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SG6050 (sg6050-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: SG6050 (sg6050-il)
Reynolds number: 200,000
Max Cl/Cd: 73.22 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sg6050-il-200000-n5.txt
Download as CSV file: xf-sg6050-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6279   0.12971   0.12574  -0.0292   1.0000   0.0148
 -15.750  -0.6590   0.11849   0.11439  -0.0345   1.0000   0.0147
 -15.500  -0.6875   0.10827   0.10403  -0.0396   1.0000   0.0146
 -15.250  -0.7168   0.09816   0.09378  -0.0448   1.0000   0.0145
 -15.000  -0.7448   0.08875   0.08421  -0.0499   1.0000   0.0144
 -14.750  -0.7703   0.08043   0.07573  -0.0546   1.0000   0.0143
 -14.500  -0.7928   0.07294   0.06810  -0.0589   1.0000   0.0143
 -14.250  -0.8122   0.06623   0.06125  -0.0629   1.0000   0.0142
 -14.000  -0.8288   0.06008   0.05497  -0.0667   1.0000   0.0143
 -13.750  -0.8423   0.05438   0.04913  -0.0704   1.0000   0.0144
 -13.500  -0.8527   0.04910   0.04369  -0.0741   1.0000   0.0145
 -13.250  -0.8604   0.04438   0.03882  -0.0775   1.0000   0.0147
 -13.000  -0.8665   0.04041   0.03470  -0.0801   1.0000   0.0149
 -12.750  -0.8723   0.03732   0.03148  -0.0811   1.0000   0.0152
 -12.500  -0.8791   0.03503   0.02907  -0.0801   1.0000   0.0155
 -12.250  -0.8906   0.03347   0.02741  -0.0768   1.0000   0.0157
 -12.000  -0.8894   0.03196   0.02577  -0.0750   0.9959   0.0163
 -11.750  -0.8703   0.03012   0.02379  -0.0765   0.9857   0.0173
 -11.500  -0.8500   0.02856   0.02210  -0.0775   0.9741   0.0188
 -11.250  -0.8288   0.02713   0.02054  -0.0783   0.9625   0.0207
 -11.000  -0.8065   0.02584   0.01913  -0.0789   0.9519   0.0233
 -10.750  -0.7828   0.02469   0.01791  -0.0795   0.9422   0.0268
 -10.500  -0.7597   0.02381   0.01697  -0.0796   0.9315   0.0311
 -10.250  -0.7351   0.02312   0.01620  -0.0798   0.9223   0.0360
 -10.000  -0.7106   0.02255   0.01551  -0.0798   0.9130   0.0408
  -9.750  -0.6858   0.02210   0.01493  -0.0796   0.9041   0.0454
  -9.500  -0.6615   0.02166   0.01440  -0.0795   0.8956   0.0493
  -9.250  -0.6365   0.02130   0.01390  -0.0793   0.8875   0.0535
  -9.000  -0.6121   0.02090   0.01343  -0.0791   0.8799   0.0578
  -8.750  -0.5862   0.02069   0.01308  -0.0791   0.8730   0.0630
  -8.500  -0.5619   0.02025   0.01258  -0.0789   0.8656   0.0673
  -8.250  -0.5369   0.01988   0.01212  -0.0786   0.8597   0.0711
  -8.000  -0.5112   0.01948   0.01158  -0.0786   0.8527   0.0743
  -7.750  -0.4865   0.01893   0.01095  -0.0783   0.8466   0.0772
  -7.500  -0.4614   0.01845   0.01042  -0.0781   0.8411   0.0803
  -7.250  -0.4354   0.01803   0.00992  -0.0781   0.8346   0.0835
  -7.000  -0.4091   0.01767   0.00943  -0.0780   0.8292   0.0867
  -6.750  -0.3833   0.01719   0.00891  -0.0779   0.8239   0.0901
  -6.500  -0.3568   0.01677   0.00846  -0.0779   0.8179   0.0939
  -6.250  -0.3299   0.01644   0.00803  -0.0780   0.8128   0.0985
  -6.000  -0.3030   0.01608   0.00761  -0.0780   0.8081   0.1038
  -5.750  -0.2758   0.01572   0.00724  -0.0782   0.8024   0.1106
  -5.500  -0.2484   0.01539   0.00687  -0.0783   0.7973   0.1189
  -5.000  -0.1935   0.01466   0.00619  -0.0787   0.7875   0.1529
  -4.750  -0.1663   0.01421   0.00587  -0.0790   0.7823   0.1889
  -4.500  -0.1392   0.01376   0.00562  -0.0792   0.7779   0.2440
  -4.250  -0.1112   0.01354   0.00554  -0.0795   0.7731   0.2912
  -4.000  -0.0826   0.01345   0.00549  -0.0798   0.7678   0.3230
  -3.750  -0.0537   0.01341   0.00540  -0.0800   0.7630   0.3449
  -3.500  -0.0248   0.01338   0.00531  -0.0803   0.7587   0.3605
  -3.250   0.0042   0.01335   0.00525  -0.0806   0.7530   0.3731
  -3.000   0.0332   0.01332   0.00516  -0.0808   0.7478   0.3849
  -2.750   0.0622   0.01328   0.00504  -0.0811   0.7435   0.3959
  -2.500   0.0910   0.01323   0.00502  -0.0814   0.7375   0.4091
  -2.250   0.1196   0.01319   0.00498  -0.0816   0.7321   0.4276
  -2.000   0.1483   0.01312   0.00491  -0.0818   0.7277   0.4425
  -1.750   0.1774   0.01308   0.00484  -0.0822   0.7220   0.4498
  -1.500   0.2062   0.01299   0.00477  -0.0824   0.7165   0.4557
  -1.250   0.2352   0.01294   0.00467  -0.0827   0.7117   0.4625
  -1.000   0.2641   0.01288   0.00463  -0.0830   0.7061   0.4694
  -0.750   0.2929   0.01282   0.00460  -0.0833   0.7002   0.4769
  -0.500   0.3218   0.01277   0.00452  -0.0835   0.6952   0.4854
  -0.250   0.3505   0.01272   0.00453  -0.0838   0.6891   0.4952
   0.000   0.3792   0.01266   0.00451  -0.0841   0.6829   0.5063
   0.250   0.4079   0.01260   0.00446  -0.0843   0.6777   0.5205
   0.500   0.4362   0.01254   0.00452  -0.0845   0.6705   0.5385
   0.750   0.4644   0.01245   0.00451  -0.0846   0.6644   0.5626
   1.000   0.4922   0.01235   0.00456  -0.0847   0.6579   0.5980
   1.250   0.5192   0.01222   0.00463  -0.0845   0.6511   0.6487
   1.500   0.5448   0.01205   0.00467  -0.0839   0.6452   0.7141
   1.750   0.5667   0.01192   0.00485  -0.0822   0.6378   0.7938
   2.000   0.5891   0.01188   0.00492  -0.0806   0.6314   0.8696
   2.250   0.6150   0.01191   0.00499  -0.0799   0.6240   0.9119
   2.500   0.6449   0.01194   0.00502  -0.0802   0.6166   0.9434
   2.750   0.6782   0.01200   0.00508  -0.0814   0.6085   0.9694
   3.000   0.7134   0.01207   0.00512  -0.0831   0.6001   0.9910
   3.250   0.7434   0.01214   0.00518  -0.0837   0.5914   1.0000
   3.500   0.7699   0.01226   0.00525  -0.0836   0.5832   1.0000
   3.750   0.7963   0.01240   0.00539  -0.0835   0.5742   1.0000
   4.000   0.8229   0.01254   0.00548  -0.0834   0.5659   1.0000
   4.250   0.8494   0.01269   0.00564  -0.0833   0.5563   1.0000
   4.500   0.8758   0.01286   0.00579  -0.0832   0.5473   1.0000
   4.750   0.9021   0.01304   0.00596  -0.0831   0.5375   1.0000
   5.000   0.9282   0.01323   0.00615  -0.0829   0.5277   1.0000
   5.250   0.9541   0.01345   0.00633  -0.0827   0.5177   1.0000
   5.500   0.9795   0.01367   0.00655  -0.0825   0.5061   1.0000
   5.750   1.0047   0.01390   0.00679  -0.0821   0.4944   1.0000
   6.000   1.0294   0.01417   0.00703  -0.0818   0.4828   1.0000
   6.250   1.0537   0.01445   0.00729  -0.0813   0.4708   1.0000
   6.500   1.0778   0.01473   0.00759  -0.0808   0.4583   1.0000
   6.750   1.1012   0.01504   0.00791  -0.0802   0.4455   1.0000
   7.000   1.1239   0.01539   0.00824  -0.0795   0.4323   1.0000
   7.250   1.1458   0.01576   0.00860  -0.0787   0.4191   1.0000
   7.500   1.1670   0.01616   0.00898  -0.0778   0.4057   1.0000
   7.750   1.1874   0.01657   0.00940  -0.0767   0.3918   1.0000
   8.000   1.2068   0.01702   0.00984  -0.0755   0.3771   1.0000
   8.250   1.2247   0.01751   0.01033  -0.0741   0.3616   1.0000
   8.500   1.2410   0.01804   0.01085  -0.0724   0.3459   1.0000
   8.750   1.2556   0.01862   0.01142  -0.0705   0.3304   1.0000
   9.000   1.2669   0.01924   0.01203  -0.0680   0.3152   1.0000
   9.250   1.2773   0.01996   0.01274  -0.0654   0.2996   1.0000
   9.500   1.2871   0.02078   0.01355  -0.0630   0.2834   1.0000
   9.750   1.2954   0.02176   0.01448  -0.0606   0.2661   1.0000
  10.000   1.3036   0.02283   0.01552  -0.0584   0.2476   1.0000
  10.250   1.3107   0.02403   0.01669  -0.0562   0.2286   1.0000
  10.500   1.3169   0.02538   0.01800  -0.0542   0.2104   1.0000
  10.750   1.3227   0.02685   0.01943  -0.0522   0.1935   1.0000
  11.000   1.3279   0.02842   0.02096  -0.0504   0.1778   1.0000
  11.250   1.3327   0.03009   0.02261  -0.0487   0.1629   1.0000
  11.500   1.3368   0.03189   0.02438  -0.0471   0.1484   1.0000
  11.750   1.3399   0.03381   0.02627  -0.0456   0.1340   1.0000
  12.000   1.3425   0.03585   0.02829  -0.0442   0.1201   1.0000
  12.250   1.3441   0.03801   0.03041  -0.0428   0.1072   1.0000
  12.500   1.3455   0.04025   0.03263  -0.0416   0.0953   1.0000
  12.750   1.3474   0.04250   0.03488  -0.0405   0.0847   1.0000
  13.000   1.3492   0.04480   0.03720  -0.0395   0.0760   1.0000
  13.250   1.3507   0.04721   0.03963  -0.0386   0.0689   1.0000
  13.500   1.3516   0.04975   0.04221  -0.0379   0.0625   1.0000
  13.750   1.3535   0.05227   0.04478  -0.0372   0.0568   1.0000
  14.000   1.3530   0.05511   0.04766  -0.0367   0.0519   1.0000
  14.250   1.3545   0.05781   0.05044  -0.0363   0.0472   1.0000
  14.500   1.3535   0.06086   0.05354  -0.0360   0.0434   1.0000
  14.750   1.3538   0.06384   0.05661  -0.0359   0.0397   1.0000
  15.000   1.3515   0.06719   0.06001  -0.0358   0.0367   1.0000
  15.250   1.3508   0.07041   0.06333  -0.0359   0.0338   1.0000
  15.500   1.3472   0.07409   0.06708  -0.0361   0.0314   1.0000
  15.750   1.3452   0.07762   0.07071  -0.0364   0.0290   1.0000
  16.000   1.3412   0.08148   0.07467  -0.0368   0.0270   1.0000
  16.250   1.3361   0.08554   0.07881  -0.0375   0.0254   1.0000
  16.500   1.3324   0.08950   0.08289  -0.0381   0.0238   1.0000
  16.750   1.3268   0.09379   0.08727  -0.0390   0.0224   1.0000
  17.000   1.3197   0.09839   0.09194  -0.0402   0.0215   1.0000
  17.250   1.3152   0.10263   0.09632  -0.0412   0.0203   1.0000
  17.500   1.3097   0.10709   0.10090  -0.0425   0.0194   1.0000
  17.750   1.3034   0.11176   0.10567  -0.0440   0.0187   1.0000
  18.000   1.2959   0.11667   0.11068  -0.0457   0.0181   1.0000
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