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AS5048 (18%) (as5048-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: AS5048 (18%) (as5048-il)
Reynolds number: 100,000
Max Cl/Cd: 40.44 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5048-il-100000-n5.txt
Download as CSV file: xf-as5048-il-100000-n5.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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6223   0.09629   0.09049  -0.0570   1.0000   0.0226
 -13.750  -0.6488   0.08890   0.08294  -0.0606   1.0000   0.0223
 -13.500  -0.6736   0.08266   0.07653  -0.0630   1.0000   0.0222
 -13.250  -0.6965   0.07723   0.07091  -0.0644   1.0000   0.0221
 -13.000  -0.7169   0.07252   0.06601  -0.0650   1.0000   0.0220
 -12.750  -0.7352   0.06836   0.06166  -0.0649   1.0000   0.0221
 -12.500  -0.7517   0.06462   0.05771  -0.0643   1.0000   0.0222
 -12.250  -0.7659   0.06129   0.05417  -0.0631   1.0000   0.0224
 -12.000  -0.7785   0.05826   0.05091  -0.0616   1.0000   0.0226
 -11.750  -0.7893   0.05552   0.04794  -0.0596   1.0000   0.0228
 -11.500  -0.7985   0.05302   0.04520  -0.0571   1.0000   0.0230
 -11.250  -0.8060   0.05077   0.04271  -0.0543   1.0000   0.0233
 -11.000  -0.8115   0.04877   0.04047  -0.0511   1.0000   0.0235
 -10.750  -0.8141   0.04695   0.03844  -0.0478   1.0000   0.0236
 -10.250  -0.7725   0.04246   0.03373  -0.0484   0.9852   0.0243
 -10.000  -0.7449   0.04041   0.03155  -0.0494   0.9566   0.0248
  -9.750  -0.7072   0.03840   0.02938  -0.0519   0.9350   0.0256
  -9.500  -0.6640   0.03655   0.02734  -0.0550   0.9221   0.0266
  -9.250  -0.6204   0.03493   0.02550  -0.0583   0.9109   0.0285
  -9.000  -0.5797   0.03349   0.02406  -0.0616   0.8997   0.0303
  -8.750  -0.5409   0.03219   0.02264  -0.0642   0.8891   0.0319
  -8.500  -0.5086   0.03099   0.02127  -0.0660   0.8782   0.0333
  -8.250  -0.4849   0.02969   0.01995  -0.0670   0.8680   0.0351
  -8.000  -0.4634   0.02860   0.01874  -0.0676   0.8591   0.0378
  -7.750  -0.4452   0.02756   0.01757  -0.0674   0.8512   0.0403
  -7.500  -0.4296   0.02652   0.01644  -0.0669   0.8440   0.0428
  -7.250  -0.4121   0.02563   0.01540  -0.0663   0.8381   0.0462
  -7.000  -0.3997   0.02477   0.01453  -0.0648   0.8321   0.0513
  -6.750  -0.3867   0.02396   0.01372  -0.0633   0.8271   0.0601
  -6.500  -0.3748   0.02289   0.01283  -0.0617   0.8230   0.0881
  -6.250  -0.3789   0.02106   0.01183  -0.0583   0.8186   0.2162
  -6.000  -0.3865   0.01932   0.01097  -0.0541   0.8137   0.3615
  -5.750  -0.3673   0.02004   0.01275  -0.0505   0.8100   0.5272
  -5.500  -0.3434   0.02077   0.01339  -0.0492   0.8065   0.5797
  -5.000  -0.2927   0.02320   0.01558  -0.0459   0.8007   0.6371
  -4.750  -0.2619   0.02376   0.01604  -0.0455   0.7977   0.6425
  -4.500  -0.2430   0.02351   0.01561  -0.0447   0.7941   0.6535
  -4.250  -0.2120   0.02386   0.01585  -0.0447   0.7912   0.6573
  -4.000  -0.1843   0.02397   0.01582  -0.0446   0.7886   0.6631
  -3.750  -0.1620   0.02371   0.01538  -0.0444   0.7862   0.6714
  -3.500  -0.1363   0.02386   0.01549  -0.0438   0.7830   0.6749
  -3.250  -0.1123   0.02387   0.01542  -0.0433   0.7796   0.6798
  -3.000  -0.0932   0.02352   0.01493  -0.0428   0.7763   0.6876
  -2.750  -0.0657   0.02360   0.01495  -0.0426   0.7736   0.6904
  -2.500  -0.0384   0.02361   0.01488  -0.0425   0.7709   0.6939
  -2.250  -0.0134   0.02354   0.01471  -0.0424   0.7682   0.6985
  -2.000   0.0050   0.02330   0.01440  -0.0417   0.7644   0.7046
  -1.750   0.0295   0.02335   0.01444  -0.0412   0.7609   0.7072
  -1.500   0.0549   0.02336   0.01440  -0.0409   0.7576   0.7102
  -1.250   0.0811   0.02331   0.01429  -0.0409   0.7546   0.7138
  -1.000   0.1078   0.02318   0.01407  -0.0413   0.7520   0.7180
  -0.750   0.1271   0.02312   0.01400  -0.0405   0.7476   0.7218
  -0.500   0.1502   0.02317   0.01406  -0.0398   0.7434   0.7241
  -0.250   0.1759   0.02317   0.01405  -0.0397   0.7397   0.7266
   0.000   0.2037   0.02313   0.01396  -0.0400   0.7365   0.7292
   0.250   0.2278   0.02313   0.01395  -0.0397   0.7325   0.7324
   0.500   0.2484   0.02315   0.01396  -0.0391   0.7270   0.7360
   0.750   0.2745   0.02309   0.01389  -0.0392   0.7224   0.7385
   1.000   0.3039   0.02304   0.01381  -0.0396   0.7187   0.7404
   1.250   0.3241   0.02315   0.01398  -0.0384   0.7126   0.7428
   1.500   0.3479   0.02316   0.01403  -0.0380   0.7067   0.7453
   1.750   0.3774   0.02306   0.01391  -0.0385   0.7023   0.7477
   2.000   0.4003   0.02311   0.01398  -0.0380   0.6963   0.7503
   2.250   0.4239   0.02313   0.01403  -0.0377   0.6898   0.7533
   2.500   0.4538   0.02300   0.01390  -0.0382   0.6851   0.7556
   2.750   0.4747   0.02308   0.01406  -0.0371   0.6781   0.7576
   3.000   0.4991   0.02304   0.01408  -0.0366   0.6712   0.7596
   3.250   0.5313   0.02280   0.01385  -0.0374   0.6664   0.7616
   3.500   0.5477   0.02291   0.01408  -0.0356   0.6563   0.7644
   3.750   0.5800   0.02254   0.01370  -0.0363   0.6497   0.7671
   4.000   0.5983   0.02253   0.01379  -0.0349   0.6382   0.7700
   4.250   0.6245   0.02227   0.01357  -0.0346   0.6289   0.7722
   4.500   0.6475   0.02206   0.01345  -0.0336   0.6186   0.7741
   4.750   0.6666   0.02201   0.01353  -0.0322   0.6067   0.7764
   5.000   0.6891   0.02185   0.01346  -0.0312   0.5952   0.7790
   5.250   0.7140   0.02163   0.01330  -0.0306   0.5837   0.7819
   5.500   0.7354   0.02154   0.01330  -0.0296   0.5692   0.7849
   5.750   0.7581   0.02143   0.01324  -0.0288   0.5533   0.7878
   6.000   0.7803   0.02129   0.01314  -0.0277   0.5360   0.7901
   6.250   0.8012   0.02120   0.01310  -0.0264   0.5159   0.7926
   6.500   0.8235   0.02113   0.01299  -0.0252   0.4937   0.7952
   6.750   0.8447   0.02116   0.01293  -0.0240   0.4696   0.7983
   7.000   0.8628   0.02139   0.01308  -0.0225   0.4434   0.8019
   7.250   0.8792   0.02174   0.01333  -0.0208   0.4177   0.8056
   7.500   0.8909   0.02216   0.01369  -0.0182   0.3936   0.8088
   7.750   0.9018   0.02268   0.01413  -0.0156   0.3707   0.8123
   8.000   0.9135   0.02332   0.01472  -0.0135   0.3480   0.8161
   8.250   0.9255   0.02404   0.01538  -0.0116   0.3267   0.8203
   8.500   0.9368   0.02482   0.01611  -0.0097   0.3073   0.8244
   8.750   0.9471   0.02561   0.01688  -0.0077   0.2899   0.8288
   9.000   0.9578   0.02645   0.01773  -0.0059   0.2738   0.8343
   9.250   0.9692   0.02734   0.01863  -0.0044   0.2590   0.8404
   9.500   0.9789   0.02821   0.01955  -0.0025   0.2457   0.8470
   9.750   0.9890   0.02915   0.02053  -0.0009   0.2336   0.8550
  10.000   0.9969   0.03014   0.02155   0.0010   0.2228   0.8644
  10.250   1.0053   0.03107   0.02259   0.0029   0.2120   0.8771
  10.500   1.0106   0.03198   0.02360   0.0053   0.2030   0.8985
  10.750   1.0155   0.03290   0.02459   0.0075   0.1942   0.9872
  11.000   1.0282   0.03404   0.02578   0.0077   0.1846   1.0000
  11.250   1.0391   0.03544   0.02713   0.0081   0.1761   1.0000
  11.500   1.0520   0.03674   0.02853   0.0083   0.1669   1.0000
  11.750   1.0621   0.03820   0.02996   0.0087   0.1594   1.0000
  12.000   1.0729   0.03965   0.03150   0.0091   0.1512   1.0000
  12.250   1.0814   0.04124   0.03308   0.0096   0.1442   1.0000
  12.500   1.0909   0.04280   0.03475   0.0100   0.1368   1.0000
  12.750   1.0975   0.04455   0.03648   0.0105   0.1308   1.0000
  13.000   1.1058   0.04624   0.03831   0.0109   0.1238   1.0000
  13.250   1.1104   0.04819   0.04024   0.0114   0.1185   1.0000
  13.500   1.1178   0.05001   0.04220   0.0117   0.1125   1.0000
  13.750   1.1221   0.05208   0.04432   0.0120   0.1074   1.0000
  14.000   1.1259   0.05422   0.04650   0.0124   0.1029   1.0000
  14.250   1.1307   0.05638   0.04880   0.0126   0.0981   1.0000
  14.500   1.1326   0.05879   0.05125   0.0127   0.0942   1.0000
  14.750   1.1354   0.06121   0.05372   0.0128   0.0905   1.0000
  15.000   1.1378   0.06376   0.05642   0.0128   0.0866   1.0000
  15.250   1.1386   0.06650   0.05924   0.0126   0.0834   1.0000
  15.500   1.1396   0.06919   0.06191   0.0125   0.0807   1.0000
  15.750   1.1402   0.07220   0.06513   0.0121   0.0777   1.0000
  16.000   1.1394   0.07538   0.06846   0.0116   0.0748   1.0000
  16.250   1.1381   0.07863   0.07178   0.0109   0.0724   1.0000
  16.500   1.1382   0.08167   0.07483   0.0103   0.0704   1.0000
  16.750   1.1352   0.08538   0.07872   0.0094   0.0683   1.0000
  17.000   1.1304   0.08945   0.08299   0.0082   0.0662   1.0000
  17.250   1.1252   0.09361   0.08729   0.0067   0.0642   1.0000
  17.500   1.1213   0.09760   0.09137   0.0053   0.0624   1.0000
  17.750   1.1201   0.10112   0.09492   0.0040   0.0609   1.0000
  18.000   1.1145   0.10553   0.09946   0.0022   0.0594   1.0000
  18.250   1.1004   0.11167   0.10586  -0.0007   0.0582   1.0000
  18.500   1.0847   0.11825   0.11265  -0.0040   0.0570   1.0000
  18.750   1.0672   0.12538   0.11998  -0.0079   0.0559   1.0000
  19.000   1.0470   0.13334   0.12813  -0.0125   0.0549   1.0000
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