Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

FX 76-MP-140 (fx76mp140-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 76-MP-140 (fx76mp140-il)
Reynolds number: 500,000
Max Cl/Cd: 138.22 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76mp140-il-500000.txt
Download as CSV file: xf-fx76mp140-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500   0.1454   0.09918   0.09554  -0.1528   0.8254   0.0285
 -11.250   0.1377   0.09453   0.09091  -0.1580   0.8234   0.0310
 -11.000   0.1427   0.09086   0.08727  -0.1595   0.8217   0.0312
 -10.750   0.1636   0.08956   0.08596  -0.1586   0.8200   0.0318
 -10.500   0.1770   0.08773   0.08413  -0.1594   0.8182   0.0327
 -10.250   0.1862   0.08521   0.08161  -0.1609   0.8163   0.0330
 -10.000   0.1763   0.08017   0.07660  -0.1661   0.8138   0.0359
  -9.750   0.1845   0.07702   0.07344  -0.1670   0.8120   0.0364
  -9.500   0.2046   0.07609   0.07248  -0.1668   0.8104   0.0371
  -9.250   0.2184   0.07421   0.07058  -0.1679   0.8082   0.0383
  -9.000   0.0058   0.03517   0.03155  -0.1918   0.7999   0.0313
  -8.750   0.0232   0.03482   0.03123  -0.1916   0.7978   0.0317
  -8.500   0.0187   0.03069   0.02683  -0.1936   0.7950   0.0321
  -8.000   0.0502   0.02743   0.02322  -0.1949   0.7908   0.0334
  -7.750   0.0565   0.02344   0.01870  -0.1955   0.7887   0.0341
  -7.500   0.0736   0.02128   0.01617  -0.1954   0.7865   0.0349
  -7.250   0.0948   0.01979   0.01436  -0.1953   0.7843   0.0355
  -7.000   0.1185   0.01868   0.01297  -0.1953   0.7821   0.0362
  -6.750   0.1427   0.01752   0.01173  -0.1954   0.7802   0.0371
  -6.500   0.1693   0.01703   0.01119  -0.1956   0.7785   0.0380
  -6.250   0.1967   0.01659   0.01064  -0.1958   0.7767   0.0392
  -6.000   0.2246   0.01611   0.01003  -0.1960   0.7750   0.0405
  -5.750   0.2526   0.01578   0.00952  -0.1963   0.7732   0.0416
  -5.500   0.2770   0.01496   0.00868  -0.1960   0.7714   0.0432
  -5.250   0.3026   0.01465   0.00838  -0.1958   0.7692   0.0447
  -5.000   0.3290   0.01435   0.00804  -0.1956   0.7668   0.0466
  -4.750   0.3561   0.01404   0.00764  -0.1955   0.7645   0.0486
  -4.500   0.3835   0.01364   0.00726  -0.1956   0.7623   0.0513
  -4.250   0.4121   0.01344   0.00701  -0.1958   0.7604   0.0540
  -4.000   0.4409   0.01312   0.00662  -0.1961   0.7586   0.0567
  -3.750   0.4699   0.01291   0.00640  -0.1965   0.7568   0.0597
  -3.500   0.4961   0.01282   0.00631  -0.1963   0.7546   0.0628
  -3.250   0.5217   0.01260   0.00608  -0.1959   0.7522   0.0659
  -3.000   0.5480   0.01239   0.00591  -0.1957   0.7496   0.0697
  -2.750   0.5756   0.01224   0.00574  -0.1957   0.7470   0.0736
  -2.500   0.6040   0.01196   0.00545  -0.1959   0.7447   0.0786
  -2.250   0.6332   0.01179   0.00526  -0.1962   0.7426   0.0840
  -2.000   0.6628   0.01161   0.00507  -0.1966   0.7406   0.0913
  -1.750   0.6895   0.01156   0.00503  -0.1965   0.7382   0.0996
  -1.500   0.7144   0.01139   0.00495  -0.1960   0.7353   0.1116
  -1.250   0.7408   0.01126   0.00487  -0.1958   0.7325   0.1278
  -1.000   0.7686   0.01110   0.00476  -0.1958   0.7298   0.1505
  -0.750   0.7974   0.01090   0.00463  -0.1961   0.7272   0.1813
  -0.250   0.8531   0.01059   0.00455  -0.1964   0.7220   0.2790
   0.000   0.8766   0.01035   0.00459  -0.1957   0.7185   0.3693
   0.250   0.8996   0.00987   0.00465  -0.1951   0.7152   0.5700
   0.500   0.9221   0.00958   0.00477  -0.1938   0.7122   0.7403
   0.750   0.9488   0.00951   0.00473  -0.1933   0.7094   0.7913
   1.000   0.9732   0.00950   0.00475  -0.1925   0.7059   0.8210
   1.250   0.9947   0.00948   0.00478  -0.1911   0.7016   0.8427
   1.500   1.0182   0.00942   0.00475  -0.1900   0.6977   0.8659
   1.750   1.0429   0.00935   0.00468  -0.1892   0.6945   0.8887
   2.000   1.0683   0.00930   0.00463  -0.1886   0.6911   0.9080
   2.250   1.0893   0.00924   0.00465  -0.1872   0.6863   0.9341
   2.500   1.1364   0.00917   0.00461  -0.1915   0.6820   0.9943
   2.750   1.1599   0.00919   0.00456  -0.1907   0.6780   1.0000
   3.000   1.1860   0.00925   0.00461  -0.1905   0.6730   1.0000
   3.250   1.2105   0.00930   0.00466  -0.1899   0.6671   1.0000
   3.500   1.2381   0.00933   0.00462  -0.1900   0.6619   1.0000
   3.750   1.2616   0.00942   0.00472  -0.1893   0.6557   1.0000
   4.000   1.2858   0.00949   0.00478  -0.1887   0.6493   1.0000
   4.250   1.3117   0.00959   0.00482  -0.1884   0.6436   1.0000
   4.500   1.3328   0.00970   0.00496  -0.1872   0.6359   1.0000
   4.750   1.3573   0.00982   0.00500  -0.1867   0.6288   1.0000
   5.000   1.3767   0.00996   0.00518  -0.1851   0.6196   1.0000
   5.250   1.3970   0.01012   0.00529  -0.1838   0.6102   1.0000
   5.500   1.4148   0.01030   0.00544  -0.1819   0.5995   1.0000
   5.750   1.4304   0.01051   0.00564  -0.1796   0.5888   1.0000
   6.000   1.4466   0.01077   0.00586  -0.1775   0.5782   1.0000
   6.250   1.4621   0.01108   0.00612  -0.1753   0.5669   1.0000
   6.500   1.4768   0.01143   0.00644  -0.1731   0.5545   1.0000
   6.750   1.4908   0.01185   0.00683  -0.1708   0.5416   1.0000
   7.000   1.5047   0.01232   0.00726  -0.1686   0.5296   1.0000
   7.250   1.5184   0.01286   0.00775  -0.1665   0.5180   1.0000
   7.500   1.5337   0.01340   0.00828  -0.1648   0.5067   1.0000
   7.750   1.5483   0.01401   0.00888  -0.1631   0.4960   1.0000
   8.250   1.5767   0.01543   0.01027  -0.1598   0.4734   1.0000
   8.500   1.5907   0.01623   0.01105  -0.1583   0.4625   1.0000
   8.750   1.6020   0.01720   0.01199  -0.1565   0.4501   1.0000
   9.000   1.6146   0.01814   0.01292  -0.1549   0.4380   1.0000
   9.250   1.6257   0.01921   0.01397  -0.1533   0.4242   1.0000
   9.500   1.6362   0.02033   0.01507  -0.1516   0.4110   1.0000
   9.750   1.6465   0.02147   0.01618  -0.1499   0.3995   1.0000
  10.000   1.6564   0.02265   0.01735  -0.1482   0.3879   1.0000
  10.250   1.6668   0.02381   0.01851  -0.1465   0.3757   1.0000
  10.500   1.6756   0.02508   0.01976  -0.1448   0.3641   1.0000
  10.750   1.6822   0.02650   0.02115  -0.1428   0.3510   1.0000
  11.000   1.6873   0.02806   0.02266  -0.1407   0.3366   1.0000
  11.250   1.6939   0.02954   0.02412  -0.1389   0.3234   1.0000
  11.500   1.7007   0.03104   0.02561  -0.1371   0.3099   1.0000
  11.750   1.7044   0.03281   0.02734  -0.1351   0.2941   1.0000
  12.000   1.7090   0.03452   0.02902  -0.1332   0.2796   1.0000
  12.250   1.7129   0.03635   0.03081  -0.1314   0.2658   1.0000
  12.500   1.7171   0.03818   0.03261  -0.1296   0.2528   1.0000
  12.750   1.7189   0.04025   0.03463  -0.1277   0.2384   1.0000
  13.000   1.7205   0.04235   0.03667  -0.1258   0.2235   1.0000
  13.250   1.7216   0.04456   0.03885  -0.1240   0.2107   1.0000
  13.500   1.7236   0.04671   0.04097  -0.1224   0.1983   1.0000
  13.750   1.7270   0.04879   0.04305  -0.1209   0.1873   1.0000
  14.000   1.7294   0.05096   0.04520  -0.1194   0.1773   1.0000
  14.250   1.7298   0.05337   0.04760  -0.1179   0.1682   1.0000
  14.500   1.7333   0.05552   0.04976  -0.1166   0.1590   1.0000
  14.750   1.7346   0.05793   0.05218  -0.1153   0.1515   1.0000
  15.000   1.7363   0.06030   0.05457  -0.1141   0.1430   1.0000
  15.250   1.7380   0.06271   0.05699  -0.1129   0.1350   1.0000
  15.500   1.7357   0.06556   0.05984  -0.1116   0.1256   1.0000
  15.750   1.7356   0.06822   0.06250  -0.1105   0.1162   1.0000
  16.000   1.7323   0.07128   0.06555  -0.1094   0.1059   1.0000
  16.250   1.7264   0.07466   0.06891  -0.1083   0.0933   1.0000
  16.500   1.7152   0.07864   0.07282  -0.1071   0.0784   1.0000
  16.750   1.7007   0.08310   0.07719  -0.1059   0.0620   1.0000
  17.000   1.6854   0.08777   0.08180  -0.1050   0.0498   1.0000
<< Back to FX 76-MP-140 (fx76mp140-il)

Polar data table (+)

Polar graphs


<< Back to FX 76-MP-140 (fx76mp140-il)