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MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 150 23.89% (mh150-il)
Reynolds number: 500,000
Max Cl/Cd: 88.06 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh150-il-500000-n5.txt
Download as CSV file: xf-mh150-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.6351   0.11749   0.11340  -0.0582   0.9346   0.0192
 -18.500  -0.6401   0.11367   0.10951  -0.0595   0.9183   0.0195
 -18.250  -0.6455   0.10973   0.10547  -0.0610   0.9038   0.0198
 -18.000  -0.6483   0.10594   0.10159  -0.0626   0.8908   0.0202
 -17.750  -0.6516   0.10206   0.09761  -0.0644   0.8796   0.0206
 -17.500  -0.6531   0.09842   0.09387  -0.0661   0.8684   0.0211
 -17.250  -0.6544   0.09477   0.09012  -0.0679   0.8588   0.0215
 -17.000  -0.6548   0.09123   0.08648  -0.0697   0.8491   0.0220
 -16.750  -0.6572   0.08749   0.08264  -0.0716   0.8405   0.0225
 -16.500  -0.6597   0.08365   0.07872  -0.0737   0.8323   0.0231
 -16.250  -0.6609   0.08008   0.07507  -0.0756   0.8236   0.0238
 -16.000  -0.6617   0.07659   0.07148  -0.0775   0.8160   0.0246
 -15.750  -0.6605   0.07334   0.06816  -0.0793   0.8082   0.0254
 -15.500  -0.6621   0.06978   0.06451  -0.0813   0.8005   0.0262
 -15.250  -0.6629   0.06636   0.06102  -0.0833   0.7935   0.0271
 -15.000  -0.6621   0.06314   0.05772  -0.0852   0.7861   0.0282
 -14.750  -0.6613   0.05996   0.05445  -0.0870   0.7786   0.0293
 -14.500  -0.6610   0.05676   0.05118  -0.0889   0.7720   0.0305
 -14.250  -0.6597   0.05365   0.04801  -0.0908   0.7652   0.0319
 -14.000  -0.6578   0.05069   0.04497  -0.0927   0.7580   0.0334
 -13.750  -0.6560   0.04775   0.04194  -0.0945   0.7513   0.0350
 -13.500  -0.6524   0.04499   0.03913  -0.0963   0.7449   0.0369
 -13.250  -0.6501   0.04211   0.03619  -0.0982   0.7380   0.0388
 -13.000  -0.6452   0.03959   0.03359  -0.0999   0.7314   0.0412
 -12.750  -0.6409   0.03700   0.03095  -0.1018   0.7253   0.0437
 -12.500  -0.6346   0.03466   0.02856  -0.1035   0.7185   0.0466
 -12.250  -0.6279   0.03237   0.02620  -0.1052   0.7119   0.0499
 -12.000  -0.6197   0.03021   0.02399  -0.1069   0.7062   0.0534
 -11.750  -0.6092   0.02824   0.02199  -0.1086   0.6999   0.0575
 -11.500  -0.5974   0.02639   0.02010  -0.1103   0.6932   0.0621
 -11.000  -0.5715   0.02309   0.01674  -0.1134   0.6813   0.0727
 -10.750  -0.5555   0.02168   0.01532  -0.1151   0.6751   0.0790
 -10.500  -0.5352   0.02039   0.01399  -0.1172   0.6687   0.0861
 -10.250  -0.5118   0.01923   0.01281  -0.1196   0.6629   0.0937
 -10.000  -0.4856   0.01820   0.01178  -0.1220   0.6569   0.1018
  -9.750  -0.4573   0.01731   0.01087  -0.1245   0.6509   0.1100
  -9.500  -0.4274   0.01655   0.01006  -0.1270   0.6450   0.1187
  -9.250  -0.3957   0.01578   0.00930  -0.1297   0.6395   0.1288
  -9.000  -0.3628   0.01508   0.00861  -0.1325   0.6331   0.1408
  -8.750  -0.3293   0.01445   0.00798  -0.1351   0.6270   0.1538
  -8.000  -0.2290   0.01310   0.00667  -0.1414   0.6103   0.1945
  -7.750  -0.1961   0.01282   0.00637  -0.1430   0.6042   0.2063
  -7.500  -0.1631   0.01258   0.00613  -0.1445   0.5990   0.2160
  -7.250  -0.1306   0.01242   0.00593  -0.1457   0.5938   0.2250
  -7.000  -0.0977   0.01224   0.00574  -0.1470   0.5881   0.2330
  -6.750  -0.0659   0.01215   0.00558  -0.1480   0.5823   0.2406
  -6.500  -0.0331   0.01201   0.00543  -0.1492   0.5772   0.2472
  -6.250  -0.0007   0.01191   0.00530  -0.1503   0.5715   0.2539
  -6.000   0.0310   0.01187   0.00519  -0.1511   0.5661   0.2593
  -5.750   0.0631   0.01179   0.00507  -0.1522   0.5609   0.2647
  -5.500   0.0957   0.01170   0.00497  -0.1532   0.5559   0.2702
  -5.250   0.1275   0.01166   0.00488  -0.1541   0.5502   0.2752
  -5.000   0.1590   0.01165   0.00479  -0.1549   0.5448   0.2792
  -4.750   0.1911   0.01160   0.00472  -0.1559   0.5401   0.2841
  -4.500   0.2234   0.01154   0.00465  -0.1568   0.5353   0.2889
  -4.250   0.2551   0.01153   0.00460  -0.1577   0.5299   0.2933
  -4.000   0.2862   0.01156   0.00455  -0.1583   0.5245   0.2970
  -3.750   0.3181   0.01153   0.00450  -0.1593   0.5199   0.3017
  -3.500   0.3503   0.01150   0.00447  -0.1602   0.5157   0.3065
  -3.250   0.3819   0.01150   0.00445  -0.1611   0.5109   0.3112
  -3.000   0.4129   0.01155   0.00443  -0.1617   0.5058   0.3153
  -2.750   0.4441   0.01158   0.00442  -0.1625   0.5009   0.3201
  -2.500   0.4762   0.01156   0.00441  -0.1635   0.4967   0.3253
  -2.250   0.5076   0.01158   0.00442  -0.1643   0.4923   0.3303
  -2.000   0.5385   0.01163   0.00443  -0.1649   0.4879   0.3345
  -1.750   0.5693   0.01169   0.00445  -0.1656   0.4836   0.3385
  -1.500   0.6007   0.01172   0.00448  -0.1665   0.4797   0.3437
  -1.250   0.6321   0.01175   0.00452  -0.1673   0.4755   0.3493
  -1.000   0.6628   0.01182   0.00455  -0.1679   0.4710   0.3542
  -0.750   0.6932   0.01190   0.00460  -0.1685   0.4666   0.3586
  -0.250   0.7547   0.01204   0.00474  -0.1700   0.4594   0.3703
   0.000   0.7852   0.01211   0.00481  -0.1706   0.4558   0.3763
   0.250   0.8158   0.01218   0.00489  -0.1713   0.4519   0.3825
   0.500   0.8458   0.01229   0.00498  -0.1719   0.4478   0.3890
   0.750   0.8750   0.01243   0.00509  -0.1723   0.4436   0.3953
   1.000   0.9051   0.01252   0.00519  -0.1729   0.4404   0.4012
   1.250   0.9355   0.01260   0.00531  -0.1736   0.4370   0.4087
   1.500   0.9651   0.01272   0.00543  -0.1741   0.4334   0.4165
   1.750   0.9942   0.01285   0.00556  -0.1745   0.4299   0.4236
   2.000   1.0230   0.01301   0.00571  -0.1749   0.4264   0.4313
   2.250   1.0515   0.01317   0.00587  -0.1753   0.4232   0.4387
   2.500   1.0807   0.01329   0.00602  -0.1757   0.4201   0.4456
   2.750   1.1096   0.01342   0.00618  -0.1762   0.4165   0.4535
   3.000   1.1375   0.01359   0.00636  -0.1764   0.4129   0.4618
   3.250   1.1650   0.01378   0.00655  -0.1766   0.4096   0.4697
   3.500   1.1917   0.01400   0.00678  -0.1767   0.4065   0.4784
   3.750   1.2191   0.01419   0.00698  -0.1769   0.4039   0.4860
   4.000   1.2467   0.01435   0.00719  -0.1771   0.4012   0.4934
   4.250   1.2735   0.01454   0.00741  -0.1772   0.3980   0.5014
   4.500   1.2990   0.01477   0.00765  -0.1771   0.3946   0.5092
   4.750   1.3236   0.01503   0.00793  -0.1769   0.3913   0.5173
   5.000   1.3453   0.01533   0.00823  -0.1762   0.3882   0.5258
   5.250   1.3684   0.01559   0.00851  -0.1757   0.3858   0.5331
   5.500   1.3931   0.01582   0.00881  -0.1755   0.3834   0.5405
   5.750   1.4171   0.01611   0.00915  -0.1752   0.3806   0.5489
   6.000   1.4398   0.01646   0.00951  -0.1748   0.3775   0.5565
   6.250   1.4615   0.01685   0.00993  -0.1743   0.3743   0.5643
   6.500   1.4818   0.01730   0.01040  -0.1736   0.3713   0.5724
   6.750   1.5020   0.01778   0.01088  -0.1729   0.3687   0.5797
   7.000   1.5247   0.01814   0.01132  -0.1725   0.3666   0.5874
   7.250   1.5462   0.01856   0.01181  -0.1721   0.3639   0.5954
   7.500   1.5664   0.01906   0.01233  -0.1715   0.3610   0.6027
   7.750   1.5856   0.01962   0.01293  -0.1708   0.3580   0.6098
   8.000   1.6036   0.02025   0.01360  -0.1700   0.3553   0.6175
   8.250   1.6202   0.02098   0.01433  -0.1691   0.3525   0.6248
   8.500   1.6390   0.02161   0.01502  -0.1684   0.3502   0.6313
   8.750   1.6584   0.02220   0.01569  -0.1679   0.3477   0.6386
   9.000   1.6764   0.02290   0.01644  -0.1672   0.3451   0.6459
   9.250   1.6934   0.02366   0.01723  -0.1665   0.3424   0.6521
   9.500   1.7086   0.02454   0.01817  -0.1656   0.3395   0.6586
   9.750   1.7224   0.02553   0.01918  -0.1646   0.3367   0.6655
  10.000   1.7354   0.02659   0.02026  -0.1636   0.3340   0.6719
  10.250   1.7524   0.02740   0.02116  -0.1630   0.3318   0.6778
  10.500   1.7679   0.02832   0.02216  -0.1623   0.3292   0.6843
  10.750   1.7814   0.02939   0.02329  -0.1615   0.3263   0.6910
  11.000   1.7939   0.03055   0.02448  -0.1606   0.3234   0.6967
  11.250   1.8033   0.03193   0.02591  -0.1595   0.3203   0.7023
  11.500   1.8116   0.03341   0.02740  -0.1583   0.3173   0.7084
  11.750   1.8250   0.03457   0.02866  -0.1576   0.3149   0.7147
  12.000   1.8372   0.03583   0.02999  -0.1569   0.3120   0.7200
  12.250   1.8468   0.03730   0.03153  -0.1560   0.3089   0.7255
  12.500   1.8551   0.03890   0.03318  -0.1551   0.3059   0.7314
  12.750   1.8613   0.04073   0.03503  -0.1541   0.3029   0.7371
  13.000   1.8682   0.04251   0.03686  -0.1531   0.3000   0.7419
  13.250   1.8784   0.04404   0.03850  -0.1525   0.2974   0.7472
  13.500   1.8861   0.04581   0.04034  -0.1517   0.2944   0.7529
  13.750   1.8929   0.04770   0.04228  -0.1510   0.2912   0.7584
  14.000   1.8956   0.04998   0.04461  -0.1501   0.2878   0.7628
  14.250   1.8973   0.05236   0.04702  -0.1491   0.2844   0.7674
  14.500   1.9040   0.05433   0.04909  -0.1485   0.2818   0.7727
  14.750   1.9099   0.05638   0.05122  -0.1479   0.2786   0.7781
  15.000   1.9112   0.05893   0.05384  -0.1472   0.2749   0.7823
  15.250   1.9110   0.06162   0.05656  -0.1464   0.2711   0.7866
  15.500   1.9095   0.06450   0.05950  -0.1457   0.2678   0.7911
  15.750   1.9135   0.06683   0.06191  -0.1452   0.2645   0.7961
  16.000   1.9124   0.06973   0.06489  -0.1446   0.2606   0.8004
  16.250   1.9095   0.07280   0.06801  -0.1440   0.2565   0.8044
  16.500   1.9032   0.07631   0.07155  -0.1434   0.2526   0.8084
  16.750   1.9046   0.07901   0.07434  -0.1431   0.2489   0.8129
  17.250   1.8932   0.08601   0.08145  -0.1423   0.2401   0.8207
  17.500   1.8867   0.08966   0.08516  -0.1420   0.2361   0.8246
  17.750   1.8839   0.09290   0.08848  -0.1418   0.2317   0.8288
  18.000   1.8745   0.09698   0.09261  -0.1417   0.2269   0.8325
  18.250   1.8671   0.10075   0.09640  -0.1416   0.2224   0.8360
  18.500   1.8608   0.10449   0.10022  -0.1417   0.2179   0.8397
  18.750   1.8537   0.10833   0.10411  -0.1419   0.2128   0.8437
  19.000   1.8424   0.11273   0.10853  -0.1422   0.2079   0.8476
  19.250   1.8390   0.11617   0.11204  -0.1425   0.2031   0.8516
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