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AS5048 (18%) (as5048-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: AS5048 (18%) (as5048-il)
Reynolds number: 500,000
Max Cl/Cd: 81.45 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-as5048-il-500000.txt
Download as CSV file: xf-as5048-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5048 (18%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.7720   0.04169   0.03671  -0.0834   0.8820   0.0156
 -12.000  -0.7639   0.03879   0.03328  -0.0833   0.8270   0.0152
 -11.750  -0.7594   0.03634   0.03051  -0.0817   0.8115   0.0150
 -11.500  -0.7508   0.03431   0.02820  -0.0804   0.8024   0.0150
 -11.250  -0.7379   0.03242   0.02607  -0.0793   0.7959   0.0151
 -11.000  -0.7212   0.03071   0.02413  -0.0784   0.7906   0.0152
 -10.750  -0.6998   0.02914   0.02235  -0.0778   0.7863   0.0153
 -10.500  -0.6768   0.02781   0.02087  -0.0772   0.7829   0.0154
 -10.250  -0.6544   0.02671   0.01964  -0.0766   0.7795   0.0156
 -10.000  -0.6331   0.02579   0.01859  -0.0760   0.7762   0.0159
  -9.750  -0.6131   0.02501   0.01768  -0.0754   0.7730   0.0162
  -9.500  -0.5893   0.02398   0.01662  -0.0744   0.7701   0.0166
  -9.250  -0.5706   0.02313   0.01578  -0.0736   0.7674   0.0171
  -9.000  -0.5526   0.02234   0.01498  -0.0728   0.7650   0.0175
  -8.750  -0.5350   0.02156   0.01418  -0.0721   0.7626   0.0181
  -8.500  -0.5176   0.02078   0.01336  -0.0713   0.7602   0.0187
  -8.250  -0.4990   0.02012   0.01263  -0.0707   0.7579   0.0194
  -8.000  -0.4860   0.01909   0.01156  -0.0694   0.7558   0.0203
  -7.750  -0.4706   0.01829   0.01076  -0.0685   0.7536   0.0212
  -7.500  -0.4543   0.01764   0.01007  -0.0674   0.7514   0.0222
  -7.250  -0.4402   0.01707   0.00946  -0.0657   0.7495   0.0231
  -7.000  -0.4266   0.01652   0.00887  -0.0638   0.7474   0.0239
  -6.750  -0.4114   0.01586   0.00820  -0.0623   0.7455   0.0253
  -6.500  -0.3915   0.01543   0.00775  -0.0614   0.7437   0.0270
  -6.250  -0.3714   0.01497   0.00727  -0.0605   0.7419   0.0292
  -6.000  -0.3501   0.01457   0.00685  -0.0597   0.7401   0.0322
  -5.750  -0.3286   0.01417   0.00643  -0.0590   0.7382   0.0369
  -5.500  -0.3110   0.01348   0.00589  -0.0577   0.7363   0.0688
  -5.250  -0.3128   0.01134   0.00485  -0.0543   0.7344   0.2977
  -5.000  -0.3037   0.00977   0.00415  -0.0521   0.7330   0.4837
  -4.750  -0.2796   0.00956   0.00426  -0.0515   0.7314   0.5719
  -4.500  -0.2512   0.00974   0.00445  -0.0515   0.7296   0.6012
  -4.250  -0.2222   0.00995   0.00464  -0.0517   0.7277   0.6155
  -4.000  -0.1930   0.01022   0.00491  -0.0518   0.7259   0.6271
  -3.750  -0.1636   0.01046   0.00505  -0.0521   0.7241   0.6367
  -3.500  -0.1341   0.01069   0.00531  -0.0523   0.7223   0.6426
  -3.250  -0.1045   0.01096   0.00552  -0.0526   0.7205   0.6498
  -3.000  -0.0749   0.01117   0.00569  -0.0529   0.7187   0.6555
  -2.750  -0.0457   0.01137   0.00590  -0.0531   0.7168   0.6592
  -2.500  -0.0169   0.01143   0.00595  -0.0534   0.7151   0.6625
  -2.250   0.0120   0.01147   0.00596  -0.0537   0.7129   0.6660
  -2.000   0.0411   0.01150   0.00595  -0.0541   0.7107   0.6691
  -1.750   0.0701   0.01147   0.00589  -0.0545   0.7085   0.6715
  -1.500   0.0992   0.01146   0.00588  -0.0548   0.7062   0.6735
  -1.250   0.1286   0.01149   0.00589  -0.0552   0.7039   0.6756
  -1.000   0.1583   0.01159   0.00594  -0.0557   0.7014   0.6779
  -0.750   0.1867   0.01161   0.00596  -0.0559   0.6983   0.6805
  -0.500   0.2150   0.01156   0.00591  -0.0561   0.6948   0.6829
  -0.250   0.2439   0.01152   0.00585  -0.0565   0.6913   0.6850
   0.000   0.2735   0.01152   0.00579  -0.0570   0.6884   0.6869
   0.250   0.3030   0.01144   0.00569  -0.0575   0.6857   0.6885
   0.500   0.3324   0.01146   0.00569  -0.0580   0.6828   0.6899
   0.750   0.3600   0.01138   0.00567  -0.0580   0.6794   0.6914
   1.000   0.3882   0.01133   0.00564  -0.0582   0.6757   0.6930
   1.250   0.4172   0.01127   0.00559  -0.0585   0.6721   0.6946
   1.500   0.4469   0.01120   0.00548  -0.0590   0.6680   0.6962
   1.750   0.4744   0.01111   0.00539  -0.0590   0.6623   0.6979
   2.000   0.5023   0.01098   0.00527  -0.0590   0.6562   0.6998
   2.250   0.5315   0.01090   0.00516  -0.0594   0.6518   0.7015
   2.500   0.5604   0.01087   0.00512  -0.0597   0.6476   0.7029
   2.750   0.5881   0.01080   0.00510  -0.0598   0.6423   0.7042
   3.000   0.6159   0.01063   0.00496  -0.0599   0.6368   0.7057
   3.250   0.6440   0.01054   0.00487  -0.0600   0.6315   0.7073
   3.500   0.6708   0.01045   0.00487  -0.0599   0.6245   0.7088
   3.750   0.6984   0.01037   0.00480  -0.0599   0.6179   0.7103
   4.000   0.7254   0.01030   0.00479  -0.0598   0.6088   0.7118
   4.250   0.7522   0.01024   0.00472  -0.0596   0.5988   0.7133
   4.500   0.7787   0.01020   0.00470  -0.0594   0.5862   0.7149
   4.750   0.8045   0.01019   0.00469  -0.0591   0.5700   0.7167
   5.000   0.8290   0.01026   0.00470  -0.0585   0.5478   0.7185
   5.250   0.8511   0.01045   0.00476  -0.0575   0.5175   0.7201
   5.500   0.8712   0.01074   0.00490  -0.0561   0.4831   0.7214
   5.750   0.8905   0.01105   0.00510  -0.0547   0.4502   0.7230
   6.000   0.9093   0.01143   0.00536  -0.0531   0.4185   0.7245
   6.250   0.9274   0.01186   0.00566  -0.0515   0.3883   0.7261
   6.500   0.9464   0.01225   0.00597  -0.0501   0.3608   0.7278
   6.750   0.9643   0.01269   0.00631  -0.0485   0.3350   0.7298
   7.000   0.9817   0.01314   0.00666  -0.0469   0.3089   0.7318
   7.250   0.9984   0.01361   0.00703  -0.0451   0.2846   0.7338
   7.500   1.0151   0.01407   0.00740  -0.0434   0.2628   0.7355
   7.750   1.0292   0.01453   0.00777  -0.0412   0.2443   0.7371
   8.000   1.0429   0.01494   0.00814  -0.0389   0.2284   0.7389
   8.250   1.0582   0.01540   0.00858  -0.0370   0.2143   0.7408
   8.500   1.0742   0.01589   0.00906  -0.0353   0.2022   0.7428
   8.750   1.0890   0.01646   0.00959  -0.0335   0.1912   0.7448
   9.000   1.1059   0.01695   0.01010  -0.0321   0.1817   0.7470
   9.250   1.1214   0.01752   0.01067  -0.0305   0.1728   0.7495
   9.500   1.1364   0.01814   0.01128  -0.0290   0.1644   0.7519
   9.750   1.1522   0.01875   0.01191  -0.0277   0.1570   0.7541
  10.000   1.1658   0.01945   0.01262  -0.0262   0.1489   0.7564
  10.250   1.1810   0.02011   0.01334  -0.0250   0.1416   0.7589
  10.500   1.1936   0.02098   0.01421  -0.0236   0.1338   0.7615
  10.750   1.2084   0.02178   0.01506  -0.0226   0.1265   0.7642
  11.000   1.2197   0.02287   0.01614  -0.0215   0.1185   0.7671
  11.250   1.2346   0.02378   0.01709  -0.0208   0.1112   0.7700
  11.500   1.2454   0.02501   0.01832  -0.0198   0.1038   0.7730
  11.750   1.2584   0.02609   0.01945  -0.0191   0.0969   0.7764
  12.000   1.2684   0.02741   0.02080  -0.0182   0.0906   0.7802
  12.250   1.2795   0.02868   0.02210  -0.0175   0.0848   0.7845
  12.500   1.2879   0.03018   0.02362  -0.0166   0.0795   0.7889
  12.750   1.2985   0.03147   0.02499  -0.0158   0.0749   0.7941
  13.000   1.3032   0.03323   0.02678  -0.0147   0.0704   0.8001
  13.250   1.3143   0.03452   0.02817  -0.0141   0.0671   0.8070
  13.500   1.3221   0.03605   0.02978  -0.0133   0.0637   0.8164
  13.750   1.3238   0.03805   0.03187  -0.0122   0.0604   0.8300
  14.000   1.3304   0.03927   0.03334  -0.0107   0.0583   0.8658
  14.250   1.3137   0.04002   0.03430  -0.0044   0.0571   1.0000
  14.500   1.3204   0.04183   0.03613  -0.0039   0.0546   1.0000
  14.750   1.3213   0.04416   0.03848  -0.0032   0.0522   1.0000
  15.000   1.3268   0.04614   0.04052  -0.0028   0.0504   1.0000
  15.250   1.3336   0.04805   0.04252  -0.0025   0.0486   1.0000
  15.500   1.3382   0.05023   0.04474  -0.0023   0.0468   1.0000
  15.750   1.3387   0.05285   0.04739  -0.0021   0.0452   1.0000
  16.000   1.3347   0.05598   0.05058  -0.0018   0.0436   1.0000
  16.250   1.3407   0.05820   0.05290  -0.0019   0.0425   1.0000
  16.500   1.3444   0.06067   0.05546  -0.0020   0.0411   1.0000
  16.750   1.3461   0.06345   0.05831  -0.0022   0.0398   1.0000
  17.000   1.3443   0.06666   0.06157  -0.0026   0.0387   1.0000
  17.250   1.3370   0.07055   0.06551  -0.0030   0.0375   1.0000
  17.500   1.3351   0.07390   0.06896  -0.0035   0.0366   1.0000
  17.750   1.3356   0.07706   0.07223  -0.0042   0.0357   1.0000
  18.000   1.3341   0.08051   0.07578  -0.0050   0.0348   1.0000
  18.250   1.3315   0.08413   0.07948  -0.0059   0.0340   1.0000
  18.500   1.3272   0.08802   0.08346  -0.0070   0.0332   1.0000
  18.750   1.3206   0.09228   0.08779  -0.0083   0.0325   1.0000
  19.000   1.3117   0.09680   0.09236  -0.0096   0.0317   1.0000
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