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SG6051 (sg6051-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: SG6051 (sg6051-il)
Reynolds number: 500,000
Max Cl/Cd: 112.95 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sg6051-il-500000.txt
Download as CSV file: xf-sg6051-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.3230   0.08031   0.07828  -0.0570   0.9814   0.0166
 -10.000  -0.3153   0.07760   0.07557  -0.0585   0.9725   0.0171
  -9.750  -0.4941   0.07008   0.06805  -0.0580   0.9949   0.0123
  -9.250  -0.6192   0.02658   0.02237  -0.0810   0.9445   0.0103
  -9.000  -0.6046   0.02399   0.01938  -0.0799   0.9367   0.0104
  -8.750  -0.5868   0.02218   0.01724  -0.0789   0.9302   0.0106
  -8.500  -0.5658   0.02067   0.01547  -0.0782   0.9240   0.0109
  -8.250  -0.5436   0.01936   0.01393  -0.0776   0.9181   0.0113
  -8.000  -0.5210   0.01827   0.01260  -0.0769   0.9131   0.0117
  -7.750  -0.4959   0.01731   0.01146  -0.0767   0.9074   0.0122
  -7.500  -0.4725   0.01610   0.01008  -0.0762   0.9022   0.0129
  -7.250  -0.4474   0.01544   0.00934  -0.0759   0.8978   0.0137
  -7.000  -0.4204   0.01487   0.00868  -0.0760   0.8926   0.0150
  -6.750  -0.3944   0.01416   0.00785  -0.0758   0.8877   0.0167
  -6.250  -0.3389   0.01376   0.00742  -0.0760   0.8786   0.0258
  -6.000  -0.3111   0.01355   0.00721  -0.0762   0.8739   0.0309
  -5.750  -0.2833   0.01344   0.00699  -0.0762   0.8697   0.0341
  -5.500  -0.2558   0.01302   0.00656  -0.0765   0.8651   0.0377
  -5.250  -0.2274   0.01287   0.00637  -0.0767   0.8602   0.0409
  -5.000  -0.1998   0.01255   0.00598  -0.0768   0.8560   0.0448
  -4.750  -0.1718   0.01233   0.00575  -0.0770   0.8519   0.0491
  -4.500  -0.1431   0.01210   0.00547  -0.0773   0.8471   0.0523
  -4.250  -0.1151   0.01170   0.00500  -0.0775   0.8428   0.0553
  -4.000  -0.0873   0.01130   0.00455  -0.0776   0.8390   0.0598
  -3.750  -0.0583   0.01106   0.00428  -0.0780   0.8344   0.0642
  -3.500  -0.0296   0.01074   0.00394  -0.0783   0.8298   0.0711
  -3.250  -0.0010   0.01053   0.00368  -0.0785   0.8258   0.0797
  -3.000   0.0276   0.01017   0.00343  -0.0788   0.8217   0.1058
  -2.750   0.0559   0.00957   0.00321  -0.0794   0.8170   0.1985
  -2.500   0.0835   0.00888   0.00308  -0.0800   0.8127   0.3679
  -2.250   0.1121   0.00874   0.00302  -0.0802   0.8089   0.4212
  -2.000   0.1412   0.00857   0.00296  -0.0807   0.8041   0.4592
  -1.750   0.1700   0.00840   0.00289  -0.0810   0.7994   0.4964
  -1.500   0.1986   0.00824   0.00282  -0.0813   0.7952   0.5372
  -1.250   0.2272   0.00803   0.00280  -0.0816   0.7905   0.5976
  -1.000   0.2548   0.00771   0.00279  -0.0816   0.7853   0.6872
  -0.750   0.2785   0.00731   0.00282  -0.0805   0.7809   0.8196
  -0.500   0.2974   0.00706   0.00283  -0.0777   0.7761   0.9309
  -0.250   0.3403   0.00699   0.00276  -0.0808   0.7713   0.9945
   0.000   0.3769   0.00698   0.00268  -0.0829   0.7668   1.0000
   0.250   0.4039   0.00701   0.00265  -0.0828   0.7620   1.0000
   0.500   0.4315   0.00703   0.00263  -0.0829   0.7563   1.0000
   0.750   0.4593   0.00706   0.00259  -0.0830   0.7514   1.0000
   1.000   0.4874   0.00710   0.00260  -0.0832   0.7457   1.0000
   1.250   0.5157   0.00713   0.00260  -0.0834   0.7395   1.0000
   1.500   0.5440   0.00719   0.00260  -0.0835   0.7339   1.0000
   1.750   0.5725   0.00722   0.00263  -0.0838   0.7270   1.0000
   2.000   0.6009   0.00728   0.00263  -0.0840   0.7208   1.0000
   2.250   0.6295   0.00732   0.00268  -0.0843   0.7130   1.0000
   2.500   0.6579   0.00739   0.00269  -0.0845   0.7060   1.0000
   2.750   0.6865   0.00743   0.00276  -0.0847   0.6975   1.0000
   3.000   0.7149   0.00750   0.00280  -0.0849   0.6897   1.0000
   3.250   0.7434   0.00755   0.00286  -0.0852   0.6800   1.0000
   3.500   0.7718   0.00762   0.00293  -0.0854   0.6707   1.0000
   3.750   0.7999   0.00771   0.00299  -0.0856   0.6605   1.0000
   4.000   0.8281   0.00779   0.00307  -0.0857   0.6484   1.0000
   4.250   0.8561   0.00789   0.00317  -0.0859   0.6360   1.0000
   4.500   0.8838   0.00800   0.00328  -0.0860   0.6213   1.0000
   4.750   0.9112   0.00815   0.00340  -0.0860   0.6042   1.0000
   5.000   0.9384   0.00831   0.00354  -0.0860   0.5850   1.0000
   5.250   0.9646   0.00854   0.00370  -0.0859   0.5591   1.0000
   5.500   0.9899   0.00885   0.00390  -0.0856   0.5233   1.0000
   5.750   1.0143   0.00925   0.00415  -0.0852   0.4862   1.0000
   6.000   1.0376   0.00974   0.00448  -0.0846   0.4430   1.0000
   6.250   1.0590   0.01040   0.00491  -0.0838   0.3891   1.0000
   6.500   1.0785   0.01121   0.00543  -0.0827   0.3291   1.0000
   6.750   1.0974   0.01205   0.00598  -0.0816   0.2741   1.0000
   7.000   1.1159   0.01288   0.00657  -0.0804   0.2248   1.0000
   7.250   1.1338   0.01373   0.00718  -0.0791   0.1805   1.0000
   7.500   1.1507   0.01459   0.00783  -0.0776   0.1393   1.0000
   7.750   1.1669   0.01547   0.00850  -0.0760   0.1040   1.0000
   8.000   1.1825   0.01632   0.00920  -0.0743   0.0773   1.0000
   8.250   1.1975   0.01716   0.00992  -0.0725   0.0598   1.0000
   8.500   1.2128   0.01792   0.01066  -0.0706   0.0500   1.0000
   8.750   1.2285   0.01856   0.01133  -0.0688   0.0444   1.0000
   9.000   1.2374   0.01950   0.01225  -0.0659   0.0390   1.0000
   9.250   1.2534   0.02009   0.01292  -0.0642   0.0361   1.0000
   9.500   1.2658   0.02095   0.01378  -0.0622   0.0326   1.0000
   9.750   1.2767   0.02196   0.01487  -0.0600   0.0296   1.0000
  10.000   1.2910   0.02278   0.01575  -0.0584   0.0270   1.0000
  10.250   1.2978   0.02416   0.01715  -0.0560   0.0241   1.0000
  10.500   1.3093   0.02526   0.01835  -0.0542   0.0221   1.0000
  10.750   1.3210   0.02637   0.01951  -0.0526   0.0202   1.0000
  11.000   1.3263   0.02800   0.02118  -0.0504   0.0186   1.0000
  11.250   1.3323   0.02964   0.02292  -0.0484   0.0174   1.0000
  11.500   1.3435   0.03087   0.02425  -0.0470   0.0164   1.0000
  11.750   1.3532   0.03225   0.02570  -0.0456   0.0155   1.0000
  12.000   1.3611   0.03379   0.02731  -0.0441   0.0148   1.0000
  12.250   1.3637   0.03584   0.02941  -0.0422   0.0141   1.0000
  12.500   1.3608   0.03847   0.03216  -0.0399   0.0136   1.0000
  12.750   1.3688   0.04014   0.03395  -0.0387   0.0133   1.0000
  13.000   1.3749   0.04200   0.03593  -0.0374   0.0129   1.0000
  13.250   1.3803   0.04397   0.03801  -0.0362   0.0124   1.0000
  13.500   1.3855   0.04600   0.04014  -0.0352   0.0120   1.0000
  13.750   1.3903   0.04807   0.04231  -0.0343   0.0116   1.0000
  14.000   1.3941   0.05027   0.04459  -0.0335   0.0112   1.0000
  14.250   1.3959   0.05276   0.04716  -0.0327   0.0109   1.0000
  14.500   1.3936   0.05578   0.05028  -0.0317   0.0106   1.0000
  14.750   1.3852   0.05955   0.05419  -0.0302   0.0103   1.0000
  15.000   1.3857   0.06248   0.05728  -0.0299   0.0101   1.0000
  15.250   1.3848   0.06567   0.06064  -0.0296   0.0100   1.0000
  15.500   1.3823   0.06916   0.06429  -0.0296   0.0098   1.0000
  15.750   1.3780   0.07295   0.06825  -0.0297   0.0096   1.0000
  16.000   1.3725   0.07703   0.07250  -0.0300   0.0095   1.0000
  16.250   1.3657   0.08143   0.07707  -0.0307   0.0093   1.0000
  16.500   1.3580   0.08613   0.08193  -0.0317   0.0092   1.0000
  16.750   1.3493   0.09110   0.08707  -0.0330   0.0091   1.0000
  17.000   1.3392   0.09645   0.09258  -0.0347   0.0089   1.0000
  17.250   1.3291   0.10203   0.09831  -0.0368   0.0088   1.0000
  17.500   1.3180   0.10798   0.10442  -0.0393   0.0087   1.0000
  17.750   1.3055   0.11439   0.11099  -0.0422   0.0086   1.0000
  18.000   1.2919   0.12119   0.11795  -0.0456   0.0086   1.0000
  18.250   1.2788   0.12816   0.12508  -0.0493   0.0085   1.0000
  18.500   1.2620   0.13620   0.13328  -0.0538   0.0085   1.0000
  18.750   1.2443   0.14486   0.14212  -0.0590   0.0085   1.0000
  19.000   1.2185   0.15598   0.15346  -0.0658   0.0086   1.0000
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