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NASA SC(2)-0612 AIRFOIL (sc20612-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0612 AIRFOIL (sc20612-il)
Reynolds number: 500,000
Max Cl/Cd: 63.65 at α=1°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20612-il-500000.txt
Download as CSV file: xf-sc20612-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0612 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -1.0056   0.07247   0.06883  -0.0563   1.0000   0.0249
 -16.000  -1.0305   0.06485   0.06099  -0.0610   1.0000   0.0249
 -15.750  -1.0470   0.05925   0.05520  -0.0639   1.0000   0.0250
 -15.500  -1.0591   0.05474   0.05053  -0.0658   1.0000   0.0251
 -15.250  -1.0677   0.05089   0.04652  -0.0671   1.0000   0.0253
 -15.000  -1.0738   0.04754   0.04302  -0.0679   1.0000   0.0254
 -14.750  -1.0773   0.04461   0.03994  -0.0683   1.0000   0.0256
 -14.500  -1.0786   0.04203   0.03723  -0.0684   1.0000   0.0259
 -14.250  -1.0785   0.03970   0.03476  -0.0681   1.0000   0.0261
 -14.000  -1.0773   0.03760   0.03252  -0.0675   1.0000   0.0264
 -13.750  -1.0755   0.03571   0.03051  -0.0666   1.0000   0.0267
 -13.500  -1.0737   0.03406   0.02872  -0.0651   1.0000   0.0270
 -13.250  -1.0731   0.03263   0.02717  -0.0631   1.0000   0.0272
 -13.000  -1.0752   0.03145   0.02589  -0.0602   1.0000   0.0274
 -12.750  -1.0748   0.03040   0.02472  -0.0575   1.0000   0.0277
 -12.500  -1.0709   0.02862   0.02286  -0.0555   1.0000   0.0282
 -12.250  -1.0623   0.02747   0.02168  -0.0539   1.0000   0.0287
 -12.000  -1.0506   0.02654   0.02073  -0.0528   1.0000   0.0291
 -11.750  -1.0368   0.02565   0.01979  -0.0518   1.0000   0.0296
 -11.500  -1.0215   0.02476   0.01884  -0.0510   1.0000   0.0302
 -11.250  -1.0047   0.02391   0.01791  -0.0503   1.0000   0.0308
 -11.000  -0.9868   0.02309   0.01700  -0.0497   1.0000   0.0315
 -10.750  -0.9677   0.02237   0.01618  -0.0491   1.0000   0.0321
 -10.500  -0.9492   0.02134   0.01509  -0.0485   1.0000   0.0329
 -10.250  -0.9288   0.02054   0.01430  -0.0482   1.0000   0.0338
 -10.000  -0.9068   0.01997   0.01373  -0.0480   1.0000   0.0347
  -9.750  -0.8841   0.01945   0.01317  -0.0479   1.0000   0.0358
  -9.500  -0.8607   0.01898   0.01263  -0.0477   1.0000   0.0370
  -9.250  -0.8371   0.01830   0.01192  -0.0479   1.0000   0.0384
  -9.000  -0.8113   0.01778   0.01142  -0.0483   0.9998   0.0399
  -8.750  -0.7775   0.01735   0.01097  -0.0502   0.9987   0.0418
  -8.500  -0.7436   0.01699   0.01054  -0.0519   0.9975   0.0436
  -8.250  -0.7096   0.01624   0.00982  -0.0541   0.9964   0.0463
  -8.000  -0.6743   0.01591   0.00949  -0.0562   0.9951   0.0492
  -7.750  -0.6383   0.01536   0.00893  -0.0586   0.9941   0.0526
  -7.500  -0.6024   0.01500   0.00859  -0.0608   0.9931   0.0562
  -7.250  -0.5689   0.01465   0.00821  -0.0624   0.9912   0.0595
  -7.000  -0.5342   0.01416   0.00778  -0.0645   0.9896   0.0639
  -6.750  -0.4997   0.01394   0.00753  -0.0662   0.9880   0.0676
  -6.500  -0.4634   0.01345   0.00707  -0.0686   0.9867   0.0723
  -6.250  -0.4275   0.01318   0.00681  -0.0707   0.9855   0.0766
  -6.000  -0.3908   0.01284   0.00648  -0.0730   0.9845   0.0817
  -5.750  -0.3539   0.01254   0.00622  -0.0753   0.9836   0.0879
  -5.500  -0.3164   0.01222   0.00593  -0.0778   0.9829   0.0959
  -5.250  -0.2785   0.01189   0.00568  -0.0803   0.9823   0.1090
  -5.000  -0.2456   0.01149   0.00542  -0.0819   0.9796   0.1323
  -4.750  -0.2071   0.01087   0.00511  -0.0850   0.9783   0.1936
  -4.500  -0.1633   0.00995   0.00475  -0.0897   0.9783   0.3207
  -4.250  -0.1152   0.00893   0.00445  -0.0955   0.9797   0.4934
  -4.000  -0.0795   0.00877   0.00454  -0.0973   0.9776   0.5689
  -3.750  -0.0449   0.00877   0.00458  -0.0986   0.9753   0.5968
  -3.500  -0.0090   0.00878   0.00460  -0.1002   0.9734   0.6131
  -3.250   0.0281   0.00878   0.00459  -0.1020   0.9719   0.6255
  -3.000   0.0655   0.00879   0.00460  -0.1040   0.9708   0.6359
  -2.750   0.1033   0.00880   0.00464  -0.1059   0.9698   0.6444
  -2.500   0.1338   0.00884   0.00466  -0.1062   0.9644   0.6535
  -2.250   0.1705   0.00882   0.00470  -0.1076   0.9616   0.6609
  -2.000   0.2095   0.00879   0.00467  -0.1096   0.9589   0.6701
  -1.750   0.2455   0.00866   0.00461  -0.1104   0.9533   0.6771
  -1.500   0.2763   0.00859   0.00456  -0.1102   0.9441   0.6838
  -1.250   0.3068   0.00851   0.00444  -0.1102   0.9336   0.6892
  -1.000   0.3341   0.00836   0.00432  -0.1094   0.9204   0.6922
  -0.750   0.3614   0.00831   0.00428  -0.1087   0.9075   0.6948
  -0.500   0.3893   0.00828   0.00423  -0.1082   0.8935   0.6974
  -0.250   0.4178   0.00828   0.00422  -0.1080   0.8802   0.7004
   0.000   0.4467   0.00828   0.00419  -0.1078   0.8644   0.7036
   0.250   0.4758   0.00830   0.00415  -0.1078   0.8429   0.7064
   0.500   0.5041   0.00832   0.00408  -0.1075   0.8149   0.7087
   0.750   0.5306   0.00841   0.00407  -0.1068   0.7745   0.7105
   1.000   0.5550   0.00872   0.00409  -0.1057   0.7003   0.7122
   1.250   0.5729   0.00973   0.00431  -0.1035   0.5307   0.7139
   1.500   0.5930   0.01081   0.00467  -0.1022   0.3747   0.7158
   1.750   0.6159   0.01165   0.00498  -0.1015   0.2593   0.7179
   2.000   0.6407   0.01231   0.00527  -0.1011   0.1806   0.7204
   2.250   0.6668   0.01286   0.00553  -0.1009   0.1312   0.7229
   2.500   0.6941   0.01326   0.00579  -0.1009   0.1085   0.7250
   2.750   0.7218   0.01359   0.00602  -0.1009   0.0956   0.7268
   3.000   0.7489   0.01382   0.00623  -0.1006   0.0884   0.7285
   3.250   0.7753   0.01415   0.00654  -0.1003   0.0824   0.7301
   3.500   0.8022   0.01439   0.00681  -0.1000   0.0782   0.7317
   3.750   0.8282   0.01480   0.00718  -0.0996   0.0733   0.7335
   4.000   0.8552   0.01507   0.00748  -0.0993   0.0699   0.7354
   4.250   0.8822   0.01534   0.00775  -0.0991   0.0663   0.7375
   4.500   0.9075   0.01589   0.00825  -0.0986   0.0623   0.7397
   4.750   0.9351   0.01612   0.00852  -0.0985   0.0593   0.7424
   5.000   0.9619   0.01648   0.00884  -0.0984   0.0558   0.7448
   5.250   0.9867   0.01696   0.00934  -0.0978   0.0526   0.7467
   5.500   1.0125   0.01726   0.00969  -0.0973   0.0497   0.7484
   5.750   1.0367   0.01779   0.01019  -0.0966   0.0471   0.7502
   6.000   1.0615   0.01827   0.01073  -0.0959   0.0449   0.7521
   6.250   1.0872   0.01861   0.01110  -0.0955   0.0427   0.7542
   6.500   1.1121   0.01905   0.01152  -0.0949   0.0408   0.7566
   6.750   1.1356   0.01973   0.01224  -0.0942   0.0392   0.7591
   7.000   1.1609   0.02019   0.01274  -0.0937   0.0378   0.7617
   7.250   1.1856   0.02065   0.01323  -0.0931   0.0364   0.7637
   7.500   1.2089   0.02114   0.01375  -0.0923   0.0353   0.7656
   7.750   1.2292   0.02216   0.01479  -0.0910   0.0342   0.7675
   8.000   1.2525   0.02270   0.01544  -0.0901   0.0334   0.7696
   8.250   1.2753   0.02329   0.01612  -0.0892   0.0324   0.7719
   8.500   1.2980   0.02386   0.01674  -0.0883   0.0314   0.7744
   8.750   1.3202   0.02446   0.01736  -0.0874   0.0306   0.7769
   9.000   1.3410   0.02532   0.01824  -0.0863   0.0299   0.7794
   9.250   1.3592   0.02669   0.01968  -0.0849   0.0292   0.7816
   9.500   1.3789   0.02747   0.02061  -0.0835   0.0287   0.7838
   9.750   1.3978   0.02837   0.02165  -0.0820   0.0282   0.7861
  10.000   1.4158   0.02934   0.02275  -0.0804   0.0277   0.7886
  10.250   1.4331   0.03034   0.02387  -0.0788   0.0272   0.7912
  10.500   1.4495   0.03135   0.02498  -0.0771   0.0267   0.7939
  10.750   1.4651   0.03239   0.02609  -0.0754   0.0263   0.7967
  11.000   1.4785   0.03343   0.02722  -0.0733   0.0259   0.7991
  11.250   1.4893   0.03467   0.02855  -0.0709   0.0256   0.8014
  11.500   1.4956   0.03632   0.03031  -0.0679   0.0253   0.8038
  11.750   1.4951   0.03900   0.03320  -0.0643   0.0249   0.8063
  12.000   1.4979   0.04041   0.03481  -0.0610   0.0248   0.8092
  12.250   1.4993   0.04209   0.03668  -0.0579   0.0246   0.8120
  12.500   1.4987   0.04399   0.03879  -0.0548   0.0243   0.8144
  12.750   1.4957   0.04616   0.04118  -0.0519   0.0241   0.8167
  13.000   1.4899   0.04874   0.04397  -0.0491   0.0239   0.8191
  13.250   1.4815   0.05169   0.04715  -0.0467   0.0238   0.8215
  13.500   1.4701   0.05515   0.05083  -0.0448   0.0236   0.8241
  13.750   1.4556   0.05921   0.05511  -0.0436   0.0235   0.8266
  14.000   1.4373   0.06408   0.06021  -0.0432   0.0234   0.8288
  14.250   1.4148   0.06995   0.06633  -0.0441   0.0234   0.8307
  14.500   1.3862   0.07746   0.07412  -0.0469   0.0234   0.8323
  14.750   1.3465   0.08819   0.08515  -0.0530   0.0235   0.8334
  15.000   1.2750   0.10883   0.10621  -0.0680   0.0238   0.8330
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