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MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 150 23.89% (mh150-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.32 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh150-il-1000000.txt
Download as CSV file: xf-mh150-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.7097   0.10027   0.09668  -0.0654   0.9467   0.0190
 -18.000  -0.7164   0.09649   0.09282  -0.0666   0.9298   0.0193
 -17.750  -0.7263   0.09204   0.08826  -0.0684   0.9146   0.0197
 -17.500  -0.7312   0.08823   0.08436  -0.0700   0.9006   0.0200
 -17.250  -0.7373   0.08418   0.08019  -0.0720   0.8874   0.0204
 -17.000  -0.7393   0.08058   0.07651  -0.0738   0.8764   0.0208
 -16.750  -0.7430   0.07682   0.07264  -0.0757   0.8653   0.0212
 -16.500  -0.7430   0.07349   0.06922  -0.0775   0.8559   0.0216
 -16.250  -0.7442   0.07002   0.06564  -0.0794   0.8459   0.0221
 -16.000  -0.7490   0.06616   0.06169  -0.0815   0.8372   0.0227
 -15.750  -0.7533   0.06235   0.05781  -0.0837   0.8285   0.0233
 -15.500  -0.7566   0.05874   0.05409  -0.0858   0.8194   0.0240
 -15.250  -0.7564   0.05552   0.05081  -0.0877   0.8122   0.0247
 -14.750  -0.7588   0.04888   0.04399  -0.0917   0.7956   0.0265
 -14.500  -0.7593   0.04563   0.04068  -0.0938   0.7888   0.0277
 -14.250  -0.7556   0.04291   0.03789  -0.0955   0.7811   0.0289
 -14.000  -0.7557   0.03981   0.03470  -0.0975   0.7732   0.0305
 -13.750  -0.7525   0.03704   0.03189  -0.0995   0.7667   0.0322
 -13.500  -0.7492   0.03435   0.02913  -0.1013   0.7592   0.0342
 -13.250  -0.7437   0.03193   0.02664  -0.1031   0.7516   0.0366
 -13.000  -0.7379   0.02947   0.02415  -0.1050   0.7458   0.0394
 -12.750  -0.7291   0.02731   0.02195  -0.1068   0.7387   0.0426
 -12.500  -0.7184   0.02533   0.01991  -0.1086   0.7310   0.0465
 -12.250  -0.7058   0.02343   0.01800  -0.1105   0.7253   0.0510
 -12.000  -0.6916   0.02169   0.01626  -0.1124   0.7189   0.0563
 -11.750  -0.6766   0.02020   0.01473  -0.1141   0.7120   0.0619
 -11.500  -0.6554   0.01881   0.01334  -0.1166   0.7058   0.0685
 -11.000  -0.6038   0.01644   0.01097  -0.1220   0.6932   0.0835
 -10.750  -0.5744   0.01549   0.01000  -0.1249   0.6864   0.0917
 -10.500  -0.5426   0.01462   0.00916  -0.1278   0.6815   0.1003
 -10.250  -0.5098   0.01388   0.00843  -0.1306   0.6752   0.1092
 -10.000  -0.4763   0.01326   0.00778  -0.1332   0.6684   0.1183
  -9.750  -0.4418   0.01267   0.00721  -0.1359   0.6629   0.1278
  -9.500  -0.4073   0.01216   0.00672  -0.1383   0.6576   0.1376
  -9.250  -0.3737   0.01174   0.00630  -0.1402   0.6514   0.1475
  -9.000  -0.3406   0.01140   0.00594  -0.1420   0.6444   0.1576
  -8.750  -0.3068   0.01106   0.00562  -0.1437   0.6396   0.1680
  -8.500  -0.2730   0.01074   0.00532  -0.1454   0.6340   0.1795
  -8.250  -0.2394   0.01044   0.00504  -0.1470   0.6280   0.1931
  -8.000  -0.2058   0.01020   0.00481  -0.1486   0.6220   0.2072
  -7.750  -0.1720   0.00996   0.00462  -0.1501   0.6169   0.2206
  -7.500  -0.1389   0.00981   0.00447  -0.1513   0.6109   0.2314
  -7.250  -0.1066   0.00973   0.00435  -0.1523   0.6046   0.2397
  -7.000  -0.0738   0.00963   0.00423  -0.1533   0.5997   0.2462
  -6.750  -0.0408   0.00952   0.00412  -0.1545   0.5944   0.2532
  -6.500  -0.0089   0.00949   0.00404  -0.1553   0.5884   0.2583
  -6.250   0.0232   0.00946   0.00395  -0.1562   0.5816   0.2636
  -6.000   0.0564   0.00936   0.00386  -0.1573   0.5776   0.2696
  -5.750   0.0886   0.00932   0.00380  -0.1582   0.5723   0.2745
  -5.500   0.1201   0.00935   0.00375  -0.1589   0.5663   0.2777
  -5.250   0.1527   0.00929   0.00367  -0.1599   0.5603   0.2833
  -5.000   0.1855   0.00922   0.00361  -0.1609   0.5560   0.2882
  -4.750   0.2176   0.00920   0.00356  -0.1618   0.5509   0.2924
  -4.500   0.2490   0.00924   0.00353  -0.1624   0.5453   0.2957
  -4.250   0.2809   0.00924   0.00349  -0.1633   0.5398   0.2995
  -4.000   0.3139   0.00917   0.00343  -0.1644   0.5354   0.3049
  -3.750   0.3459   0.00916   0.00341  -0.1652   0.5302   0.3092
  -3.500   0.3773   0.00920   0.00340  -0.1659   0.5247   0.3130
  -3.250   0.4085   0.00926   0.00340  -0.1666   0.5198   0.3159
  -3.000   0.4413   0.00920   0.00336  -0.1676   0.5160   0.3214
  -2.750   0.4735   0.00919   0.00335  -0.1685   0.5113   0.3266
  -2.500   0.5049   0.00924   0.00336  -0.1693   0.5060   0.3312
  -2.250   0.5357   0.00932   0.00339  -0.1699   0.5005   0.3351
  -2.000   0.5680   0.00930   0.00338  -0.1708   0.4970   0.3404
  -1.750   0.6001   0.00930   0.00339  -0.1717   0.4928   0.3465
  -1.500   0.6314   0.00935   0.00342  -0.1725   0.4882   0.3517
  -1.250   0.6619   0.00946   0.00347  -0.1730   0.4830   0.3557
  -1.000   0.6937   0.00947   0.00349  -0.1739   0.4795   0.3615
  -0.750   0.7257   0.00948   0.00352  -0.1748   0.4758   0.3683
  -0.500   0.7567   0.00953   0.00357  -0.1755   0.4715   0.3742
  -0.250   0.7871   0.00964   0.00363  -0.1760   0.4668   0.3790
   0.000   0.8180   0.00973   0.00371  -0.1768   0.4619   0.3869
   0.250   0.8495   0.00975   0.00376  -0.1776   0.4593   0.3937
   0.500   0.8802   0.00981   0.00382  -0.1782   0.4559   0.3991
   0.750   0.9115   0.00986   0.00389  -0.1790   0.4521   0.4084
   1.000   0.9415   0.00998   0.00399  -0.1796   0.4479   0.4161
   1.250   0.9707   0.01015   0.00411  -0.1800   0.4429   0.4223
   1.500   1.0022   0.01016   0.00418  -0.1808   0.4404   0.4313
   1.750   1.0327   0.01024   0.00427  -0.1814   0.4372   0.4390
   2.000   1.0627   0.01034   0.00437  -0.1820   0.4336   0.4465
   2.250   1.0924   0.01046   0.00450  -0.1825   0.4299   0.4558
   2.500   1.1208   0.01065   0.00466  -0.1828   0.4255   0.4634
   2.750   1.1507   0.01074   0.00478  -0.1834   0.4227   0.4720
   3.000   1.1809   0.01082   0.00490  -0.1839   0.4202   0.4805
   3.250   1.2099   0.01094   0.00502  -0.1843   0.4169   0.4872
   3.500   1.2390   0.01107   0.00517  -0.1848   0.4133   0.4962
   3.750   1.2667   0.01127   0.00535  -0.1850   0.4094   0.5046
   4.000   1.2936   0.01150   0.00556  -0.1850   0.4053   0.5118
   4.250   1.3231   0.01158   0.00571  -0.1856   0.4034   0.5212
   4.500   1.3517   0.01171   0.00586  -0.1859   0.4008   0.5292
   4.750   1.3794   0.01186   0.00603  -0.1861   0.3977   0.5361
   5.000   1.4065   0.01205   0.00623  -0.1862   0.3944   0.5445
   5.250   1.4319   0.01231   0.00647  -0.1861   0.3906   0.5521
   5.500   1.4566   0.01259   0.00674  -0.1858   0.3869   0.5591
   5.750   1.4843   0.01271   0.00693  -0.1860   0.3851   0.5679
   6.000   1.5108   0.01288   0.00713  -0.1860   0.3827   0.5756
   6.250   1.5357   0.01309   0.00736  -0.1858   0.3798   0.5820
   6.500   1.5577   0.01333   0.00763  -0.1851   0.3767   0.5900
   6.750   1.5787   0.01367   0.00797  -0.1843   0.3736   0.5977
   7.000   1.5980   0.01412   0.00840  -0.1833   0.3697   0.6037
   7.250   1.6225   0.01435   0.00870  -0.1831   0.3678   0.6119
   7.500   1.6464   0.01460   0.00900  -0.1828   0.3656   0.6197
   7.750   1.6687   0.01493   0.00935  -0.1822   0.3632   0.6260
   8.000   1.6902   0.01530   0.00976  -0.1817   0.3605   0.6335
   8.250   1.7095   0.01577   0.01026  -0.1808   0.3576   0.6408
   8.500   1.7267   0.01638   0.01085  -0.1798   0.3541   0.6474
   8.750   1.7445   0.01697   0.01146  -0.1788   0.3511   0.6539
   9.000   1.7667   0.01734   0.01191  -0.1784   0.3494   0.6611
   9.250   1.7875   0.01779   0.01241  -0.1779   0.3472   0.6679
   9.500   1.8070   0.01833   0.01297  -0.1773   0.3446   0.6736
   9.750   1.8247   0.01898   0.01366  -0.1765   0.3418   0.6808
  10.000   1.8397   0.01979   0.01450  -0.1754   0.3386   0.6872
  10.250   1.8516   0.02083   0.01552  -0.1740   0.3347   0.6931
  10.500   1.8709   0.02143   0.01618  -0.1735   0.3329   0.6993
  10.750   1.8898   0.02205   0.01688  -0.1730   0.3308   0.7057
  11.000   1.9067   0.02281   0.01769  -0.1723   0.3284   0.7119
  11.250   1.9221   0.02369   0.01859  -0.1714   0.3257   0.7173
  11.500   1.9341   0.02481   0.01975  -0.1703   0.3227   0.7236
  11.750   1.9434   0.02611   0.02107  -0.1690   0.3194   0.7293
  12.000   1.9548   0.02729   0.02228  -0.1679   0.3166   0.7351
  12.250   1.9714   0.02812   0.02318  -0.1673   0.3148   0.7406
  12.500   1.9856   0.02914   0.02428  -0.1665   0.3125   0.7464
  12.750   1.9975   0.03032   0.02551  -0.1656   0.3097   0.7520
  13.000   2.0065   0.03175   0.02697  -0.1645   0.3069   0.7575
  13.250   2.0120   0.03349   0.02873  -0.1632   0.3036   0.7626
  13.500   2.0177   0.03523   0.03051  -0.1619   0.3002   0.7679
  13.750   2.0311   0.03640   0.03176  -0.1613   0.2983   0.7733
  14.000   2.0431   0.03768   0.03309  -0.1606   0.2957   0.7785
  14.250   2.0503   0.03939   0.03487  -0.1596   0.2928   0.7835
  14.500   2.0552   0.04130   0.03682  -0.1586   0.2895   0.7885
  14.750   2.0530   0.04391   0.03944  -0.1572   0.2854   0.7932
  15.000   2.0622   0.04549   0.04108  -0.1564   0.2829   0.7980
  15.250   2.0700   0.04725   0.04292  -0.1557   0.2803   0.8028
  15.500   2.0758   0.04916   0.04489  -0.1549   0.2770   0.8076
  15.750   2.0739   0.05188   0.04765  -0.1538   0.2732   0.8122
  16.000   2.0681   0.05495   0.05072  -0.1526   0.2686   0.8162
  16.250   2.0746   0.05691   0.05277  -0.1520   0.2661   0.8206
  16.500   2.0788   0.05905   0.05498  -0.1512   0.2625   0.8251
  16.750   2.0719   0.06238   0.05835  -0.1502   0.2577   0.8294
  17.000   2.0621   0.06605   0.06202  -0.1492   0.2526   0.8333
  17.250   2.0642   0.06852   0.06458  -0.1486   0.2487   0.8373
  17.500   2.0576   0.07187   0.06796  -0.1478   0.2434   0.8410
  17.750   2.0410   0.07639   0.07250  -0.1469   0.2377   0.8446
  18.000   2.0394   0.07933   0.07551  -0.1464   0.2334   0.8490
  18.250   2.0293   0.08318   0.07939  -0.1458   0.2278   0.8525
  18.500   2.0112   0.08801   0.08425  -0.1452   0.2220   0.8556
  18.750   2.0065   0.09133   0.08762  -0.1448   0.2165   0.8595
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