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NASA SC(2)-0614 AIRFOIL (sc20614-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0614 AIRFOIL (sc20614-il)
Reynolds number: 500,000
Max Cl/Cd: 64.29 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20614-il-500000-n5.txt
Download as CSV file: xf-sc20614-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0614 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0726   0.11154   0.10754  -0.0362   1.0000   0.0236
 -19.500  -1.0931   0.10386   0.09971  -0.0405   1.0000   0.0237
 -19.250  -1.1110   0.09680   0.09250  -0.0443   1.0000   0.0238
 -19.000  -1.1263   0.09033   0.08590  -0.0478   1.0000   0.0238
 -18.750  -1.1388   0.08444   0.07986  -0.0509   1.0000   0.0240
 -18.500  -1.1491   0.07904   0.07433  -0.0538   1.0000   0.0241
 -18.250  -1.1570   0.07414   0.06930  -0.0563   1.0000   0.0242
 -18.000  -1.1630   0.06963   0.06467  -0.0585   1.0000   0.0243
 -17.750  -1.1693   0.06529   0.06024  -0.0605   1.0000   0.0244
 -17.500  -1.1740   0.06131   0.05617  -0.0622   1.0000   0.0246
 -17.250  -1.1765   0.05772   0.05249  -0.0637   1.0000   0.0248
 -17.000  -1.1772   0.05450   0.04919  -0.0649   1.0000   0.0250
 -16.750  -1.1763   0.05157   0.04619  -0.0658   1.0000   0.0252
 -16.500  -1.1738   0.04893   0.04347  -0.0666   1.0000   0.0255
 -16.250  -1.1701   0.04652   0.04098  -0.0672   1.0000   0.0257
 -16.000  -1.1655   0.04428   0.03867  -0.0676   1.0000   0.0260
 -15.750  -1.1596   0.04226   0.03658  -0.0678   1.0000   0.0262
 -15.500  -1.1531   0.04039   0.03464  -0.0679   1.0000   0.0266
 -15.250  -1.1462   0.03865   0.03282  -0.0679   1.0000   0.0269
 -15.000  -1.1383   0.03704   0.03114  -0.0677   1.0000   0.0273
 -14.750  -1.1298   0.03554   0.02957  -0.0674   1.0000   0.0276
 -14.500  -1.1208   0.03415   0.02810  -0.0669   1.0000   0.0280
 -14.250  -1.1121   0.03281   0.02669  -0.0663   1.0000   0.0283
 -14.000  -1.1059   0.03137   0.02522  -0.0655   1.0000   0.0287
 -13.750  -1.0988   0.03014   0.02396  -0.0644   1.0000   0.0290
 -13.500  -1.0922   0.02904   0.02284  -0.0629   1.0000   0.0294
 -13.250  -1.0865   0.02805   0.02182  -0.0611   1.0000   0.0298
 -13.000  -1.0828   0.02715   0.02089  -0.0588   1.0000   0.0302
 -12.750  -1.0831   0.02634   0.02005  -0.0556   1.0000   0.0306
 -12.500  -1.0907   0.02564   0.01931  -0.0510   1.0000   0.0309
 -12.250  -1.0692   0.02469   0.01832  -0.0518   0.9979   0.0315
 -12.000  -1.0425   0.02378   0.01735  -0.0535   0.9956   0.0322
 -11.750  -1.0152   0.02285   0.01638  -0.0553   0.9936   0.0330
 -11.500  -0.9883   0.02201   0.01554  -0.0569   0.9916   0.0340
 -11.250  -0.9614   0.02128   0.01479  -0.0583   0.9889   0.0351
 -11.000  -0.9326   0.02059   0.01406  -0.0599   0.9865   0.0363
 -10.750  -0.9022   0.01990   0.01333  -0.0618   0.9845   0.0375
 -10.500  -0.8709   0.01920   0.01265  -0.0639   0.9829   0.0389
 -10.250  -0.8385   0.01860   0.01203  -0.0660   0.9817   0.0404
 -10.000  -0.8053   0.01804   0.01144  -0.0682   0.9807   0.0420
  -9.750  -0.7777   0.01747   0.01086  -0.0692   0.9769   0.0435
  -9.500  -0.7464   0.01694   0.01033  -0.0709   0.9744   0.0454
  -9.250  -0.7138   0.01647   0.00984  -0.0727   0.9724   0.0475
  -9.000  -0.6808   0.01597   0.00933  -0.0747   0.9707   0.0495
  -8.750  -0.6472   0.01548   0.00885  -0.0767   0.9691   0.0518
  -8.500  -0.6132   0.01506   0.00841  -0.0787   0.9677   0.0540
  -8.250  -0.5833   0.01465   0.00800  -0.0798   0.9641   0.0560
  -8.000  -0.5522   0.01424   0.00761  -0.0811   0.9610   0.0584
  -7.750  -0.5198   0.01390   0.00726  -0.0826   0.9585   0.0611
  -7.500  -0.4868   0.01352   0.00690  -0.0842   0.9562   0.0639
  -7.250  -0.4532   0.01316   0.00655  -0.0859   0.9542   0.0672
  -7.000  -0.4210   0.01288   0.00625  -0.0872   0.9515   0.0702
  -6.750  -0.3904   0.01254   0.00595  -0.0882   0.9474   0.0742
  -6.500  -0.3586   0.01224   0.00567  -0.0895   0.9440   0.0788
  -6.250  -0.3258   0.01191   0.00539  -0.0909   0.9412   0.0847
  -6.000  -0.2925   0.01162   0.00512  -0.0924   0.9386   0.0914
  -5.750  -0.2608   0.01133   0.00488  -0.0935   0.9348   0.1002
  -5.500  -0.2290   0.01104   0.00464  -0.0947   0.9305   0.1108
  -5.250  -0.1962   0.01073   0.00441  -0.0961   0.9270   0.1257
  -5.000  -0.1629   0.01043   0.00419  -0.0976   0.9241   0.1451
  -4.750  -0.1289   0.01006   0.00395  -0.0993   0.9211   0.1722
  -4.500  -0.0954   0.00970   0.00375  -0.1010   0.9170   0.2069
  -4.250  -0.0608   0.00930   0.00352  -0.1029   0.9130   0.2493
  -4.000  -0.0240   0.00880   0.00326  -0.1055   0.9097   0.3132
  -3.750   0.0153   0.00816   0.00295  -0.1087   0.9070   0.3978
  -3.500   0.0538   0.00765   0.00280  -0.1117   0.9039   0.4898
  -3.250   0.0863   0.00753   0.00283  -0.1127   0.8992   0.5325
  -3.000   0.1177   0.00750   0.00287  -0.1133   0.8944   0.5598
  -2.750   0.1488   0.00751   0.00287  -0.1138   0.8900   0.5770
  -2.500   0.1789   0.00753   0.00291  -0.1141   0.8828   0.5887
  -2.250   0.2092   0.00754   0.00287  -0.1143   0.8742   0.5973
  -2.000   0.2385   0.00757   0.00292  -0.1143   0.8629   0.6056
  -1.750   0.2681   0.00761   0.00290  -0.1144   0.8492   0.6147
  -1.500   0.2969   0.00768   0.00295  -0.1142   0.8345   0.6218
  -1.250   0.3265   0.00776   0.00294  -0.1142   0.8169   0.6288
  -1.000   0.3545   0.00784   0.00298  -0.1139   0.7911   0.6335
  -0.750   0.3826   0.00797   0.00299  -0.1136   0.7616   0.6370
  -0.500   0.4108   0.00812   0.00301  -0.1134   0.7285   0.6403
  -0.250   0.4377   0.00839   0.00302  -0.1129   0.6698   0.6434
   0.000   0.4603   0.00911   0.00315  -0.1118   0.5464   0.6456
   0.250   0.4836   0.00981   0.00340  -0.1110   0.4466   0.6471
   0.500   0.5087   0.01036   0.00362  -0.1106   0.3672   0.6484
   0.750   0.5343   0.01089   0.00383  -0.1102   0.2961   0.6499
   1.000   0.5604   0.01134   0.00404  -0.1099   0.2405   0.6514
   1.250   0.5875   0.01170   0.00422  -0.1098   0.2034   0.6531
   1.500   0.6148   0.01202   0.00440  -0.1097   0.1724   0.6551
   1.750   0.6423   0.01233   0.00458  -0.1096   0.1493   0.6571
   2.000   0.6700   0.01260   0.00475  -0.1095   0.1314   0.6589
   2.250   0.6977   0.01288   0.00493  -0.1095   0.1146   0.6607
   2.500   0.7252   0.01315   0.00512  -0.1094   0.1019   0.6622
   2.750   0.7525   0.01340   0.00534  -0.1092   0.0925   0.6636
   3.000   0.7799   0.01364   0.00556  -0.1090   0.0855   0.6651
   3.250   0.8069   0.01392   0.00580  -0.1088   0.0792   0.6666
   3.500   0.8341   0.01418   0.00604  -0.1086   0.0739   0.6683
   3.750   0.8611   0.01446   0.00629  -0.1083   0.0696   0.6701
   4.000   0.8883   0.01471   0.00653  -0.1081   0.0660   0.6719
   4.250   0.9150   0.01502   0.00681  -0.1078   0.0627   0.6738
   4.500   0.9420   0.01528   0.00707  -0.1076   0.0603   0.6757
   4.750   0.9688   0.01556   0.00733  -0.1073   0.0578   0.6776
   5.000   0.9947   0.01588   0.00765  -0.1069   0.0557   0.6791
   5.250   1.0207   0.01617   0.00797  -0.1064   0.0540   0.6806
   5.500   1.0466   0.01647   0.00830  -0.1060   0.0522   0.6824
   5.750   1.0721   0.01681   0.00865  -0.1055   0.0504   0.6846
   6.000   1.0970   0.01721   0.00904  -0.1049   0.0486   0.6870
   6.250   1.1226   0.01752   0.00938  -0.1044   0.0471   0.6894
   6.500   1.1479   0.01786   0.00975  -0.1038   0.0456   0.6916
   6.750   1.1727   0.01824   0.01012  -0.1033   0.0441   0.6935
   7.000   1.1964   0.01867   0.01056  -0.1025   0.0427   0.6952
   7.250   1.2206   0.01904   0.01098  -0.1017   0.0416   0.6969
   7.500   1.2445   0.01942   0.01142  -0.1009   0.0403   0.6988
   7.750   1.2680   0.01983   0.01185  -0.1001   0.0390   0.7009
   8.000   1.2909   0.02028   0.01231  -0.0992   0.0378   0.7032
   8.250   1.3134   0.02075   0.01281  -0.0982   0.0367   0.7057
   8.500   1.3361   0.02118   0.01329  -0.0973   0.0355   0.7082
   8.750   1.3580   0.02164   0.01379  -0.0962   0.0345   0.7102
   9.000   1.3791   0.02213   0.01432  -0.0950   0.0335   0.7120
   9.250   1.3990   0.02267   0.01489  -0.0937   0.0327   0.7139
   9.500   1.4183   0.02323   0.01551  -0.0922   0.0320   0.7160
   9.750   1.4371   0.02379   0.01613  -0.0906   0.0314   0.7182
  10.000   1.4549   0.02437   0.01678  -0.0889   0.0307   0.7205
  10.250   1.4702   0.02496   0.01742  -0.0868   0.0301   0.7228
  10.500   1.4847   0.02559   0.01810  -0.0845   0.0295   0.7250
  10.750   1.4998   0.02628   0.01885  -0.0825   0.0290   0.7270
  11.000   1.5142   0.02705   0.01967  -0.0804   0.0285   0.7291
  11.250   1.5275   0.02792   0.02060  -0.0783   0.0280   0.7315
  11.500   1.5417   0.02874   0.02151  -0.0763   0.0276   0.7341
  11.750   1.5553   0.02960   0.02246  -0.0744   0.0272   0.7366
  12.000   1.5683   0.03052   0.02346  -0.0724   0.0267   0.7390
  12.250   1.5804   0.03151   0.02453  -0.0705   0.0264   0.7413
  12.500   1.5918   0.03257   0.02568  -0.0685   0.0260   0.7434
  12.750   1.6023   0.03369   0.02689  -0.0665   0.0257   0.7454
  13.000   1.6119   0.03490   0.02819  -0.0646   0.0254   0.7476
  13.250   1.6204   0.03624   0.02961  -0.0626   0.0251   0.7500
  13.500   1.6275   0.03771   0.03117  -0.0607   0.0248   0.7524
  13.750   1.6331   0.03936   0.03289  -0.0588   0.0245   0.7549
  14.000   1.6366   0.04125   0.03487  -0.0569   0.0243   0.7572
  14.250   1.6402   0.04319   0.03691  -0.0552   0.0241   0.7593
  14.500   1.6440   0.04515   0.03900  -0.0537   0.0239   0.7613
  14.750   1.6467   0.04729   0.04129  -0.0523   0.0238   0.7634
  15.000   1.6481   0.04965   0.04378  -0.0511   0.0236   0.7656
  15.250   1.6480   0.05223   0.04650  -0.0501   0.0234   0.7679
  15.500   1.6463   0.05510   0.04949  -0.0493   0.0232   0.7701
  15.750   1.6433   0.05824   0.05277  -0.0488   0.0231   0.7724
  16.000   1.6393   0.06170   0.05636  -0.0487   0.0229   0.7745
  16.250   1.6336   0.06553   0.06034  -0.0489   0.0227   0.7764
  16.500   1.6261   0.06983   0.06479  -0.0497   0.0226   0.7782
  16.750   1.6168   0.07466   0.06978  -0.0510   0.0224   0.7802
  17.000   1.6057   0.08006   0.07535  -0.0529   0.0223   0.7822
  17.250   1.5914   0.08625   0.08170  -0.0555   0.0222   0.7841
  17.500   1.5743   0.09323   0.08885  -0.0589   0.0221   0.7859
  17.750   1.5542   0.10103   0.09683  -0.0630   0.0220   0.7875
  18.000   1.5304   0.10971   0.10569  -0.0678   0.0219   0.7889
  18.250   1.5035   0.11919   0.11535  -0.0733   0.0219   0.7900
  18.500   1.4742   0.12940   0.12575  -0.0796   0.0218   0.7909
  18.750   1.4432   0.14024   0.13677  -0.0866   0.0218   0.7917
  19.000   1.4105   0.15177   0.14848  -0.0944   0.0217   0.7923
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