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NASA SC(2)-0614 AIRFOIL (sc20614-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0614 AIRFOIL (sc20614-il)
Reynolds number: 200,000
Max Cl/Cd: 44.47 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20614-il-200000-n5.txt
Download as CSV file: xf-sc20614-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.9142   0.09122   0.08596  -0.0521   1.0000   0.0346
 -16.500  -0.9533   0.08016   0.07460  -0.0590   1.0000   0.0347
 -16.250  -0.9745   0.07312   0.06733  -0.0629   1.0000   0.0348
 -16.000  -0.9892   0.06757   0.06158  -0.0657   1.0000   0.0351
 -15.750  -1.0000   0.06294   0.05676  -0.0677   1.0000   0.0354
 -15.500  -1.0081   0.05892   0.05256  -0.0692   1.0000   0.0357
 -15.250  -1.0142   0.05542   0.04887  -0.0701   1.0000   0.0361
 -15.000  -1.0179   0.05230   0.04557  -0.0706   1.0000   0.0365
 -14.750  -1.0199   0.04948   0.04256  -0.0708   1.0000   0.0369
 -14.500  -1.0196   0.04699   0.03988  -0.0708   1.0000   0.0373
 -14.250  -1.0139   0.04521   0.03808  -0.0705   1.0000   0.0377
 -14.000  -1.0081   0.04354   0.03637  -0.0702   1.0000   0.0382
 -13.750  -1.0021   0.04196   0.03474  -0.0697   1.0000   0.0387
 -13.500  -0.9961   0.04046   0.03318  -0.0689   1.0000   0.0393
 -13.250  -0.9903   0.03902   0.03166  -0.0680   1.0000   0.0400
 -13.000  -0.9847   0.03764   0.03019  -0.0668   1.0000   0.0407
 -12.750  -0.9793   0.03634   0.02878  -0.0652   1.0000   0.0415
 -12.500  -0.9741   0.03513   0.02743  -0.0634   1.0000   0.0422
 -12.250  -0.9693   0.03403   0.02628  -0.0613   1.0000   0.0428
 -12.000  -0.9666   0.03309   0.02534  -0.0588   1.0000   0.0433
 -11.750  -0.9667   0.03226   0.02450  -0.0557   1.0000   0.0439
 -11.500  -0.9673   0.03147   0.02370  -0.0523   1.0000   0.0445
 -11.250  -0.9624   0.03062   0.02281  -0.0500   1.0000   0.0452
 -11.000  -0.9554   0.02978   0.02191  -0.0479   1.0000   0.0462
 -10.750  -0.9462   0.02896   0.02102  -0.0461   1.0000   0.0473
 -10.500  -0.9350   0.02816   0.02013  -0.0445   1.0000   0.0485
 -10.250  -0.9168   0.02728   0.01928  -0.0444   0.9991   0.0498
 -10.000  -0.8876   0.02643   0.01840  -0.0463   0.9967   0.0515
  -9.750  -0.8579   0.02563   0.01753  -0.0480   0.9944   0.0535
  -9.500  -0.8277   0.02482   0.01666  -0.0497   0.9923   0.0555
  -9.250  -0.7988   0.02403   0.01588  -0.0513   0.9893   0.0573
  -9.000  -0.7684   0.02337   0.01519  -0.0530   0.9865   0.0598
  -8.750  -0.7371   0.02274   0.01449  -0.0546   0.9841   0.0625
  -8.500  -0.7049   0.02204   0.01383  -0.0567   0.9821   0.0652
  -8.250  -0.6718   0.02146   0.01321  -0.0588   0.9803   0.0683
  -8.000  -0.6436   0.02089   0.01261  -0.0597   0.9764   0.0712
  -7.750  -0.6123   0.02027   0.01203  -0.0614   0.9734   0.0746
  -7.500  -0.5796   0.01978   0.01151  -0.0632   0.9711   0.0786
  -7.250  -0.5456   0.01919   0.01096  -0.0654   0.9693   0.0828
  -7.000  -0.5103   0.01870   0.01047  -0.0677   0.9678   0.0879
  -6.750  -0.4805   0.01821   0.01000  -0.0689   0.9639   0.0930
  -6.500  -0.4483   0.01774   0.00955  -0.0705   0.9607   0.0994
  -6.250  -0.4140   0.01724   0.00910  -0.0726   0.9584   0.1072
  -6.000  -0.3785   0.01678   0.00869  -0.0749   0.9565   0.1171
  -5.750  -0.3417   0.01630   0.00828  -0.0775   0.9551   0.1315
  -5.500  -0.3037   0.01577   0.00787  -0.0804   0.9539   0.1521
  -5.250  -0.2669   0.01523   0.00749  -0.0831   0.9519   0.1821
  -5.000  -0.2339   0.01466   0.00714  -0.0851   0.9479   0.2263
  -4.750  -0.1940   0.01387   0.00672  -0.0889   0.9461   0.2988
  -4.500  -0.1510   0.01298   0.00636  -0.0935   0.9450   0.4046
  -4.250  -0.1147   0.01270   0.00658  -0.0955   0.9431   0.5084
  -4.000  -0.0817   0.01281   0.00685  -0.0962   0.9409   0.5507
  -3.750  -0.0451   0.01285   0.00686  -0.0979   0.9391   0.5777
  -3.500  -0.0132   0.01295   0.00696  -0.0986   0.9359   0.5930
  -3.250   0.0147   0.01311   0.00713  -0.0984   0.9311   0.6037
  -3.000   0.0468   0.01325   0.00727  -0.0990   0.9280   0.6165
  -2.750   0.0808   0.01338   0.00738  -0.1001   0.9256   0.6289
  -2.500   0.1109   0.01362   0.00768  -0.0999   0.9232   0.6357
  -2.250   0.1414   0.01381   0.00786  -0.1002   0.9190   0.6467
  -2.000   0.1649   0.01416   0.00828  -0.0985   0.9134   0.6522
  -1.750   0.1980   0.01418   0.00829  -0.0994   0.9099   0.6579
  -1.500   0.2349   0.01405   0.00814  -0.1012   0.9070   0.6629
  -1.250   0.2602   0.01415   0.00829  -0.1001   0.8992   0.6654
  -1.000   0.2923   0.01403   0.00819  -0.1004   0.8921   0.6682
  -0.750   0.3231   0.01382   0.00798  -0.1005   0.8800   0.6710
  -0.500   0.3566   0.01352   0.00763  -0.1012   0.8655   0.6738
  -0.250   0.3914   0.01320   0.00724  -0.1023   0.8472   0.6777
   0.000   0.4197   0.01309   0.00711  -0.1017   0.8276   0.6791
   0.250   0.4479   0.01303   0.00704  -0.1012   0.8069   0.6807
   0.500   0.4768   0.01299   0.00696  -0.1009   0.7853   0.6824
   0.750   0.5055   0.01297   0.00687  -0.1006   0.7553   0.6842
   1.000   0.5339   0.01300   0.00675  -0.1002   0.7065   0.6861
   1.250   0.5585   0.01335   0.00659  -0.0991   0.5991   0.6883
   1.500   0.5773   0.01427   0.00675  -0.0974   0.4631   0.6909
   1.750   0.5995   0.01507   0.00702  -0.0967   0.3646   0.6937
   2.000   0.6204   0.01578   0.00738  -0.0954   0.2877   0.6951
   2.250   0.6433   0.01638   0.00770  -0.0946   0.2331   0.6966
   2.500   0.6675   0.01688   0.00800  -0.0940   0.1934   0.6981
   3.000   0.7186   0.01774   0.00859  -0.0934   0.1427   0.7018
   3.250   0.7452   0.01811   0.00889  -0.0932   0.1264   0.7040
   3.500   0.7723   0.01849   0.00918  -0.0933   0.1135   0.7064
   3.750   0.8000   0.01889   0.00949  -0.0935   0.1036   0.7090
   4.000   0.8254   0.01925   0.00986  -0.0930   0.0967   0.7104
   4.250   0.8493   0.01972   0.01028  -0.0923   0.0909   0.7118
   4.500   0.8742   0.02009   0.01071  -0.0916   0.0859   0.7134
   4.750   0.8983   0.02056   0.01116  -0.0910   0.0815   0.7153
   5.000   0.9228   0.02102   0.01163  -0.0904   0.0778   0.7175
   5.250   0.9479   0.02146   0.01209  -0.0899   0.0741   0.7200
   5.500   0.9722   0.02202   0.01260  -0.0895   0.0711   0.7226
   5.750   0.9982   0.02248   0.01310  -0.0893   0.0683   0.7255
   6.000   1.0210   0.02296   0.01363  -0.0883   0.0657   0.7271
   6.250   1.0433   0.02351   0.01419  -0.0874   0.0634   0.7287
   6.500   1.0658   0.02409   0.01481  -0.0864   0.0612   0.7305
   6.750   1.0889   0.02462   0.01541  -0.0856   0.0590   0.7325
   7.000   1.1116   0.02518   0.01600  -0.0848   0.0570   0.7347
   7.250   1.1334   0.02585   0.01666  -0.0840   0.0554   0.7371
   7.500   1.1563   0.02653   0.01740  -0.0832   0.0538   0.7397
   7.750   1.1787   0.02719   0.01813  -0.0824   0.0519   0.7422
   8.000   1.1986   0.02782   0.01883  -0.0811   0.0504   0.7440
   8.250   1.2175   0.02853   0.01956  -0.0797   0.0490   0.7460
   8.500   1.2368   0.02934   0.02045  -0.0784   0.0477   0.7482
   8.750   1.2563   0.03014   0.02138  -0.0772   0.0463   0.7506
   9.000   1.2752   0.03097   0.02229  -0.0759   0.0451   0.7531
   9.250   1.2931   0.03180   0.02317  -0.0745   0.0441   0.7557
   9.500   1.3091   0.03266   0.02405  -0.0729   0.0433   0.7585
   9.750   1.3218   0.03363   0.02506  -0.0706   0.0425   0.7602
  10.000   1.3365   0.03465   0.02628  -0.0687   0.0416   0.7622
  10.250   1.3506   0.03572   0.02752  -0.0668   0.0406   0.7644
  10.500   1.3641   0.03680   0.02872  -0.0650   0.0397   0.7671
  10.750   1.3770   0.03789   0.02992  -0.0632   0.0389   0.7700
  11.000   1.3893   0.03902   0.03111  -0.0615   0.0382   0.7731
  11.250   1.4008   0.04023   0.03238  -0.0598   0.0377   0.7757
  11.500   1.4104   0.04161   0.03381  -0.0578   0.0372   0.7776
  11.750   1.4180   0.04329   0.03574  -0.0557   0.0367   0.7797
  12.000   1.4243   0.04510   0.03778  -0.0537   0.0361   0.7820
  12.250   1.4292   0.04703   0.03992  -0.0517   0.0356   0.7844
  12.500   1.4327   0.04909   0.04217  -0.0499   0.0351   0.7870
  12.750   1.4350   0.05128   0.04454  -0.0483   0.0347   0.7897
  13.000   1.4361   0.05360   0.04702  -0.0468   0.0343   0.7922
  13.250   1.4357   0.05600   0.04959  -0.0453   0.0339   0.7941
  13.500   1.4345   0.05854   0.05228  -0.0441   0.0336   0.7962
  13.750   1.4327   0.06124   0.05512  -0.0432   0.0333   0.7984
  14.000   1.4301   0.06416   0.05816  -0.0426   0.0330   0.8008
  14.250   1.4271   0.06725   0.06136  -0.0424   0.0328   0.8034
  14.500   1.4225   0.07071   0.06492  -0.0425   0.0325   0.8060
  14.750   1.4094   0.07557   0.07000  -0.0433   0.0323   0.8084
  15.000   1.3882   0.08184   0.07659  -0.0453   0.0321   0.8099
  15.250   1.3632   0.08943   0.08449  -0.0487   0.0320   0.8113
  15.500   1.3326   0.09895   0.09433  -0.0542   0.0319   0.8125
  15.750   1.2898   0.11216   0.10790  -0.0631   0.0319   0.8131
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