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FX 76-MP-140 (fx76mp140-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX 76-MP-140 (fx76mp140-il)
Reynolds number: 200,000
Max Cl/Cd: 78.13 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76mp140-il-200000.txt
Download as CSV file: xf-fx76mp140-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250   0.1694   0.10094   0.09653  -0.1593   0.9015   0.0522
 -11.000   0.1769   0.09845   0.09403  -0.1615   0.8982   0.0544
 -10.750   0.1616   0.09677   0.09236  -0.1678   0.8938   0.0559
 -10.500   0.1900   0.09277   0.08833  -0.1654   0.8923   0.0571
 -10.250   0.1977   0.09081   0.08639  -0.1650   0.8892   0.0579
 -10.000   0.2057   0.08885   0.08444  -0.1651   0.8860   0.0595
  -9.750   0.2106   0.08681   0.08240  -0.1659   0.8828   0.0622
  -9.500   0.1874   0.08582   0.08145  -0.1710   0.8776   0.0646
  -9.250   0.2125   0.08175   0.07734  -0.1696   0.8763   0.0659
  -9.000   0.2215   0.08009   0.07571  -0.1678   0.8733   0.0670
  -8.750   0.2268   0.07852   0.07417  -0.1667   0.8699   0.0690
  -8.500   0.2287   0.07684   0.07251  -0.1665   0.8662   0.0716
  -8.250   0.2181   0.07515   0.07085  -0.1682   0.8618   0.0741
  -8.000   0.1749   0.07498   0.07082  -0.1674   0.8548   0.0750
  -7.750   0.1985   0.07126   0.06709  -0.1656   0.8533   0.0762
  -7.500   0.2153   0.06969   0.06551  -0.1636   0.8507   0.0778
  -7.250   0.2191   0.06818   0.06401  -0.1625   0.8471   0.0790
  -7.000   0.2204   0.06662   0.06245  -0.1618   0.8440   0.0812
  -6.750   0.2056   0.06593   0.06183  -0.1592   0.8393   0.0831
  -6.500   0.1712   0.06456   0.06053  -0.1619   0.8304   0.0861
  -6.250   0.1680   0.05923   0.05508  -0.1682   0.8266   0.0879
  -6.000   0.1873   0.05779   0.05368  -0.1660   0.8252   0.0891
  -5.750   0.1452   0.05897   0.05495  -0.1571   0.8141   0.0889
  -5.500   0.1626   0.05730   0.05328  -0.1565   0.8116   0.0905
  -5.250   0.1860   0.05495   0.05084  -0.1593   0.8097   0.0962
  -5.000   0.1375   0.05695   0.05296  -0.1474   0.7978   0.0939
  -4.750   0.1600   0.05123   0.04687  -0.1559   0.7942   0.1026
  -4.500   0.1889   0.04926   0.04489  -0.1571   0.7929   0.1050
  -4.250   0.1753   0.03489   0.02863  -0.1606   0.7818   0.0663
  -4.000   0.2029   0.03434   0.02809  -0.1610   0.7790   0.0687
  -3.750   0.2408   0.03257   0.02595  -0.1633   0.7777   0.0711
  -3.500   0.2831   0.03090   0.02381  -0.1659   0.7767   0.0741
  -3.250   0.3239   0.02951   0.02227  -0.1684   0.7758   0.0784
  -3.000   0.2968   0.03101   0.02378  -0.1601   0.7643   0.0788
  -2.750   0.3299   0.03039   0.02305  -0.1609   0.7620   0.0832
  -2.500   0.3685   0.02940   0.02185  -0.1625   0.7606   0.0884
  -2.250   0.4077   0.02863   0.02109  -0.1644   0.7596   0.0943
  -2.000   0.4497   0.02797   0.02027  -0.1665   0.7588   0.1008
  -1.750   0.4248   0.02947   0.02180  -0.1586   0.7467   0.1016
  -1.500   0.5317   0.02626   0.01856  -0.1707   0.7574   0.1177
  -1.250   0.4966   0.02812   0.02044  -0.1609   0.7435   0.1170
  -1.000   0.5369   0.02737   0.01973  -0.1627   0.7427   0.1287
  -0.750   0.5302   0.02853   0.02089  -0.1576   0.7333   0.1335
  -0.500   0.5904   0.02692   0.01939  -0.1623   0.7365   0.1585
  -0.250   0.6449   0.02574   0.01833  -0.1665   0.7378   0.2006
   0.000   0.6970   0.02446   0.01740  -0.1705   0.7390   0.2909
   0.500   0.6759   0.02616   0.01976  -0.1586   0.7189   0.4645
   0.750   0.7162   0.02436   0.01890  -0.1585   0.7211   0.8425
   1.000   0.7736   0.02324   0.01782  -0.1628   0.7219   1.0000
   1.250   0.8281   0.02236   0.01677  -0.1670   0.7232   1.0000
   1.500   0.8109   0.02379   0.01820  -0.1601   0.7106   1.0000
   1.750   0.8545   0.02323   0.01752  -0.1625   0.7098   1.0000
   2.000   0.9001   0.02260   0.01679  -0.1652   0.7091   1.0000
   2.250   0.9454   0.02193   0.01602  -0.1679   0.7083   1.0000
   2.500   0.9288   0.02322   0.01733  -0.1609   0.6961   1.0000
   2.750   0.9725   0.02258   0.01661  -0.1632   0.6950   1.0000
   3.000   1.0187   0.02189   0.01585  -0.1661   0.6941   1.0000
   3.250   1.0641   0.02122   0.01512  -0.1689   0.6931   1.0000
   3.500   1.1100   0.02057   0.01441  -0.1718   0.6920   1.0000
   3.750   1.0931   0.02172   0.01560  -0.1644   0.6803   1.0000
   4.000   1.1398   0.02099   0.01483  -0.1674   0.6788   1.0000
   4.250   1.1877   0.02025   0.01404  -0.1706   0.6774   1.0000
   4.500   1.1783   0.02107   0.01490  -0.1643   0.6670   1.0000
   4.750   1.2233   0.02034   0.01414  -0.1670   0.6644   1.0000
   5.000   1.2724   0.01958   0.01334  -0.1704   0.6621   1.0000
   5.250   1.2725   0.02010   0.01389  -0.1656   0.6531   1.0000
   5.500   1.3101   0.01963   0.01341  -0.1672   0.6488   1.0000
   5.750   1.3616   0.01891   0.01265  -0.1712   0.6458   1.0000
   6.000   1.3564   0.01952   0.01331  -0.1654   0.6357   1.0000
   6.250   1.4026   0.01885   0.01260  -0.1684   0.6308   1.0000
   6.500   1.4065   0.01929   0.01308  -0.1642   0.6212   1.0000
   6.750   1.4477   0.01874   0.01248  -0.1663   0.6145   1.0000
   7.000   1.4508   0.01920   0.01298  -0.1621   0.6035   1.0000
   7.250   1.4774   0.01906   0.01281  -0.1618   0.5943   1.0000
   7.500   1.4953   0.01923   0.01296  -0.1601   0.5842   1.0000
   7.750   1.5071   0.01968   0.01343  -0.1577   0.5737   1.0000
   8.000   1.5352   0.01965   0.01336  -0.1577   0.5641   1.0000
   8.250   1.5452   0.02017   0.01388  -0.1550   0.5522   1.0000
   8.500   1.5546   0.02080   0.01452  -0.1524   0.5404   1.0000
   8.750   1.5720   0.02120   0.01489  -0.1509   0.5291   1.0000
   9.000   1.5912   0.02158   0.01523  -0.1498   0.5181   1.0000
   9.250   1.5965   0.02250   0.01620  -0.1468   0.5063   1.0000
   9.500   1.6103   0.02317   0.01685  -0.1451   0.4953   1.0000
   9.750   1.6292   0.02364   0.01727  -0.1440   0.4846   1.0000
  10.000   1.6321   0.02478   0.01848  -0.1410   0.4728   1.0000
  10.250   1.6423   0.02568   0.01939  -0.1390   0.4616   1.0000
  10.500   1.6559   0.02642   0.02008  -0.1374   0.4503   1.0000
  10.750   1.6606   0.02761   0.02131  -0.1348   0.4383   1.0000
  11.000   1.6660   0.02883   0.02257  -0.1325   0.4263   1.0000
  11.250   1.6722   0.03001   0.02374  -0.1302   0.4138   1.0000
  11.500   1.6801   0.03113   0.02481  -0.1282   0.4017   1.0000
  11.750   1.6817   0.03266   0.02640  -0.1257   0.3891   1.0000
  12.000   1.6833   0.03425   0.02801  -0.1233   0.3758   1.0000
  12.250   1.6848   0.03590   0.02966  -0.1209   0.3623   1.0000
  12.500   1.6866   0.03760   0.03135  -0.1187   0.3491   1.0000
  12.750   1.6870   0.03945   0.03317  -0.1165   0.3354   1.0000
  13.000   1.6879   0.04136   0.03507  -0.1144   0.3223   1.0000
  13.250   1.6874   0.04349   0.03723  -0.1124   0.3088   1.0000
  13.500   1.6878   0.04561   0.03937  -0.1106   0.2959   1.0000
  13.750   1.6876   0.04783   0.04161  -0.1088   0.2831   1.0000
  14.000   1.6874   0.05012   0.04387  -0.1071   0.2713   1.0000
  14.250   1.6868   0.05252   0.04627  -0.1055   0.2594   1.0000
  14.500   1.6869   0.05495   0.04875  -0.1041   0.2481   1.0000
  14.750   1.6867   0.05744   0.05125  -0.1028   0.2376   1.0000
  15.250   1.6835   0.06290   0.05675  -0.1003   0.2163   1.0000
  15.500   1.6821   0.06571   0.05960  -0.0993   0.2065   1.0000
  15.750   1.6790   0.06871   0.06258  -0.0983   0.1974   1.0000
  16.000   1.6776   0.07168   0.06565  -0.0975   0.1877   1.0000
  16.250   1.6746   0.07484   0.06884  -0.0968   0.1789   1.0000
  16.500   1.6712   0.07812   0.07217  -0.0962   0.1702   1.0000
  16.750   1.6682   0.08144   0.07557  -0.0957   0.1614   1.0000
  17.000   1.6615   0.08525   0.07939  -0.0954   0.1528   1.0000
  17.250   1.6568   0.08893   0.08318  -0.0952   0.1430   1.0000
  17.500   1.6492   0.09306   0.08737  -0.0952   0.1319   1.0000
  17.750   1.6388   0.09766   0.09201  -0.0954   0.1196   1.0000
  18.000   1.6250   0.10283   0.09717  -0.0958   0.1055   1.0000
  18.250   1.6078   0.10859   0.10288  -0.0966   0.0903   1.0000
  18.500   1.5910   0.11437   0.10861  -0.0976   0.0766   1.0000
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