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MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 150 23.89% (mh150-il)
Reynolds number: 500,000
Max Cl/Cd: 90.52 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh150-il-500000.txt
Download as CSV file: xf-mh150-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.6343   0.08872   0.08454  -0.0784   0.9619   0.0302
 -16.750  -0.6393   0.08559   0.08136  -0.0788   0.9430   0.0309
 -16.500  -0.6423   0.08270   0.07838  -0.0791   0.9263   0.0318
 -16.250  -0.6438   0.07962   0.07520  -0.0800   0.9120   0.0328
 -16.000  -0.6494   0.07603   0.07155  -0.0813   0.8998   0.0338
 -15.750  -0.6537   0.07248   0.06792  -0.0827   0.8880   0.0349
 -15.500  -0.6538   0.06931   0.06466  -0.0842   0.8776   0.0364
 -15.250  -0.6587   0.06563   0.06089  -0.0860   0.8673   0.0378
 -15.000  -0.6617   0.06211   0.05731  -0.0879   0.8581   0.0396
 -14.750  -0.6626   0.05885   0.05395  -0.0896   0.8486   0.0416
 -14.500  -0.6683   0.05510   0.05013  -0.0916   0.8401   0.0436
 -14.250  -0.6678   0.05196   0.04693  -0.0935   0.8316   0.0463
 -14.000  -0.6725   0.04835   0.04325  -0.0956   0.8231   0.0489
 -13.750  -0.6735   0.04516   0.03998  -0.0976   0.8153   0.0521
 -13.500  -0.6740   0.04198   0.03677  -0.0997   0.8072   0.0558
 -13.250  -0.6750   0.03888   0.03359  -0.1017   0.7994   0.0597
 -13.000  -0.6732   0.03607   0.03072  -0.1036   0.7921   0.0642
 -12.750  -0.6691   0.03351   0.02813  -0.1055   0.7843   0.0692
 -12.500  -0.6650   0.03100   0.02555  -0.1073   0.7768   0.0746
 -12.250  -0.6583   0.02867   0.02320  -0.1092   0.7699   0.0802
 -12.000  -0.6487   0.02658   0.02109  -0.1110   0.7627   0.0864
 -11.750  -0.6366   0.02475   0.01920  -0.1128   0.7556   0.0929
 -11.500  -0.6220   0.02320   0.01761  -0.1144   0.7489   0.0999
 -11.250  -0.6088   0.02168   0.01609  -0.1159   0.7420   0.1070
 -11.000  -0.5894   0.02031   0.01468  -0.1181   0.7354   0.1148
 -10.750  -0.5665   0.01914   0.01347  -0.1204   0.7290   0.1232
 -10.500  -0.5406   0.01807   0.01241  -0.1229   0.7227   0.1320
 -10.000  -0.4826   0.01630   0.01056  -0.1281   0.7097   0.1511
  -9.750  -0.4506   0.01550   0.00977  -0.1310   0.7040   0.1611
  -9.500  -0.4176   0.01482   0.00909  -0.1337   0.6977   0.1716
  -9.250  -0.3842   0.01427   0.00851  -0.1361   0.6913   0.1833
  -9.000  -0.3510   0.01384   0.00805  -0.1383   0.6852   0.1962
  -8.750  -0.3176   0.01345   0.00768  -0.1402   0.6795   0.2092
  -8.500  -0.2842   0.01311   0.00735  -0.1420   0.6735   0.2212
  -8.250  -0.2514   0.01290   0.00709  -0.1435   0.6674   0.2318
  -8.000  -0.2186   0.01277   0.00690  -0.1448   0.6617   0.2417
  -7.750  -0.1856   0.01255   0.00670  -0.1462   0.6556   0.2501
  -7.500  -0.1531   0.01247   0.00653  -0.1473   0.6497   0.2577
  -7.250  -0.1209   0.01237   0.00635  -0.1484   0.6438   0.2644
  -7.000  -0.0881   0.01223   0.00624  -0.1496   0.6385   0.2710
  -6.750  -0.0557   0.01219   0.00610  -0.1506   0.6324   0.2769
  -6.500  -0.0238   0.01207   0.00593  -0.1515   0.6265   0.2829
  -6.250   0.0084   0.01202   0.00585  -0.1525   0.6210   0.2886
  -6.000   0.0408   0.01196   0.00575  -0.1535   0.6156   0.2939
  -5.750   0.0729   0.01191   0.00562  -0.1544   0.6097   0.2985
  -5.500   0.1044   0.01183   0.00551  -0.1553   0.6038   0.3040
  -5.250   0.1364   0.01179   0.00545  -0.1562   0.5986   0.3089
  -5.000   0.1685   0.01176   0.00537  -0.1570   0.5931   0.3135
  -4.750   0.2003   0.01174   0.00527  -0.1579   0.5876   0.3175
  -4.500   0.2316   0.01170   0.00519  -0.1587   0.5817   0.3228
  -4.250   0.2636   0.01164   0.00515  -0.1595   0.5769   0.3275
  -4.000   0.2954   0.01162   0.00509  -0.1604   0.5714   0.3321
  -3.750   0.3270   0.01166   0.00503  -0.1611   0.5662   0.3360
  -3.500   0.3581   0.01164   0.00498  -0.1619   0.5608   0.3413
  -3.250   0.3900   0.01158   0.00496  -0.1628   0.5562   0.3463
  -3.000   0.4216   0.01158   0.00494  -0.1636   0.5509   0.3512
  -2.750   0.4528   0.01164   0.00490  -0.1643   0.5457   0.3558
  -2.500   0.4839   0.01167   0.00489  -0.1650   0.5405   0.3613
  -2.250   0.5157   0.01163   0.00490  -0.1659   0.5363   0.3667
  -2.000   0.5471   0.01165   0.00491  -0.1667   0.5315   0.3721
  -1.750   0.5781   0.01171   0.00490  -0.1673   0.5268   0.3767
  -1.500   0.6089   0.01178   0.00492  -0.1681   0.5216   0.3825
  -1.250   0.6403   0.01177   0.00497  -0.1689   0.5174   0.3887
  -1.000   0.6715   0.01181   0.00500  -0.1696   0.5128   0.3948
  -0.750   0.7022   0.01188   0.00502  -0.1703   0.5083   0.4003
  -0.500   0.7330   0.01195   0.00508  -0.1710   0.5038   0.4072
  -0.250   0.7636   0.01205   0.00517  -0.1716   0.4996   0.4140
   0.000   0.7944   0.01212   0.00523  -0.1723   0.4958   0.4205
   0.250   0.8253   0.01214   0.00531  -0.1731   0.4915   0.4286
   0.500   0.8555   0.01224   0.00539  -0.1736   0.4871   0.4363
   0.750   0.8850   0.01244   0.00549  -0.1741   0.4824   0.4432
   1.000   0.9156   0.01249   0.00562  -0.1748   0.4789   0.4515
   1.250   0.9458   0.01257   0.00573  -0.1754   0.4752   0.4598
   1.500   0.9757   0.01268   0.00583  -0.1760   0.4713   0.4679
   1.750   1.0052   0.01280   0.00597  -0.1765   0.4675   0.4767
   2.000   1.0341   0.01303   0.00614  -0.1769   0.4632   0.4852
   2.250   1.0636   0.01315   0.00630  -0.1774   0.4598   0.4933
   2.500   1.0928   0.01325   0.00645  -0.1778   0.4562   0.5019
   2.750   1.1216   0.01340   0.00659  -0.1782   0.4525   0.5099
   3.000   1.1501   0.01355   0.00677  -0.1785   0.4488   0.5186
   3.250   1.1778   0.01379   0.00698  -0.1787   0.4451   0.5276
   3.500   1.2061   0.01402   0.00720  -0.1790   0.4417   0.5358
   3.750   1.2341   0.01414   0.00741  -0.1793   0.4388   0.5442
   4.000   1.2616   0.01431   0.00760  -0.1794   0.4354   0.5526
   4.250   1.2887   0.01450   0.00780  -0.1796   0.4319   0.5603
   4.500   1.3149   0.01473   0.00804  -0.1795   0.4284   0.5684
   4.750   1.3413   0.01508   0.00832  -0.1796   0.4244   0.5769
   5.000   1.3676   0.01526   0.00858  -0.1795   0.4219   0.5848
   5.250   1.3932   0.01546   0.00885  -0.1794   0.4191   0.5928
   5.500   1.4185   0.01569   0.00910  -0.1793   0.4160   0.6006
   5.750   1.4429   0.01594   0.00937  -0.1790   0.4128   0.6080
   6.000   1.4658   0.01624   0.00968  -0.1784   0.4096   0.6158
   6.250   1.4893   0.01664   0.01003  -0.1780   0.4058   0.6237
   6.500   1.5105   0.01690   0.01037  -0.1772   0.4036   0.6309
   6.750   1.5320   0.01719   0.01075  -0.1765   0.4010   0.6383
   7.000   1.5536   0.01753   0.01113  -0.1759   0.3981   0.6460
   7.250   1.5747   0.01790   0.01152  -0.1752   0.3951   0.6531
   7.500   1.5948   0.01831   0.01196  -0.1744   0.3922   0.6601
   7.750   1.6156   0.01879   0.01242  -0.1737   0.3891   0.6676
   8.000   1.6372   0.01925   0.01289  -0.1732   0.3862   0.6747
   8.250   1.6553   0.01971   0.01346  -0.1722   0.3839   0.6814
   8.500   1.6737   0.02021   0.01403  -0.1713   0.3811   0.6884
   8.750   1.6924   0.02075   0.01459  -0.1705   0.3784   0.6954
   9.000   1.7101   0.02130   0.01520  -0.1696   0.3757   0.7018
   9.250   1.7274   0.02192   0.01584  -0.1686   0.3728   0.7084
   9.500   1.7483   0.02250   0.01636  -0.1680   0.3693   0.7153
   9.750   1.7636   0.02319   0.01716  -0.1670   0.3673   0.7215
  10.000   1.7786   0.02393   0.01800  -0.1659   0.3649   0.7276
  10.250   1.7939   0.02470   0.01884  -0.1650   0.3621   0.7343
  10.500   1.8090   0.02551   0.01969  -0.1641   0.3593   0.7406
  10.750   1.8234   0.02633   0.02055  -0.1630   0.3565   0.7463
  11.000   1.8387   0.02715   0.02136  -0.1620   0.3534   0.7525
  11.250   1.8546   0.02800   0.02223  -0.1612   0.3505   0.7590
  11.500   1.8652   0.02910   0.02346  -0.1600   0.3481   0.7644
  11.750   1.8763   0.03021   0.02466  -0.1589   0.3452   0.7702
  12.000   1.8875   0.03137   0.02587  -0.1579   0.3424   0.7765
  12.250   1.8991   0.03250   0.02703  -0.1569   0.3395   0.7820
  12.500   1.9113   0.03352   0.02806  -0.1558   0.3365   0.7873
  12.750   1.9244   0.03454   0.02911  -0.1548   0.3335   0.7934
  13.000   1.9316   0.03612   0.03080  -0.1538   0.3310   0.7992
  13.250   1.9384   0.03769   0.03247  -0.1527   0.3282   0.8040
  13.500   1.9467   0.03918   0.03404  -0.1517   0.3253   0.8096
  13.750   1.9548   0.04076   0.03564  -0.1508   0.3222   0.8157
  14.000   1.9653   0.04200   0.03688  -0.1498   0.3189   0.8205
  14.250   1.9739   0.04348   0.03842  -0.1489   0.3161   0.8256
  14.500   1.9765   0.04569   0.04076  -0.1480   0.3132   0.8314
  14.750   1.9805   0.04778   0.04294  -0.1472   0.3100   0.8366
  15.000   1.9847   0.04980   0.04503  -0.1464   0.3067   0.8415
  15.250   1.9913   0.05156   0.04678  -0.1455   0.3034   0.8471
  15.500   2.0000   0.05311   0.04834  -0.1448   0.3000   0.8525
  15.750   1.9975   0.05597   0.05136  -0.1440   0.2969   0.8573
  16.000   1.9961   0.05879   0.05428  -0.1433   0.2933   0.8628
  16.250   1.9978   0.06127   0.05681  -0.1428   0.2896   0.8681
  16.500   2.0023   0.06326   0.05879  -0.1420   0.2859   0.8732
  16.750   2.0025   0.06590   0.06152  -0.1415   0.2825   0.8789
  17.000   1.9951   0.06955   0.06530  -0.1410   0.2785   0.8841
  17.250   1.9919   0.07265   0.06847  -0.1405   0.2744   0.8896
  17.500   1.9933   0.07515   0.07095  -0.1400   0.2703   0.8958
  17.750   1.9902   0.07821   0.07411  -0.1396   0.2664   0.9015
  18.000   1.9790   0.08241   0.07843  -0.1394   0.2619   0.9075
  18.250   1.9729   0.08591   0.08197  -0.1391   0.2573   0.9145
  18.500   1.9746   0.08829   0.08433  -0.1387   0.2527   0.9245
  18.750   1.9569   0.09326   0.08948  -0.1385   0.2480   0.9377
  19.000   1.9477   0.09690   0.09317  -0.1383   0.2430   0.9999
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