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FX 76-MP-140 (fx76mp140-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 76-MP-140 (fx76mp140-il)
Reynolds number: 200,000
Max Cl/Cd: 78.27 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76mp140-il-200000-n5.txt
Download as CSV file: xf-fx76mp140-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000   0.1124   0.10599   0.10094  -0.1467   0.8367   0.0250
 -11.750   0.1167   0.10265   0.09760  -0.1483   0.8342   0.0261
 -11.500   0.1150   0.09837   0.09332  -0.1507   0.8317   0.0267
 -11.000   0.1349   0.09351   0.08844  -0.1529   0.8276   0.0271
 -10.750   0.1458   0.09128   0.08618  -0.1541   0.8258   0.0277
 -10.500   0.1544   0.08887   0.08377  -0.1554   0.8239   0.0290
 -10.250   0.1577   0.08587   0.08080  -0.1564   0.8215   0.0285
 -10.000   0.1613   0.08312   0.07807  -0.1574   0.8187   0.0297
  -9.750   0.1588   0.07936   0.07432  -0.1591   0.8160   0.0305
  -9.500   0.1602   0.07605   0.07102  -0.1604   0.8134   0.0306
  -9.250   0.1628   0.07307   0.06806  -0.1615   0.8111   0.0315
  -9.000   0.1720   0.07124   0.06620  -0.1622   0.8092   0.0320
  -8.750   0.1801   0.06921   0.06416  -0.1631   0.8073   0.0331
  -8.500   0.1773   0.06620   0.06121  -0.1635   0.8045   0.0331
  -8.250   0.1720   0.06300   0.05807  -0.1640   0.8012   0.0333
  -8.000   0.1643   0.05963   0.05475  -0.1644   0.7978   0.0336
  -7.750   0.1484   0.05590   0.05107  -0.1648   0.7945   0.0334
  -7.500   0.0578   0.03135   0.02568  -0.1848   0.7884   0.0344
  -7.250   0.0624   0.02641   0.01986  -0.1862   0.7849   0.0359
  -7.000   0.0835   0.02539   0.01872  -0.1861   0.7823   0.0366
  -6.750   0.1067   0.02459   0.01781  -0.1861   0.7801   0.0374
  -6.500   0.1309   0.02361   0.01663  -0.1863   0.7781   0.0383
  -6.250   0.1566   0.02254   0.01530  -0.1867   0.7762   0.0396
  -6.000   0.1835   0.02147   0.01388  -0.1871   0.7746   0.0414
  -5.750   0.2113   0.02090   0.01323  -0.1876   0.7731   0.0429
  -5.500   0.2331   0.02059   0.01291  -0.1869   0.7704   0.0443
  -5.250   0.2560   0.02013   0.01234  -0.1863   0.7675   0.0460
  -5.000   0.2808   0.01958   0.01161  -0.1860   0.7649   0.0479
  -4.750   0.3066   0.01916   0.01117  -0.1859   0.7626   0.0497
  -4.500   0.3337   0.01888   0.01084  -0.1860   0.7607   0.0522
  -4.250   0.3621   0.01849   0.01032  -0.1862   0.7589   0.0551
  -4.000   0.3912   0.01809   0.00987  -0.1866   0.7572   0.0577
  -3.750   0.4176   0.01789   0.00965  -0.1865   0.7550   0.0608
  -3.500   0.4382   0.01780   0.00953  -0.1853   0.7512   0.0639
  -3.250   0.4625   0.01757   0.00931  -0.1849   0.7482   0.0672
  -3.000   0.4889   0.01738   0.00910  -0.1847   0.7456   0.0712
  -2.750   0.5168   0.01714   0.00880  -0.1848   0.7435   0.0751
  -2.500   0.5459   0.01685   0.00852  -0.1852   0.7417   0.0802
  -2.250   0.5762   0.01662   0.00822  -0.1857   0.7400   0.0859
  -2.000   0.5963   0.01660   0.00829  -0.1845   0.7362   0.0916
  -1.750   0.6185   0.01659   0.00828  -0.1835   0.7325   0.0992
  -1.500   0.6445   0.01643   0.00816  -0.1833   0.7295   0.1082
  -1.250   0.6728   0.01624   0.00797  -0.1834   0.7270   0.1200
  -1.000   0.7029   0.01602   0.00778  -0.1839   0.7250   0.1374
  -0.750   0.7310   0.01587   0.00767  -0.1841   0.7226   0.1595
  -0.500   0.7476   0.01600   0.00792  -0.1822   0.7176   0.1823
  -0.250   0.7717   0.01591   0.00794  -0.1816   0.7141   0.2171
   0.000   0.7992   0.01569   0.00786  -0.1817   0.7114   0.2685
   0.250   0.8289   0.01537   0.00774  -0.1822   0.7091   0.3492
   0.500   0.8523   0.01505   0.00783  -0.1816   0.7058   0.4853
   0.750   0.8631   0.01492   0.00826  -0.1782   0.7004   0.6654
   1.000   0.8831   0.01480   0.00833  -0.1762   0.6966   0.7740
   1.250   0.9086   0.01465   0.00821  -0.1754   0.6938   0.8262
   1.500   0.9325   0.01456   0.00813  -0.1744   0.6906   0.8631
   1.750   0.9460   0.01473   0.00838  -0.1716   0.6846   0.8990
   2.000   0.9796   0.01456   0.00823  -0.1728   0.6807   1.0000
   2.250   1.0111   0.01448   0.00806  -0.1735   0.6774   1.0000
   2.500   1.0298   0.01469   0.00825  -0.1720   0.6714   1.0000
   2.750   1.0521   0.01480   0.00833  -0.1711   0.6658   1.0000
   3.000   1.0828   0.01473   0.00819  -0.1716   0.6619   1.0000
   3.250   1.1008   0.01496   0.00841  -0.1700   0.6558   1.0000
   3.500   1.1206   0.01511   0.00854  -0.1686   0.6500   1.0000
   3.750   1.1521   0.01504   0.00841  -0.1693   0.6458   1.0000
   4.000   1.1637   0.01537   0.00876  -0.1665   0.6382   1.0000
   4.250   1.1879   0.01545   0.00880  -0.1659   0.6323   1.0000
   4.500   1.2096   0.01560   0.00892  -0.1649   0.6258   1.0000
   4.750   1.2272   0.01583   0.00915  -0.1631   0.6177   1.0000
   5.000   1.2500   0.01597   0.00925  -0.1623   0.6107   1.0000
   5.250   1.2664   0.01627   0.00954  -0.1605   0.6018   1.0000
   5.500   1.2874   0.01649   0.00974  -0.1595   0.5943   1.0000
   5.750   1.3057   0.01678   0.01002  -0.1580   0.5853   1.0000
   6.000   1.3244   0.01710   0.01033  -0.1567   0.5769   1.0000
   6.250   1.3447   0.01737   0.01055  -0.1556   0.5674   1.0000
   6.500   1.3592   0.01786   0.01104  -0.1537   0.5568   1.0000
   6.750   1.3776   0.01823   0.01137  -0.1524   0.5464   1.0000
   7.000   1.3938   0.01871   0.01180  -0.1508   0.5350   1.0000
   7.250   1.4070   0.01932   0.01239  -0.1489   0.5225   1.0000
   7.500   1.4203   0.01997   0.01300  -0.1470   0.5094   1.0000
   7.750   1.4351   0.02059   0.01358  -0.1453   0.4981   1.0000
   8.000   1.4484   0.02131   0.01427  -0.1436   0.4866   1.0000
   8.250   1.4610   0.02210   0.01507  -0.1418   0.4755   1.0000
   8.500   1.4731   0.02292   0.01586  -0.1401   0.4638   1.0000
   8.750   1.4846   0.02380   0.01669  -0.1382   0.4517   1.0000
   9.000   1.4948   0.02478   0.01768  -0.1363   0.4395   1.0000
   9.250   1.5059   0.02574   0.01864  -0.1346   0.4285   1.0000
   9.500   1.5164   0.02675   0.01963  -0.1328   0.4177   1.0000
   9.750   1.5274   0.02778   0.02069  -0.1312   0.4072   1.0000
  10.000   1.5378   0.02884   0.02177  -0.1295   0.3972   1.0000
  10.250   1.5475   0.02995   0.02288  -0.1278   0.3870   1.0000
  10.500   1.5573   0.03111   0.02408  -0.1262   0.3768   1.0000
  10.750   1.5664   0.03232   0.02529  -0.1245   0.3669   1.0000
  11.000   1.5744   0.03364   0.02662  -0.1228   0.3562   1.0000
  11.250   1.5823   0.03500   0.02801  -0.1212   0.3451   1.0000
  11.500   1.5886   0.03650   0.02952  -0.1194   0.3338   1.0000
  11.750   1.5943   0.03808   0.03109  -0.1177   0.3226   1.0000
  12.000   1.6001   0.03971   0.03275  -0.1161   0.3104   1.0000
  12.250   1.6048   0.04146   0.03451  -0.1145   0.2983   1.0000
  12.500   1.6082   0.04337   0.03642  -0.1128   0.2860   1.0000
  12.750   1.6095   0.04552   0.03854  -0.1111   0.2717   1.0000
  13.000   1.6105   0.04774   0.04075  -0.1095   0.2584   1.0000
  13.250   1.6128   0.04991   0.04293  -0.1080   0.2454   1.0000
  13.500   1.6148   0.05217   0.04519  -0.1067   0.2333   1.0000
  13.750   1.6155   0.05460   0.04762  -0.1053   0.2211   1.0000
  14.000   1.6157   0.05712   0.05013  -0.1040   0.2107   1.0000
  14.250   1.6167   0.05963   0.05267  -0.1029   0.1998   1.0000
  14.500   1.6187   0.06206   0.05514  -0.1019   0.1904   1.0000
  14.750   1.6177   0.06487   0.05796  -0.1008   0.1813   1.0000
  15.000   1.6197   0.06741   0.06054  -0.1000   0.1725   1.0000
  15.250   1.6193   0.07025   0.06341  -0.0992   0.1643   1.0000
  15.500   1.6173   0.07332   0.06650  -0.0984   0.1554   1.0000
  15.750   1.6173   0.07620   0.06944  -0.0978   0.1466   1.0000
  16.000   1.6145   0.07949   0.07275  -0.0972   0.1387   1.0000
  16.250   1.6128   0.08270   0.07602  -0.0968   0.1289   1.0000
  16.500   1.6109   0.08598   0.07934  -0.0965   0.1202   1.0000
  16.750   1.6061   0.08967   0.08305  -0.0963   0.1110   1.0000
  17.000   1.6006   0.09352   0.08692  -0.0963   0.1014   1.0000
  17.250   1.5966   0.09722   0.09067  -0.0963   0.0908   1.0000
  17.750   1.5794   0.10607   0.09951  -0.0971   0.0676   1.0000
  18.000   1.5695   0.11077   0.10420  -0.0977   0.0572   1.0000
  18.250   1.5597   0.11552   0.10895  -0.0985   0.0497   1.0000
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