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SG6050 (sg6050-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SG6050 (sg6050-il)
Reynolds number: 1,000,000
Max Cl/Cd: 126.51 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sg6050-il-1000000.txt
Download as CSV file: xf-sg6050-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9166   0.08443   0.08127  -0.0469   1.0000   0.0070
 -16.250  -0.9364   0.07751   0.07424  -0.0506   1.0000   0.0070
 -16.000  -0.9579   0.07071   0.06734  -0.0542   1.0000   0.0069
 -15.750  -0.9785   0.06419   0.06070  -0.0578   1.0000   0.0069
 -15.500  -0.9971   0.05801   0.05441  -0.0613   1.0000   0.0069
 -15.250  -1.0138   0.05202   0.04831  -0.0649   1.0000   0.0069
 -15.000  -1.0252   0.04647   0.04264  -0.0685   1.0000   0.0069
 -14.750  -1.0319   0.04130   0.03734  -0.0725   1.0000   0.0070
 -14.500  -1.0388   0.03608   0.03197  -0.0768   1.0000   0.0070
 -14.250  -1.0458   0.03177   0.02750  -0.0799   1.0000   0.0070
 -14.000  -1.0522   0.02874   0.02434  -0.0803   1.0000   0.0071
 -13.750  -1.0580   0.02668   0.02216  -0.0786   1.0000   0.0072
 -13.500  -1.0637   0.02525   0.02064  -0.0752   1.0000   0.0072
 -13.000  -1.0297   0.02253   0.01773  -0.0756   0.9933   0.0075
 -12.750  -1.0070   0.02145   0.01658  -0.0761   0.9830   0.0077
 -12.500  -0.9879   0.02057   0.01561  -0.0755   0.9655   0.0079
 -12.250  -0.9710   0.01982   0.01476  -0.0742   0.9447   0.0080
 -12.000  -0.9539   0.01916   0.01396  -0.0727   0.9255   0.0082
 -11.750  -0.9343   0.01853   0.01321  -0.0717   0.9093   0.0084
 -11.500  -0.9128   0.01793   0.01250  -0.0711   0.8956   0.0087
 -11.250  -0.8899   0.01739   0.01185  -0.0706   0.8842   0.0089
 -11.000  -0.8675   0.01673   0.01108  -0.0701   0.8740   0.0092
 -10.750  -0.8444   0.01607   0.01032  -0.0698   0.8644   0.0098
 -10.500  -0.8198   0.01556   0.00973  -0.0696   0.8560   0.0104
 -10.250  -0.7943   0.01511   0.00921  -0.0695   0.8479   0.0110
 -10.000  -0.7692   0.01457   0.00860  -0.0694   0.8410   0.0122
  -9.750  -0.7435   0.01404   0.00802  -0.0693   0.8341   0.0142
  -9.500  -0.7190   0.01336   0.00732  -0.0692   0.8276   0.0210
  -9.250  -0.6932   0.01275   0.00681  -0.0693   0.8216   0.0338
  -9.000  -0.6656   0.01247   0.00654  -0.0695   0.8156   0.0404
  -8.750  -0.6378   0.01226   0.00631  -0.0697   0.8099   0.0449
  -8.500  -0.6091   0.01207   0.00609  -0.0700   0.8049   0.0476
  -8.250  -0.5808   0.01184   0.00586  -0.0703   0.7996   0.0509
  -8.000  -0.5522   0.01170   0.00567  -0.0706   0.7946   0.0534
  -7.750  -0.5231   0.01159   0.00551  -0.0710   0.7900   0.0548
  -7.500  -0.4947   0.01129   0.00520  -0.0713   0.7853   0.0583
  -7.250  -0.4659   0.01112   0.00503  -0.0717   0.7806   0.0614
  -7.000  -0.4368   0.01103   0.00488  -0.0720   0.7760   0.0637
  -6.750  -0.4077   0.01082   0.00464  -0.0724   0.7718   0.0662
  -6.500  -0.3788   0.01057   0.00439  -0.0728   0.7675   0.0697
  -6.250  -0.3497   0.01041   0.00420  -0.0732   0.7632   0.0727
  -6.000  -0.3204   0.01031   0.00405  -0.0736   0.7588   0.0750
  -5.750  -0.2911   0.01006   0.00381  -0.0740   0.7548   0.0799
  -5.500  -0.2617   0.00986   0.00362  -0.0745   0.7505   0.0847
  -5.250  -0.2323   0.00974   0.00344  -0.0749   0.7460   0.0884
  -5.000  -0.2030   0.00952   0.00325  -0.0753   0.7415   0.0976
  -4.750  -0.1735   0.00928   0.00306  -0.0758   0.7370   0.1109
  -4.500  -0.1443   0.00901   0.00287  -0.0763   0.7324   0.1347
  -4.250  -0.1154   0.00868   0.00267  -0.0768   0.7279   0.1747
  -4.000  -0.0865   0.00823   0.00247  -0.0773   0.7239   0.2374
  -3.750  -0.0570   0.00794   0.00236  -0.0779   0.7195   0.2859
  -3.500  -0.0273   0.00782   0.00230  -0.0784   0.7150   0.3153
  -3.250   0.0024   0.00779   0.00226  -0.0789   0.7103   0.3334
  -3.000   0.0327   0.00772   0.00224  -0.0794   0.7062   0.3476
  -2.750   0.0628   0.00767   0.00220  -0.0799   0.7014   0.3578
  -2.500   0.0928   0.00768   0.00216  -0.0804   0.6967   0.3653
  -2.250   0.1228   0.00765   0.00213  -0.0809   0.6921   0.3726
  -2.000   0.1530   0.00763   0.00211  -0.0814   0.6870   0.3792
  -1.750   0.1830   0.00761   0.00207  -0.0819   0.6817   0.3855
  -1.500   0.2129   0.00761   0.00205  -0.0824   0.6765   0.3916
  -1.250   0.2431   0.00760   0.00203  -0.0829   0.6710   0.3976
  -1.000   0.2730   0.00757   0.00203  -0.0834   0.6654   0.4091
  -0.750   0.3029   0.00758   0.00202  -0.0839   0.6602   0.4182
  -0.500   0.3329   0.00754   0.00201  -0.0844   0.6546   0.4246
  -0.250   0.3628   0.00755   0.00199  -0.0849   0.6486   0.4292
   0.000   0.3927   0.00756   0.00198  -0.0854   0.6430   0.4331
   0.250   0.4227   0.00752   0.00197  -0.0859   0.6368   0.4388
   0.750   0.4823   0.00753   0.00198  -0.0869   0.6238   0.4505
   1.000   0.5119   0.00753   0.00199  -0.0874   0.6165   0.4586
   1.250   0.5417   0.00753   0.00201  -0.0879   0.6097   0.4681
   1.500   0.5713   0.00752   0.00204  -0.0884   0.6023   0.4817
   1.750   0.6008   0.00750   0.00208  -0.0889   0.5952   0.5032
   2.000   0.6304   0.00742   0.00212  -0.0894   0.5875   0.5441
   2.250   0.6597   0.00729   0.00219  -0.0900   0.5799   0.6167
   2.500   0.6888   0.00710   0.00227  -0.0905   0.5715   0.7078
   2.750   0.7158   0.00689   0.00241  -0.0903   0.5636   0.8233
   3.000   0.7418   0.00687   0.00252  -0.0898   0.5548   0.8812
   3.500   0.7927   0.00699   0.00269  -0.0887   0.5366   0.9290
   3.750   0.8164   0.00705   0.00277  -0.0877   0.5265   0.9484
   4.000   0.8401   0.00714   0.00283  -0.0867   0.5160   0.9683
   4.250   0.8679   0.00724   0.00290  -0.0868   0.5049   0.9856
   4.500   0.9008   0.00733   0.00297  -0.0881   0.4937   0.9976
   4.750   0.9297   0.00748   0.00308  -0.0885   0.4827   1.0000
   5.000   0.9576   0.00767   0.00322  -0.0888   0.4704   1.0000
   5.250   0.9858   0.00784   0.00335  -0.0891   0.4576   1.0000
   5.500   1.0137   0.00803   0.00350  -0.0893   0.4453   1.0000
   5.750   1.0412   0.00823   0.00367  -0.0895   0.4332   1.0000
   6.000   1.0684   0.00846   0.00385  -0.0896   0.4208   1.0000
   6.500   1.1220   0.00895   0.00424  -0.0897   0.3929   1.0000
   6.750   1.1483   0.00921   0.00445  -0.0897   0.3784   1.0000
   7.000   1.1744   0.00948   0.00468  -0.0897   0.3640   1.0000
   7.250   1.1999   0.00977   0.00493  -0.0895   0.3492   1.0000
   7.500   1.2242   0.01013   0.00521  -0.0891   0.3310   1.0000
   7.750   1.2472   0.01057   0.00554  -0.0886   0.3085   1.0000
   8.000   1.2693   0.01103   0.00589  -0.0879   0.2855   1.0000
   8.250   1.2908   0.01151   0.00627  -0.0871   0.2653   1.0000
   8.500   1.3119   0.01197   0.00666  -0.0862   0.2458   1.0000
   8.750   1.3310   0.01252   0.00711  -0.0850   0.2243   1.0000
   9.000   1.3483   0.01313   0.00760  -0.0835   0.2029   1.0000
   9.250   1.3633   0.01380   0.00815  -0.0816   0.1806   1.0000
   9.500   1.3741   0.01453   0.00877  -0.0789   0.1603   1.0000
   9.750   1.3842   0.01527   0.00944  -0.0762   0.1429   1.0000
  10.000   1.3946   0.01609   0.01018  -0.0737   0.1267   1.0000
  10.250   1.4052   0.01697   0.01099  -0.0714   0.1122   1.0000
  10.500   1.4163   0.01787   0.01184  -0.0693   0.0999   1.0000
  10.750   1.4272   0.01885   0.01277  -0.0674   0.0885   1.0000
  11.000   1.4379   0.01989   0.01378  -0.0656   0.0782   1.0000
  11.250   1.4479   0.02102   0.01487  -0.0638   0.0690   1.0000
  11.500   1.4575   0.02224   0.01606  -0.0622   0.0606   1.0000
  11.750   1.4669   0.02352   0.01732  -0.0606   0.0533   1.0000
  12.000   1.4768   0.02479   0.01858  -0.0592   0.0472   1.0000
  12.250   1.4857   0.02618   0.01997  -0.0578   0.0414   1.0000
  12.500   1.4932   0.02771   0.02150  -0.0564   0.0360   1.0000
  12.750   1.4996   0.02936   0.02314  -0.0549   0.0309   1.0000
  13.000   1.5057   0.03107   0.02485  -0.0536   0.0265   1.0000
  13.250   1.5110   0.03288   0.02668  -0.0523   0.0225   1.0000
  13.500   1.5154   0.03481   0.02862  -0.0510   0.0190   1.0000
  13.750   1.5187   0.03685   0.03069  -0.0498   0.0160   1.0000
  14.000   1.5218   0.03897   0.03285  -0.0486   0.0139   1.0000
  14.250   1.5251   0.04115   0.03507  -0.0476   0.0125   1.0000
  14.500   1.5283   0.04340   0.03737  -0.0467   0.0115   1.0000
  14.750   1.5325   0.04559   0.03962  -0.0459   0.0109   1.0000
  15.000   1.5350   0.04802   0.04211  -0.0452   0.0103   1.0000
  15.250   1.5356   0.05072   0.04487  -0.0446   0.0099   1.0000
  15.500   1.5357   0.05354   0.04776  -0.0440   0.0095   1.0000
  15.750   1.5381   0.05614   0.05044  -0.0437   0.0092   1.0000
  16.000   1.5394   0.05892   0.05331  -0.0434   0.0090   1.0000
  16.250   1.5397   0.06188   0.05635  -0.0432   0.0088   1.0000
  16.500   1.5393   0.06499   0.05954  -0.0431   0.0086   1.0000
  16.750   1.5374   0.06833   0.06296  -0.0431   0.0084   1.0000
  17.000   1.5342   0.07185   0.06656  -0.0432   0.0082   1.0000
  17.250   1.5294   0.07567   0.07046  -0.0434   0.0080   1.0000
  17.500   1.5224   0.07986   0.07474  -0.0438   0.0078   1.0000
  17.750   1.5131   0.08443   0.07942  -0.0443   0.0077   1.0000
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