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FX 76-MP-120 (fx76mp120-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 76-MP-120 (fx76mp120-il)
Reynolds number: 1,000,000
Max Cl/Cd: 192.61 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76mp120-il-1000000.txt
Download as CSV file: xf-fx76mp120-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 76-MP-120                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250   0.2024   0.08474   0.08194  -0.1471   0.7975   0.0137
 -11.000   0.2090   0.08192   0.07913  -0.1480   0.7959   0.0140
 -10.750   0.2088   0.07788   0.07510  -0.1497   0.7942   0.0150
 -10.500   0.2143   0.07492   0.07213  -0.1507   0.7924   0.0150
 -10.250   0.2175   0.07137   0.06859  -0.1518   0.7906   0.0151
 -10.000   0.1738   0.08553   0.08260  -0.1563   0.7976   0.0151
  -9.750   0.1813   0.08231   0.07939  -0.1581   0.7957   0.0151
  -9.500   0.1911   0.07965   0.07674  -0.1596   0.7936   0.0151
  -9.250   0.1987   0.07677   0.07386  -0.1605   0.7917   0.0156
  -9.000  -0.0306   0.02023   0.01656  -0.2057   0.7820   0.0122
  -8.750  -0.0087   0.01833   0.01445  -0.2071   0.7800   0.0126
  -8.500   0.0165   0.01739   0.01340  -0.2078   0.7782   0.0129
  -8.250   0.0429   0.01690   0.01283  -0.2082   0.7763   0.0134
  -8.000   0.0690   0.01605   0.01184  -0.2088   0.7745   0.0139
  -7.750   0.0958   0.01527   0.01088  -0.2094   0.7725   0.0144
  -7.500   0.1232   0.01448   0.00989  -0.2100   0.7703   0.0148
  -7.250   0.1500   0.01392   0.00923  -0.2103   0.7689   0.0151
  -7.000   0.1758   0.01248   0.00756  -0.2109   0.7671   0.0160
  -6.750   0.2033   0.01205   0.00707  -0.2112   0.7652   0.0165
  -6.500   0.2312   0.01173   0.00670  -0.2114   0.7633   0.0173
  -6.250   0.2592   0.01136   0.00624  -0.2117   0.7614   0.0180
  -6.000   0.2873   0.01105   0.00584  -0.2119   0.7596   0.0187
  -5.750   0.3154   0.01052   0.00520  -0.2122   0.7577   0.0198
  -5.500   0.3442   0.01032   0.00495  -0.2126   0.7554   0.0210
  -5.250   0.3719   0.01011   0.00472  -0.2127   0.7538   0.0223
  -5.000   0.3998   0.00990   0.00447  -0.2128   0.7519   0.0234
  -4.750   0.4276   0.00949   0.00401  -0.2130   0.7499   0.0253
  -4.500   0.4558   0.00935   0.00386  -0.2131   0.7478   0.0273
  -4.250   0.4841   0.00928   0.00376  -0.2132   0.7458   0.0291
  -4.000   0.5123   0.00897   0.00342  -0.2135   0.7438   0.0322
  -3.750   0.5410   0.00891   0.00331  -0.2137   0.7414   0.0347
  -3.500   0.5690   0.00877   0.00315  -0.2138   0.7392   0.0370
  -3.250   0.5966   0.00858   0.00298  -0.2138   0.7370   0.0405
  -3.000   0.6244   0.00850   0.00290  -0.2139   0.7345   0.0434
  -2.750   0.6524   0.00834   0.00271  -0.2140   0.7321   0.0470
  -2.500   0.6803   0.00824   0.00262  -0.2141   0.7297   0.0511
  -2.250   0.7087   0.00822   0.00255  -0.2142   0.7273   0.0543
  -2.000   0.7369   0.00809   0.00243  -0.2144   0.7248   0.0608
  -1.750   0.7642   0.00802   0.00237  -0.2143   0.7224   0.0654
  -1.500   0.7917   0.00790   0.00228  -0.2143   0.7196   0.0732
  -1.250   0.8193   0.00785   0.00223  -0.2143   0.7167   0.0797
  -1.000   0.8469   0.00776   0.00216  -0.2144   0.7138   0.0912
  -0.750   0.8751   0.00774   0.00213  -0.2145   0.7107   0.1039
  -0.500   0.9019   0.00766   0.00211  -0.2144   0.7079   0.1191
  -0.250   0.9290   0.00759   0.00209  -0.2143   0.7046   0.1405
   0.000   0.9560   0.00750   0.00209  -0.2143   0.7013   0.1760
   0.250   0.9832   0.00742   0.00209  -0.2143   0.6981   0.2250
   0.500   1.0100   0.00730   0.00214  -0.2143   0.6948   0.3021
   0.750   1.0359   0.00708   0.00221  -0.2141   0.6910   0.4235
   1.000   1.0600   0.00670   0.00234  -0.2137   0.6873   0.6592
   1.250   1.0838   0.00659   0.00245  -0.2128   0.6834   0.7817
   1.500   1.1083   0.00658   0.00252  -0.2121   0.6794   0.8266
   1.750   1.1322   0.00654   0.00257  -0.2112   0.6747   0.8642
   2.000   1.1552   0.00651   0.00259  -0.2102   0.6700   0.9009
   2.250   1.1890   0.00645   0.00260  -0.2116   0.6654   1.0000
   2.500   1.2156   0.00651   0.00265  -0.2115   0.6602   1.0000
   2.750   1.2414   0.00659   0.00269  -0.2112   0.6546   1.0000
   3.000   1.2672   0.00668   0.00276  -0.2109   0.6487   1.0000
   3.250   1.2928   0.00676   0.00283  -0.2106   0.6423   1.0000
   3.500   1.3175   0.00688   0.00290  -0.2101   0.6358   1.0000
   3.750   1.3425   0.00697   0.00299  -0.2097   0.6285   1.0000
   4.000   1.3662   0.00711   0.00310  -0.2089   0.6207   1.0000
   4.250   1.3899   0.00724   0.00320  -0.2082   0.6117   1.0000
   4.500   1.4126   0.00740   0.00333  -0.2074   0.6021   1.0000
   4.750   1.4339   0.00759   0.00348  -0.2062   0.5921   1.0000
   5.000   1.4557   0.00777   0.00363  -0.2051   0.5814   1.0000
   5.250   1.4766   0.00797   0.00380  -0.2039   0.5709   1.0000
   5.500   1.4951   0.00820   0.00399  -0.2022   0.5595   1.0000
   5.750   1.5107   0.00847   0.00421  -0.1998   0.5474   1.0000
   6.000   1.5266   0.00875   0.00446  -0.1976   0.5343   1.0000
   6.250   1.5426   0.00906   0.00472  -0.1955   0.5209   1.0000
   6.500   1.5585   0.00937   0.00501  -0.1933   0.5086   1.0000
   6.750   1.5737   0.00973   0.00532  -0.1911   0.4963   1.0000
   7.000   1.5872   0.01014   0.00570  -0.1886   0.4826   1.0000
   7.250   1.6007   0.01060   0.00611  -0.1862   0.4700   1.0000
   7.500   1.6134   0.01111   0.00658  -0.1837   0.4572   1.0000
   7.750   1.6272   0.01163   0.00707  -0.1816   0.4438   1.0000
   8.000   1.6405   0.01221   0.00763  -0.1794   0.4302   1.0000
   8.250   1.6538   0.01285   0.00825  -0.1774   0.4170   1.0000
   8.500   1.6669   0.01357   0.00893  -0.1754   0.4037   1.0000
   8.750   1.6797   0.01436   0.00969  -0.1736   0.3904   1.0000
   9.000   1.6913   0.01530   0.01058  -0.1716   0.3745   1.0000
   9.250   1.6995   0.01650   0.01170  -0.1694   0.3539   1.0000
   9.500   1.7049   0.01794   0.01301  -0.1669   0.3282   1.0000
   9.750   1.7096   0.01946   0.01441  -0.1644   0.3048   1.0000
  10.000   1.7144   0.02097   0.01581  -0.1619   0.2807   1.0000
  10.250   1.7205   0.02242   0.01717  -0.1597   0.2625   1.0000
  10.500   1.7258   0.02390   0.01858  -0.1574   0.2441   1.0000
  10.750   1.7322   0.02532   0.01994  -0.1552   0.2280   1.0000
  11.000   1.7360   0.02694   0.02147  -0.1528   0.2090   1.0000
  11.250   1.7421   0.02840   0.02290  -0.1507   0.1959   1.0000
  11.500   1.7452   0.03010   0.02451  -0.1483   0.1790   1.0000
  11.750   1.7497   0.03174   0.02611  -0.1462   0.1654   1.0000
  12.000   1.7497   0.03372   0.02800  -0.1437   0.1479   1.0000
  12.250   1.7518   0.03559   0.02980  -0.1414   0.1330   1.0000
  12.500   1.7527   0.03759   0.03175  -0.1391   0.1178   1.0000
  12.750   1.7517   0.03978   0.03385  -0.1367   0.1008   1.0000
  13.000   1.7489   0.04215   0.03614  -0.1343   0.0855   1.0000
  13.250   1.7442   0.04474   0.03864  -0.1317   0.0692   1.0000
  13.500   1.7402   0.04734   0.04117  -0.1294   0.0548   1.0000
  13.750   1.7370   0.04993   0.04372  -0.1272   0.0440   1.0000
  14.000   1.7327   0.05266   0.04641  -0.1251   0.0341   1.0000
  14.250   1.7291   0.05539   0.04911  -0.1232   0.0258   1.0000
  14.500   1.7268   0.05809   0.05182  -0.1214   0.0200   1.0000
  14.750   1.7239   0.06091   0.05465  -0.1198   0.0153   1.0000
  15.000   1.7214   0.06371   0.05748  -0.1182   0.0121   1.0000
  15.250   1.7215   0.06633   0.06015  -0.1170   0.0104   1.0000
  15.500   1.7186   0.06935   0.06323  -0.1157   0.0087   1.0000
  15.750   1.7195   0.07201   0.06596  -0.1148   0.0079   1.0000
  16.000   1.7172   0.07513   0.06913  -0.1138   0.0072   1.0000
  16.250   1.7138   0.07840   0.07249  -0.1129   0.0066   1.0000
  16.500   1.7143   0.08127   0.07544  -0.1123   0.0063   1.0000
  16.750   1.7138   0.08434   0.07860  -0.1118   0.0060   1.0000
  17.000   1.7127   0.08756   0.08190  -0.1114   0.0057   1.0000
  17.250   1.7100   0.09105   0.08547  -0.1111   0.0054   1.0000
  17.500   1.7069   0.09466   0.08917  -0.1110   0.0053   1.0000
  17.750   1.6981   0.09916   0.09377  -0.1111   0.0050   1.0000
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