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NASA SC(2)-0414 AIRFOIL (sc20414-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0414 AIRFOIL (sc20414-il)
Reynolds number: 500,000
Max Cl/Cd: 63.37 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20414-il-500000-n5.txt
Download as CSV file: xf-sc20414-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0414 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  -1.1232   0.12246   0.11854  -0.0177   1.0000   0.0232
 -19.500  -1.1430   0.11474   0.11071  -0.0220   1.0000   0.0233
 -19.250  -1.1620   0.10738   0.10322  -0.0260   1.0000   0.0234
 -19.000  -1.1793   0.10037   0.09609  -0.0298   1.0000   0.0235
 -18.750  -1.1950   0.09379   0.08939  -0.0333   1.0000   0.0237
 -18.500  -1.2086   0.08770   0.08317  -0.0365   1.0000   0.0238
 -18.250  -1.2196   0.08212   0.07748  -0.0394   1.0000   0.0239
 -18.000  -1.2284   0.07702   0.07227  -0.0419   1.0000   0.0241
 -17.750  -1.2352   0.07238   0.06750  -0.0441   1.0000   0.0242
 -17.500  -1.2400   0.06813   0.06315  -0.0460   1.0000   0.0244
 -17.250  -1.2430   0.06429   0.05921  -0.0476   1.0000   0.0246
 -17.000  -1.2446   0.06078   0.05559  -0.0489   1.0000   0.0249
 -16.750  -1.2447   0.05754   0.05225  -0.0501   1.0000   0.0251
 -16.500  -1.2435   0.05456   0.04918  -0.0510   1.0000   0.0253
 -16.250  -1.2412   0.05182   0.04633  -0.0517   1.0000   0.0256
 -16.000  -1.2377   0.04930   0.04372  -0.0522   1.0000   0.0259
 -15.750  -1.2326   0.04702   0.04134  -0.0526   1.0000   0.0261
 -15.500  -1.2266   0.04491   0.03913  -0.0528   1.0000   0.0264
 -15.250  -1.2215   0.04278   0.03693  -0.0530   1.0000   0.0267
 -15.000  -1.2163   0.04076   0.03486  -0.0530   1.0000   0.0271
 -14.750  -1.2093   0.03896   0.03300  -0.0529   1.0000   0.0275
 -14.500  -1.2008   0.03733   0.03133  -0.0528   1.0000   0.0278
 -14.250  -1.1910   0.03585   0.02979  -0.0526   1.0000   0.0283
 -14.000  -1.1808   0.03443   0.02832  -0.0523   1.0000   0.0287
 -13.750  -1.1697   0.03311   0.02694  -0.0519   1.0000   0.0291
 -13.500  -1.1582   0.03185   0.02561  -0.0515   1.0000   0.0295
 -13.250  -1.1461   0.03067   0.02437  -0.0510   1.0000   0.0300
 -13.000  -1.1333   0.02956   0.02320  -0.0505   1.0000   0.0304
 -12.750  -1.1212   0.02843   0.02202  -0.0499   1.0000   0.0309
 -12.500  -1.1093   0.02733   0.02090  -0.0492   1.0000   0.0314
 -12.250  -1.0966   0.02635   0.01989  -0.0484   1.0000   0.0320
 -12.000  -1.0835   0.02547   0.01899  -0.0475   1.0000   0.0326
 -11.750  -1.0711   0.02465   0.01814  -0.0463   1.0000   0.0333
 -11.500  -1.0604   0.02390   0.01736  -0.0447   1.0000   0.0340
 -11.250  -1.0538   0.02321   0.01663  -0.0422   1.0000   0.0346
 -11.000  -1.0467   0.02256   0.01594  -0.0397   1.0000   0.0351
 -10.750  -1.0376   0.02179   0.01516  -0.0379   1.0000   0.0358
 -10.500  -1.0258   0.02110   0.01447  -0.0363   1.0000   0.0366
 -10.250  -1.0121   0.02047   0.01383  -0.0351   1.0000   0.0374
 -10.000  -0.9827   0.01981   0.01314  -0.0366   0.9983   0.0385
  -9.750  -0.9516   0.01919   0.01248  -0.0384   0.9962   0.0397
  -9.500  -0.9198   0.01853   0.01180  -0.0404   0.9942   0.0410
  -9.250  -0.8874   0.01792   0.01121  -0.0425   0.9925   0.0426
  -9.000  -0.8566   0.01739   0.01066  -0.0440   0.9898   0.0443
  -8.750  -0.8246   0.01691   0.01014  -0.0457   0.9873   0.0458
  -8.500  -0.7917   0.01633   0.00959  -0.0477   0.9850   0.0475
  -8.250  -0.7577   0.01586   0.00911  -0.0497   0.9831   0.0495
  -8.000  -0.7231   0.01544   0.00867  -0.0517   0.9816   0.0516
  -7.750  -0.6908   0.01497   0.00822  -0.0533   0.9791   0.0539
  -7.500  -0.6596   0.01457   0.00784  -0.0546   0.9755   0.0564
  -7.250  -0.6269   0.01422   0.00746  -0.0561   0.9726   0.0587
  -7.000  -0.5933   0.01378   0.00706  -0.0578   0.9700   0.0617
  -6.500  -0.5288   0.01306   0.00637  -0.0606   0.9622   0.0688
  -6.250  -0.4963   0.01273   0.00606  -0.0619   0.9581   0.0733
  -6.000  -0.4627   0.01238   0.00574  -0.0635   0.9548   0.0785
  -5.750  -0.4311   0.01209   0.00548  -0.0646   0.9503   0.0843
  -5.500  -0.3994   0.01176   0.00520  -0.0657   0.9452   0.0917
  -5.250  -0.3669   0.01145   0.00493  -0.0670   0.9408   0.0999
  -5.000  -0.3350   0.01117   0.00468  -0.0681   0.9358   0.1092
  -4.750  -0.3036   0.01085   0.00445  -0.0692   0.9297   0.1225
  -4.500  -0.2715   0.01056   0.00421  -0.0703   0.9245   0.1392
  -4.250  -0.2395   0.01023   0.00398  -0.0715   0.9193   0.1591
  -4.000  -0.2072   0.00986   0.00375  -0.0729   0.9132   0.1903
  -3.500  -0.1394   0.00892   0.00323  -0.0765   0.9021   0.2915
  -3.250  -0.1027   0.00825   0.00291  -0.0792   0.8963   0.3788
  -3.000  -0.0641   0.00753   0.00264  -0.0824   0.8909   0.4890
  -2.750  -0.0313   0.00735   0.00264  -0.0834   0.8841   0.5440
  -2.500  -0.0004   0.00733   0.00265  -0.0839   0.8764   0.5678
  -2.250   0.0301   0.00734   0.00266  -0.0843   0.8693   0.5834
  -2.000   0.0603   0.00735   0.00268  -0.0846   0.8597   0.5966
  -1.750   0.0902   0.00740   0.00267  -0.0847   0.8468   0.6087
  -1.500   0.1192   0.00747   0.00271  -0.0846   0.8315   0.6169
  -1.250   0.1488   0.00755   0.00271  -0.0847   0.8139   0.6261
  -1.000   0.1773   0.00766   0.00279  -0.0844   0.7930   0.6341
  -0.750   0.2065   0.00779   0.00282  -0.0844   0.7691   0.6417
  -0.500   0.2360   0.00789   0.00282  -0.0845   0.7477   0.6463
  -0.250   0.2645   0.00800   0.00288  -0.0844   0.7247   0.6498
   0.000   0.2933   0.00813   0.00293  -0.0843   0.6985   0.6532
   0.250   0.3220   0.00829   0.00296  -0.0843   0.6658   0.6561
   0.500   0.3499   0.00853   0.00298  -0.0842   0.6126   0.6582
   0.750   0.3753   0.00910   0.00308  -0.0837   0.5093   0.6602
   1.000   0.4008   0.00977   0.00327  -0.0834   0.4045   0.6622
   1.250   0.4272   0.01031   0.00346  -0.0833   0.3269   0.6638
   1.500   0.4541   0.01073   0.00363  -0.0832   0.2668   0.6653
   1.750   0.4814   0.01111   0.00381  -0.0831   0.2186   0.6668
   2.000   0.5091   0.01143   0.00398  -0.0831   0.1854   0.6683
   2.250   0.5370   0.01172   0.00415  -0.0831   0.1594   0.6698
   2.750   0.5933   0.01223   0.00448  -0.0832   0.1255   0.6731
   3.000   0.6216   0.01247   0.00465  -0.0832   0.1135   0.6749
   3.250   0.6500   0.01268   0.00483  -0.0833   0.1043   0.6766
   3.500   0.6782   0.01292   0.00501  -0.0833   0.0962   0.6784
   3.750   0.7063   0.01317   0.00520  -0.0834   0.0893   0.6804
   4.000   0.7343   0.01339   0.00541  -0.0833   0.0844   0.6823
   4.250   0.7617   0.01365   0.00565  -0.0832   0.0795   0.6841
   4.500   0.7894   0.01388   0.00589  -0.0831   0.0755   0.6858
   4.750   0.8169   0.01413   0.00613  -0.0829   0.0713   0.6874
   5.000   0.8442   0.01439   0.00639  -0.0828   0.0677   0.6890
   5.250   0.8716   0.01465   0.00664  -0.0826   0.0644   0.6907
   5.500   0.8985   0.01495   0.00691  -0.0824   0.0612   0.6925
   5.750   0.9258   0.01521   0.00718  -0.0823   0.0585   0.6944
   6.000   0.9527   0.01551   0.00746  -0.0821   0.0558   0.6962
   6.250   0.9792   0.01584   0.00778  -0.0818   0.0536   0.6981
   6.500   1.0060   0.01614   0.00810  -0.0816   0.0516   0.7000
   6.750   1.0321   0.01646   0.00843  -0.0812   0.0497   0.7017
   7.000   1.0575   0.01684   0.00882  -0.0808   0.0478   0.7034
   7.250   1.0833   0.01716   0.00918  -0.0804   0.0462   0.7051
   7.500   1.1089   0.01750   0.00955  -0.0799   0.0445   0.7068
   7.750   1.1339   0.01790   0.00995  -0.0794   0.0430   0.7086
   8.000   1.1584   0.01834   0.01040  -0.0788   0.0418   0.7104
   8.250   1.1833   0.01872   0.01083  -0.0783   0.0406   0.7123
   8.500   1.2078   0.01912   0.01127  -0.0777   0.0394   0.7143
   8.750   1.2319   0.01956   0.01173  -0.0771   0.0383   0.7162
   9.000   1.2552   0.02006   0.01223  -0.0764   0.0372   0.7180
   9.250   1.2785   0.02053   0.01273  -0.0756   0.0362   0.7198
   9.500   1.3015   0.02097   0.01325  -0.0748   0.0352   0.7217
   9.750   1.3238   0.02145   0.01379  -0.0739   0.0344   0.7237
  10.000   1.3455   0.02197   0.01435  -0.0729   0.0336   0.7258
  10.250   1.3664   0.02254   0.01495  -0.0718   0.0328   0.7278
  10.500   1.3860   0.02319   0.01563  -0.0705   0.0322   0.7299
  10.750   1.4062   0.02376   0.01628  -0.0693   0.0316   0.7320
  11.000   1.4254   0.02436   0.01695  -0.0680   0.0310   0.7341
  11.250   1.4437   0.02499   0.01764  -0.0665   0.0304   0.7362
  11.500   1.4609   0.02562   0.01833  -0.0649   0.0298   0.7381
  11.750   1.4755   0.02626   0.01903  -0.0629   0.0292   0.7400
  12.000   1.4873   0.02697   0.01980  -0.0604   0.0288   0.7420
  12.250   1.4997   0.02782   0.02071  -0.0582   0.0283   0.7441
  12.500   1.5112   0.02878   0.02174  -0.0561   0.0279   0.7463
  12.750   1.5239   0.02968   0.02274  -0.0542   0.0275   0.7486
  13.000   1.5358   0.03066   0.02382  -0.0523   0.0272   0.7509
  13.250   1.5469   0.03173   0.02498  -0.0504   0.0268   0.7533
  13.500   1.5571   0.03289   0.02622  -0.0486   0.0265   0.7558
  13.750   1.5665   0.03411   0.02755  -0.0468   0.0261   0.7583
  14.000   1.5750   0.03543   0.02898  -0.0450   0.0258   0.7608
  14.250   1.5827   0.03686   0.03052  -0.0434   0.0255   0.7634
  14.500   1.5894   0.03844   0.03219  -0.0419   0.0253   0.7660
  14.750   1.5949   0.04018   0.03402  -0.0405   0.0250   0.7684
  15.000   1.5989   0.04212   0.03605  -0.0392   0.0248   0.7707
  15.250   1.6009   0.04433   0.03835  -0.0380   0.0245   0.7729
  15.500   1.6008   0.04683   0.04095  -0.0371   0.0243   0.7749
  15.750   1.5980   0.04971   0.04394  -0.0363   0.0241   0.7769
  16.000   1.5978   0.05247   0.04685  -0.0359   0.0239   0.7791
  16.250   1.5956   0.05557   0.05011  -0.0357   0.0238   0.7814
  16.500   1.5918   0.05901   0.05369  -0.0359   0.0236   0.7836
  16.750   1.5857   0.06291   0.05775  -0.0365   0.0234   0.7859
  17.000   1.5782   0.06728   0.06227  -0.0376   0.0232   0.7880
  17.250   1.5681   0.07226   0.06740  -0.0392   0.0231   0.7900
  17.500   1.5548   0.07802   0.07334  -0.0416   0.0229   0.7917
  17.750   1.5391   0.08455   0.08005  -0.0447   0.0228   0.7933
  18.000   1.5193   0.09207   0.08775  -0.0486   0.0227   0.7949
  18.250   1.4956   0.10056   0.09644  -0.0532   0.0226   0.7963
  18.500   1.4676   0.11009   0.10616  -0.0586   0.0226   0.7975
  18.750   1.4360   0.12046   0.11672  -0.0647   0.0225   0.7984
  19.000   1.4023   0.13150   0.12795  -0.0715   0.0225   0.7992
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