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=5


Details Polar file
Airfoil: FX 76-MP-140 (fx76mp140-il)
Reynolds number: 500,000
Max Cl/Cd: 131.52 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76mp140-il-500000-n5.txt
Download as CSV file: xf-fx76mp140-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2910   0.03175   0.02755  -0.1866   0.7833   0.0191
 -11.500  -0.3027   0.02728   0.02278  -0.1904   0.7804   0.0192
 -11.250  -0.2956   0.02521   0.02053  -0.1910   0.7783   0.0195
 -11.000  -0.2810   0.02384   0.01904  -0.1913   0.7763   0.0197
 -10.750  -0.2615   0.02295   0.01803  -0.1915   0.7745   0.0201
 -10.500  -0.2405   0.02213   0.01711  -0.1916   0.7728   0.0206
 -10.250  -0.2199   0.02128   0.01616  -0.1917   0.7713   0.0211
 -10.000  -0.1984   0.02046   0.01521  -0.1917   0.7697   0.0217
  -9.750  -0.1765   0.01960   0.01418  -0.1917   0.7680   0.0223
  -9.500  -0.1534   0.01882   0.01323  -0.1918   0.7663   0.0228
  -9.250  -0.1297   0.01818   0.01255  -0.1918   0.7646   0.0234
  -9.000  -0.1050   0.01763   0.01192  -0.1919   0.7629   0.0238
  -8.750  -0.0798   0.01711   0.01131  -0.1919   0.7611   0.0244
  -8.500  -0.0544   0.01656   0.01065  -0.1920   0.7595   0.0249
  -8.250  -0.0284   0.01604   0.01000  -0.1921   0.7580   0.0255
  -8.000  -0.0020   0.01553   0.00937  -0.1923   0.7566   0.0260
  -7.750   0.0240   0.01505   0.00877  -0.1923   0.7550   0.0265
  -7.500   0.0498   0.01458   0.00826  -0.1923   0.7533   0.0271
  -7.250   0.0763   0.01423   0.00788  -0.1923   0.7514   0.0278
  -7.000   0.1032   0.01395   0.00755  -0.1924   0.7496   0.0287
  -6.750   0.1302   0.01364   0.00719  -0.1924   0.7478   0.0296
  -6.500   0.1573   0.01331   0.00678  -0.1925   0.7459   0.0305
  -6.250   0.1846   0.01298   0.00638  -0.1926   0.7442   0.0314
  -6.000   0.2122   0.01271   0.00609  -0.1927   0.7426   0.0324
  -5.750   0.2402   0.01250   0.00582  -0.1929   0.7410   0.0337
  -5.500   0.2683   0.01229   0.00554  -0.1931   0.7393   0.0352
  -5.250   0.2951   0.01205   0.00528  -0.1930   0.7375   0.0366
  -5.000   0.3223   0.01186   0.00509  -0.1930   0.7356   0.0383
  -4.750   0.3496   0.01169   0.00491  -0.1930   0.7334   0.0402
  -4.500   0.3770   0.01151   0.00469  -0.1930   0.7310   0.0421
  -4.250   0.4045   0.01131   0.00448  -0.1930   0.7287   0.0440
  -4.000   0.4324   0.01116   0.00430  -0.1931   0.7266   0.0461
  -3.750   0.4606   0.01104   0.00412  -0.1932   0.7246   0.0481
  -3.500   0.4884   0.01089   0.00398  -0.1933   0.7227   0.0508
  -3.250   0.5153   0.01078   0.00388  -0.1932   0.7203   0.0536
  -3.000   0.5424   0.01068   0.00378  -0.1931   0.7178   0.0564
  -2.750   0.5696   0.01055   0.00367  -0.1931   0.7152   0.0602
  -2.500   0.5971   0.01045   0.00355  -0.1930   0.7124   0.0639
  -2.250   0.6248   0.01032   0.00342  -0.1930   0.7099   0.0682
  -2.000   0.6529   0.01024   0.00331  -0.1931   0.7076   0.0734
  -1.750   0.6793   0.01016   0.00327  -0.1929   0.7048   0.0794
  -1.500   0.7060   0.01009   0.00323  -0.1928   0.7017   0.0862
  -1.250   0.7328   0.01001   0.00318  -0.1926   0.6987   0.0963
  -1.000   0.7600   0.00993   0.00313  -0.1926   0.6959   0.1081
  -0.750   0.7873   0.00986   0.00307  -0.1925   0.6928   0.1220
  -0.500   0.8136   0.00981   0.00307  -0.1923   0.6894   0.1384
  -0.250   0.8396   0.00975   0.00308  -0.1920   0.6854   0.1576
   0.000   0.8658   0.00969   0.00307  -0.1918   0.6816   0.1820
   0.250   0.8921   0.00960   0.00307  -0.1916   0.6781   0.2194
   0.500   0.9181   0.00951   0.00309  -0.1914   0.6747   0.2685
   0.750   0.9430   0.00941   0.00316  -0.1909   0.6701   0.3290
   1.000   0.9674   0.00925   0.00320  -0.1904   0.6650   0.4145
   1.250   0.9911   0.00903   0.00325  -0.1898   0.6604   0.5413
   1.500   1.0116   0.00882   0.00346  -0.1883   0.6552   0.6992
   1.750   1.0339   0.00881   0.00358  -0.1871   0.6502   0.7638
   2.000   1.0576   0.00887   0.00363  -0.1862   0.6454   0.7904
   2.250   1.0804   0.00892   0.00373  -0.1852   0.6398   0.8121
   2.500   1.1029   0.00898   0.00381  -0.1841   0.6339   0.8308
   2.750   1.1245   0.00904   0.00388  -0.1828   0.6283   0.8535
   3.000   1.1453   0.00909   0.00398  -0.1814   0.6214   0.8767
   3.250   1.1668   0.00911   0.00404  -0.1801   0.6139   0.9152
   3.500   1.2047   0.00916   0.00414  -0.1825   0.6047   1.0000
   3.750   1.2265   0.00934   0.00425  -0.1815   0.5959   1.0000
   4.000   1.2479   0.00952   0.00440  -0.1804   0.5865   1.0000
   4.250   1.2674   0.00972   0.00455  -0.1789   0.5781   1.0000
   4.500   1.2856   0.00995   0.00474  -0.1771   0.5683   1.0000
   4.750   1.3037   0.01020   0.00495  -0.1754   0.5578   1.0000
   5.000   1.3204   0.01052   0.00520  -0.1734   0.5468   1.0000
   5.250   1.3357   0.01088   0.00551  -0.1713   0.5343   1.0000
   5.500   1.3515   0.01127   0.00585  -0.1693   0.5215   1.0000
   5.750   1.3658   0.01174   0.00625  -0.1671   0.5079   1.0000
   6.000   1.3798   0.01226   0.00672  -0.1650   0.4945   1.0000
   6.250   1.3943   0.01282   0.00724  -0.1631   0.4831   1.0000
   6.500   1.4086   0.01346   0.00782  -0.1613   0.4696   1.0000
   6.750   1.4228   0.01415   0.00847  -0.1596   0.4557   1.0000
   7.250   1.4513   0.01572   0.00996  -0.1566   0.4303   1.0000
   7.500   1.4650   0.01661   0.01081  -0.1551   0.4184   1.0000
   7.750   1.4820   0.01733   0.01153  -0.1541   0.4082   1.0000
   8.000   1.4971   0.01819   0.01237  -0.1529   0.3986   1.0000
   8.250   1.5114   0.01911   0.01327  -0.1517   0.3879   1.0000
   8.500   1.5269   0.01997   0.01413  -0.1506   0.3785   1.0000
   8.750   1.5394   0.02101   0.01514  -0.1491   0.3682   1.0000
   9.000   1.5538   0.02194   0.01608  -0.1480   0.3583   1.0000
   9.250   1.5648   0.02310   0.01721  -0.1464   0.3451   1.0000
   9.500   1.5734   0.02442   0.01848  -0.1447   0.3310   1.0000
   9.750   1.5821   0.02573   0.01975  -0.1429   0.3179   1.0000
  10.000   1.5911   0.02704   0.02103  -0.1412   0.3059   1.0000
  10.250   1.6035   0.02812   0.02212  -0.1399   0.2960   1.0000
  10.500   1.6124   0.02947   0.02345  -0.1383   0.2851   1.0000
  10.750   1.6204   0.03090   0.02485  -0.1367   0.2731   1.0000
  11.000   1.6244   0.03267   0.02654  -0.1347   0.2560   1.0000
  11.500   1.6374   0.03588   0.02969  -0.1313   0.2294   1.0000
  11.750   1.6422   0.03767   0.03143  -0.1296   0.2151   1.0000
  12.000   1.6445   0.03970   0.03339  -0.1277   0.1995   1.0000
  12.250   1.6500   0.04149   0.03515  -0.1261   0.1875   1.0000
  12.500   1.6552   0.04334   0.03699  -0.1246   0.1773   1.0000
  12.750   1.6596   0.04528   0.03891  -0.1231   0.1675   1.0000
  13.000   1.6633   0.04732   0.04092  -0.1216   0.1564   1.0000
  13.250   1.6678   0.04932   0.04291  -0.1202   0.1470   1.0000
  13.500   1.6711   0.05145   0.04502  -0.1188   0.1387   1.0000
  13.750   1.6746   0.05358   0.04716  -0.1175   0.1289   1.0000
  14.000   1.6775   0.05582   0.04939  -0.1162   0.1199   1.0000
  14.250   1.6801   0.05812   0.05169  -0.1150   0.1126   1.0000
  14.500   1.6814   0.06058   0.05414  -0.1137   0.1034   1.0000
  14.750   1.6839   0.06294   0.05651  -0.1126   0.0952   1.0000
  15.000   1.6814   0.06583   0.05939  -0.1113   0.0839   1.0000
  15.250   1.6760   0.06907   0.06258  -0.1100   0.0710   1.0000
  15.500   1.6675   0.07274   0.06619  -0.1087   0.0569   1.0000
  15.750   1.6596   0.07640   0.06982  -0.1076   0.0468   1.0000
  16.000   1.6545   0.07978   0.07321  -0.1066   0.0408   1.0000
  16.250   1.6510   0.08305   0.07652  -0.1059   0.0364   1.0000
  16.500   1.6488   0.08622   0.07974  -0.1053   0.0329   1.0000
<< Back to FX 76-MP-140 (fx76mp140-il)

Polar data table (+)

Polar graphs


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