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WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il)
Reynolds number: 500,000
Max Cl/Cd: 117.45 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx72150b-il-500000-n5.txt
Download as CSV file: xf-fx72150b-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750   0.2676   0.09953   0.09519  -0.1528   0.6704   0.0130
 -10.500   0.2755   0.09719   0.09283  -0.1539   0.6663   0.0130
 -10.250   0.2797   0.09480   0.09042  -0.1553   0.6626   0.0131
 -10.000   0.2922   0.09243   0.08804  -0.1556   0.6591   0.0132
  -9.750   0.3008   0.09006   0.08568  -0.1566   0.6553   0.0132
  -9.500   0.3116   0.08825   0.08385  -0.1572   0.6515   0.0135
  -9.250   0.3208   0.08622   0.08181  -0.1580   0.6476   0.0138
  -9.000   0.3292   0.08414   0.07970  -0.1588   0.6443   0.0139
  -8.750   0.3381   0.08203   0.07760  -0.1597   0.6411   0.0142
  -8.500   0.3465   0.07987   0.07544  -0.1605   0.6377   0.0144
  -8.250   0.3547   0.07776   0.07334  -0.1613   0.6341   0.0148
  -8.000   0.3627   0.07573   0.07130  -0.1620   0.6307   0.0149
  -7.750   0.3677   0.07329   0.06885  -0.1631   0.6277   0.0157
  -7.500   0.3710   0.07079   0.06637  -0.1644   0.6248   0.0159
  -7.250   0.3756   0.06840   0.06400  -0.1654   0.6217   0.0159
  -7.000   0.3803   0.06602   0.06164  -0.1661   0.6185   0.0160
  -6.750   0.3843   0.06380   0.05941  -0.1664   0.6154   0.0160
  -6.500   0.3873   0.06184   0.05745  -0.1662   0.6126   0.0160
  -6.250   0.3933   0.06020   0.05583  -0.1658   0.6100   0.0162
  -6.000   0.4041   0.05874   0.05439  -0.1659   0.6072   0.0164
  -5.750   0.4137   0.05697   0.05263  -0.1668   0.6043   0.0166
  -5.500   0.4240   0.05499   0.05065  -0.1683   0.6014   0.0168
  -4.250   0.6158   0.01813   0.01219  -0.2343   0.5895   0.0133
  -4.000   0.6498   0.01699   0.01080  -0.2367   0.5869   0.0136
  -3.750   0.6829   0.01600   0.00956  -0.2386   0.5844   0.0139
  -3.500   0.7147   0.01525   0.00859  -0.2401   0.5820   0.0143
  -3.000   0.7774   0.01405   0.00698  -0.2424   0.5778   0.0156
  -2.750   0.8084   0.01354   0.00633  -0.2434   0.5757   0.0159
  -2.500   0.8391   0.01312   0.00584  -0.2444   0.5736   0.0162
  -2.250   0.8691   0.01287   0.00555  -0.2452   0.5714   0.0168
  -2.000   0.8988   0.01268   0.00532  -0.2459   0.5692   0.0174
  -1.750   0.9285   0.01253   0.00509  -0.2466   0.5671   0.0184
  -1.500   0.9579   0.01242   0.00490  -0.2472   0.5650   0.0193
  -1.250   0.9874   0.01231   0.00477  -0.2479   0.5632   0.0205
  -1.000   1.0166   0.01226   0.00470  -0.2484   0.5616   0.0227
  -0.750   1.0462   0.01217   0.00461  -0.2491   0.5600   0.0252
  -0.500   1.0754   0.01212   0.00453  -0.2497   0.5582   0.0282
  -0.250   1.1043   0.01211   0.00450  -0.2502   0.5563   0.0330
   0.000   1.1328   0.01209   0.00451  -0.2507   0.5544   0.0463
   0.250   1.1616   0.01207   0.00454  -0.2513   0.5525   0.0831
   0.500   1.1913   0.01195   0.00461  -0.2522   0.5507   0.1850
   0.750   1.2222   0.01173   0.00478  -0.2536   0.5491   0.3909
   1.000   1.2497   0.01182   0.00496  -0.2538   0.5476   0.4695
   1.250   1.2769   0.01191   0.00510  -0.2540   0.5462   0.4963
   1.500   1.3037   0.01203   0.00525  -0.2540   0.5446   0.5231
   1.750   1.3304   0.01215   0.00539  -0.2541   0.5431   0.5402
   2.000   1.3569   0.01228   0.00553  -0.2541   0.5414   0.5505
   2.250   1.3832   0.01241   0.00565  -0.2541   0.5399   0.5577
   2.500   1.4095   0.01255   0.00580  -0.2541   0.5384   0.5632
   2.750   1.4356   0.01270   0.00593  -0.2541   0.5371   0.5684
   3.000   1.4615   0.01286   0.00607  -0.2541   0.5358   0.5729
   3.250   1.4874   0.01302   0.00623  -0.2541   0.5345   0.5766
   3.500   1.5133   0.01320   0.00641  -0.2541   0.5332   0.5809
   3.750   1.5394   0.01339   0.00659  -0.2542   0.5319   0.5856
   4.250   1.5899   0.01369   0.00698  -0.2540   0.5299   0.5958
   4.500   1.6147   0.01385   0.00719  -0.2538   0.5286   0.6015
   4.750   1.6390   0.01402   0.00740  -0.2535   0.5272   0.6071
   5.000   1.6631   0.01419   0.00762  -0.2532   0.5257   0.6127
   5.250   1.6867   0.01437   0.00786  -0.2529   0.5242   0.6192
   5.500   1.7098   0.01456   0.00809  -0.2524   0.5228   0.6258
   5.750   1.7324   0.01475   0.00834  -0.2519   0.5215   0.6335
   6.000   1.7547   0.01496   0.00858  -0.2513   0.5203   0.6426
   6.250   1.7771   0.01517   0.00886  -0.2507   0.5192   0.6531
   6.500   1.8000   0.01539   0.00913  -0.2503   0.5180   0.6638
   6.750   1.8234   0.01563   0.00942  -0.2499   0.5169   0.6754
   7.000   1.8468   0.01587   0.00973  -0.2496   0.5157   0.6894
   7.500   1.8847   0.01637   0.01048  -0.2474   0.5129   0.7331
   7.750   1.8997   0.01650   0.01088  -0.2456   0.5106   0.8367
   8.000   1.9105   0.01678   0.01127  -0.2430   0.5073   1.0000
   8.250   1.9254   0.01718   0.01170  -0.2413   0.5040   1.0000
   8.500   1.9423   0.01760   0.01210  -0.2400   0.5007   1.0000
   8.750   1.9555   0.01812   0.01274  -0.2382   0.4978   1.0000
   9.000   1.9678   0.01871   0.01341  -0.2363   0.4940   1.0000
   9.250   1.9791   0.01936   0.01411  -0.2343   0.4895   1.0000
   9.500   1.9914   0.02005   0.01479  -0.2325   0.4854   1.0000
   9.750   2.0019   0.02086   0.01572  -0.2306   0.4808   1.0000
  10.000   2.0093   0.02185   0.01676  -0.2283   0.4744   1.0000
  10.250   2.0156   0.02298   0.01793  -0.2260   0.4676   1.0000
  10.500   2.0189   0.02436   0.01937  -0.2234   0.4578   1.0000
  10.750   2.0205   0.02593   0.02100  -0.2208   0.4455   1.0000
  11.000   2.0142   0.02815   0.02320  -0.2174   0.4286   1.0000
  11.250   1.9983   0.03125   0.02623  -0.2132   0.4098   1.0000
  11.500   1.9827   0.03465   0.02959  -0.2094   0.3878   1.0000
  11.750   1.9551   0.03944   0.03428  -0.2049   0.3605   1.0000
  12.000   1.9299   0.04438   0.03915  -0.2012   0.3419   1.0000
  12.500   1.8811   0.05501   0.04967  -0.1949   0.2977   1.0000
  12.750   1.8550   0.06089   0.05548  -0.1921   0.2778   1.0000
  13.000   1.8336   0.06648   0.06102  -0.1900   0.2557   1.0000
  13.250   1.8091   0.07263   0.06708  -0.1879   0.2321   1.0000
  13.500   1.7888   0.07843   0.07280  -0.1863   0.2091   1.0000
  13.750   1.7712   0.08404   0.07831  -0.1850   0.1867   1.0000
  14.000   1.7568   0.08930   0.08348  -0.1839   0.1642   1.0000
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