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FX 76-MP-160 (fx76mp160-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 76-MP-160 (fx76mp160-il)
Reynolds number: 500,000
Max Cl/Cd: 109.31 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76mp160-il-500000-n5.txt
Download as CSV file: xf-fx76mp160-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.3622   0.07606   0.07180  -0.1407   0.8188   0.0219
 -15.000  -0.3919   0.06738   0.06297  -0.1473   0.8167   0.0218
 -14.500  -0.4348   0.05328   0.04863  -0.1592   0.8124   0.0219
 -14.000  -0.4598   0.04118   0.03623  -0.1706   0.8079   0.0217
 -13.500  -0.4715   0.03134   0.02604  -0.1811   0.8030   0.0219
 -13.250  -0.4726   0.02854   0.02313  -0.1831   0.8006   0.0220
 -13.000  -0.4712   0.02658   0.02108  -0.1836   0.7980   0.0220
 -12.750  -0.4716   0.02486   0.01928  -0.1831   0.7951   0.0221
 -12.500  -0.4710   0.02359   0.01793  -0.1816   0.7927   0.0221
 -12.250  -0.4696   0.02254   0.01679  -0.1799   0.7904   0.0223
 -12.000  -0.4582   0.02166   0.01583  -0.1789   0.7885   0.0224
 -11.750  -0.4439   0.02087   0.01495  -0.1781   0.7867   0.0227
 -11.500  -0.4269   0.02017   0.01416  -0.1774   0.7851   0.0228
 -11.250  -0.4080   0.01953   0.01344  -0.1769   0.7834   0.0231
 -11.000  -0.3885   0.01893   0.01278  -0.1764   0.7821   0.0232
 -10.750  -0.3680   0.01836   0.01215  -0.1759   0.7807   0.0234
 -10.500  -0.3463   0.01783   0.01158  -0.1755   0.7792   0.0237
 -10.250  -0.3238   0.01733   0.01103  -0.1751   0.7776   0.0240
 -10.000  -0.3007   0.01687   0.01050  -0.1748   0.7760   0.0243
  -9.750  -0.2768   0.01643   0.01001  -0.1746   0.7743   0.0246
  -9.500  -0.2525   0.01602   0.00954  -0.1744   0.7725   0.0250
  -9.250  -0.2277   0.01562   0.00909  -0.1742   0.7709   0.0254
  -9.000  -0.2021   0.01527   0.00870  -0.1742   0.7694   0.0259
  -8.750  -0.1760   0.01497   0.00836  -0.1742   0.7680   0.0266
  -8.500  -0.1495   0.01468   0.00804  -0.1742   0.7666   0.0275
  -8.250  -0.1226   0.01442   0.00774  -0.1743   0.7652   0.0287
  -8.000  -0.0958   0.01417   0.00744  -0.1743   0.7638   0.0299
  -7.750  -0.0694   0.01393   0.00719  -0.1742   0.7626   0.0316
  -7.500  -0.0428   0.01371   0.00693  -0.1741   0.7609   0.0334
  -7.250  -0.0161   0.01347   0.00667  -0.1741   0.7591   0.0348
  -7.000   0.0107   0.01323   0.00640  -0.1740   0.7572   0.0362
  -6.750   0.0378   0.01302   0.00615  -0.1740   0.7552   0.0379
  -6.500   0.0652   0.01284   0.00592  -0.1740   0.7532   0.0392
  -6.250   0.0923   0.01255   0.00561  -0.1741   0.7511   0.0408
  -6.000   0.1200   0.01233   0.00536  -0.1742   0.7491   0.0423
  -5.750   0.1481   0.01215   0.00513  -0.1743   0.7473   0.0437
  -5.500   0.1765   0.01200   0.00494  -0.1745   0.7456   0.0448
  -5.250   0.2043   0.01183   0.00478  -0.1746   0.7440   0.0463
  -5.000   0.2312   0.01166   0.00464  -0.1746   0.7421   0.0484
  -4.750   0.2585   0.01151   0.00451  -0.1745   0.7398   0.0501
  -4.500   0.2859   0.01137   0.00438  -0.1745   0.7372   0.0528
  -4.250   0.3136   0.01124   0.00425  -0.1745   0.7346   0.0560
  -4.000   0.3415   0.01112   0.00413  -0.1745   0.7322   0.0605
  -3.750   0.3697   0.01100   0.00399  -0.1746   0.7299   0.0639
  -3.500   0.3981   0.01088   0.00384  -0.1748   0.7278   0.0674
  -3.250   0.4269   0.01080   0.00373  -0.1750   0.7257   0.0703
  -3.000   0.4539   0.01067   0.00365  -0.1749   0.7234   0.0749
  -2.750   0.4810   0.01051   0.00360  -0.1749   0.7207   0.0862
  -2.500   0.5083   0.01041   0.00352  -0.1748   0.7174   0.0996
  -2.250   0.5359   0.01032   0.00343  -0.1747   0.7139   0.1067
  -2.000   0.5638   0.01020   0.00334  -0.1748   0.7109   0.1142
  -1.750   0.5920   0.01010   0.00326  -0.1749   0.7079   0.1256
  -1.500   0.6191   0.01005   0.00323  -0.1748   0.7044   0.1380
  -1.250   0.6459   0.01000   0.00320  -0.1746   0.7001   0.1441
  -1.000   0.6730   0.00994   0.00316  -0.1744   0.6961   0.1526
  -0.750   0.7004   0.00986   0.00312  -0.1744   0.6923   0.1628
  -0.500   0.7278   0.00980   0.00306  -0.1743   0.6881   0.1772
  -0.250   0.7538   0.00977   0.00308  -0.1740   0.6825   0.1909
   0.000   0.7799   0.00973   0.00306  -0.1736   0.6764   0.1995
   0.250   0.8062   0.00969   0.00303  -0.1733   0.6707   0.2127
   0.500   0.8324   0.00963   0.00306  -0.1731   0.6656   0.2409
   0.750   0.8584   0.00961   0.00309  -0.1728   0.6599   0.2598
   1.000   0.8836   0.00955   0.00310  -0.1723   0.6531   0.2938
   1.250   0.9085   0.00953   0.00313  -0.1718   0.6457   0.3245
   1.500   0.9320   0.00949   0.00317  -0.1710   0.6359   0.3719
   1.750   0.9553   0.00944   0.00324  -0.1703   0.6264   0.4282
   2.000   0.9778   0.00939   0.00332  -0.1693   0.6159   0.4919
   2.250   0.9994   0.00937   0.00343  -0.1682   0.6047   0.5593
   2.500   1.0183   0.00938   0.00361  -0.1664   0.5926   0.6407
   2.750   1.0373   0.00949   0.00380  -0.1647   0.5812   0.6927
   3.000   1.0538   0.00967   0.00400  -0.1624   0.5696   0.7186
   3.250   1.0678   0.00989   0.00417  -0.1596   0.5566   0.7378
   3.500   1.0830   0.01010   0.00436  -0.1571   0.5437   0.7505
   3.750   1.0954   0.01041   0.00461  -0.1541   0.5295   0.7599
   4.250   1.1170   0.01112   0.00523  -0.1477   0.5035   0.7767
   4.500   1.1282   0.01151   0.00557  -0.1447   0.4920   0.7846
   4.750   1.1405   0.01189   0.00592  -0.1420   0.4785   0.7912
   5.000   1.1525   0.01231   0.00631  -0.1393   0.4668   0.7988
   5.250   1.1607   0.01285   0.00679  -0.1361   0.4541   0.8057
   5.500   1.1728   0.01330   0.00724  -0.1335   0.4439   0.8126
   5.750   1.1818   0.01389   0.00780  -0.1306   0.4334   0.8204
   6.000   1.1943   0.01440   0.00832  -0.1283   0.4211   0.8266
   6.250   1.2053   0.01502   0.00890  -0.1259   0.4095   0.8323
   6.500   1.2157   0.01570   0.00954  -0.1235   0.3974   0.8382
   6.750   1.2263   0.01641   0.01022  -0.1212   0.3859   0.8455
   7.000   1.2377   0.01715   0.01092  -0.1191   0.3770   0.8512
   7.500   1.2680   0.01840   0.01221  -0.1162   0.3582   0.8696
   7.750   1.2842   0.01903   0.01286  -0.1149   0.3497   0.8851
   8.000   1.3050   0.01978   0.01365  -0.1149   0.3380   0.9078
   8.500   1.3410   0.02164   0.01544  -0.1144   0.3156   1.0000
   8.750   1.3571   0.02238   0.01617  -0.1134   0.3068   1.0000
   9.000   1.3689   0.02338   0.01712  -0.1119   0.2975   1.0000
   9.250   1.3850   0.02413   0.01788  -0.1109   0.2880   1.0000
   9.500   1.3977   0.02512   0.01882  -0.1095   0.2786   1.0000
   9.750   1.4099   0.02614   0.01981  -0.1082   0.2689   1.0000
  10.000   1.4218   0.02720   0.02083  -0.1068   0.2611   1.0000
  10.250   1.4368   0.02808   0.02172  -0.1058   0.2558   1.0000
  10.500   1.4516   0.02899   0.02265  -0.1049   0.2499   1.0000
  10.750   1.4641   0.03006   0.02371  -0.1037   0.2434   1.0000
  11.000   1.4780   0.03104   0.02470  -0.1027   0.2380   1.0000
  11.250   1.4934   0.03193   0.02562  -0.1018   0.2319   1.0000
  11.500   1.5047   0.03315   0.02683  -0.1006   0.2240   1.0000
  11.750   1.5173   0.03427   0.02795  -0.0996   0.2187   1.0000
  12.000   1.5298   0.03541   0.02910  -0.0986   0.2129   1.0000
  12.250   1.5399   0.03677   0.03046  -0.0974   0.2075   1.0000
  12.500   1.5512   0.03804   0.03174  -0.0964   0.2026   1.0000
  12.750   1.5643   0.03918   0.03292  -0.0956   0.1969   1.0000
  13.000   1.5745   0.04056   0.03431  -0.0945   0.1914   1.0000
  13.250   1.5827   0.04216   0.03591  -0.0934   0.1858   1.0000
  13.500   1.5945   0.04344   0.03723  -0.0925   0.1773   1.0000
  13.750   1.6002   0.04528   0.03903  -0.0913   0.1679   1.0000
  14.000   1.6057   0.04716   0.04089  -0.0902   0.1597   1.0000
  14.250   1.6117   0.04902   0.04274  -0.0891   0.1542   1.0000
  14.500   1.6206   0.05065   0.04443  -0.0883   0.1494   1.0000
  14.750   1.6284   0.05240   0.04622  -0.0875   0.1442   1.0000
  15.000   1.6326   0.05452   0.04834  -0.0865   0.1385   1.0000
  15.250   1.6395   0.05642   0.05028  -0.0857   0.1332   1.0000
  15.500   1.6427   0.05867   0.05253  -0.0849   0.1243   1.0000
  15.750   1.6429   0.06131   0.05517  -0.0840   0.1171   1.0000
  16.000   1.6440   0.06388   0.05774  -0.0832   0.1114   1.0000
  16.250   1.6465   0.06638   0.06028  -0.0826   0.1079   1.0000
  16.500   1.6515   0.06859   0.06255  -0.0821   0.1039   1.0000
  16.750   1.6532   0.07122   0.06523  -0.0816   0.0996   1.0000
  17.000   1.6517   0.07427   0.06830  -0.0811   0.0948   1.0000
  17.250   1.6543   0.07688   0.07099  -0.0808   0.0907   1.0000
  17.500   1.6532   0.07998   0.07410  -0.0805   0.0847   1.0000
  17.750   1.6502   0.08336   0.07752  -0.0804   0.0804   1.0000
  18.000   1.6474   0.08676   0.08095  -0.0804   0.0765   1.0000
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