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SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il)
Reynolds number: 500,000
Max Cl/Cd: 65.95 at α=0.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-nasasc2-0714-il-500000.txt
Download as CSV file: xf-nasasc2-0714-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SC(2)-0714 Supercritical airfoil (coordinates fr
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.9645   0.09555   0.09181  -0.0618   1.0000   0.0307
 -18.250  -0.9992   0.08559   0.08162  -0.0678   1.0000   0.0307
 -18.000  -1.0245   0.07796   0.07380  -0.0720   1.0000   0.0309
 -17.750  -1.0403   0.07229   0.06799  -0.0747   1.0000   0.0311
 -17.500  -1.0485   0.06797   0.06359  -0.0765   1.0000   0.0313
 -17.250  -1.0539   0.06424   0.05977  -0.0779   1.0000   0.0315
 -17.000  -1.0576   0.06094   0.05639  -0.0790   1.0000   0.0317
 -16.750  -1.0605   0.05792   0.05330  -0.0798   1.0000   0.0320
 -16.500  -1.0635   0.05509   0.05039  -0.0802   1.0000   0.0322
 -16.250  -1.0665   0.05246   0.04767  -0.0803   1.0000   0.0325
 -16.000  -1.0696   0.04998   0.04510  -0.0802   1.0000   0.0328
 -15.750  -1.0729   0.04770   0.04271  -0.0796   1.0000   0.0330
 -15.500  -1.0760   0.04558   0.04050  -0.0787   1.0000   0.0333
 -15.250  -1.0784   0.04370   0.03852  -0.0775   1.0000   0.0337
 -15.000  -1.0806   0.04198   0.03670  -0.0759   1.0000   0.0340
 -14.750  -1.0831   0.04039   0.03502  -0.0740   1.0000   0.0343
 -14.500  -1.0856   0.03894   0.03347  -0.0719   1.0000   0.0347
 -14.250  -1.0881   0.03762   0.03205  -0.0695   1.0000   0.0350
 -14.000  -1.0911   0.03643   0.03077  -0.0668   1.0000   0.0353
 -13.750  -1.0945   0.03537   0.02962  -0.0639   1.0000   0.0355
 -13.500  -1.0961   0.03391   0.02808  -0.0609   1.0000   0.0360
 -13.250  -1.0966   0.03281   0.02695  -0.0578   1.0000   0.0364
 -13.000  -1.1004   0.03196   0.02608  -0.0541   1.0000   0.0368
 -12.750  -1.1081   0.03120   0.02531  -0.0498   1.0000   0.0371
 -12.500  -1.1067   0.03038   0.02446  -0.0470   1.0000   0.0375
 -12.250  -1.0990   0.02953   0.02357  -0.0454   0.9999   0.0380
 -12.000  -1.0733   0.02856   0.02255  -0.0470   0.9985   0.0388
 -11.750  -1.0465   0.02763   0.02154  -0.0486   0.9968   0.0397
 -11.500  -1.0175   0.02680   0.02062  -0.0506   0.9952   0.0406
 -11.250  -0.9881   0.02593   0.01965  -0.0524   0.9938   0.0415
 -11.000  -0.9614   0.02487   0.01862  -0.0536   0.9929   0.0428
 -10.750  -0.9366   0.02414   0.01789  -0.0544   0.9907   0.0438
 -10.500  -0.9091   0.02346   0.01719  -0.0557   0.9887   0.0449
 -10.250  -0.8802   0.02282   0.01650  -0.0571   0.9870   0.0461
 -10.000  -0.8494   0.02226   0.01588  -0.0588   0.9855   0.0472
  -9.750  -0.8197   0.02143   0.01502  -0.0603   0.9842   0.0486
  -9.500  -0.7873   0.02072   0.01435  -0.0624   0.9830   0.0502
  -9.250  -0.7533   0.02020   0.01382  -0.0646   0.9821   0.0518
  -9.000  -0.7192   0.01972   0.01332  -0.0669   0.9814   0.0534
  -8.750  -0.6925   0.01930   0.01285  -0.0675   0.9789   0.0547
  -8.500  -0.6636   0.01850   0.01206  -0.0689   0.9766   0.0569
  -8.250  -0.6308   0.01797   0.01156  -0.0709   0.9748   0.0590
  -8.000  -0.5968   0.01753   0.01112  -0.0730   0.9734   0.0611
  -7.750  -0.5623   0.01718   0.01073  -0.0750   0.9722   0.0631
  -7.500  -0.5253   0.01651   0.01011  -0.0780   0.9713   0.0667
  -7.250  -0.4884   0.01613   0.00975  -0.0806   0.9705   0.0702
  -7.000  -0.4510   0.01575   0.00935  -0.0833   0.9698   0.0739
  -6.750  -0.4129   0.01529   0.00896  -0.0862   0.9692   0.0799
  -6.500  -0.3748   0.01492   0.00863  -0.0890   0.9687   0.0874
  -6.250  -0.3363   0.01458   0.00834  -0.0918   0.9681   0.0975
  -6.000  -0.3097   0.01425   0.00806  -0.0923   0.9642   0.1086
  -5.750  -0.2740   0.01385   0.00777  -0.0946   0.9624   0.1253
  -5.500  -0.2356   0.01341   0.00748  -0.0976   0.9612   0.1512
  -5.250  -0.1942   0.01285   0.00717  -0.1015   0.9606   0.2006
  -5.000  -0.1449   0.01193   0.00673  -0.1077   0.9612   0.3060
  -4.750  -0.0821   0.01065   0.00626  -0.1173   0.9645   0.4928
  -4.500  -0.0479   0.01060   0.00643  -0.1187   0.9624   0.5605
  -4.250  -0.0145   0.01065   0.00649  -0.1198   0.9603   0.5832
  -4.000   0.0198   0.01072   0.00655  -0.1211   0.9586   0.5990
  -3.750   0.0540   0.01081   0.00667  -0.1222   0.9570   0.6096
  -3.500   0.0906   0.01089   0.00675  -0.1237   0.9557   0.6202
  -3.250   0.1285   0.01098   0.00684  -0.1255   0.9547   0.6301
  -3.000   0.1678   0.01096   0.00683  -0.1276   0.9539   0.6358
  -2.750   0.1885   0.01108   0.00699  -0.1257   0.9468   0.6397
  -2.500   0.2271   0.01101   0.00693  -0.1275   0.9443   0.6458
  -2.250   0.2663   0.01094   0.00688  -0.1293   0.9425   0.6526
  -2.000   0.3027   0.01094   0.00696  -0.1300   0.9402   0.6577
  -1.750   0.3346   0.01079   0.00683  -0.1298   0.9328   0.6635
  -1.500   0.3754   0.01026   0.00624  -0.1318   0.9250   0.6678
  -1.250   0.4032   0.01002   0.00603  -0.1311   0.9154   0.6695
  -1.000   0.4330   0.00989   0.00593  -0.1309   0.9082   0.6712
  -0.750   0.4596   0.00987   0.00593  -0.1301   0.8987   0.6730
  -0.500   0.4908   0.00974   0.00579  -0.1303   0.8895   0.6746
  -0.250   0.5186   0.00967   0.00574  -0.1300   0.8767   0.6764
   0.000   0.5480   0.00961   0.00566  -0.1299   0.8607   0.6786
   0.250   0.5785   0.00953   0.00552  -0.1301   0.8390   0.6811
   0.500   0.6091   0.00949   0.00535  -0.1304   0.8044   0.6834
   0.750   0.6371   0.00966   0.00519  -0.1301   0.7339   0.6852
   1.000   0.6533   0.01043   0.00532  -0.1274   0.6029   0.6864
   1.250   0.6677   0.01147   0.00568  -0.1247   0.4638   0.6876
   1.500   0.6862   0.01235   0.00603  -0.1230   0.3497   0.6887
   1.750   0.7075   0.01308   0.00633  -0.1218   0.2629   0.6898
   2.000   0.7306   0.01368   0.00661  -0.1210   0.1990   0.6910
   2.250   0.7550   0.01418   0.00687  -0.1204   0.1558   0.6922
   2.500   0.7806   0.01458   0.00713  -0.1200   0.1284   0.6936
   2.750   0.8063   0.01498   0.00739  -0.1196   0.1089   0.6952
   3.000   0.8327   0.01532   0.00765  -0.1193   0.0971   0.6970
   3.250   0.8598   0.01561   0.00790  -0.1191   0.0892   0.6989
   3.500   0.8864   0.01598   0.00820  -0.1189   0.0826   0.7008
   3.750   0.9144   0.01624   0.00844  -0.1190   0.0788   0.7026
   4.000   0.9401   0.01651   0.00870  -0.1185   0.0750   0.7041
   4.250   0.9638   0.01695   0.00912  -0.1176   0.0712   0.7053
   4.500   0.9893   0.01722   0.00943  -0.1170   0.0686   0.7066
   4.750   1.0142   0.01755   0.00977  -0.1164   0.0659   0.7077
   5.000   1.0371   0.01811   0.01030  -0.1154   0.0630   0.7090
   5.250   1.0614   0.01853   0.01076  -0.1146   0.0610   0.7103
   5.500   1.0863   0.01887   0.01113  -0.1140   0.0589   0.7118
   5.750   1.1108   0.01926   0.01152  -0.1134   0.0568   0.7134
   6.000   1.1325   0.01997   0.01219  -0.1123   0.0545   0.7151
   6.250   1.1560   0.02050   0.01276  -0.1115   0.0531   0.7168
   6.500   1.1806   0.02090   0.01320  -0.1108   0.0516   0.7186
   6.750   1.2047   0.02137   0.01368  -0.1102   0.0501   0.7203
   7.000   1.2270   0.02180   0.01413  -0.1091   0.0487   0.7217
   7.250   1.2467   0.02258   0.01491  -0.1077   0.0472   0.7230
   7.500   1.2675   0.02326   0.01565  -0.1064   0.0460   0.7242
   7.750   1.2894   0.02370   0.01617  -0.1052   0.0450   0.7256
   8.000   1.3105   0.02422   0.01676  -0.1040   0.0439   0.7270
   8.250   1.3310   0.02476   0.01733  -0.1026   0.0429   0.7286
   8.500   1.3507   0.02532   0.01791  -0.1012   0.0420   0.7303
   8.750   1.3693   0.02601   0.01861  -0.0997   0.0412   0.7321
   9.000   1.3870   0.02733   0.01994  -0.0982   0.0402   0.7339
   9.250   1.4032   0.02784   0.02054  -0.0961   0.0397   0.7357
   9.500   1.4189   0.02844   0.02123  -0.0940   0.0390   0.7373
   9.750   1.4353   0.02910   0.02198  -0.0921   0.0382   0.7388
  10.000   1.4511   0.02979   0.02276  -0.0901   0.0375   0.7402
  10.250   1.4664   0.03054   0.02358  -0.0881   0.0369   0.7417
  10.500   1.4811   0.03134   0.02443  -0.0861   0.0363   0.7432
  10.750   1.4951   0.03221   0.02535  -0.0841   0.0358   0.7449
  11.000   1.5083   0.03335   0.02652  -0.0821   0.0353   0.7467
  11.250   1.5200   0.03523   0.02849  -0.0801   0.0346   0.7486
  11.500   1.5312   0.03628   0.02967  -0.0778   0.0344   0.7508
  11.750   1.5417   0.03746   0.03099  -0.0756   0.0340   0.7528
  12.000   1.5512   0.03878   0.03244  -0.0734   0.0336   0.7545
  12.250   1.5592   0.04017   0.03397  -0.0711   0.0332   0.7560
  12.500   1.5658   0.04166   0.03560  -0.0687   0.0329   0.7575
  12.750   1.5710   0.04327   0.03735  -0.0663   0.0325   0.7590
  13.000   1.5751   0.04498   0.03919  -0.0640   0.0322   0.7605
  13.250   1.5784   0.04678   0.04112  -0.0618   0.0319   0.7622
  13.500   1.5811   0.04866   0.04312  -0.0597   0.0316   0.7640
  13.750   1.5833   0.05062   0.04518  -0.0579   0.0313   0.7658
  14.000   1.5850   0.05268   0.04733  -0.0562   0.0310   0.7678
  14.250   1.5852   0.05502   0.04976  -0.0547   0.0308   0.7697
  14.500   1.5849   0.05751   0.05232  -0.0534   0.0305   0.7715
  14.750   1.5807   0.06049   0.05542  -0.0522   0.0303   0.7730
  15.000   1.5714   0.06424   0.05933  -0.0512   0.0301   0.7744
  15.250   1.5536   0.06927   0.06456  -0.0506   0.0299   0.7755
  15.500   1.5350   0.07459   0.07011  -0.0509   0.0297   0.7767
  15.750   1.5193   0.07989   0.07563  -0.0521   0.0297   0.7781
  16.000   1.5005   0.08612   0.08208  -0.0543   0.0296   0.7793
  16.250   1.4778   0.09351   0.08970  -0.0578   0.0296   0.7804
  16.500   1.4504   0.10240   0.09882  -0.0629   0.0296   0.7814
  16.750   1.4161   0.11345   0.11013  -0.0702   0.0296   0.7820
  17.000   1.3645   0.12934   0.12634  -0.0818   0.0296   0.7819
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