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FX 76-MP-140 (fx76mp140-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 76-MP-140 (fx76mp140-il)
Reynolds number: 1,000,000
Max Cl/Cd: 181.59 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76mp140-il-1000000.txt
Download as CSV file: xf-fx76mp140-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 76-MP-140                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000   0.0267   0.11452   0.11158  -0.1286   0.7991   0.0160
 -12.750   0.0356   0.11147   0.10853  -0.1301   0.7978   0.0163
 -12.500  -0.3785   0.02646   0.02287  -0.1951   0.7921   0.0184
 -12.250  -0.3681   0.02472   0.02096  -0.1963   0.7896   0.0188
 -12.000  -0.3559   0.02336   0.01948  -0.1964   0.7881   0.0190
 -11.750  -0.3396   0.02231   0.01830  -0.1964   0.7864   0.0192
 -11.500  -0.3315   0.02027   0.01607  -0.1962   0.7845   0.0197
 -11.250  -0.3120   0.01938   0.01511  -0.1962   0.7828   0.0201
 -11.000  -0.2896   0.01877   0.01445  -0.1961   0.7812   0.0205
 -10.750  -0.2661   0.01825   0.01385  -0.1961   0.7796   0.0209
 -10.500  -0.2410   0.01793   0.01349  -0.1961   0.7781   0.0215
 -10.250  -0.2175   0.01728   0.01271  -0.1962   0.7764   0.0219
 -10.000  -0.1923   0.01682   0.01214  -0.1963   0.7744   0.0224
  -9.750  -0.1666   0.01645   0.01166  -0.1964   0.7725   0.0227
  -9.500  -0.1455   0.01532   0.01041  -0.1962   0.7713   0.0233
  -9.250  -0.1206   0.01481   0.00987  -0.1962   0.7699   0.0239
  -9.000  -0.0942   0.01453   0.00957  -0.1962   0.7684   0.0244
  -8.750  -0.0679   0.01416   0.00914  -0.1963   0.7668   0.0250
  -8.500  -0.0407   0.01398   0.00891  -0.1963   0.7651   0.0258
  -8.250  -0.0140   0.01361   0.00845  -0.1964   0.7635   0.0263
  -8.000   0.0134   0.01338   0.00815  -0.1965   0.7619   0.0267
  -7.750   0.0383   0.01253   0.00720  -0.1965   0.7603   0.0274
  -7.500   0.0657   0.01221   0.00684  -0.1967   0.7584   0.0281
  -7.250   0.0938   0.01200   0.00657  -0.1969   0.7561   0.0287
  -7.000   0.1208   0.01171   0.00626  -0.1969   0.7551   0.0294
  -6.750   0.1480   0.01144   0.00595  -0.1969   0.7537   0.0302
  -6.500   0.1754   0.01118   0.00565  -0.1969   0.7521   0.0308
  -6.250   0.2023   0.01077   0.00519  -0.1970   0.7503   0.0319
  -6.000   0.2301   0.01056   0.00498  -0.1971   0.7486   0.0331
  -5.750   0.2581   0.01038   0.00478  -0.1972   0.7468   0.0343
  -5.500   0.2863   0.01022   0.00456  -0.1973   0.7449   0.0357
  -5.250   0.3139   0.00990   0.00421  -0.1974   0.7429   0.0374
  -5.000   0.3425   0.00978   0.00407  -0.1976   0.7406   0.0392
  -4.750   0.3706   0.00969   0.00395  -0.1977   0.7387   0.0411
  -4.500   0.3978   0.00943   0.00370  -0.1977   0.7371   0.0435
  -4.250   0.4255   0.00929   0.00358  -0.1977   0.7352   0.0457
  -4.000   0.4535   0.00920   0.00347  -0.1977   0.7332   0.0478
  -3.750   0.4813   0.00900   0.00326  -0.1978   0.7311   0.0504
  -3.500   0.5093   0.00887   0.00313  -0.1978   0.7288   0.0528
  -3.250   0.5374   0.00879   0.00302  -0.1979   0.7266   0.0550
  -3.000   0.5660   0.00869   0.00288  -0.1981   0.7240   0.0578
  -2.750   0.5936   0.00858   0.00280  -0.1981   0.7221   0.0611
  -2.500   0.6210   0.00850   0.00273  -0.1981   0.7200   0.0641
  -2.250   0.6485   0.00836   0.00262  -0.1980   0.7177   0.0700
  -2.000   0.6762   0.00828   0.00254  -0.1980   0.7152   0.0747
  -1.750   0.7036   0.00815   0.00244  -0.1980   0.7127   0.0836
  -1.500   0.7314   0.00806   0.00236  -0.1980   0.7099   0.0935
  -1.250   0.7594   0.00801   0.00232  -0.1981   0.7069   0.1061
  -1.000   0.7860   0.00791   0.00229  -0.1979   0.7045   0.1229
  -0.750   0.8130   0.00782   0.00227  -0.1978   0.7016   0.1441
  -0.500   0.8399   0.00773   0.00224  -0.1977   0.6986   0.1674
  -0.250   0.8668   0.00764   0.00222  -0.1976   0.6954   0.1967
   0.000   0.8940   0.00759   0.00221  -0.1976   0.6917   0.2342
   0.250   0.9196   0.00745   0.00223  -0.1972   0.6884   0.2857
   0.500   0.9451   0.00729   0.00226  -0.1969   0.6847   0.3601
   0.750   0.9693   0.00700   0.00231  -0.1964   0.6812   0.5089
   1.000   0.9913   0.00671   0.00244  -0.1953   0.6776   0.6983
   1.250   1.0157   0.00669   0.00253  -0.1945   0.6738   0.7575
   1.500   1.0408   0.00669   0.00259  -0.1940   0.6697   0.7851
   1.750   1.0659   0.00672   0.00263  -0.1934   0.6653   0.8038
   2.000   1.0905   0.00679   0.00268  -0.1927   0.6607   0.8228
   2.250   1.1147   0.00680   0.00274  -0.1920   0.6556   0.8391
   2.500   1.1384   0.00683   0.00279  -0.1911   0.6498   0.8522
   2.750   1.1616   0.00690   0.00284  -0.1901   0.6444   0.8649
   3.000   1.1855   0.00693   0.00291  -0.1894   0.6384   0.8779
   3.250   1.2077   0.00698   0.00298  -0.1882   0.6323   0.8937
   3.500   1.2299   0.00701   0.00305  -0.1871   0.6261   0.9189
   3.750   1.2766   0.00703   0.00314  -0.1915   0.6178   1.0000
   4.000   1.3010   0.00717   0.00325  -0.1910   0.6091   1.0000
   4.250   1.3233   0.00736   0.00337  -0.1901   0.5980   1.0000
   4.500   1.3464   0.00753   0.00350  -0.1893   0.5866   1.0000
   4.750   1.3676   0.00774   0.00367  -0.1882   0.5745   1.0000
   5.000   1.3866   0.00799   0.00386  -0.1866   0.5628   1.0000
   5.250   1.4052   0.00828   0.00408  -0.1850   0.5502   1.0000
   5.500   1.4254   0.00857   0.00432  -0.1837   0.5366   1.0000
   5.750   1.4454   0.00890   0.00460  -0.1825   0.5228   1.0000
   6.000   1.4660   0.00925   0.00490  -0.1814   0.5107   1.0000
   6.250   1.4862   0.00964   0.00524  -0.1804   0.4992   1.0000
   6.500   1.5076   0.01001   0.00558  -0.1796   0.4879   1.0000
   6.750   1.5287   0.01041   0.00595  -0.1788   0.4768   1.0000
   7.000   1.5480   0.01089   0.00640  -0.1778   0.4658   1.0000
   7.250   1.5656   0.01146   0.00692  -0.1765   0.4527   1.0000
   7.500   1.5839   0.01200   0.00744  -0.1754   0.4405   1.0000
   7.750   1.5998   0.01268   0.00807  -0.1740   0.4274   1.0000
   8.000   1.6138   0.01347   0.00881  -0.1724   0.4132   1.0000
   8.250   1.6278   0.01429   0.00959  -0.1708   0.4014   1.0000
   8.500   1.6426   0.01508   0.01036  -0.1694   0.3893   1.0000
   8.750   1.6569   0.01592   0.01118  -0.1680   0.3777   1.0000
   9.000   1.6693   0.01689   0.01211  -0.1663   0.3660   1.0000
   9.250   1.6795   0.01800   0.01317  -0.1645   0.3519   1.0000
   9.500   1.6897   0.01914   0.01426  -0.1626   0.3379   1.0000
   9.750   1.6994   0.02029   0.01536  -0.1608   0.3237   1.0000
  10.000   1.7080   0.02153   0.01655  -0.1588   0.3091   1.0000
  10.250   1.7162   0.02280   0.01777  -0.1568   0.2942   1.0000
  10.500   1.7217   0.02425   0.01915  -0.1546   0.2775   1.0000
  10.750   1.7291   0.02560   0.02045  -0.1526   0.2639   1.0000
  11.000   1.7362   0.02698   0.02179  -0.1506   0.2509   1.0000
  11.250   1.7401   0.02860   0.02334  -0.1483   0.2343   1.0000
  11.500   1.7457   0.03015   0.02483  -0.1463   0.2206   1.0000
  11.750   1.7501   0.03182   0.02644  -0.1442   0.2064   1.0000
  12.000   1.7547   0.03351   0.02808  -0.1422   0.1933   1.0000
  12.250   1.7572   0.03538   0.02987  -0.1401   0.1780   1.0000
  12.500   1.7617   0.03715   0.03160  -0.1383   0.1674   1.0000
  12.750   1.7676   0.03883   0.03326  -0.1366   0.1573   1.0000
  13.000   1.7742   0.04050   0.03493  -0.1351   0.1498   1.0000
  13.250   1.7781   0.04238   0.03678  -0.1333   0.1400   1.0000
  13.500   1.7844   0.04413   0.03853  -0.1319   0.1322   1.0000
  13.750   1.7885   0.04607   0.04044  -0.1303   0.1234   1.0000
  14.000   1.7904   0.04827   0.04261  -0.1287   0.1142   1.0000
  14.250   1.7953   0.05021   0.04455  -0.1273   0.1064   1.0000
  14.500   1.7961   0.05255   0.04688  -0.1257   0.0968   1.0000
  14.750   1.7940   0.05521   0.04948  -0.1240   0.0842   1.0000
  15.000   1.7857   0.05856   0.05274  -0.1220   0.0697   1.0000
  15.250   1.7746   0.06228   0.05638  -0.1201   0.0533   1.0000
  15.500   1.7650   0.06590   0.05995  -0.1183   0.0429   1.0000
  16.000   1.7599   0.07193   0.06602  -0.1160   0.0335   1.0000
  16.250   1.7585   0.07486   0.06898  -0.1150   0.0302   1.0000
  16.500   1.7567   0.07787   0.07203  -0.1142   0.0278   1.0000
  16.750   1.7554   0.08084   0.07506  -0.1134   0.0258   1.0000
  17.000   1.7548   0.08377   0.07804  -0.1127   0.0243   1.0000
  17.250   1.7514   0.08710   0.08142  -0.1120   0.0228   1.0000
  17.500   1.7506   0.09012   0.08451  -0.1115   0.0217   1.0000
  17.750   1.7489   0.09328   0.08773  -0.1111   0.0205   1.0000
  18.000   1.7441   0.09684   0.09135  -0.1108   0.0194   1.0000
  18.250   1.7396   0.10037   0.09495  -0.1105   0.0183   1.0000
  18.500   1.7386   0.10349   0.09815  -0.1103   0.0175   1.0000
  18.750   1.7347   0.10703   0.10176  -0.1103   0.0165   1.0000
  19.000   1.7274   0.11105   0.10583  -0.1103   0.0155   1.0000
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