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SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il)
Reynolds number: 200,000
Max Cl/Cd: 43.75 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nasasc2-0714-il-200000-n5.txt
Download as CSV file: xf-nasasc2-0714-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SC(2)-0714 Supercritical airfoil (coordinates fr
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8390   0.09522   0.09007  -0.0598   1.0000   0.0347
 -16.500  -0.8944   0.08117   0.07567  -0.0685   1.0000   0.0347
 -16.250  -0.9245   0.07305   0.06728  -0.0728   1.0000   0.0348
 -16.000  -0.9470   0.06692   0.06091  -0.0756   1.0000   0.0351
 -15.750  -0.9648   0.06201   0.05576  -0.0771   1.0000   0.0353
 -15.500  -0.9796   0.05796   0.05148  -0.0778   1.0000   0.0356
 -15.250  -0.9820   0.05550   0.04897  -0.0776   1.0000   0.0359
 -15.000  -0.9835   0.05329   0.04672  -0.0771   1.0000   0.0362
 -14.750  -0.9849   0.05124   0.04461  -0.0764   1.0000   0.0365
 -14.500  -0.9862   0.04933   0.04263  -0.0755   1.0000   0.0369
 -14.250  -0.9880   0.04749   0.04072  -0.0743   1.0000   0.0372
 -14.000  -0.9901   0.04575   0.03890  -0.0728   1.0000   0.0376
 -13.750  -0.9920   0.04411   0.03717  -0.0710   1.0000   0.0380
 -13.500  -0.9941   0.04258   0.03555  -0.0690   1.0000   0.0385
 -13.250  -0.9963   0.04114   0.03400  -0.0667   1.0000   0.0389
 -13.000  -0.9985   0.03980   0.03256  -0.0641   1.0000   0.0394
 -12.750  -1.0012   0.03857   0.03120  -0.0612   1.0000   0.0400
 -12.500  -1.0051   0.03745   0.02996  -0.0580   1.0000   0.0405
 -12.250  -1.0106   0.03644   0.02883  -0.0543   1.0000   0.0410
 -12.000  -1.0117   0.03542   0.02774  -0.0512   1.0000   0.0415
 -11.750  -1.0064   0.03442   0.02675  -0.0491   1.0000   0.0421
 -11.500  -0.9962   0.03345   0.02577  -0.0479   0.9996   0.0428
 -11.250  -0.9731   0.03239   0.02466  -0.0490   0.9978   0.0437
 -11.000  -0.9493   0.03136   0.02356  -0.0501   0.9959   0.0448
 -10.750  -0.9244   0.03037   0.02246  -0.0511   0.9942   0.0459
 -10.500  -0.8984   0.02945   0.02141  -0.0522   0.9927   0.0472
 -10.250  -0.8750   0.02850   0.02043  -0.0528   0.9905   0.0484
 -10.000  -0.8495   0.02765   0.01958  -0.0538   0.9882   0.0496
  -9.750  -0.8227   0.02688   0.01879  -0.0550   0.9861   0.0511
  -9.500  -0.7953   0.02615   0.01800  -0.0561   0.9844   0.0526
  -9.250  -0.7669   0.02545   0.01723  -0.0573   0.9829   0.0542
  -9.000  -0.7379   0.02472   0.01648  -0.0587   0.9817   0.0559
  -8.750  -0.7109   0.02403   0.01581  -0.0598   0.9796   0.0577
  -8.500  -0.6843   0.02342   0.01518  -0.0607   0.9769   0.0598
  -8.250  -0.6556   0.02283   0.01456  -0.0618   0.9747   0.0619
  -8.000  -0.6258   0.02222   0.01392  -0.0632   0.9730   0.0641
  -7.750  -0.5943   0.02161   0.01335  -0.0651   0.9714   0.0670
  -7.500  -0.5613   0.02110   0.01284  -0.0671   0.9701   0.0705
  -7.250  -0.5272   0.02057   0.01229  -0.0693   0.9689   0.0741
  -7.000  -0.4922   0.02004   0.01181  -0.0718   0.9679   0.0787
  -6.750  -0.4661   0.01965   0.01139  -0.0722   0.9647   0.0835
  -6.500  -0.4345   0.01914   0.01095  -0.0739   0.9624   0.0900
  -6.250  -0.4013   0.01873   0.01055  -0.0758   0.9604   0.0977
  -6.000  -0.3669   0.01832   0.01018  -0.0780   0.9588   0.1076
  -5.750  -0.3312   0.01787   0.00982  -0.0804   0.9575   0.1205
  -5.500  -0.2943   0.01744   0.00948  -0.0831   0.9563   0.1376
  -5.250  -0.2558   0.01695   0.00913  -0.0863   0.9553   0.1637
  -5.000  -0.2150   0.01633   0.00877  -0.0902   0.9547   0.2107
  -4.750  -0.1696   0.01546   0.00834  -0.0955   0.9544   0.2969
  -4.500  -0.1209   0.01448   0.00813  -0.1016   0.9546   0.4486
  -4.250  -0.0925   0.01472   0.00882  -0.1012   0.9526   0.5340
  -4.000  -0.0686   0.01496   0.00911  -0.1003   0.9482   0.5686
  -3.750  -0.0393   0.01520   0.00937  -0.1003   0.9451   0.5882
  -3.500  -0.0060   0.01534   0.00948  -0.1014   0.9428   0.6022
  -3.250   0.0285   0.01546   0.00956  -0.1027   0.9411   0.6129
  -3.000   0.0609   0.01569   0.00979  -0.1032   0.9394   0.6207
  -2.750   0.0941   0.01591   0.00999  -0.1041   0.9367   0.6338
  -2.500   0.1082   0.01649   0.01066  -0.1003   0.9295   0.6405
  -2.250   0.1415   0.01672   0.01088  -0.1012   0.9270   0.6514
  -2.000   0.1702   0.01698   0.01119  -0.1005   0.9246   0.6543
  -1.750   0.2057   0.01699   0.01122  -0.1017   0.9229   0.6569
  -1.500   0.2288   0.01702   0.01126  -0.1005   0.9145   0.6604
  -1.250   0.2717   0.01666   0.01088  -0.1036   0.9107   0.6651
  -1.000   0.3176   0.01622   0.01043  -0.1072   0.9080   0.6684
  -0.750   0.3452   0.01604   0.01029  -0.1065   0.8988   0.6698
  -0.500   0.3894   0.01535   0.00961  -0.1086   0.8888   0.6711
  -0.250   0.4190   0.01495   0.00922  -0.1081   0.8705   0.6727
   0.000   0.4512   0.01465   0.00894  -0.1084   0.8539   0.6743
   0.250   0.4836   0.01439   0.00868  -0.1089   0.8339   0.6760
   0.500   0.5232   0.01402   0.00823  -0.1107   0.8001   0.6779
   0.750   0.5656   0.01376   0.00769  -0.1130   0.7279   0.6799
   1.000   0.5951   0.01416   0.00743  -0.1129   0.6082   0.6825
   1.250   0.6155   0.01497   0.00755  -0.1117   0.4855   0.6856
   1.500   0.6318   0.01579   0.00791  -0.1094   0.3916   0.6866
   1.750   0.6502   0.01655   0.00827  -0.1077   0.3068   0.6878
   2.000   0.6709   0.01721   0.00862  -0.1064   0.2428   0.6891
   2.250   0.6937   0.01776   0.00893  -0.1055   0.1970   0.6905
   2.500   0.7172   0.01826   0.00925  -0.1048   0.1638   0.6923
   2.750   0.7418   0.01870   0.00957  -0.1042   0.1405   0.6945
   3.000   0.7677   0.01911   0.00988  -0.1040   0.1230   0.6969
   3.250   0.7950   0.01947   0.01016  -0.1041   0.1100   0.6990
   3.500   0.8233   0.01981   0.01044  -0.1045   0.1000   0.7012
   3.750   0.8509   0.02020   0.01076  -0.1048   0.0924   0.7031
   4.000   0.8752   0.02056   0.01114  -0.1040   0.0864   0.7040
   4.250   0.8987   0.02101   0.01155  -0.1032   0.0816   0.7050
   4.500   0.9230   0.02139   0.01198  -0.1025   0.0775   0.7061
   4.750   0.9468   0.02183   0.01242  -0.1017   0.0739   0.7073
   5.000   0.9700   0.02234   0.01291  -0.1009   0.0707   0.7087
   5.250   0.9940   0.02278   0.01340  -0.1002   0.0678   0.7102
   5.500   1.0177   0.02326   0.01391  -0.0995   0.0652   0.7121
   5.750   1.0406   0.02387   0.01448  -0.0988   0.0629   0.7141
   6.000   1.0646   0.02444   0.01508  -0.0982   0.0608   0.7161
   6.250   1.0894   0.02497   0.01567  -0.0979   0.0585   0.7182
   6.500   1.1142   0.02555   0.01624  -0.0976   0.0564   0.7203
   6.750   1.1344   0.02621   0.01692  -0.0963   0.0548   0.7213
   7.000   1.1546   0.02700   0.01774  -0.0950   0.0534   0.7224
   7.250   1.1759   0.02764   0.01850  -0.0939   0.0519   0.7236
   7.500   1.1967   0.02832   0.01926  -0.0927   0.0503   0.7249
   7.750   1.2169   0.02900   0.01999  -0.0914   0.0489   0.7264
   8.000   1.2363   0.02972   0.02074  -0.0902   0.0477   0.7280
   8.250   1.2548   0.03065   0.02166  -0.0888   0.0466   0.7297
   8.500   1.2743   0.03144   0.02260  -0.0875   0.0456   0.7316
   8.750   1.2928   0.03231   0.02359  -0.0861   0.0445   0.7338
   9.000   1.3106   0.03320   0.02458  -0.0846   0.0435   0.7362
   9.250   1.3273   0.03408   0.02554  -0.0830   0.0425   0.7381
   9.500   1.3422   0.03495   0.02649  -0.0811   0.0417   0.7394
   9.750   1.3567   0.03586   0.02745  -0.0792   0.0410   0.7408
  10.000   1.3709   0.03696   0.02859  -0.0774   0.0403   0.7423
  10.250   1.3849   0.03814   0.02998  -0.0756   0.0395   0.7439
  10.500   1.3978   0.03942   0.03145  -0.0737   0.0387   0.7456
  10.750   1.4097   0.04077   0.03297  -0.0717   0.0380   0.7474
  11.000   1.4205   0.04218   0.03452  -0.0698   0.0374   0.7494
  11.250   1.4303   0.04362   0.03611  -0.0678   0.0368   0.7514
  11.500   1.4393   0.04511   0.03771  -0.0659   0.0364   0.7535
  11.750   1.4467   0.04665   0.03936  -0.0639   0.0359   0.7553
  12.000   1.4524   0.04822   0.04105  -0.0618   0.0356   0.7568
  12.250   1.4575   0.04990   0.04284  -0.0597   0.0352   0.7584
  12.500   1.4616   0.05175   0.04478  -0.0578   0.0349   0.7601
  12.750   1.4619   0.05409   0.04729  -0.0558   0.0345   0.7619
  13.000   1.4572   0.05697   0.05046  -0.0538   0.0342   0.7636
  13.250   1.4500   0.06020   0.05396  -0.0522   0.0338   0.7654
  13.500   1.4407   0.06382   0.05785  -0.0510   0.0334   0.7670
  13.750   1.4287   0.06791   0.06220  -0.0503   0.0331   0.7687
  14.000   1.4145   0.07255   0.06709  -0.0503   0.0329   0.7702
  14.250   1.3971   0.07795   0.07275  -0.0513   0.0326   0.7717
  14.500   1.3754   0.08436   0.07942  -0.0533   0.0325   0.7725
  14.750   1.3478   0.09252   0.08788  -0.0572   0.0323   0.7732
  15.000   1.3071   0.10440   0.10012  -0.0646   0.0323   0.7736
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