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NASA SC(2)-0414 AIRFOIL (sc20414-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0414 AIRFOIL (sc20414-il)
Reynolds number: 500,000
Max Cl/Cd: 57.95 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20414-il-500000.txt
Download as CSV file: xf-sc20414-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -1.0665   0.11354   0.10996  -0.0269   1.0000   0.0305
 -18.500  -1.1084   0.10133   0.09749  -0.0345   1.0000   0.0305
 -18.250  -1.1367   0.09224   0.08818  -0.0401   1.0000   0.0305
 -18.000  -1.1580   0.08479   0.08052  -0.0444   1.0000   0.0306
 -17.750  -1.1747   0.07849   0.07403  -0.0479   1.0000   0.0307
 -17.500  -1.1905   0.07279   0.06816  -0.0503   1.0000   0.0309
 -17.250  -1.1976   0.06857   0.06383  -0.0518   1.0000   0.0311
 -17.000  -1.1997   0.06511   0.06030  -0.0529   1.0000   0.0314
 -16.750  -1.2000   0.06195   0.05706  -0.0539   1.0000   0.0316
 -16.500  -1.1995   0.05898   0.05402  -0.0549   1.0000   0.0319
 -16.250  -1.1983   0.05619   0.05115  -0.0556   1.0000   0.0321
 -16.000  -1.1964   0.05353   0.04841  -0.0562   1.0000   0.0324
 -15.750  -1.1941   0.05101   0.04579  -0.0567   1.0000   0.0328
 -15.500  -1.1916   0.04862   0.04330  -0.0570   1.0000   0.0331
 -15.250  -1.1883   0.04638   0.04095  -0.0571   1.0000   0.0335
 -15.000  -1.1839   0.04428   0.03874  -0.0571   1.0000   0.0339
 -14.750  -1.1785   0.04232   0.03667  -0.0570   1.0000   0.0343
 -14.500  -1.1720   0.04050   0.03473  -0.0568   1.0000   0.0347
 -14.250  -1.1647   0.03882   0.03292  -0.0566   1.0000   0.0350
 -14.000  -1.1564   0.03708   0.03110  -0.0559   1.0000   0.0356
 -13.750  -1.1459   0.03565   0.02966  -0.0553   1.0000   0.0362
 -13.500  -1.1342   0.03441   0.02841  -0.0549   1.0000   0.0367
 -13.250  -1.1223   0.03321   0.02717  -0.0545   1.0000   0.0373
 -13.000  -1.1099   0.03205   0.02597  -0.0539   1.0000   0.0379
 -12.750  -1.0973   0.03093   0.02478  -0.0533   1.0000   0.0385
 -12.500  -1.0844   0.02985   0.02362  -0.0526   1.0000   0.0392
 -12.250  -1.0710   0.02886   0.02255  -0.0518   1.0000   0.0398
 -12.000  -1.0579   0.02788   0.02149  -0.0508   1.0000   0.0403
 -11.750  -1.0464   0.02673   0.02036  -0.0495   1.0000   0.0412
 -11.500  -1.0346   0.02587   0.01950  -0.0481   1.0000   0.0419
 -11.250  -1.0247   0.02511   0.01874  -0.0463   1.0000   0.0427
 -11.000  -1.0183   0.02444   0.01805  -0.0438   1.0000   0.0434
 -10.750  -1.0118   0.02379   0.01736  -0.0412   1.0000   0.0443
 -10.250  -0.9900   0.02245   0.01591  -0.0375   1.0000   0.0460
 -10.000  -0.9803   0.02156   0.01506  -0.0356   1.0000   0.0471
  -9.750  -0.9665   0.02092   0.01444  -0.0343   1.0000   0.0481
  -9.500  -0.9507   0.02035   0.01385  -0.0332   1.0000   0.0493
  -9.250  -0.9333   0.01982   0.01328  -0.0324   1.0000   0.0506
  -9.000  -0.9143   0.01939   0.01279  -0.0317   1.0000   0.0518
  -8.750  -0.8968   0.01855   0.01200  -0.0311   1.0000   0.0536
  -8.500  -0.8651   0.01804   0.01150  -0.0328   0.9988   0.0556
  -8.250  -0.8299   0.01760   0.01102  -0.0350   0.9970   0.0579
  -8.000  -0.7951   0.01688   0.01031  -0.0374   0.9953   0.0604
  -7.750  -0.7590   0.01637   0.00982  -0.0399   0.9938   0.0631
  -7.500  -0.7227   0.01600   0.00943  -0.0421   0.9922   0.0659
  -7.250  -0.6882   0.01534   0.00881  -0.0444   0.9896   0.0695
  -7.000  -0.6523   0.01493   0.00842  -0.0466   0.9872   0.0731
  -6.750  -0.6155   0.01443   0.00792  -0.0491   0.9852   0.0771
  -6.500  -0.5781   0.01400   0.00754  -0.0516   0.9835   0.0821
  -6.250  -0.5401   0.01355   0.00712  -0.0543   0.9822   0.0880
  -6.000  -0.5018   0.01318   0.00678  -0.0569   0.9812   0.0948
  -5.750  -0.4674   0.01270   0.00637  -0.0588   0.9778   0.1038
  -5.500  -0.4310   0.01225   0.00601  -0.0611   0.9751   0.1158
  -5.250  -0.3928   0.01181   0.00566  -0.0638   0.9731   0.1337
  -5.000  -0.3531   0.01125   0.00528  -0.0669   0.9717   0.1611
  -4.750  -0.3124   0.01059   0.00487  -0.0705   0.9706   0.2111
  -4.500  -0.2700   0.00969   0.00438  -0.0747   0.9696   0.2970
  -4.250  -0.2239   0.00849   0.00379  -0.0802   0.9690   0.4339
  -4.000  -0.1815   0.00791   0.00368  -0.0838   0.9679   0.5466
  -3.750  -0.1493   0.00786   0.00369  -0.0846   0.9623   0.5778
  -3.500  -0.1149   0.00785   0.00371  -0.0858   0.9583   0.5964
  -3.250  -0.0799   0.00786   0.00369  -0.0871   0.9550   0.6113
  -3.000  -0.0494   0.00793   0.00378  -0.0873   0.9492   0.6212
  -2.750  -0.0180   0.00795   0.00378  -0.0877   0.9431   0.6296
  -2.500   0.0127   0.00802   0.00386  -0.0879   0.9381   0.6361
  -2.250   0.0420   0.00810   0.00390  -0.0879   0.9299   0.6437
  -2.000   0.0706   0.00816   0.00396  -0.0875   0.9227   0.6494
  -1.750   0.0971   0.00827   0.00409  -0.0867   0.9113   0.6553
  -1.500   0.1259   0.00836   0.00411  -0.0864   0.9002   0.6617
  -1.250   0.1525   0.00844   0.00418  -0.0855   0.8879   0.6667
  -1.000   0.1780   0.00862   0.00438  -0.0842   0.8733   0.6720
  -0.750   0.2059   0.00875   0.00448  -0.0838   0.8591   0.6776
  -0.500   0.2361   0.00882   0.00447  -0.0840   0.8467   0.6816
  -0.250   0.2632   0.00885   0.00450  -0.0833   0.8339   0.6845
   0.000   0.2906   0.00895   0.00462  -0.0828   0.8207   0.6873
   0.250   0.3190   0.00904   0.00469  -0.0825   0.8080   0.6901
   0.500   0.3482   0.00908   0.00468  -0.0825   0.7934   0.6924
   0.750   0.3778   0.00911   0.00465  -0.0826   0.7755   0.6948
   1.000   0.4074   0.00914   0.00462  -0.0828   0.7535   0.6972
   1.250   0.4370   0.00921   0.00457  -0.0830   0.7253   0.6991
   1.500   0.4657   0.00931   0.00451  -0.0830   0.6857   0.7008
   1.750   0.4918   0.00953   0.00450  -0.0824   0.6208   0.7024
   2.000   0.5134   0.01030   0.00468  -0.0812   0.4863   0.7040
   2.250   0.5360   0.01116   0.00498  -0.0803   0.3668   0.7056
   2.500   0.5610   0.01178   0.00523  -0.0800   0.2853   0.7072
   2.750   0.5867   0.01233   0.00547  -0.0797   0.2206   0.7088
   3.000   0.6135   0.01277   0.00569  -0.0796   0.1777   0.7106
   3.250   0.6409   0.01313   0.00590  -0.0796   0.1502   0.7125
   3.500   0.6687   0.01346   0.00611  -0.0797   0.1314   0.7145
   3.750   0.6969   0.01375   0.00632  -0.0798   0.1187   0.7164
   4.000   0.7251   0.01405   0.00655  -0.0799   0.1090   0.7182
   4.250   0.7529   0.01435   0.00677  -0.0799   0.1007   0.7198
   4.500   0.7802   0.01456   0.00699  -0.0798   0.0945   0.7215
   4.750   0.8059   0.01496   0.00734  -0.0793   0.0881   0.7232
   5.000   0.8329   0.01520   0.00762  -0.0791   0.0839   0.7250
   5.250   0.8587   0.01560   0.00798  -0.0786   0.0795   0.7271
   5.500   0.8852   0.01594   0.00835  -0.0783   0.0758   0.7291
   5.750   0.9124   0.01622   0.00862  -0.0782   0.0723   0.7311
   6.000   0.9377   0.01672   0.00908  -0.0778   0.0689   0.7331
   6.250   0.9653   0.01697   0.00936  -0.0777   0.0664   0.7351
   6.500   0.9922   0.01729   0.00967  -0.0776   0.0638   0.7370
   6.750   1.0166   0.01787   0.01019  -0.0771   0.0611   0.7387
   7.000   1.0427   0.01811   0.01050  -0.0767   0.0591   0.7404
   7.250   1.0680   0.01843   0.01086  -0.0762   0.0569   0.7421
   7.500   1.0917   0.01894   0.01135  -0.0755   0.0549   0.7440
   7.750   1.1151   0.01950   0.01196  -0.0747   0.0532   0.7461
   8.000   1.1399   0.01992   0.01242  -0.0741   0.0516   0.7482
   8.250   1.1643   0.02036   0.01288  -0.0735   0.0500   0.7504
   8.500   1.1872   0.02096   0.01346  -0.0728   0.0485   0.7526
   8.750   1.2097   0.02167   0.01419  -0.0720   0.0471   0.7547
   9.000   1.2336   0.02211   0.01470  -0.0714   0.0458   0.7566
   9.250   1.2560   0.02260   0.01525  -0.0704   0.0446   0.7584
   9.500   1.2775   0.02315   0.01582  -0.0694   0.0436   0.7602
   9.750   1.2969   0.02396   0.01664  -0.0682   0.0426   0.7622
  10.000   1.3160   0.02487   0.01761  -0.0668   0.0417   0.7643
  10.250   1.3366   0.02548   0.01832  -0.0657   0.0409   0.7666
  10.500   1.3565   0.02615   0.01908  -0.0645   0.0400   0.7691
  10.750   1.3758   0.02681   0.01979  -0.0633   0.0392   0.7717
  11.000   1.3940   0.02747   0.02048  -0.0619   0.0384   0.7739
  11.250   1.4098   0.02822   0.02125  -0.0602   0.0377   0.7759
  11.500   1.4219   0.02956   0.02263  -0.0580   0.0370   0.7779
  11.750   1.4322   0.03038   0.02358  -0.0553   0.0366   0.7801
  12.000   1.4445   0.03126   0.02458  -0.0531   0.0361   0.7825
  12.250   1.4568   0.03225   0.02570  -0.0511   0.0356   0.7851
  12.500   1.4684   0.03332   0.02687  -0.0492   0.0350   0.7876
  12.750   1.4794   0.03447   0.02810  -0.0473   0.0345   0.7899
  13.000   1.4893   0.03561   0.02934  -0.0454   0.0341   0.7922
  13.250   1.4983   0.03684   0.03066  -0.0434   0.0337   0.7944
  13.500   1.5066   0.03816   0.03205  -0.0416   0.0333   0.7967
  13.750   1.5140   0.03966   0.03362  -0.0399   0.0330   0.7992
  14.000   1.5195   0.04152   0.03554  -0.0382   0.0326   0.8019
  14.250   1.5205   0.04404   0.03818  -0.0363   0.0322   0.8045
  14.500   1.5225   0.04603   0.04034  -0.0348   0.0319   0.8072
  14.750   1.5228   0.04819   0.04269  -0.0335   0.0317   0.8099
  15.000   1.5213   0.05071   0.04539  -0.0323   0.0314   0.8125
  15.250   1.5187   0.05346   0.04832  -0.0314   0.0311   0.8151
  15.500   1.5150   0.05647   0.05149  -0.0309   0.0308   0.8177
  15.750   1.5095   0.05988   0.05505  -0.0307   0.0305   0.8202
  16.000   1.5018   0.06373   0.05906  -0.0310   0.0303   0.8226
  16.250   1.4920   0.06799   0.06349  -0.0318   0.0301   0.8247
  16.500   1.4803   0.07275   0.06843  -0.0331   0.0299   0.8267
  16.750   1.4665   0.07817   0.07403  -0.0351   0.0298   0.8287
  17.000   1.4498   0.08441   0.08046  -0.0379   0.0297   0.8306
  17.250   1.4301   0.09163   0.08787  -0.0418   0.0296   0.8325
  17.500   1.4039   0.10057   0.09703  -0.0471   0.0295   0.8341
  17.750   1.3658   0.11250   0.10924  -0.0549   0.0295   0.8350
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