0.4190   0.01387   0.00777  -0.1323   0.6061   0.0853
  -9.250  -0.3847   0.01327   0.00717  -0.1351   0.6007   0.0948
  -9.000  -0.3503   0.01274   0.00666  -0.1375   0.5952   0.1046
  -8.750  -0.3167   0.01232   0.00625  -0.1395   0.5888   0.1139
  -8.500  -0.2836   0.01198   0.00590  -0.1413   0.5827   0.1230
  -8.250  -0.2497   0.01160   0.00555  -0.1431   0.5784   0.1343
  -8.000  -0.2156   0.01122   0.00521  -0.1450   0.5732   0.1480
  -7.750  -0.1816   0.01088   0.00490  -0.1469   0.5670   0.1633
  -7.500  -0.1477   0.01059   0.00463  -0.1486   0.5608   0.1793
  -7.250  -0.1138   0.01033   0.00442  -0.1501   0.5563   0.1921
  -7.000  -0.0803   0.01014   0.00424  -0.1515   0.5512   0.2030
  -6.750  -0.0475   0.01003   0.00410  -0.1527   0.5454   0.2118
  -6.500  -0.0146   0.00991   0.00398  -0.1539   0.5398   0.2211
  -6.250   0.0182   0.00982   0.00387  -0.1549   0.5350   0.2281
  -6.000   0.0511   0.00972   0.00377  -0.1561   0.5299   0.2362
  -5.750   0.0831   0.00969   0.00370  -0.1569   0.5244   0.2419
  -5.500   0.1157   0.00963   0.00362  -0.1580   0.5193   0.2479
  -5.250   0.1483   0.00957   0.00356  -0.1590   0.5146   0.2536
  -5.000   0.1803   0.00956   0.00351  -0.1598   0.5093   0.2581
  -4.750   0.2123   0.00955   0.00346  -0.1607   0.5043   0.2621
  -4.500   0.2447   0.00952   0.00341  -0.1616   0.4999   0.2673
  -4.250   0.2770   0.00949   0.00337  -0.1625   0.4958   0.2718
  -4.000   0.3088   0.00950   0.00335  -0.1633   0.4907   0.2756
  -3.750   0.3402   0.00953   0.00333  -0.1640   0.4854   0.2784
  -3.500   0.3723   0.00953   0.00331  -0.1650   0.4809   0.2834
  -3.250   0.4046   0.00951   0.00329  -0.1659   0.4776   0.2880
  -3.000   0.4365   0.00952   0.00328  -0.1667   0.4737   0.2922
  -2.750   0.4679   0.00955   0.00329  -0.1674   0.4692   0.2956
  -2.500   0.4993   0.00960   0.00330  -0.1682   0.4643   0.2996
  -2.250   0.5313   0.00961   0.00330  -0.1691   0.4603   0.3052
  -2.000   0.5630   0.00962   0.00332  -0.1699   0.4565   0.3102
  -1.750   0.5943   0.00966   0.00334  -0.1706   0.4527   0.3142
  -1.500   0.6254   0.00972   0.00337  -0.1713   0.4487   0.3175
  -1.250   0.6567   0.00978   0.00341  -0.1721   0.4445   0.3224
  -1.000   0.6881   0.00981   0.00344  -0.1729   0.4414   0.3273
  -0.750   0.7195   0.00985   0.00348  -0.1736   0.4381   0.3323
  -0.500   0.7503   0.00992   0.00353  -0.1742   0.4341   0.3360
  -0.250   0.7812   0.00999   0.00358  -0.1749   0.4299   0.3412
   0.000   0.8118   0.01007   0.00366  -0.1756   0.4257   0.3466
   0.250   0.8426   0.01014   0.00372  -0.1763   0.4228   0.3518
   0.500   0.8733   0.01020   0.00379  -0.1769   0.4201   0.3565
   0.750   0.9043   0.01026   0.00386  -0.1777   0.4170   0.3636
   1.000   0.9348   0.01034   0.00394  -0.1783   0.4135   0.3702
   1.250   0.9646   0.01046   0.00404  -0.1788   0.4096   0.3756
   1.500   0.9942   0.01059   0.00416  -0.1793   0.4054   0.3813
   1.750   1.0248   0.01065   0.00425  -0.1800   0.4030   0.3884
   2.000   1.0548   0.01074   0.00434  -0.1805   0.4001   0.3953
   2.250   1.0846   0.01084   0.00445  -0.1811   0.3971   0.4022
   2.500   1.1143   0.01095   0.00458  -0.1816   0.3939   0.4106
   2.750   1.1431   0.01110   0.00472  -0.1820   0.3906   0.4176
   3.000   1.1717   0.01126   0.00487  -0.1823   0.3871   0.4239
   3.250   1.2014   0.01135   0.00500  -0.1828   0.3849   0.4319
   3.500   1.2303   0.01147   0.00514  -0.1832   0.3820   0.4391
   3.750   1.2588   0.01161   0.00529  -0.1836   0.3788   0.4461
   4.000   1.2871   0.01176   0.00546  -0.1839   0.3757   0.4554
   4.250   1.3143   0.01196   0.00565  -0.1841   0.3725   0.4632
   4.500   1.3413   0.01216   0.00586  -0.1842   0.3693   0.4707
   4.750   1.3694   0.01229   0.00603  -0.1845   0.3673   0.4787
   5.000   1.3967   0.01245   0.00621  -0.1846   0.3648   0.4856
   5.250   1.4235   0.01263   0.00641  -0.1847   0.3618   0.4928
   5.500   1.4495   0.01284   0.00664  -0.1847   0.3588   0.5018
   5.750   1.4742   0.01308   0.00689  -0.1844   0.3560   0.5094
   6.000   1.4964   0.01335   0.00717  -0.1837   0.3528   0.5172
   6.250   1.5192   0.01359   0.00744  -0.1832   0.3505   0.5248
   6.500   1.5434   0.01382   0.00771  -0.1829   0.3483   0.5318
   6.750   1.5673   0.01409   0.00801  -0.1826   0.3458   0.5399
   7.000   1.5902   0.01439   0.00835  -0.1822   0.3433   0.5483
   7.250   1.6116   0.01477   0.00874  -0.1816   0.3404   0.5553
   7.500   1.6320   0.01520   0.00919  -0.1808   0.3372   0.5632
   7.750   1.6516   0.01569   0.00970  -0.1801   0.3342   0.5711
   8.000   1.6738   0.01604   0.01009  -0.1796   0.3326   0.5782
   8.250   1.6955   0.01644   0.01054  -0.1792   0.3305   0.5857
   8.500   1.7160   0.01690   0.01105  -0.1786   0.3279   0.5936
   8.750   1.7353   0.01744   0.01161  -0.1779   0.3253   0.6008
   9.000   1.7533   0.01807   0.01226  -0.1771   0.3225   0.6074
   9.250   1.7701   0.01879   0.01302  -0.1762   0.3195   0.6147
   9.500   1.7870   0.01951   0.01377  -0.1754   0.3167   0.6218
   9.750   1.8065   0.02009   0.01439  -0.1748   0.3148   0.6279
  10.000   1.8246   0.02078   0.01514  -0.1742   0.3122   0.6347
  10.250   1.8414   0.02155   0.01595  -0.1734   0.3092   0.6417
  10.500   1.8554   0.02252   0.01694  -0.1724   0.3060   0.6480
  10.750   1.8681   0.02360   0.01804  -0.1714   0.3027   0.6537
  11.000   1.8816   0.02466   0.01915  -0.1704   0.3001   0.6601
  11.250   1.8982   0.02548   0.02003  -0.1698   0.2980   0.6668
  11.500   1.9121   0.02651   0.02110  -0.1689   0.2954   0.6726
  11.750   1.9252   0.02761   0.02225  -0.1680   0.2926   0.6784
  12.000   1.9352   0.02897   0.02365  -0.1670   0.2895   0.6846
  12.250   1.9435   0.03046   0.02517  -0.1658   0.2863   0.6906
  12.750   1.9651   0.03314   0.02795  -0.1639   0.2812   0.7014
  13.000   1.9751   0.03458   0.02946  -0.1630   0.2784   0.7074
  13.250   1.9834   0.03618   0.03110  -0.1620   0.2753   0.7132
  13.750   1.9909   0.04025   0.03524  -0.1597   0.2682   0.7229
  14.000   1.9994   0.04192   0.03698  -0.1589   0.2657   0.7284
  14.250   2.0070   0.04368   0.03879  -0.1581   0.2626   0.7339
  14.500   2.0098   0.04590   0.04105  -0.1570   0.2590   0.7385
  14.750   2.0091   0.04847   0.04366  -0.1559   0.2550   0.7430
  15.000   2.0097   0.05098   0.04623  -0.1549   0.2516   0.7476
  15.250   2.0153   0.05298   0.04829  -0.1541   0.2483   0.7529
  15.500   2.0147   0.05566   0.05102  -0.1532   0.2445   0.7575
  15.750   2.0099   0.05874   0.05412  -0.1521   0.2400   0.7614
  16.000   2.0062   0.06179   0.05724  -0.1512   0.2363   0.7656
  16.250   2.0079   0.06428   0.05978  -0.1505   0.2324   0.7701
  16.500   2.0009   0.06774   0.06329  -0.1496   0.2279   0.7743
  16.750   1.9875   0.07190   0.06748  -0.1486   0.2230   0.7780
  17.000   1.9871   0.07468   0.07031  -0.1481   0.2189   0.7819
  17.250   1.9766   0.07863   0.07431  -0.1473   0.2136   0.7857
  17.500   1.9623   0.08302   0.07873  -0.1466   0.2079   0.7891
  17.750   1.9537   0.08681   0.08257  -0.1461   0.2026   0.7928
  18.000   1.9348   0.09187   0.08766  -0.1456   0.1964   0.7959
  18.250   1.9270   0.09565   0.09147  -0.1454   0.1911   0.7993
  18.500   1.9113   0.10042   0.09628  -0.1452   0.1852   0.8024
  18.750   1.8983   0.10487   0.10076  -0.1451   0.1798   0.8058
  19.000   1.8866   0.10926   0.10519  -0.1452   0.1740   0.8092
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