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SG6051 (sg6051-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SG6051 (sg6051-il)
Reynolds number: 1,000,000
Max Cl/Cd: 133.55 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sg6051-il-1000000.txt
Download as CSV file: xf-sg6051-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6051                                          
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.7264   0.05777   0.05613  -0.0571   1.0000   0.0061
 -11.500  -0.7818   0.03846   0.03628  -0.0770   0.9777   0.0059
 -11.250  -0.7965   0.03381   0.03124  -0.0760   0.9527   0.0059
 -11.000  -0.7986   0.03031   0.02737  -0.0745   0.9380   0.0058
 -10.750  -0.7919   0.02756   0.02427  -0.0733   0.9276   0.0058
 -10.500  -0.7786   0.02532   0.02174  -0.0726   0.9191   0.0059
 -10.250  -0.7617   0.02363   0.01979  -0.0719   0.9122   0.0060
 -10.000  -0.7419   0.02216   0.01812  -0.0715   0.9056   0.0061
  -9.750  -0.7213   0.02084   0.01657  -0.0710   0.8998   0.0062
  -9.500  -0.6991   0.01956   0.01509  -0.0708   0.8943   0.0063
  -9.250  -0.6760   0.01839   0.01372  -0.0705   0.8890   0.0064
  -9.000  -0.6526   0.01733   0.01246  -0.0702   0.8842   0.0064
  -8.750  -0.6276   0.01637   0.01136  -0.0701   0.8795   0.0065
  -8.500  -0.6021   0.01554   0.01038  -0.0701   0.8746   0.0067
  -8.250  -0.5763   0.01485   0.00954  -0.0700   0.8701   0.0068
  -8.000  -0.5494   0.01426   0.00884  -0.0701   0.8660   0.0069
  -7.750  -0.5238   0.01319   0.00762  -0.0701   0.8615   0.0075
  -7.500  -0.4968   0.01263   0.00697  -0.0702   0.8572   0.0079
  -7.250  -0.4693   0.01221   0.00647  -0.0703   0.8530   0.0084
  -7.000  -0.4411   0.01180   0.00599  -0.0706   0.8488   0.0090
  -6.750  -0.4129   0.01143   0.00555  -0.0708   0.8445   0.0095
  -6.500  -0.3851   0.01097   0.00503  -0.0709   0.8403   0.0113
  -6.250  -0.3568   0.01058   0.00463  -0.0712   0.8362   0.0158
  -6.000  -0.3281   0.01033   0.00444  -0.0716   0.8319   0.0230
  -5.750  -0.2991   0.01028   0.00437  -0.0719   0.8277   0.0261
  -5.500  -0.2706   0.01009   0.00416  -0.0722   0.8236   0.0296
  -5.250  -0.2414   0.00998   0.00406  -0.0727   0.8197   0.0321
  -5.000  -0.2121   0.00990   0.00395  -0.0731   0.8155   0.0335
  -4.750  -0.1835   0.00959   0.00360  -0.0734   0.8115   0.0372
  -4.500  -0.1545   0.00945   0.00344  -0.0738   0.8075   0.0398
  -4.250  -0.1251   0.00933   0.00331  -0.0742   0.8034   0.0421
  -4.000  -0.0960   0.00910   0.00305  -0.0746   0.7991   0.0460
  -3.750  -0.0670   0.00894   0.00287  -0.0750   0.7951   0.0503
  -3.500  -0.0376   0.00882   0.00273  -0.0754   0.7911   0.0533
  -3.250  -0.0082   0.00860   0.00251  -0.0758   0.7868   0.0607
  -3.000   0.0211   0.00843   0.00235  -0.0762   0.7825   0.0709
  -2.750   0.0502   0.00824   0.00221  -0.0767   0.7785   0.0949
  -2.500   0.0795   0.00791   0.00209  -0.0772   0.7741   0.1457
  -2.250   0.1085   0.00747   0.00194  -0.0778   0.7695   0.2369
  -2.000   0.1371   0.00703   0.00186  -0.0784   0.7650   0.3613
  -1.750   0.1666   0.00690   0.00183  -0.0789   0.7602   0.4011
  -1.500   0.1961   0.00681   0.00179  -0.0794   0.7553   0.4263
  -1.250   0.2254   0.00674   0.00174  -0.0798   0.7507   0.4521
  -1.000   0.2549   0.00664   0.00172  -0.0803   0.7461   0.4761
  -0.750   0.2844   0.00653   0.00169  -0.0808   0.7413   0.5071
  -0.500   0.3135   0.00637   0.00168  -0.0813   0.7365   0.5664
  -0.250   0.3421   0.00599   0.00171  -0.0817   0.7318   0.6936
   0.000   0.3682   0.00560   0.00177  -0.0813   0.7266   0.8329
   0.250   0.3881   0.00538   0.00179  -0.0791   0.7213   0.9335
   0.500   0.4166   0.00529   0.00173  -0.0790   0.7156   0.9852
   1.000   0.4842   0.00531   0.00167  -0.0819   0.7035   1.0000
   1.250   0.5130   0.00534   0.00168  -0.0822   0.6968   1.0000
   1.500   0.5416   0.00541   0.00169  -0.0825   0.6899   1.0000
   1.750   0.5706   0.00544   0.00171  -0.0828   0.6822   1.0000
   2.000   0.5994   0.00551   0.00174  -0.0832   0.6749   1.0000
   2.250   0.6284   0.00556   0.00178  -0.0836   0.6665   1.0000
   2.500   0.6573   0.00563   0.00182  -0.0839   0.6578   1.0000
   2.750   0.6861   0.00572   0.00187  -0.0843   0.6484   1.0000
   3.000   0.7151   0.00579   0.00193  -0.0846   0.6388   1.0000
   3.250   0.7438   0.00589   0.00199  -0.0850   0.6276   1.0000
   3.500   0.7724   0.00600   0.00207  -0.0853   0.6153   1.0000
   3.750   0.8010   0.00612   0.00216  -0.0856   0.6026   1.0000
   4.000   0.8294   0.00625   0.00225  -0.0859   0.5861   1.0000
   4.250   0.8574   0.00642   0.00236  -0.0861   0.5654   1.0000
   4.500   0.8849   0.00664   0.00250  -0.0863   0.5402   1.0000
   4.750   0.9119   0.00693   0.00267  -0.0864   0.5087   1.0000
   5.000   0.9379   0.00731   0.00288  -0.0863   0.4689   1.0000
   5.250   0.9634   0.00775   0.00315  -0.0862   0.4268   1.0000
   5.500   0.9880   0.00827   0.00345  -0.0860   0.3782   1.0000
   5.750   1.0112   0.00891   0.00382  -0.0855   0.3237   1.0000
   6.000   1.0345   0.00951   0.00420  -0.0851   0.2760   1.0000
   6.250   1.0574   0.01011   0.00460  -0.0846   0.2322   1.0000
   6.500   1.0797   0.01074   0.00502  -0.0840   0.1910   1.0000
   6.750   1.1012   0.01141   0.00547  -0.0833   0.1509   1.0000
   7.000   1.1225   0.01206   0.00594  -0.0825   0.1164   1.0000
   7.250   1.1439   0.01266   0.00640  -0.0817   0.0901   1.0000
   7.500   1.1650   0.01325   0.00687  -0.0809   0.0694   1.0000
   7.750   1.1863   0.01379   0.00733  -0.0800   0.0546   1.0000
   8.000   1.2074   0.01432   0.00781  -0.0792   0.0440   1.0000
   8.250   1.2284   0.01482   0.00829  -0.0783   0.0370   1.0000
   8.500   1.2484   0.01536   0.00879  -0.0772   0.0318   1.0000
   8.750   1.2693   0.01579   0.00926  -0.0762   0.0291   1.0000
   9.000   1.2887   0.01629   0.00976  -0.0751   0.0265   1.0000
   9.250   1.3057   0.01690   0.01039  -0.0735   0.0234   1.0000
   9.500   1.3245   0.01733   0.01087  -0.0722   0.0218   1.0000
   9.750   1.3380   0.01795   0.01148  -0.0700   0.0195   1.0000
  10.000   1.3516   0.01862   0.01220  -0.0679   0.0172   1.0000
  10.250   1.3665   0.01927   0.01286  -0.0662   0.0152   1.0000
  10.500   1.3782   0.02018   0.01380  -0.0641   0.0133   1.0000
  10.750   1.3932   0.02090   0.01457  -0.0625   0.0123   1.0000
  11.000   1.4065   0.02176   0.01546  -0.0609   0.0113   1.0000
  11.250   1.4147   0.02303   0.01680  -0.0586   0.0103   1.0000
  11.500   1.4281   0.02395   0.01778  -0.0571   0.0100   1.0000
  11.750   1.4409   0.02493   0.01882  -0.0556   0.0095   1.0000
  12.000   1.4531   0.02597   0.01992  -0.0542   0.0091   1.0000
  12.250   1.4647   0.02709   0.02110  -0.0527   0.0086   1.0000
  12.500   1.4740   0.02840   0.02246  -0.0511   0.0082   1.0000
  12.750   1.4786   0.03013   0.02429  -0.0492   0.0078   1.0000
  13.000   1.4804   0.03216   0.02643  -0.0471   0.0076   1.0000
  13.250   1.4892   0.03360   0.02795  -0.0458   0.0074   1.0000
  13.500   1.4969   0.03518   0.02962  -0.0445   0.0073   1.0000
  13.750   1.5033   0.03690   0.03143  -0.0432   0.0071   1.0000
  14.000   1.5091   0.03872   0.03334  -0.0419   0.0069   1.0000
  14.250   1.5142   0.04062   0.03532  -0.0408   0.0067   1.0000
  14.500   1.5187   0.04262   0.03741  -0.0397   0.0065   1.0000
  14.750   1.5229   0.04470   0.03957  -0.0387   0.0063   1.0000
  15.000   1.5256   0.04701   0.04196  -0.0379   0.0061   1.0000
  15.250   1.5258   0.04965   0.04470  -0.0370   0.0059   1.0000
  15.500   1.5221   0.05283   0.04798  -0.0363   0.0058   1.0000
  15.750   1.5129   0.05678   0.05207  -0.0356   0.0056   1.0000
  16.000   1.4990   0.06145   0.05690  -0.0352   0.0055   1.0000
  16.250   1.4941   0.06520   0.06077  -0.0352   0.0054   1.0000
  16.500   1.4926   0.06862   0.06431  -0.0354   0.0053   1.0000
  16.750   1.4894   0.07238   0.06818  -0.0358   0.0053   1.0000
  17.000   1.4841   0.07653   0.07245  -0.0364   0.0052   1.0000
  17.250   1.4780   0.08087   0.07692  -0.0373   0.0052   1.0000
  17.500   1.4706   0.08553   0.08170  -0.0383   0.0051   1.0000
  17.750   1.4614   0.09061   0.08691  -0.0397   0.0050   1.0000
  18.000   1.4512   0.09599   0.09241  -0.0414   0.0050   1.0000
  18.250   1.4403   0.10158   0.09813  -0.0433   0.0049   1.0000
  18.500   1.4275   0.10762   0.10430  -0.0456   0.0049   1.0000
  18.750   1.4147   0.11385   0.11066  -0.0481   0.0048   1.0000
  19.000   1.4002   0.12052   0.11746  -0.0510   0.0048   1.0000
  19.250   1.3863   0.12724   0.12431  -0.0542   0.0048   1.0000
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