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WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il)
Reynolds number: 1,000,000
Max Cl/Cd: 154.45 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx72150b-il-1000000.txt
Download as CSV file: xf-fx72150b-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 72-MS-150B 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750   0.3208   0.08813   0.08463  -0.1614   0.6669   0.0114
  -9.500   0.3294   0.08608   0.08254  -0.1622   0.6628   0.0117
  -9.250   0.3383   0.08385   0.08031  -0.1631   0.6591   0.0123
  -9.000   0.3471   0.08156   0.07803  -0.1641   0.6558   0.0126
  -8.750   0.3523   0.07898   0.07546  -0.1656   0.6522   0.0130
  -8.500   0.3568   0.07668   0.07315  -0.1669   0.6483   0.0130
  -8.250   0.3626   0.07437   0.07082  -0.1678   0.6443   0.0130
  -8.000   0.3712   0.07215   0.06862  -0.1687   0.6413   0.0131
  -7.750   0.3793   0.06958   0.06606  -0.1690   0.6379   0.0132
  -7.500   0.3894   0.06780   0.06427  -0.1693   0.6340   0.0133
  -7.250   0.3990   0.06616   0.06261  -0.1696   0.6301   0.0135
  -7.000   0.4074   0.06441   0.06086  -0.1700   0.6267   0.0137
  -6.750   0.4155   0.06260   0.05907  -0.1704   0.6235   0.0140
  -6.500   0.4219   0.06074   0.05721  -0.1707   0.6202   0.0142
  -6.250   0.4256   0.05890   0.05538  -0.1705   0.6168   0.0149
  -6.000   0.4231   0.05582   0.05230  -0.1727   0.6135   0.0159
  -5.750   0.4329   0.05286   0.04936  -0.1757   0.6106   0.0160
  -5.500   0.4439   0.04944   0.04596  -0.1793   0.6081   0.0161
  -5.250   0.4578   0.04775   0.04428  -0.1806   0.6051   0.0163
  -5.000   0.4750   0.04567   0.04217  -0.1834   0.6022   0.0164
  -4.750   0.4943   0.04348   0.03997  -0.1868   0.5992   0.0167
  -4.500   0.5175   0.04080   0.03723  -0.1917   0.5959   0.0171
  -4.250   0.5535   0.03631   0.03272  -0.2021   0.5939   0.0178
  -4.000   0.6375   0.02297   0.01874  -0.2297   0.5920   0.0196
  -3.750   0.6702   0.02156   0.01722  -0.2327   0.5896   0.0199
  -3.500   0.7045   0.02007   0.01557  -0.2358   0.5871   0.0204
  -3.250   0.7611   0.01434   0.00898  -0.2441   0.5848   0.0179
  -3.000   0.7975   0.01262   0.00687  -0.2465   0.5822   0.0174
  -2.750   0.8290   0.01192   0.00597  -0.2476   0.5794   0.0174
  -2.500   0.8605   0.01139   0.00535  -0.2487   0.5777   0.0176
  -2.250   0.8909   0.01109   0.00499  -0.2494   0.5757   0.0182
  -2.000   0.9214   0.01080   0.00464  -0.2502   0.5737   0.0187
  -1.750   0.9516   0.01057   0.00435  -0.2510   0.5714   0.0191
  -1.500   0.9827   0.01024   0.00397  -0.2520   0.5691   0.0201
  -1.250   1.0119   0.01016   0.00386  -0.2526   0.5667   0.0214
  -1.000   1.0408   0.01016   0.00379  -0.2531   0.5639   0.0227
  -0.750   1.0714   0.00999   0.00362  -0.2539   0.5626   0.0249
  -0.500   1.1013   0.00990   0.00352  -0.2546   0.5610   0.0287
  -0.250   1.1309   0.00983   0.00346  -0.2553   0.5593   0.0349
   0.000   1.1602   0.00979   0.00345  -0.2558   0.5576   0.0512
   0.250   1.1909   0.00961   0.00349  -0.2569   0.5558   0.1509
   0.500   1.2232   0.00924   0.00364  -0.2587   0.5540   0.4184
   0.750   1.2508   0.00933   0.00375  -0.2589   0.5522   0.4712
   1.000   1.2782   0.00946   0.00387  -0.2591   0.5502   0.4923
   1.250   1.3056   0.00962   0.00402  -0.2592   0.5480   0.5098
   1.500   1.3332   0.00970   0.00411  -0.2595   0.5471   0.5224
   1.750   1.3606   0.00979   0.00422  -0.2596   0.5461   0.5380
   2.000   1.3880   0.00988   0.00434  -0.2598   0.5449   0.5509
   2.250   1.4153   0.00998   0.00444  -0.2600   0.5436   0.5582
   2.500   1.4424   0.01007   0.00455  -0.2602   0.5422   0.5645
   2.750   1.4693   0.01018   0.00466  -0.2603   0.5408   0.5699
   3.000   1.4961   0.01029   0.00477  -0.2604   0.5393   0.5756
   3.250   1.5226   0.01040   0.00490  -0.2605   0.5379   0.5807
   3.500   1.5490   0.01055   0.00504  -0.2606   0.5364   0.5860
   3.750   1.5753   0.01071   0.00519  -0.2607   0.5350   0.5907
   4.000   1.6021   0.01088   0.00538  -0.2609   0.5333   0.5956
   4.250   1.6293   0.01108   0.00557  -0.2612   0.5318   0.6010
   4.500   1.6555   0.01118   0.00571  -0.2612   0.5311   0.6066
   4.750   1.6815   0.01128   0.00586  -0.2613   0.5303   0.6127
   5.000   1.7073   0.01140   0.00603  -0.2613   0.5295   0.6197
   5.250   1.7330   0.01152   0.00620  -0.2613   0.5285   0.6270
   5.500   1.7585   0.01164   0.00638  -0.2613   0.5274   0.6352
   5.750   1.7837   0.01177   0.00655  -0.2612   0.5262   0.6436
   6.000   1.8085   0.01190   0.00674  -0.2611   0.5249   0.6533
   6.250   1.8331   0.01204   0.00692  -0.2609   0.5235   0.6637
   6.500   1.8572   0.01218   0.00712  -0.2607   0.5221   0.6760
   7.000   1.9039   0.01257   0.00758  -0.2600   0.5166   0.7132
   7.250   1.9223   0.01266   0.00780  -0.2586   0.5145   0.7495
   7.500   1.9352   0.01253   0.00801  -0.2560   0.5124   1.0000
   7.750   1.9537   0.01271   0.00824  -0.2548   0.5102   1.0000
   8.000   1.9716   0.01292   0.00849  -0.2534   0.5077   1.0000
   8.250   1.9879   0.01320   0.00878  -0.2518   0.5046   1.0000
   8.500   2.0053   0.01358   0.00914  -0.2504   0.5006   1.0000
   8.750   2.0199   0.01388   0.00953  -0.2486   0.4976   1.0000
   9.000   2.0344   0.01424   0.00995  -0.2469   0.4931   1.0000
   9.250   2.0457   0.01481   0.01051  -0.2447   0.4879   1.0000
   9.500   2.0594   0.01534   0.01108  -0.2429   0.4830   1.0000
   9.750   2.0744   0.01585   0.01165  -0.2415   0.4778   1.0000
  10.000   2.0824   0.01672   0.01251  -0.2390   0.4713   1.0000
  10.250   2.0953   0.01740   0.01326  -0.2374   0.4627   1.0000
  10.500   2.1015   0.01849   0.01435  -0.2349   0.4523   1.0000
  10.750   2.1054   0.01979   0.01564  -0.2322   0.4366   1.0000
  11.000   2.0974   0.02193   0.01770  -0.2281   0.4166   1.0000
  11.250   2.0827   0.02470   0.02039  -0.2235   0.3962   1.0000
  11.500   2.0616   0.02816   0.02374  -0.2185   0.3660   1.0000
  11.750   2.0361   0.03232   0.02780  -0.2135   0.3436   1.0000
  12.000   2.0144   0.03651   0.03193  -0.2094   0.3223   1.0000
  12.250   1.9885   0.04144   0.03677  -0.2053   0.2971   1.0000
  12.500   1.9633   0.04660   0.04186  -0.2018   0.2766   1.0000
  12.750   1.9396   0.05187   0.04707  -0.1987   0.2533   1.0000
  13.000   1.9133   0.05770   0.05281  -0.1958   0.2307   1.0000
  13.250   1.8910   0.06327   0.05831  -0.1934   0.2086   1.0000
  13.500   1.8697   0.06894   0.06390  -0.1913   0.1873   1.0000
  13.750   1.8514   0.07439   0.06926  -0.1896   0.1655   1.0000
  14.000   1.8309   0.08027   0.07503  -0.1880   0.1410   1.0000
  14.250   1.8140   0.08583   0.08049  -0.1868   0.1191   1.0000
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