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FX 76-MP-160 (fx76mp160-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX 76-MP-160 (fx76mp160-il)
Reynolds number: 200,000
Max Cl/Cd: 76.28 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76mp160-il-200000.txt
Download as CSV file: xf-fx76mp160-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000   0.1034   0.10547   0.10108  -0.1490   0.9232   0.0736
 -11.750   0.1119   0.10284   0.09844  -0.1510   0.9197   0.0757
 -11.500   0.0894   0.09890   0.09452  -0.1579   0.9152   0.0783
 -11.250   0.1167   0.09601   0.09160  -0.1578   0.9133   0.0789
 -11.000   0.1379   0.09348   0.08903  -0.1593   0.9112   0.0798
 -10.750   0.1533   0.09115   0.08667  -0.1608   0.9088   0.0812
 -10.500   0.1578   0.08913   0.08467  -0.1609   0.9054   0.0830
 -10.000   0.1449   0.08259   0.07818  -0.1656   0.8975   0.0874
  -9.750  -0.0927   0.04744   0.04282  -0.1810   0.8815   0.0559
  -9.500  -0.1094   0.04534   0.04063  -0.1797   0.8772   0.0556
  -9.250  -0.1345   0.04358   0.03875  -0.1764   0.8723   0.0554
  -9.000  -0.1581   0.04239   0.03746  -0.1716   0.8660   0.0552
  -8.750  -0.1686   0.03929   0.03399  -0.1703   0.8613   0.0551
  -8.500  -0.1643   0.03612   0.03034  -0.1703   0.8584   0.0552
  -8.250  -0.1941   0.03667   0.03084  -0.1617   0.8497   0.0552
  -8.000  -0.1926   0.03505   0.02887  -0.1593   0.8455   0.0555
  -7.750  -0.1720   0.03300   0.02646  -0.1598   0.8432   0.0565
  -7.500  -0.1406   0.03206   0.02551  -0.1612   0.8419   0.0580
  -7.250  -0.1084   0.03091   0.02418  -0.1627   0.8406   0.0603
  -7.000  -0.1686   0.03290   0.02628  -0.1483   0.8281   0.0591
  -6.750  -0.1419   0.03176   0.02482  -0.1489   0.8260   0.0615
  -6.500  -0.1079   0.03038   0.02324  -0.1507   0.8246   0.0643
  -6.250  -0.0686   0.02936   0.02208  -0.1530   0.8236   0.0684
  -6.000  -0.0929   0.03015   0.02280  -0.1446   0.8132   0.0690
  -5.750  -0.0679   0.02939   0.02202  -0.1445   0.8096   0.0727
  -5.500  -0.0366   0.02889   0.02139  -0.1454   0.8076   0.0771
  -5.250  -0.0017   0.02827   0.02078  -0.1468   0.8062   0.0810
  -5.000   0.0366   0.02784   0.02023  -0.1487   0.8052   0.0856
  -4.750   0.0761   0.02733   0.01975  -0.1508   0.8043   0.0899
  -4.500   0.0855   0.02775   0.02013  -0.1480   0.7997   0.0931
  -4.250   0.1426   0.02678   0.01912  -0.1530   0.8012   0.0997
  -3.750   0.1460   0.02751   0.01976  -0.1446   0.7865   0.1064
  -3.500   0.1910   0.02675   0.01907  -0.1474   0.7857   0.1163
  -3.250   0.2050   0.02697   0.01938  -0.1454   0.7806   0.1226
  -3.000   0.2623   0.02614   0.01851  -0.1501   0.7820   0.1386
  -2.750   0.3171   0.02508   0.01753  -0.1545   0.7834   0.1570
  -2.500   0.2717   0.02680   0.01923  -0.1430   0.7676   0.1546
  -2.250   0.3151   0.02616   0.01871  -0.1454   0.7669   0.1732
  -2.000   0.2918   0.02773   0.02028  -0.1379   0.7535   0.1761
  -1.750   0.3272   0.02728   0.01985  -0.1389   0.7511   0.1958
  -1.500   0.3668   0.02664   0.01931  -0.1407   0.7496   0.2175
  -1.250   0.4079   0.02604   0.01878  -0.1426   0.7486   0.2443
  -1.000   0.4496   0.02540   0.01829  -0.1448   0.7478   0.2771
  -0.750   0.4279   0.02707   0.02000  -0.1376   0.7344   0.2852
  -0.500   0.4647   0.02642   0.01952  -0.1388   0.7321   0.3318
  -0.250   0.5075   0.02535   0.01878  -0.1409   0.7310   0.4194
   0.000   0.5472   0.02422   0.01826  -0.1423   0.7302   0.5806
   0.250   0.5832   0.02350   0.01790  -0.1422   0.7292   0.7159
   0.500   0.6211   0.02309   0.01748  -0.1429   0.7282   0.7671
   0.750   0.6608   0.02265   0.01701  -0.1440   0.7273   0.8027
   1.000   0.6972   0.02211   0.01647  -0.1443   0.7264   0.8270
   1.250   0.6630   0.02342   0.01786  -0.1340   0.7113   0.8403
   1.500   0.6986   0.02267   0.01708  -0.1342   0.7102   0.8630
   1.750   0.7358   0.02182   0.01621  -0.1346   0.7092   0.8837
   2.000   0.7770   0.02089   0.01525  -0.1358   0.7083   0.9016
   2.250   0.8194   0.02000   0.01431  -0.1374   0.7074   0.9191
   2.500   0.7933   0.02092   0.01534  -0.1285   0.6930   0.9433
   2.750   0.8530   0.01996   0.01435  -0.1337   0.6921   1.0000
   3.000   0.9029   0.01924   0.01356  -0.1373   0.6907   1.0000
   3.250   0.9546   0.01852   0.01277  -0.1413   0.6893   1.0000
   3.500   0.9447   0.01929   0.01358  -0.1353   0.6769   1.0000
   3.750   0.9918   0.01850   0.01272  -0.1383   0.6740   1.0000
   4.000   1.0443   0.01767   0.01183  -0.1423   0.6713   1.0000
   4.250   1.0522   0.01798   0.01214  -0.1391   0.6619   1.0000
   4.500   1.0879   0.01756   0.01168  -0.1403   0.6560   1.0000
   4.750   1.1385   0.01685   0.01090  -0.1440   0.6518   1.0000
   5.000   1.1430   0.01726   0.01134  -0.1402   0.6410   1.0000
   5.250   1.1836   0.01683   0.01083  -0.1422   0.6345   1.0000
   5.500   1.2004   0.01700   0.01100  -0.1404   0.6242   1.0000
   5.750   1.2326   0.01679   0.01072  -0.1411   0.6148   1.0000
   6.000   1.2446   0.01711   0.01103  -0.1385   0.6026   1.0000
   6.250   1.2795   0.01689   0.01070  -0.1396   0.5921   1.0000
   6.500   1.2927   0.01723   0.01102  -0.1373   0.5790   1.0000
   6.750   1.3119   0.01752   0.01125  -0.1360   0.5666   1.0000
   7.000   1.3418   0.01759   0.01118  -0.1363   0.5547   1.0000
   7.250   1.3478   0.01822   0.01182  -0.1331   0.5404   1.0000
   7.500   1.3636   0.01869   0.01223  -0.1314   0.5271   1.0000
   7.750   1.3864   0.01901   0.01240  -0.1307   0.5143   1.0000
   8.000   1.3950   0.01972   0.01310  -0.1280   0.5005   1.0000
   8.250   1.4068   0.02040   0.01373  -0.1259   0.4872   1.0000
   8.500   1.4236   0.02097   0.01419  -0.1245   0.4745   1.0000
   8.750   1.4293   0.02186   0.01510  -0.1217   0.4614   1.0000
   9.000   1.4432   0.02257   0.01575  -0.1200   0.4501   1.0000
   9.250   1.4559   0.02333   0.01645  -0.1182   0.4387   1.0000
   9.500   1.4663   0.02422   0.01734  -0.1163   0.4275   1.0000
   9.750   1.4795   0.02501   0.01805  -0.1146   0.4161   1.0000
  10.000   1.4859   0.02607   0.01916  -0.1123   0.4047   1.0000
  10.250   1.4998   0.02688   0.01985  -0.1109   0.3944   1.0000
  10.500   1.5060   0.02801   0.02103  -0.1087   0.3836   1.0000
  10.750   1.5216   0.02881   0.02173  -0.1075   0.3740   1.0000
  11.000   1.5276   0.03002   0.02304  -0.1054   0.3643   1.0000
  11.250   1.5438   0.03082   0.02371  -0.1043   0.3552   1.0000
  11.500   1.5476   0.03218   0.02521  -0.1022   0.3460   1.0000
  11.750   1.5594   0.03318   0.02615  -0.1008   0.3374   1.0000
  12.000   1.5667   0.03446   0.02750  -0.0991   0.3288   1.0000
  12.250   1.5764   0.03562   0.02863  -0.0976   0.3204   1.0000
  12.500   1.5872   0.03678   0.02978  -0.0963   0.3124   1.0000
  12.750   1.5930   0.03824   0.03132  -0.0946   0.3040   1.0000
  13.000   1.6075   0.03921   0.03220  -0.0936   0.2963   1.0000
  13.250   1.6109   0.04090   0.03405  -0.0919   0.2889   1.0000
  13.500   1.6186   0.04233   0.03550  -0.0906   0.2817   1.0000
  13.750   1.6282   0.04368   0.03685  -0.0894   0.2749   1.0000
  14.000   1.6337   0.04536   0.03864  -0.0881   0.2678   1.0000
  14.250   1.6437   0.04670   0.03990  -0.0870   0.2608   1.0000
  14.500   1.6487   0.04851   0.04183  -0.0858   0.2539   1.0000
  14.750   1.6526   0.05042   0.04382  -0.0846   0.2467   1.0000
  15.000   1.6625   0.05184   0.04514  -0.0836   0.2393   1.0000
  15.250   1.6612   0.05432   0.04782  -0.0824   0.2325   1.0000
  15.500   1.6634   0.05651   0.05004  -0.0813   0.2253   1.0000
  15.750   1.6658   0.05875   0.05232  -0.0804   0.2182   1.0000
  16.000   1.6656   0.06132   0.05498  -0.0795   0.2112   1.0000
  16.250   1.6724   0.06312   0.05665  -0.0787   0.2042   1.0000
  16.500   1.6694   0.06618   0.05992  -0.0780   0.1980   1.0000
  16.750   1.6699   0.06884   0.06265  -0.0774   0.1915   1.0000
  17.000   1.6747   0.07100   0.06477  -0.0768   0.1853   1.0000
  17.250   1.6711   0.07431   0.06828  -0.0765   0.1792   1.0000
  17.500   1.6697   0.07736   0.07137  -0.0762   0.1732   1.0000
  17.750   1.6694   0.08027   0.07430  -0.0760   0.1673   1.0000
  18.000   1.6649   0.08389   0.07805  -0.0760   0.1613   1.0000
  18.250   1.6635   0.08700   0.08112  -0.0760   0.1554   1.0000
  18.500   1.6603   0.09051   0.08474  -0.0762   0.1498   1.0000
  18.750   1.6552   0.09437   0.08874  -0.0767   0.1442   1.0000
  19.000   1.6535   0.09759   0.09190  -0.0770   0.1386   1.0000
  19.250   1.6481   0.10161   0.09608  -0.0777   0.1337   1.0000
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