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WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il)
Reynolds number: 200,000
Max Cl/Cd: 58.17 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx72150a-il-200000.txt
Download as CSV file: xf-fx72150a-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 72-MS-150A AIRFOIL                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500   0.1818   0.10264   0.09798  -0.1392   0.7984   0.0341
 -10.250   0.1822   0.10105   0.09638  -0.1410   0.7926   0.0345
 -10.000   0.1878   0.09852   0.09386  -0.1419   0.7866   0.0347
  -9.750   0.2035   0.09552   0.09080  -0.1418   0.7817   0.0352
  -9.500   0.2136   0.09327   0.08853  -0.1423   0.7767   0.0360
  -9.250   0.2213   0.09113   0.08639  -0.1429   0.7708   0.0369
  -9.000   0.2288   0.08893   0.08416  -0.1438   0.7658   0.0379
  -8.750   0.2313   0.08693   0.08214  -0.1455   0.7613   0.0391
  -8.500   0.2255   0.08529   0.08057  -0.1481   0.7551   0.0395
  -8.250   0.2446   0.08218   0.07741  -0.1469   0.7508   0.0402
  -8.000   0.2574   0.08002   0.07518  -0.1471   0.7471   0.0415
  -7.750   0.2644   0.07805   0.07325  -0.1476   0.7417   0.0423
  -7.500   0.2658   0.07608   0.07130  -0.1493   0.7367   0.0446
  -7.250   0.2564   0.07411   0.06934  -0.1527   0.7323   0.0452
  -7.000   0.2772   0.07131   0.06648  -0.1511   0.7287   0.0460
  -6.750   0.2870   0.06948   0.06468  -0.1506   0.7236   0.0469
  -6.500   0.2941   0.06755   0.06274  -0.1508   0.7191   0.0483
  -6.250   0.2973   0.06573   0.06090  -0.1514   0.7154   0.0498
  -6.000   0.2950   0.06294   0.05814  -0.1593   0.7110   0.0517
  -5.750   0.3036   0.06008   0.05534  -0.1605   0.7065   0.0523
  -5.500   0.3168   0.05866   0.05390  -0.1579   0.7029   0.0534
  -5.250   0.3314   0.05660   0.05180  -0.1594   0.6996   0.0550
  -5.000   0.3644   0.04845   0.04333  -0.1832   0.6965   0.0600
  -4.750   0.3740   0.04739   0.04246  -0.1790   0.6925   0.0609
  -4.500   0.3899   0.04608   0.04118  -0.1784   0.6888   0.0626
  -4.250   0.4293   0.04071   0.03540  -0.1915   0.6855   0.0700
  -4.000   0.4501   0.03917   0.03389  -0.1914   0.6828   0.0723
  -3.750   0.4893   0.03593   0.03023  -0.1988   0.6805   0.0818
  -3.500   0.5113   0.03462   0.02898  -0.1992   0.6772   0.0859
  -3.250   0.5429   0.03251   0.02666  -0.2030   0.6738   0.0966
  -3.000   0.5757   0.03083   0.02475  -0.2061   0.6708   0.1104
  -2.750   0.6075   0.02941   0.02315  -0.2085   0.6681   0.1263
  -2.500   0.6684   0.02317   0.01530  -0.2126   0.6661   0.0444
  -2.250   0.7013   0.02193   0.01381  -0.2138   0.6640   0.0429
  -2.000   0.7306   0.02139   0.01306  -0.2142   0.6613   0.0444
  -1.750   0.7572   0.02089   0.01249  -0.2142   0.6583   0.0446
  -1.500   0.7848   0.02040   0.01197  -0.2144   0.6555   0.0446
  -1.250   0.8134   0.02002   0.01156  -0.2146   0.6530   0.0453
  -1.000   0.8436   0.01956   0.01115  -0.2155   0.6508   0.0476
  -0.750   0.8756   0.01926   0.01080  -0.2165   0.6488   0.0524
  -0.500   0.9097   0.01891   0.01042  -0.2180   0.6468   0.0721
  -0.250   0.9410   0.01836   0.01114  -0.2195   0.6444   0.5489
   0.000   0.9623   0.01895   0.01180  -0.2183   0.6414   0.5930
   0.250   0.9840   0.01942   0.01234  -0.2170   0.6388   0.6246
   0.500   1.0065   0.01982   0.01278  -0.2159   0.6365   0.6539
   0.750   1.0313   0.02009   0.01304  -0.2153   0.6346   0.6732
   1.000   1.0596   0.02029   0.01315  -0.2157   0.6329   0.6830
   1.250   1.0875   0.02046   0.01327  -0.2159   0.6314   0.6904
   1.500   1.1175   0.02070   0.01340  -0.2167   0.6299   0.6976
   1.750   1.1420   0.02113   0.01384  -0.2166   0.6281   0.7027
   2.000   1.1610   0.02177   0.01456  -0.2157   0.6255   0.7094
   2.250   1.1830   0.02231   0.01513  -0.2153   0.6229   0.7168
   2.500   1.2064   0.02271   0.01555  -0.2150   0.6206   0.7227
   2.750   1.2319   0.02308   0.01592  -0.2151   0.6186   0.7293
   3.000   1.2584   0.02339   0.01624  -0.2153   0.6170   0.7358
   3.250   1.2859   0.02367   0.01651  -0.2157   0.6156   0.7434
   3.500   1.3142   0.02394   0.01677  -0.2162   0.6143   0.7521
   3.750   1.3429   0.02427   0.01711  -0.2167   0.6131   0.7625
   4.000   1.3545   0.02545   0.01844  -0.2150   0.6106   0.7725
   4.250   1.3532   0.02730   0.02049  -0.2114   0.6067   0.7841
   4.500   1.3618   0.02859   0.02190  -0.2093   0.6038   0.7991
   4.750   1.3791   0.02927   0.02270  -0.2081   0.6017   0.8235
   5.000   1.4010   0.02932   0.02292  -0.2073   0.6000   1.0000
   5.250   1.4364   0.02925   0.02280  -0.2089   0.5986   1.0000
   5.500   1.4740   0.02908   0.02257  -0.2107   0.5973   1.0000
   5.750   1.5105   0.02911   0.02255  -0.2123   0.5961   1.0000
   6.000   1.0995   0.06461   0.05874  -0.1735   0.5493   1.0000
   6.250   1.1312   0.06448   0.05857  -0.1739   0.5485   1.0000
   6.500   1.1657   0.06396   0.05802  -0.1742   0.5478   1.0000
   6.750   1.2013   0.06328   0.05732  -0.1746   0.5473   1.0000
   7.000   1.2389   0.06230   0.05633  -0.1751   0.5469   1.0000
   7.250   1.1616   0.07300   0.06714  -0.1702   0.5273   1.0000
   7.500   1.2062   0.07133   0.06545  -0.1708   0.5288   1.0000
   7.750   1.2470   0.07002   0.06414  -0.1713   0.5296   1.0000
   8.000   1.2864   0.06882   0.06296  -0.1718   0.5301   1.0000
   8.250   1.2260   0.07795   0.07217  -0.1682   0.5119   1.0000
   8.500   1.2679   0.07635   0.07060  -0.1685   0.5130   1.0000
   8.750   1.3075   0.07498   0.06925  -0.1688   0.5137   1.0000
  10.000   1.8555   0.03190   0.02625  -0.1959   0.5319   1.0000
  11.250   1.8567   0.03576   0.03053  -0.1789   0.4956   1.0000
  11.500   1.7020   0.05296   0.04797  -0.1666   0.4862   1.0000
  11.750   1.8112   0.04242   0.03742  -0.1703   0.4777   1.0000
  12.000   1.8113   0.04379   0.03882  -0.1679   0.4641   1.0000
  12.250   1.7372   0.05439   0.04965  -0.1627   0.4577   1.0000
  12.500   1.7077   0.06032   0.05568  -0.1602   0.4450   1.0000
  12.750   1.6934   0.06457   0.06000  -0.1585   0.4294   1.0000
  13.000   1.7303   0.06199   0.05731  -0.1580   0.3997   1.0000
  13.250   1.7431   0.06187   0.05648  -0.1560   0.3286   1.0000
  13.500   1.7198   0.06725   0.06161  -0.1539   0.2905   1.0000
  13.750   1.6951   0.07317   0.06731  -0.1522   0.2567   1.0000
  14.000   1.6698   0.07945   0.07338  -0.1509   0.2230   1.0000
  14.250   1.6445   0.08600   0.07969  -0.1499   0.1869   1.0000
  14.500   1.6192   0.09275   0.08618  -0.1492   0.1480   1.0000
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