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MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 150 23.89% (mh150-il)
Reynolds number: 200,000
Max Cl/Cd: 61.44 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh150-il-200000-n5.txt
Download as CSV file: xf-mh150-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.5260   0.09589   0.09074  -0.0790   0.9328   0.0406
 -16.250  -0.5286   0.09230   0.08709  -0.0804   0.9188   0.0421
 -15.750  -0.5354   0.08511   0.07975  -0.0832   0.8938   0.0457
 -15.500  -0.5404   0.08142   0.07599  -0.0845   0.8832   0.0474
 -15.250  -0.5435   0.07783   0.07233  -0.0861   0.8726   0.0495
 -14.750  -0.5494   0.07079   0.06514  -0.0893   0.8538   0.0542
 -14.500  -0.5510   0.06748   0.06173  -0.0908   0.8447   0.0570
 -14.250  -0.5542   0.06393   0.05812  -0.0927   0.8366   0.0597
 -14.000  -0.5544   0.06075   0.05486  -0.0944   0.8278   0.0630
 -13.750  -0.5572   0.05737   0.05140  -0.0962   0.8201   0.0663
 -13.500  -0.5571   0.05422   0.04818  -0.0981   0.8122   0.0700
 -13.250  -0.5573   0.05114   0.04503  -0.0999   0.8041   0.0741
 -13.000  -0.5576   0.04814   0.04195  -0.1016   0.7969   0.0782
 -12.500  -0.5542   0.04249   0.03619  -0.1054   0.7816   0.0877
 -12.250  -0.5517   0.03995   0.03355  -0.1069   0.7749   0.0928
 -12.000  -0.5471   0.03752   0.03109  -0.1087   0.7675   0.0986
 -11.750  -0.5431   0.03511   0.02863  -0.1104   0.7600   0.1044
 -11.500  -0.5364   0.03300   0.02644  -0.1119   0.7535   0.1107
 -11.250  -0.5276   0.03102   0.02442  -0.1135   0.7466   0.1178
 -11.000  -0.5188   0.02907   0.02244  -0.1152   0.7393   0.1248
 -10.750  -0.5076   0.02741   0.02071  -0.1166   0.7328   0.1322
 -10.500  -0.4970   0.02602   0.01927  -0.1175   0.7266   0.1401
 -10.250  -0.4837   0.02460   0.01784  -0.1192   0.7195   0.1482
 -10.000  -0.4654   0.02338   0.01656  -0.1210   0.7130   0.1570
  -9.750  -0.4435   0.02233   0.01543  -0.1230   0.7073   0.1668
  -9.500  -0.4191   0.02129   0.01440  -0.1256   0.7005   0.1776
  -9.250  -0.3917   0.02042   0.01351  -0.1282   0.6941   0.1889
  -9.000  -0.3622   0.01974   0.01275  -0.1306   0.6884   0.2002
  -8.750  -0.3319   0.01922   0.01215  -0.1326   0.6822   0.2111
  -8.500  -0.3014   0.01878   0.01170  -0.1344   0.6757   0.2210
  -8.250  -0.2708   0.01843   0.01127  -0.1359   0.6700   0.2299
  -8.000  -0.2397   0.01816   0.01087  -0.1373   0.6648   0.2389
  -7.750  -0.2089   0.01789   0.01058  -0.1386   0.6583   0.2466
  -7.500  -0.1777   0.01768   0.01029  -0.1398   0.6520   0.2546
  -7.250  -0.1464   0.01748   0.00995  -0.1409   0.6466   0.2619
  -7.000  -0.1154   0.01732   0.00977  -0.1420   0.6414   0.2685
  -6.750  -0.0838   0.01716   0.00951  -0.1431   0.6353   0.2756
  -6.500  -0.0529   0.01701   0.00929  -0.1440   0.6293   0.2813
  -6.250  -0.0219   0.01690   0.00910  -0.1449   0.6241   0.2872
  -6.000   0.0096   0.01678   0.00890  -0.1459   0.6184   0.2934
  -5.750   0.0408   0.01666   0.00871  -0.1468   0.6127   0.2988
  -5.500   0.0715   0.01656   0.00859  -0.1476   0.6072   0.3038
  -5.000   0.1342   0.01641   0.00825  -0.1494   0.5964   0.3148
  -4.750   0.1649   0.01633   0.00814  -0.1501   0.5907   0.3196
  -4.500   0.1956   0.01627   0.00805  -0.1508   0.5856   0.3245
  -4.250   0.2268   0.01624   0.00791  -0.1516   0.5809   0.3299
  -4.000   0.2582   0.01620   0.00781  -0.1525   0.5752   0.3352
  -3.750   0.2886   0.01614   0.00775  -0.1532   0.5696   0.3399
  -3.500   0.3192   0.01612   0.00769  -0.1539   0.5646   0.3450
  -3.250   0.3503   0.01613   0.00761  -0.1546   0.5602   0.3505
  -3.000   0.3815   0.01612   0.00755  -0.1555   0.5549   0.3559
  -2.750   0.4118   0.01610   0.00754  -0.1561   0.5495   0.3605
  -2.500   0.4421   0.01610   0.00751  -0.1567   0.5446   0.3652
  -2.250   0.4728   0.01614   0.00747  -0.1574   0.5403   0.3706
  -2.000   0.5037   0.01617   0.00747  -0.1582   0.5355   0.3764
  -1.750   0.5339   0.01619   0.00750  -0.1588   0.5306   0.3813
  -1.500   0.5640   0.01623   0.00753  -0.1594   0.5259   0.3863
  -1.250   0.5944   0.01630   0.00752  -0.1601   0.5216   0.3921
  -1.000   0.6248   0.01637   0.00756  -0.1608   0.5169   0.3985
  -0.750   0.6546   0.01643   0.00767  -0.1613   0.5122   0.4042
  -0.500   0.6845   0.01651   0.00775  -0.1619   0.5079   0.4105
  -0.250   0.7145   0.01662   0.00778  -0.1625   0.5039   0.4170
   0.000   0.7445   0.01673   0.00785  -0.1631   0.5001   0.4232
   0.250   0.7738   0.01683   0.00803  -0.1636   0.4956   0.4299
   0.500   0.8031   0.01695   0.00815  -0.1641   0.4910   0.4377
   0.750   0.8324   0.01709   0.00825  -0.1646   0.4867   0.4449
   1.000   0.8613   0.01724   0.00839  -0.1650   0.4831   0.4519
   1.250   0.8905   0.01740   0.00855  -0.1655   0.4796   0.4596
   1.500   0.9193   0.01756   0.00874  -0.1660   0.4756   0.4670
   1.750   0.9474   0.01773   0.00896  -0.1663   0.4716   0.4746
   2.000   0.9757   0.01792   0.00913  -0.1666   0.4677   0.4835
   2.250   1.0037   0.01811   0.00929  -0.1669   0.4640   0.4914
   2.500   1.0314   0.01833   0.00953  -0.1671   0.4605   0.4993
   2.750   1.0588   0.01855   0.00978  -0.1674   0.4567   0.5078
   3.000   1.0856   0.01877   0.01006  -0.1675   0.4530   0.5151
   3.250   1.1122   0.01901   0.01032  -0.1676   0.4495   0.5235
   3.500   1.1394   0.01926   0.01053  -0.1678   0.4463   0.5328
   3.750   1.1658   0.01953   0.01080  -0.1678   0.4432   0.5404
   4.000   1.1908   0.01981   0.01116  -0.1676   0.4397   0.5487
   4.250   1.2158   0.02010   0.01148  -0.1676   0.4359   0.5572
   4.500   1.2395   0.02040   0.01185  -0.1672   0.4324   0.5645
   4.750   1.2640   0.02071   0.01217  -0.1669   0.4293   0.5733
   5.000   1.2889   0.02103   0.01247  -0.1668   0.4264   0.5817
   5.250   1.3130   0.02137   0.01282  -0.1665   0.4237   0.5891
   5.500   1.3333   0.02175   0.01329  -0.1657   0.4206   0.5976
   5.750   1.3529   0.02214   0.01375  -0.1648   0.4171   0.6054
   6.000   1.3724   0.02256   0.01425  -0.1639   0.4138   0.6125
   6.250   1.3935   0.02300   0.01470  -0.1633   0.4106   0.6210
   6.500   1.4157   0.02343   0.01512  -0.1629   0.4079   0.6289
   6.750   1.4383   0.02385   0.01553  -0.1624   0.4055   0.6359
   7.000   1.4555   0.02445   0.01625  -0.1614   0.4026   0.6440
   7.250   1.4729   0.02508   0.01696  -0.1605   0.3993   0.6516
   7.500   1.4889   0.02571   0.01770  -0.1594   0.3961   0.6580
   7.750   1.5064   0.02634   0.01836  -0.1585   0.3931   0.6657
   8.000   1.5260   0.02693   0.01894  -0.1580   0.3904   0.6737
   8.250   1.5456   0.02746   0.01949  -0.1572   0.3880   0.6797
   8.500   1.5609   0.02825   0.02036  -0.1562   0.3853   0.6868
   8.750   1.5737   0.02922   0.02144  -0.1551   0.3821   0.6945
   9.000   1.5858   0.03017   0.02250  -0.1538   0.3789   0.7002
   9.250   1.5991   0.03110   0.02350  -0.1527   0.3760   0.7066
   9.500   1.6152   0.03192   0.02434  -0.1520   0.3734   0.7142
   9.750   1.6329   0.03263   0.02504  -0.1513   0.3708   0.7205
  10.000   1.6474   0.03351   0.02599  -0.1503   0.3682   0.7264
  10.250   1.6537   0.03502   0.02763  -0.1490   0.3650   0.7330
  10.500   1.6622   0.03645   0.02917  -0.1480   0.3619   0.7398
  10.750   1.6699   0.03783   0.03065  -0.1467   0.3588   0.7450
  11.000   1.6818   0.03897   0.03184  -0.1457   0.3560   0.7512
  11.250   1.6980   0.03985   0.03271  -0.1452   0.3534   0.7584
  11.500   1.7113   0.04087   0.03376  -0.1443   0.3508   0.7638
  11.750   1.7085   0.04325   0.03633  -0.1427   0.3474   0.7691
  12.000   1.7093   0.04546   0.03867  -0.1416   0.3439   0.7752
  12.250   1.7135   0.04741   0.04070  -0.1407   0.3405   0.7810
  12.500   1.7239   0.04871   0.04204  -0.1398   0.3377   0.7863
  12.750   1.7411   0.04945   0.04276  -0.1392   0.3351   0.7929
  13.250   1.7276   0.05580   0.04943  -0.1371   0.3275   0.8028
  13.500   1.7247   0.05866   0.05240  -0.1363   0.3237   0.8079
  13.750   1.7345   0.06025   0.05401  -0.1358   0.3206   0.8144
  14.000   1.7524   0.06089   0.05462  -0.1354   0.3181   0.8203
  14.250   1.7368   0.06530   0.05923  -0.1345   0.3140   0.8246
  14.500   1.7166   0.07046   0.06457  -0.1339   0.3091   0.8290
  14.750   1.7156   0.07347   0.06765  -0.1337   0.3053   0.8347
  15.000   1.7307   0.07433   0.06851  -0.1332   0.3026   0.8404
  15.250   1.7359   0.07650   0.07072  -0.1328   0.2994   0.8464
  15.500   1.6849   0.08591   0.08042  -0.1328   0.2923   0.8487
  15.750   1.6839   0.08899   0.08355  -0.1327   0.2884   0.8536
  16.000   1.7043   0.08920   0.08375  -0.1324   0.2860   0.8605
  16.250   1.6605   0.09804   0.09280  -0.1329   0.2791   0.8631
  16.500   1.6383   0.10421   0.09910  -0.1335   0.2732   0.8672
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