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SG6050 (sg6050-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: SG6050 (sg6050-il)
Reynolds number: 50,000
Max Cl/Cd: 25.61 at α=9.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sg6050-il-50000-n5.txt
Download as CSV file: xf-sg6050-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6050                                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4481   0.10568   0.09851  -0.0526   1.0000   0.0820
 -11.500  -0.4677   0.09762   0.09054  -0.0568   1.0000   0.0837
 -11.250  -0.6005   0.07097   0.06385  -0.0758   1.0000   0.0751
 -11.000  -0.6335   0.06637   0.05921  -0.0762   1.0000   0.0748
 -10.750  -0.6665   0.06346   0.05628  -0.0731   1.0000   0.0746
 -10.500  -0.6975   0.06065   0.05336  -0.0694   1.0000   0.0748
 -10.250  -0.7265   0.05800   0.05049  -0.0651   1.0000   0.0753
 -10.000  -0.7248   0.05715   0.04980  -0.0623   1.0000   0.0780
  -9.750  -0.7326   0.05575   0.04835  -0.0590   1.0000   0.0805
  -9.500  -0.7436   0.05365   0.04604  -0.0558   1.0000   0.0831
  -9.250  -0.7511   0.05053   0.04240  -0.0539   0.9984   0.0865
  -9.000  -0.7269   0.04844   0.04022  -0.0557   0.9925   0.0922
  -8.750  -0.7055   0.04580   0.03708  -0.0574   0.9856   0.0986
  -8.500  -0.6810   0.04365   0.03467  -0.0589   0.9795   0.1043
  -8.250  -0.6548   0.04190   0.03265  -0.0603   0.9733   0.1109
  -8.000  -0.6284   0.03994   0.03029  -0.0616   0.9673   0.1167
  -7.750  -0.6003   0.03863   0.02890  -0.0628   0.9612   0.1228
  -7.500  -0.5685   0.03705   0.02684  -0.0646   0.9564   0.1294
  -7.250  -0.5436   0.03593   0.02577  -0.0650   0.9496   0.1351
  -7.000  -0.5118   0.03477   0.02435  -0.0665   0.9444   0.1427
  -6.750  -0.4824   0.03371   0.02321  -0.0675   0.9389   0.1493
  -6.500  -0.4551   0.03282   0.02217  -0.0681   0.9324   0.1584
  -6.250  -0.4221   0.03186   0.02121  -0.0698   0.9278   0.1691
  -6.000  -0.3952   0.03104   0.02034  -0.0703   0.9215   0.1808
  -5.750  -0.3669   0.03025   0.01960  -0.0712   0.9154   0.1984
  -5.500  -0.3326   0.02942   0.01892  -0.0732   0.9111   0.2269
  -5.250  -0.3086   0.02898   0.01869  -0.0732   0.9039   0.2632
  -5.000  -0.2793   0.02884   0.01866  -0.0739   0.8979   0.3129
  -4.750  -0.2442   0.02881   0.01851  -0.0754   0.8935   0.3591
  -4.500  -0.2237   0.02894   0.01850  -0.0745   0.8851   0.3887
  -4.250  -0.1927   0.02891   0.01834  -0.0753   0.8797   0.4186
  -4.000  -0.1637   0.02889   0.01825  -0.0756   0.8742   0.4452
  -3.750  -0.1410   0.02894   0.01826  -0.0749   0.8665   0.4685
  -3.500  -0.1097   0.02887   0.01818  -0.0754   0.8618   0.4951
  -3.250  -0.0867   0.02894   0.01821  -0.0747   0.8546   0.5184
  -3.000  -0.0601   0.02892   0.01818  -0.0745   0.8482   0.5390
  -2.750  -0.0262   0.02874   0.01793  -0.0755   0.8439   0.5571
  -2.500  -0.0056   0.02886   0.01796  -0.0747   0.8354   0.5706
  -2.250   0.0253   0.02875   0.01777  -0.0753   0.8298   0.5852
  -2.000   0.0558   0.02865   0.01764  -0.0758   0.8245   0.5994
  -1.750   0.0774   0.02877   0.01775  -0.0750   0.8162   0.6136
  -1.500   0.1102   0.02860   0.01756  -0.0758   0.8114   0.6310
  -1.250   0.1307   0.02876   0.01776  -0.0748   0.8031   0.6491
  -0.750   0.1892   0.02852   0.01765  -0.0748   0.7922   0.6996
  -0.500   0.2046   0.02881   0.01808  -0.0726   0.7827   0.7321
  -0.250   0.2346   0.02866   0.01808  -0.0721   0.7780   0.7792
   0.000   0.2559   0.02900   0.01854  -0.0707   0.7693   0.8433
   0.250   0.2985   0.02905   0.01857  -0.0732   0.7636   0.9185
   0.750   0.3764   0.02946   0.01875  -0.0789   0.7491   1.0000
   1.000   0.4079   0.02942   0.01855  -0.0796   0.7442   1.0000
   1.250   0.4187   0.03011   0.01914  -0.0776   0.7335   1.0000
   1.500   0.4504   0.03010   0.01902  -0.0782   0.7283   1.0000
   1.750   0.4633   0.03081   0.01967  -0.0764   0.7179   1.0000
   2.000   0.4946   0.03083   0.01959  -0.0769   0.7124   1.0000
   2.250   0.5087   0.03155   0.02028  -0.0753   0.7021   1.0000
   2.500   0.5396   0.03157   0.02024  -0.0757   0.6963   1.0000
   2.750   0.5541   0.03232   0.02097  -0.0741   0.6860   1.0000
   3.000   0.5849   0.03234   0.02096  -0.0744   0.6802   1.0000
   3.250   0.5991   0.03314   0.02176  -0.0729   0.6698   1.0000
   3.500   0.6304   0.03311   0.02171  -0.0732   0.6640   1.0000
   3.750   0.6437   0.03398   0.02260  -0.0715   0.6534   1.0000
   4.000   0.6762   0.03387   0.02250  -0.0719   0.6478   1.0000
   4.250   0.6882   0.03483   0.02348  -0.0702   0.6367   1.0000
   4.500   0.7222   0.03461   0.02329  -0.0706   0.6315   1.0000
   4.750   0.7327   0.03565   0.02438  -0.0687   0.6200   1.0000
   5.000   0.7686   0.03529   0.02405  -0.0693   0.6150   1.0000
   5.250   0.7772   0.03645   0.02529  -0.0672   0.6030   1.0000
   5.500   0.8153   0.03593   0.02480  -0.0680   0.5985   1.0000
   5.750   0.8216   0.03723   0.02618  -0.0657   0.5860   1.0000
   6.250   0.8663   0.03796   0.02706  -0.0641   0.5690   1.0000
   6.500   0.8750   0.03907   0.02825  -0.0620   0.5579   1.0000
   6.750   0.9117   0.03856   0.02784  -0.0625   0.5520   1.0000
   7.000   0.9159   0.03996   0.02932  -0.0599   0.5398   1.0000
   7.250   0.9600   0.03893   0.02839  -0.0610   0.5348   1.0000
   7.500   0.9608   0.04052   0.03008  -0.0582   0.5219   1.0000
   7.750   0.9719   0.04157   0.03124  -0.0564   0.5107   1.0000
   8.000   1.0111   0.04061   0.03039  -0.0567   0.5038   1.0000
   8.250   1.0145   0.04215   0.03204  -0.0544   0.4910   1.0000
   8.500   1.0302   0.04286   0.03287  -0.0530   0.4802   1.0000
   8.750   1.0672   0.04191   0.03202  -0.0528   0.4718   1.0000
   9.000   1.0703   0.04351   0.03375  -0.0506   0.4587   1.0000
   9.250   1.0820   0.04451   0.03486  -0.0490   0.4467   1.0000
   9.500   1.1124   0.04391   0.03437  -0.0483   0.4364   1.0000
   9.750   1.1317   0.04419   0.03476  -0.0470   0.4241   1.0000
  10.000   1.1357   0.04576   0.03645  -0.0451   0.4105   1.0000
  10.250   1.1434   0.04705   0.03786  -0.0434   0.3971   1.0000
  10.500   1.1546   0.04804   0.03896  -0.0418   0.3837   1.0000
  10.750   1.1674   0.04885   0.03986  -0.0404   0.3701   1.0000
  11.000   1.1797   0.04969   0.04078  -0.0389   0.3560   1.0000
  11.250   1.1896   0.05075   0.04190  -0.0374   0.3416   1.0000
  11.500   1.1973   0.05203   0.04324  -0.0358   0.3268   1.0000
  11.750   1.2026   0.05357   0.04487  -0.0344   0.3117   1.0000
  12.000   1.2060   0.05537   0.04672  -0.0330   0.2966   1.0000
  12.250   1.2079   0.05736   0.04878  -0.0316   0.2816   1.0000
  12.500   1.2074   0.05971   0.05119  -0.0305   0.2667   1.0000
  12.750   1.2061   0.06223   0.05376  -0.0295   0.2521   1.0000
  13.000   1.2039   0.06495   0.05654  -0.0286   0.2377   1.0000
  13.250   1.2010   0.06783   0.05947  -0.0279   0.2238   1.0000
  13.500   1.1979   0.07084   0.06253  -0.0273   0.2104   1.0000
  13.750   1.1947   0.07395   0.06569  -0.0269   0.1975   1.0000
  14.000   1.1921   0.07706   0.06882  -0.0266   0.1852   1.0000
  14.250   1.1900   0.08016   0.07190  -0.0264   0.1734   1.0000
  14.500   1.1893   0.08304   0.07471  -0.0261   0.1622   1.0000
  14.750   1.1816   0.08736   0.07919  -0.0267   0.1518   1.0000
  15.000   1.1770   0.09120   0.08308  -0.0271   0.1422   1.0000
  15.250   1.1764   0.09432   0.08613  -0.0273   0.1332   1.0000
  15.500   1.1693   0.09886   0.09083  -0.0282   0.1248   1.0000
  15.750   1.1661   0.10269   0.09469  -0.0289   0.1171   1.0000
  16.000   1.1632   0.10655   0.09860  -0.0298   0.1098   1.0000
  16.250   1.1577   0.11106   0.10325  -0.0311   0.1035   1.0000
  16.500   1.1551   0.11501   0.10724  -0.0322   0.0972   1.0000
  16.750   1.1499   0.11966   0.11199  -0.0338   0.0919   1.0000
  17.000   1.1417   0.12508   0.11758  -0.0361   0.0870   1.0000
  17.250   1.1443   0.12807   0.12050  -0.0370   0.0818   1.0000
  17.500   1.1269   0.13598   0.12872  -0.0410   0.0786   1.0000
  17.750   1.1187   0.14185   0.13471  -0.0440   0.0748   1.0000
  18.000   1.1218   0.14498   0.13780  -0.0454   0.0707   1.0000
  18.250   1.0908   0.15731   0.15042  -0.0527   0.0694   1.0000
  18.500   1.0398   0.17738   0.17060  -0.0647   0.0685   1.0000
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