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WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 154 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx72150a-il-1000000-n5.txt
Download as CSV file: xf-fx72150a-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750   0.2019   0.08802   0.08433  -0.1418   0.6257   0.0107
  -9.500   0.2087   0.08541   0.08171  -0.1430   0.6223   0.0108
  -9.250   0.2152   0.08277   0.07907  -0.1441   0.6190   0.0108
  -9.000   0.2223   0.08029   0.07659  -0.1451   0.6154   0.0108
  -8.750   0.2285   0.07768   0.07396  -0.1461   0.6121   0.0108
  -8.500   0.2357   0.07517   0.07146  -0.1472   0.6095   0.0108
  -8.000   0.2443   0.06932   0.06563  -0.1492   0.6036   0.0109
  -7.500   0.2571   0.06489   0.06120  -0.1507   0.5973   0.0110
  -7.250   0.2623   0.06253   0.05885  -0.1514   0.5947   0.0111
  -5.750   0.2998   0.04544   0.04182  -0.1641   0.5784   0.0106
  -5.500   0.3235   0.03835   0.03471  -0.1775   0.5762   0.0105
  -5.250   0.3557   0.02999   0.02605  -0.1913   0.5739   0.0104
  -5.000   0.4080   0.01502   0.00964  -0.2081   0.5719   0.0090
  -4.750   0.4396   0.01364   0.00797  -0.2098   0.5691   0.0089
  -4.500   0.4700   0.01283   0.00697  -0.2108   0.5664   0.0090
  -4.000   0.5299   0.01176   0.00564  -0.2124   0.5617   0.0091
  -3.750   0.5599   0.01135   0.00515  -0.2132   0.5598   0.0092
  -3.500   0.5898   0.01100   0.00473  -0.2139   0.5577   0.0094
  -3.250   0.6196   0.01072   0.00437  -0.2145   0.5556   0.0096
  -3.000   0.6492   0.01047   0.00407  -0.2151   0.5534   0.0099
  -2.750   0.6787   0.01028   0.00382  -0.2156   0.5510   0.0102
  -2.500   0.7079   0.01013   0.00361  -0.2161   0.5486   0.0104
  -2.250   0.7371   0.01002   0.00345  -0.2166   0.5464   0.0107
  -2.000   0.7667   0.00990   0.00331  -0.2172   0.5449   0.0108
  -1.750   0.7966   0.00972   0.00310  -0.2178   0.5432   0.0112
  -1.500   0.8261   0.00961   0.00297  -0.2183   0.5414   0.0115
  -1.250   0.8553   0.00955   0.00288  -0.2188   0.5395   0.0119
  -1.000   0.8843   0.00950   0.00282  -0.2192   0.5378   0.0124
  -0.750   0.9131   0.00948   0.00278  -0.2196   0.5361   0.0131
  -0.500   0.9418   0.00947   0.00274  -0.2199   0.5344   0.0139
  -0.250   0.9703   0.00947   0.00273  -0.2203   0.5327   0.0151
   0.000   0.9986   0.00948   0.00275  -0.2206   0.5308   0.0218
   0.250   1.0273   0.00948   0.00276  -0.2209   0.5295   0.0310
   0.500   1.0568   0.00939   0.00278  -0.2215   0.5284   0.0741
   0.750   1.0865   0.00924   0.00282  -0.2223   0.5272   0.1598
   1.000   1.1178   0.00883   0.00290  -0.2237   0.5258   0.3917
   1.250   1.1463   0.00881   0.00303  -0.2241   0.5243   0.4764
   1.500   1.1742   0.00886   0.00312  -0.2243   0.5228   0.4957
   1.750   1.2020   0.00894   0.00321  -0.2245   0.5212   0.5098
   2.000   1.2295   0.00902   0.00329  -0.2246   0.5196   0.5180
   2.250   1.2569   0.00911   0.00337  -0.2247   0.5182   0.5240
   2.500   1.2841   0.00920   0.00347  -0.2248   0.5168   0.5302
   2.750   1.3110   0.00931   0.00358  -0.2249   0.5152   0.5345
   3.000   1.3379   0.00942   0.00368  -0.2250   0.5136   0.5383
   3.250   1.3654   0.00950   0.00377  -0.2251   0.5125   0.5419
   3.500   1.3928   0.00957   0.00388  -0.2253   0.5113   0.5460
   3.750   1.4200   0.00965   0.00398  -0.2254   0.5100   0.5499
   4.000   1.4469   0.00974   0.00410  -0.2255   0.5087   0.5540
   4.250   1.4736   0.00983   0.00423  -0.2256   0.5075   0.5582
   4.500   1.5002   0.00993   0.00435  -0.2256   0.5063   0.5628
   4.750   1.5263   0.01004   0.00449  -0.2256   0.5045   0.5681
   5.000   1.5506   0.01020   0.00463  -0.2252   0.5000   0.5733
   5.500   1.6014   0.01043   0.00492  -0.2249   0.4928   0.5834
   5.750   1.6262   0.01056   0.00508  -0.2247   0.4898   0.5893
   6.000   1.6494   0.01074   0.00527  -0.2241   0.4859   0.5949
   6.250   1.6720   0.01092   0.00548  -0.2235   0.4817   0.6010
   6.500   1.6965   0.01104   0.00565  -0.2232   0.4784   0.6079
   6.750   1.7190   0.01121   0.00586  -0.2225   0.4738   0.6151
   7.000   1.7361   0.01147   0.00613  -0.2208   0.4680   0.6234
   7.500   1.7689   0.01203   0.00671  -0.2172   0.4443   0.6412
   7.750   1.7671   0.01295   0.00747  -0.2124   0.4135   0.6495
   8.000   1.7524   0.01459   0.00890  -0.2058   0.3698   0.6584
   8.250   1.7338   0.01672   0.01083  -0.1994   0.3333   0.6672
   8.500   1.7114   0.01943   0.01335  -0.1930   0.2905   0.6772
   8.750   1.7009   0.02174   0.01556  -0.1888   0.2637   0.6904
   9.000   1.6780   0.02512   0.01879  -0.1835   0.2260   0.7059
   9.250   1.6570   0.02868   0.02224  -0.1790   0.1925   0.7257
   9.500   1.6349   0.03266   0.02613  -0.1750   0.1583   0.7591
   9.750   1.6057   0.03724   0.03083  -0.1706   0.1192   1.0000
  10.000   1.5776   0.04258   0.03599  -0.1672   0.0787   1.0000
  10.250   1.5568   0.04752   0.04078  -0.1645   0.0445   1.0000
  10.500   1.5391   0.05235   0.04549  -0.1624   0.0129   1.0000
  10.750   1.5438   0.05479   0.04795  -0.1614   0.0098   1.0000
  11.000   1.5504   0.05707   0.05026  -0.1607   0.0088   1.0000
  11.250   1.5581   0.05923   0.05246  -0.1600   0.0083   1.0000
  11.500   1.5648   0.06154   0.05481  -0.1594   0.0079   1.0000
  11.750   1.5725   0.06374   0.05705  -0.1587   0.0076   1.0000
  12.000   1.5786   0.06618   0.05953  -0.1582   0.0073   1.0000
  12.250   1.5853   0.06855   0.06195  -0.1576   0.0071   1.0000
  12.500   1.5920   0.07096   0.06440  -0.1571   0.0069   1.0000
  12.750   1.5985   0.07342   0.06691  -0.1566   0.0068   1.0000
  13.000   1.6058   0.07576   0.06930  -0.1562   0.0067   1.0000
  13.250   1.6119   0.07831   0.07189  -0.1558   0.0066   1.0000
  13.500   1.6182   0.08083   0.07446  -0.1555   0.0065   1.0000
  13.750   1.6251   0.08328   0.07696  -0.1551   0.0064   1.0000
  14.000   1.6305   0.08599   0.07973  -0.1549   0.0063   1.0000
  14.250   1.6364   0.08861   0.08240  -0.1546   0.0062   1.0000
  14.500   1.6426   0.09117   0.08501  -0.1544   0.0061   1.0000
  14.750   1.6475   0.09398   0.08787  -0.1542   0.0060   1.0000
  15.000   1.6526   0.09674   0.09069  -0.1541   0.0060   1.0000
  15.250   1.6582   0.09942   0.09342  -0.1540   0.0059   1.0000
  15.500   1.6626   0.10234   0.09640  -0.1539   0.0058   1.0000
  15.750   1.6668   0.10526   0.09937  -0.1539   0.0057   1.0000
  16.000   1.6715   0.10808   0.10225  -0.1540   0.0057   1.0000
  16.250   1.6747   0.11117   0.10540  -0.1541   0.0056   1.0000
  16.500   1.6782   0.11421   0.10850  -0.1542   0.0055   1.0000
  16.750   1.6818   0.11721   0.11156  -0.1544   0.0055   1.0000
  17.000   1.6836   0.12054   0.11495  -0.1547   0.0054   1.0000
  17.250   1.6861   0.12373   0.11821  -0.1550   0.0054   1.0000
  17.500   1.6884   0.12692   0.12146  -0.1554   0.0053   1.0000
  17.750   1.6878   0.13060   0.12522  -0.1559   0.0053   1.0000
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