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WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il)
Reynolds number: 500,000
Max Cl/Cd: 121.05 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx72150a-il-500000-n5.txt
Download as CSV file: xf-fx72150a-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500   0.2057   0.08884   0.08455  -0.1391   0.6595   0.0147
  -9.250   0.2136   0.08646   0.08217  -0.1401   0.6555   0.0150
  -9.000   0.2213   0.08410   0.07981  -0.1411   0.6516   0.0153
  -8.750   0.2276   0.08159   0.07727  -0.1421   0.6476   0.0158
  -8.500   0.2305   0.07866   0.07434  -0.1438   0.6444   0.0161
  -8.250   0.2317   0.07535   0.07106  -0.1458   0.6411   0.0162
  -8.000   0.2398   0.07305   0.06877  -0.1463   0.6369   0.0163
  -7.750   0.2457   0.07057   0.06629  -0.1473   0.6332   0.0163
  -7.250   0.2654   0.06712   0.06282  -0.1477   0.6264   0.0167
  -7.000   0.2739   0.06534   0.06105  -0.1481   0.6230   0.0172
  -6.750   0.2790   0.06313   0.05886  -0.1487   0.6197   0.0174
  -6.500   0.2822   0.06099   0.05672  -0.1489   0.6164   0.0177
  -6.250   0.2837   0.05899   0.05472  -0.1491   0.6133   0.0180
  -5.750   0.2984   0.04927   0.04504  -0.1615   0.6080   0.0192
  -5.500   0.3130   0.04593   0.04170  -0.1658   0.6050   0.0194
  -5.000   0.3710   0.02934   0.02453  -0.1913   0.5996   0.0133
  -4.750   0.4017   0.02643   0.02136  -0.1958   0.5968   0.0130
  -4.500   0.4367   0.02282   0.01737  -0.2006   0.5944   0.0126
  -4.250   0.4745   0.01890   0.01291  -0.2050   0.5920   0.0120
  -4.000   0.5097   0.01628   0.00978  -0.2077   0.5894   0.0118
  -3.750   0.5413   0.01504   0.00825  -0.2090   0.5867   0.0118
  -3.500   0.5715   0.01425   0.00726  -0.2099   0.5841   0.0119
  -3.250   0.6013   0.01367   0.00652  -0.2106   0.5816   0.0122
  -2.750   0.6609   0.01280   0.00545  -0.2120   0.5773   0.0129
  -2.500   0.6908   0.01248   0.00506  -0.2126   0.5751   0.0132
  -2.250   0.7206   0.01222   0.00475  -0.2133   0.5729   0.0135
  -2.000   0.7505   0.01198   0.00447  -0.2140   0.5707   0.0140
  -1.750   0.7797   0.01184   0.00430  -0.2145   0.5686   0.0146
  -1.500   0.8086   0.01176   0.00418  -0.2150   0.5664   0.0156
  -1.250   0.8377   0.01167   0.00403  -0.2155   0.5643   0.0165
  -1.000   0.8667   0.01160   0.00393  -0.2159   0.5621   0.0173
  -0.750   0.8959   0.01154   0.00385  -0.2164   0.5601   0.0185
  -0.500   0.9249   0.01149   0.00379  -0.2168   0.5580   0.0211
  -0.250   0.9538   0.01145   0.00374  -0.2172   0.5559   0.0283
   0.000   0.9830   0.01138   0.00372  -0.2178   0.5539   0.0571
   0.250   1.0130   0.01116   0.00375  -0.2187   0.5522   0.1677
   0.500   1.0441   0.01073   0.00391  -0.2202   0.5504   0.4325
   0.750   1.0717   0.01082   0.00405  -0.2203   0.5486   0.4923
   1.000   1.0991   0.01095   0.00419  -0.2204   0.5470   0.5226
   1.250   1.1268   0.01105   0.00431  -0.2206   0.5456   0.5370
   1.500   1.1545   0.01114   0.00440  -0.2207   0.5443   0.5458
   1.750   1.1820   0.01123   0.00451  -0.2209   0.5429   0.5535
   2.000   1.2095   0.01134   0.00460  -0.2210   0.5414   0.5589
   2.250   1.2368   0.01144   0.00471  -0.2211   0.5399   0.5626
   2.500   1.2640   0.01155   0.00482  -0.2212   0.5384   0.5668
   2.750   1.2910   0.01167   0.00494  -0.2213   0.5368   0.5711
   3.000   1.3178   0.01179   0.00506  -0.2214   0.5353   0.5752
   3.250   1.3446   0.01193   0.00519  -0.2215   0.5337   0.5791
   3.500   1.3713   0.01207   0.00534  -0.2215   0.5323   0.5834
   3.750   1.3980   0.01223   0.00550  -0.2216   0.5310   0.5886
   4.000   1.4248   0.01239   0.00567  -0.2217   0.5297   0.5939
   4.250   1.4512   0.01251   0.00585  -0.2217   0.5287   0.5986
   4.500   1.4774   0.01264   0.00604  -0.2217   0.5274   0.6038
   4.750   1.5034   0.01277   0.00622  -0.2217   0.5259   0.6096
   5.000   1.5291   0.01291   0.00641  -0.2216   0.5243   0.6152
   5.250   1.5547   0.01305   0.00662  -0.2215   0.5227   0.6215
   5.500   1.5801   0.01321   0.00683  -0.2214   0.5212   0.6289
   5.750   1.6049   0.01336   0.00703  -0.2212   0.5192   0.6372
   6.000   1.6282   0.01353   0.00721  -0.2206   0.5156   0.6466
   6.250   1.6505   0.01368   0.00744  -0.2199   0.5118   0.6556
   6.750   1.6923   0.01398   0.00788  -0.2180   0.5029   0.6756
   7.000   1.7115   0.01418   0.00813  -0.2168   0.4990   0.6879
   7.250   1.7304   0.01436   0.00841  -0.2155   0.4956   0.7032
   7.500   1.7474   0.01456   0.00872  -0.2138   0.4908   0.7228
   7.750   1.7621   0.01482   0.00906  -0.2118   0.4856   0.7531
   8.000   1.7740   0.01488   0.00939  -0.2092   0.4815   1.0000
   8.250   1.7896   0.01524   0.00982  -0.2075   0.4756   1.0000
   8.500   1.7977   0.01585   0.01041  -0.2046   0.4666   1.0000
   8.750   1.8070   0.01648   0.01109  -0.2021   0.4535   1.0000
   9.000   1.8093   0.01749   0.01206  -0.1987   0.4325   1.0000
   9.250   1.7970   0.01940   0.01383  -0.1936   0.4065   1.0000
   9.500   1.7808   0.02191   0.01620  -0.1885   0.3709   1.0000
   9.750   1.7551   0.02541   0.01952  -0.1830   0.3402   1.0000
  10.000   1.7326   0.02904   0.02303  -0.1783   0.3095   1.0000
  10.250   1.7090   0.03312   0.02699  -0.1740   0.2821   1.0000
  10.500   1.6852   0.03760   0.03136  -0.1703   0.2525   1.0000
  10.750   1.6603   0.04253   0.03616  -0.1670   0.2220   1.0000
  11.000   1.6391   0.04741   0.04093  -0.1643   0.1941   1.0000
  11.250   1.6180   0.05251   0.04589  -0.1620   0.1638   1.0000
  11.500   1.5992   0.05756   0.05081  -0.1600   0.1335   1.0000
  11.750   1.5795   0.06290   0.05597  -0.1583   0.1009   1.0000
  12.000   1.5522   0.06938   0.06218  -0.1565   0.0559   1.0000
  12.250   1.5330   0.07508   0.06769  -0.1553   0.0203   1.0000
  12.500   1.5326   0.07849   0.07109  -0.1547   0.0129   1.0000
  12.750   1.5377   0.08118   0.07382  -0.1542   0.0116   1.0000
  13.000   1.5440   0.08374   0.07643  -0.1539   0.0108   1.0000
  13.250   1.5498   0.08638   0.07914  -0.1536   0.0103   1.0000
  13.500   1.5561   0.08896   0.08178  -0.1533   0.0099   1.0000
  13.750   1.5622   0.09155   0.08443  -0.1530   0.0096   1.0000
  14.000   1.5671   0.09437   0.08732  -0.1528   0.0094   1.0000
  14.250   1.5722   0.09716   0.09016  -0.1527   0.0091   1.0000
  14.500   1.5771   0.09998   0.09306  -0.1525   0.0089   1.0000
  14.750   1.5823   0.10279   0.09593  -0.1525   0.0088   1.0000
  15.000   1.5876   0.10555   0.09877  -0.1524   0.0087   1.0000
  15.250   1.5928   0.10831   0.10160  -0.1524   0.0085   1.0000
  15.500   1.5969   0.11129   0.10465  -0.1525   0.0084   1.0000
  15.750   1.6014   0.11420   0.10764  -0.1526   0.0083   1.0000
  16.000   1.6058   0.11710   0.11061  -0.1527   0.0082   1.0000
  16.250   1.6092   0.12020   0.11378  -0.1530   0.0081   1.0000
  16.500   1.6127   0.12325   0.11691  -0.1533   0.0080   1.0000
  16.750   1.6164   0.12625   0.11998  -0.1536   0.0079   1.0000
  17.000   1.6187   0.12949   0.12330  -0.1540   0.0078   1.0000
  17.250   1.6216   0.13263   0.12651  -0.1545   0.0077   1.0000
  17.500   1.6243   0.13578   0.12973  -0.1551   0.0076   1.0000
  17.750   1.6263   0.13907   0.13310  -0.1557   0.0076   1.0000
  18.000   1.6290   0.14223   0.13633  -0.1564   0.0075   1.0000
  18.250   1.6308   0.14554   0.13971  -0.1572   0.0074   1.0000
  18.500   1.6327   0.14880   0.14305  -0.1581   0.0074   1.0000
  18.750   1.6349   0.15200   0.14631  -0.1590   0.0073   1.0000
  19.000   1.6366   0.15527   0.14965  -0.1600   0.0073   1.0000
  19.250   1.6386   0.15844   0.15288  -0.1610   0.0072   1.0000
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