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FX 76-MP-160 (fx76mp160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 76-MP-160 (fx76mp160-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.62 at α=2.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76mp160-il-1000000-n5.txt
Download as CSV file: xf-fx76mp160-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 76-MP-160                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.4095   0.10466   0.10135  -0.1076   0.7983   0.0173
 -16.500  -0.4303   0.09688   0.09349  -0.1124   0.7971   0.0173
 -16.250  -0.4507   0.08935   0.08587  -0.1174   0.7957   0.0174
 -16.000  -0.4735   0.08140   0.07782  -0.1230   0.7942   0.0175
 -15.750  -0.4908   0.07449   0.07082  -0.1284   0.7925   0.0174
 -15.500  -0.5185   0.06599   0.06220  -0.1357   0.7910   0.0175
 -15.250  -0.5449   0.05712   0.05320  -0.1445   0.7894   0.0174
 -15.000  -0.5808   0.04648   0.04238  -0.1553   0.7874   0.0173
 -14.750  -0.6035   0.03640   0.03204  -0.1670   0.7851   0.0172
 -14.500  -0.6056   0.03034   0.02578  -0.1753   0.7829   0.0173
 -14.250  -0.5994   0.02734   0.02267  -0.1791   0.7813   0.0173
 -14.000  -0.5914   0.02521   0.02044  -0.1811   0.7795   0.0174
 -13.750  -0.5855   0.02334   0.01848  -0.1821   0.7776   0.0174
 -13.500  -0.5786   0.02197   0.01702  -0.1820   0.7756   0.0175
 -13.250  -0.5754   0.02091   0.01588  -0.1806   0.7735   0.0176
 -13.000  -0.5644   0.02003   0.01492  -0.1797   0.7718   0.0176
 -12.750  -0.5489   0.01931   0.01412  -0.1790   0.7701   0.0177
 -12.500  -0.5302   0.01875   0.01350  -0.1785   0.7685   0.0179
 -12.250  -0.5104   0.01822   0.01289  -0.1780   0.7669   0.0181
 -12.000  -0.4905   0.01766   0.01225  -0.1775   0.7651   0.0181
 -11.750  -0.4692   0.01713   0.01167  -0.1772   0.7639   0.0182
 -11.500  -0.4481   0.01657   0.01106  -0.1768   0.7629   0.0183
 -11.250  -0.4269   0.01596   0.01039  -0.1764   0.7619   0.0185
 -11.000  -0.4041   0.01544   0.00982  -0.1761   0.7607   0.0186
 -10.750  -0.3808   0.01494   0.00927  -0.1758   0.7594   0.0187
 -10.500  -0.3569   0.01447   0.00875  -0.1756   0.7580   0.0189
 -10.250  -0.3322   0.01405   0.00830  -0.1755   0.7565   0.0191
 -10.000  -0.3072   0.01365   0.00784  -0.1754   0.7550   0.0193
  -9.750  -0.2816   0.01328   0.00743  -0.1753   0.7535   0.0195
  -9.500  -0.2556   0.01295   0.00706  -0.1752   0.7521   0.0196
  -9.250  -0.2293   0.01263   0.00670  -0.1752   0.7508   0.0198
  -9.000  -0.2028   0.01233   0.00637  -0.1752   0.7494   0.0200
  -8.750  -0.1759   0.01206   0.00605  -0.1752   0.7478   0.0202
  -8.500  -0.1488   0.01182   0.00576  -0.1753   0.7458   0.0204
  -8.250  -0.1215   0.01157   0.00548  -0.1753   0.7442   0.0206
  -8.000  -0.0943   0.01132   0.00521  -0.1753   0.7428   0.0208
  -7.750  -0.0669   0.01108   0.00496  -0.1754   0.7411   0.0211
  -7.500  -0.0392   0.01087   0.00473  -0.1755   0.7396   0.0213
  -7.250  -0.0113   0.01066   0.00451  -0.1756   0.7381   0.0217
  -7.000   0.0166   0.01047   0.00431  -0.1757   0.7364   0.0222
  -6.750   0.0444   0.01026   0.00410  -0.1758   0.7343   0.0235
  -6.500   0.0721   0.01006   0.00392  -0.1758   0.7319   0.0251
  -6.250   0.1000   0.00990   0.00378  -0.1759   0.7297   0.0299
  -6.000   0.1282   0.00979   0.00365  -0.1760   0.7277   0.0327
  -5.750   0.1565   0.00971   0.00354  -0.1761   0.7256   0.0340
  -5.500   0.1848   0.00956   0.00340  -0.1762   0.7239   0.0351
  -5.250   0.2131   0.00942   0.00326  -0.1763   0.7217   0.0363
  -5.000   0.2415   0.00930   0.00314  -0.1765   0.7192   0.0376
  -4.750   0.2700   0.00920   0.00303  -0.1766   0.7171   0.0386
  -4.500   0.2984   0.00910   0.00292  -0.1767   0.7151   0.0393
  -4.250   0.3267   0.00898   0.00279  -0.1769   0.7131   0.0402
  -4.000   0.3548   0.00887   0.00267  -0.1769   0.7108   0.0412
  -3.750   0.3828   0.00877   0.00256  -0.1770   0.7081   0.0422
  -3.500   0.4110   0.00868   0.00247  -0.1771   0.7053   0.0430
  -3.250   0.4395   0.00859   0.00239  -0.1772   0.7022   0.0439
  -3.000   0.4676   0.00851   0.00231  -0.1773   0.6986   0.0453
  -2.750   0.4954   0.00841   0.00224  -0.1773   0.6947   0.0486
  -2.500   0.5228   0.00833   0.00217  -0.1772   0.6905   0.0578
  -2.250   0.5505   0.00829   0.00213  -0.1772   0.6864   0.0624
  -2.000   0.5787   0.00822   0.00208  -0.1773   0.6821   0.0659
  -1.750   0.6063   0.00817   0.00203  -0.1772   0.6766   0.0695
  -1.500   0.6330   0.00813   0.00198  -0.1770   0.6705   0.0740
  -1.250   0.6605   0.00807   0.00195  -0.1769   0.6649   0.0802
  -1.000   0.6877   0.00801   0.00194  -0.1768   0.6588   0.0976
  -0.750   0.7141   0.00801   0.00192  -0.1765   0.6525   0.1042
  -0.500   0.7410   0.00801   0.00191  -0.1764   0.6470   0.1087
  -0.250   0.7671   0.00802   0.00192  -0.1760   0.6385   0.1138
   0.000   0.7919   0.00804   0.00195  -0.1755   0.6295   0.1251
   0.250   0.8173   0.00808   0.00198  -0.1750   0.6177   0.1391
   0.500   0.8415   0.00815   0.00202  -0.1743   0.6056   0.1448
   0.750   0.8647   0.00826   0.00208  -0.1734   0.5925   0.1497
   1.000   0.8880   0.00836   0.00215  -0.1725   0.5800   0.1545
   1.250   0.9108   0.00846   0.00223  -0.1715   0.5690   0.1638
   1.500   0.9327   0.00856   0.00234  -0.1704   0.5563   0.1850
   1.750   0.9548   0.00870   0.00244  -0.1693   0.5425   0.1925
   2.000   0.9746   0.00887   0.00257  -0.1678   0.5285   0.2002
   2.500   1.0111   0.00914   0.00285  -0.1641   0.5042   0.2485
   3.000   1.0414   0.00944   0.00319  -0.1592   0.4766   0.3117
   3.250   1.0569   0.00969   0.00340  -0.1569   0.4620   0.3229
   3.500   1.0715   0.00991   0.00365  -0.1545   0.4501   0.3593
   3.750   1.0864   0.01016   0.00390  -0.1521   0.4393   0.3817
   4.000   1.1023   0.01033   0.00415  -0.1500   0.4302   0.4332
   4.250   1.1141   0.01061   0.00448  -0.1472   0.4154   0.4732
   4.500   1.1286   0.01086   0.00478  -0.1449   0.4039   0.5173
   4.750   1.1394   0.01118   0.00518  -0.1420   0.3917   0.5769
   5.000   1.1531   0.01143   0.00557  -0.1397   0.3838   0.6439
   5.250   1.1636   0.01188   0.00605  -0.1368   0.3726   0.6872
   5.500   1.1787   0.01225   0.00645  -0.1348   0.3634   0.7029
   5.750   1.1904   0.01274   0.00697  -0.1323   0.3542   0.7324
   6.000   1.2053   0.01321   0.00741  -0.1304   0.3438   0.7420
   6.250   1.2170   0.01379   0.00797  -0.1281   0.3331   0.7540
   6.500   1.2283   0.01443   0.00858  -0.1257   0.3221   0.7626
   6.750   1.2410   0.01503   0.00917  -0.1236   0.3128   0.7707
   7.000   1.2561   0.01555   0.00970  -0.1219   0.3050   0.7820
   7.250   1.2672   0.01629   0.01039  -0.1197   0.2931   0.7899
   7.500   1.2808   0.01693   0.01101  -0.1180   0.2815   0.7963
   7.750   1.2910   0.01777   0.01177  -0.1158   0.2688   0.8003
   8.000   1.3043   0.01848   0.01245  -0.1141   0.2611   0.8040
   8.250   1.3197   0.01908   0.01307  -0.1127   0.2557   0.8071
   8.500   1.3360   0.01965   0.01365  -0.1114   0.2511   0.8113
   8.750   1.3499   0.02035   0.01435  -0.1098   0.2441   0.8163
   9.000   1.3643   0.02104   0.01506  -0.1084   0.2394   0.8220
   9.250   1.3808   0.02164   0.01569  -0.1073   0.2343   0.8267
   9.750   1.4079   0.02319   0.01722  -0.1044   0.2191   0.8456
  10.000   1.4220   0.02397   0.01802  -0.1031   0.2141   0.8514
  10.250   1.4363   0.02475   0.01883  -0.1019   0.2093   0.8613
  10.500   1.4530   0.02553   0.01968  -0.1011   0.2038   0.8896
  10.750   1.4974   0.02644   0.02069  -0.1062   0.1984   0.9192
  11.000   1.5528   0.02781   0.02208  -0.1141   0.1900   0.9913
  11.250   1.5694   0.02894   0.02320  -0.1136   0.1837   1.0000
  11.500   1.5811   0.03012   0.02434  -0.1124   0.1722   1.0000
  11.750   1.5926   0.03131   0.02549  -0.1112   0.1644   1.0000
  12.000   1.6022   0.03266   0.02680  -0.1098   0.1570   1.0000
  12.250   1.6146   0.03382   0.02797  -0.1088   0.1520   1.0000
  12.500   1.6281   0.03491   0.02908  -0.1079   0.1473   1.0000
  12.750   1.6347   0.03652   0.03064  -0.1064   0.1376   1.0000
  13.000   1.6460   0.03781   0.03195  -0.1054   0.1317   1.0000
  13.250   1.6528   0.03942   0.03351  -0.1040   0.1223   1.0000
  13.500   1.6621   0.04087   0.03495  -0.1028   0.1175   1.0000
  13.750   1.6670   0.04272   0.03678  -0.1014   0.1107   1.0000
  14.000   1.6777   0.04408   0.03817  -0.1004   0.1074   1.0000
  14.250   1.6869   0.04560   0.03970  -0.0994   0.1029   1.0000
  14.500   1.6906   0.04759   0.04169  -0.0981   0.0970   1.0000
  14.750   1.6988   0.04919   0.04331  -0.0971   0.0930   1.0000
  15.000   1.7040   0.05112   0.04524  -0.0959   0.0869   1.0000
  15.250   1.7059   0.05333   0.04744  -0.0946   0.0809   1.0000
  15.500   1.7097   0.05542   0.04953  -0.0935   0.0767   1.0000
  15.750   1.7129   0.05757   0.05171  -0.0924   0.0737   1.0000
  16.000   1.7183   0.05950   0.05366  -0.0915   0.0708   1.0000
  16.250   1.7226   0.06162   0.05584  -0.0906   0.0684   1.0000
  16.500   1.7246   0.06393   0.05817  -0.0896   0.0650   1.0000
  17.000   1.7275   0.06878   0.06309  -0.0878   0.0586   1.0000
  17.500   1.7174   0.07499   0.06931  -0.0858   0.0476   1.0000
  17.750   1.7122   0.07822   0.07257  -0.0850   0.0444   1.0000
  18.000   1.7118   0.08095   0.07534  -0.0844   0.0425   1.0000
  18.250   1.7084   0.08410   0.07855  -0.0839   0.0409   1.0000
  18.500   1.7028   0.08749   0.08198  -0.0834   0.0389   1.0000
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