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AS5046 (16%) (as5046-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: AS5046 (16%) (as5046-il)
Reynolds number: 100,000
Max Cl/Cd: 42.34 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5046-il-100000-n5.txt
Download as CSV file: xf-as5046-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5046 (16%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.6774   0.08036   0.07447  -0.0498   1.0000   0.0209
 -12.250  -0.6925   0.07555   0.06952  -0.0516   1.0000   0.0208
 -12.000  -0.7075   0.07110   0.06493  -0.0528   1.0000   0.0208
 -11.750  -0.7217   0.06701   0.06069  -0.0535   1.0000   0.0207
 -11.500  -0.7348   0.06327   0.05677  -0.0537   1.0000   0.0207
 -11.250  -0.7466   0.05984   0.05316  -0.0533   1.0000   0.0206
 -11.000  -0.7569   0.05673   0.04986  -0.0524   1.0000   0.0206
 -10.750  -0.7660   0.05393   0.04686  -0.0509   1.0000   0.0206
 -10.500  -0.7735   0.05143   0.04416  -0.0487   1.0000   0.0205
 -10.250  -0.7756   0.04893   0.04143  -0.0467   1.0000   0.0206
 -10.000  -0.7740   0.04652   0.03877  -0.0447   1.0000   0.0206
  -9.750  -0.7693   0.04425   0.03625  -0.0428   1.0000   0.0207
  -9.250  -0.7284   0.03957   0.03117  -0.0442   0.9447   0.0217
  -9.000  -0.6944   0.03750   0.02889  -0.0470   0.9201   0.0228
  -8.750  -0.6600   0.03537   0.02644  -0.0493   0.9041   0.0240
  -8.500  -0.6255   0.03340   0.02415  -0.0508   0.8917   0.0247
  -8.250  -0.5919   0.03177   0.02226  -0.0518   0.8812   0.0252
  -8.000  -0.5621   0.03033   0.02081  -0.0524   0.8716   0.0260
  -7.750  -0.5359   0.02917   0.01961  -0.0524   0.8631   0.0269
  -7.500  -0.5129   0.02814   0.01850  -0.0521   0.8552   0.0279
  -7.250  -0.4913   0.02720   0.01744  -0.0516   0.8490   0.0294
  -7.000  -0.4729   0.02625   0.01646  -0.0509   0.8429   0.0314
  -6.750  -0.4540   0.02538   0.01555  -0.0504   0.8375   0.0339
  -6.500  -0.4342   0.02457   0.01457  -0.0498   0.8328   0.0364
  -6.250  -0.4160   0.02366   0.01363  -0.0492   0.8278   0.0391
  -6.000  -0.3959   0.02290   0.01279  -0.0486   0.8230   0.0443
  -5.750  -0.3755   0.02209   0.01198  -0.0481   0.8190   0.0534
  -5.500  -0.3575   0.02098   0.01109  -0.0474   0.8157   0.0854
  -5.250  -0.3563   0.01821   0.00986  -0.0461   0.8114   0.3317
  -5.000  -0.3406   0.01861   0.01150  -0.0422   0.8075   0.5388
  -4.750  -0.3138   0.01965   0.01243  -0.0411   0.8038   0.5996
  -4.500  -0.2875   0.02125   0.01390  -0.0390   0.8007   0.6362
  -4.250  -0.2591   0.02206   0.01460  -0.0375   0.7982   0.6444
  -4.000  -0.2334   0.02197   0.01434  -0.0377   0.7947   0.6542
  -3.750  -0.2064   0.02222   0.01449  -0.0370   0.7912   0.6591
  -3.500  -0.1801   0.02209   0.01419  -0.0373   0.7877   0.6680
  -3.250  -0.1531   0.02217   0.01415  -0.0370   0.7848   0.6726
  -3.000  -0.1258   0.02225   0.01410  -0.0367   0.7821   0.6772
  -2.750  -0.0998   0.02208   0.01382  -0.0371   0.7785   0.6842
  -2.500  -0.0738   0.02204   0.01370  -0.0370   0.7748   0.6885
  -2.250  -0.0473   0.02207   0.01366  -0.0368   0.7713   0.6920
  -2.000  -0.0203   0.02201   0.01351  -0.0369   0.7680   0.6965
  -1.750   0.0082   0.02181   0.01315  -0.0379   0.7652   0.7026
  -1.500   0.0331   0.02185   0.01319  -0.0374   0.7609   0.7052
  -1.250   0.0590   0.02186   0.01318  -0.0372   0.7568   0.7084
  -1.000   0.0860   0.02183   0.01309  -0.0373   0.7530   0.7121
  -0.750   0.1146   0.02174   0.01291  -0.0379   0.7496   0.7164
  -0.500   0.1412   0.02169   0.01282  -0.0383   0.7451   0.7200
  -0.250   0.1666   0.02171   0.01285  -0.0381   0.7401   0.7222
   0.000   0.1937   0.02169   0.01281  -0.0381   0.7357   0.7248
   0.250   0.2222   0.02165   0.01271  -0.0383   0.7319   0.7278
   0.500   0.2475   0.02166   0.01276  -0.0385   0.7254   0.7309
   0.750   0.2762   0.02158   0.01264  -0.0391   0.7199   0.7342
   1.000   0.3051   0.02151   0.01252  -0.0393   0.7156   0.7366
   1.250   0.3288   0.02156   0.01266  -0.0389   0.7079   0.7387
   1.500   0.3563   0.02150   0.01260  -0.0389   0.7022   0.7408
   1.750   0.3839   0.02147   0.01257  -0.0390   0.6965   0.7433
   2.000   0.4098   0.02147   0.01263  -0.0390   0.6888   0.7461
   2.250   0.4398   0.02133   0.01247  -0.0395   0.6833   0.7490
   2.500   0.4664   0.02133   0.01253  -0.0398   0.6745   0.7516
   2.750   0.4941   0.02115   0.01238  -0.0396   0.6673   0.7533
   3.000   0.5185   0.02108   0.01240  -0.0390   0.6572   0.7554
   3.250   0.5472   0.02080   0.01213  -0.0388   0.6491   0.7578
   3.500   0.5718   0.02071   0.01215  -0.0384   0.6369   0.7603
   3.750   0.5983   0.02055   0.01207  -0.0383   0.6255   0.7627
   4.000   0.6264   0.02033   0.01190  -0.0384   0.6146   0.7651
   4.250   0.6541   0.02015   0.01178  -0.0386   0.6016   0.7679
   4.500   0.6787   0.02002   0.01176  -0.0379   0.5866   0.7700
   4.750   0.7039   0.01987   0.01171  -0.0373   0.5706   0.7723
   5.000   0.7290   0.01974   0.01165  -0.0368   0.5516   0.7746
   5.250   0.7546   0.01963   0.01157  -0.0363   0.5295   0.7770
   5.500   0.7806   0.01952   0.01141  -0.0359   0.5046   0.7795
   5.750   0.8057   0.01955   0.01133  -0.0354   0.4758   0.7824
   6.000   0.8288   0.01976   0.01142  -0.0347   0.4452   0.7851
   6.250   0.8490   0.02008   0.01165  -0.0334   0.4146   0.7876
   6.500   0.8688   0.02052   0.01199  -0.0323   0.3854   0.7903
   6.750   0.8880   0.02104   0.01240  -0.0312   0.3577   0.7931
   7.000   0.9072   0.02160   0.01289  -0.0302   0.3315   0.7959
   7.250   0.9263   0.02222   0.01343  -0.0293   0.3079   0.7990
   7.500   0.9446   0.02283   0.01400  -0.0283   0.2866   0.8019
   7.750   0.9613   0.02346   0.01461  -0.0270   0.2679   0.8050
   8.000   0.9781   0.02411   0.01526  -0.0257   0.2512   0.8086
   8.250   0.9949   0.02481   0.01595  -0.0246   0.2357   0.8125
   8.500   1.0116   0.02554   0.01669  -0.0236   0.2214   0.8164
   8.750   1.0257   0.02626   0.01745  -0.0221   0.2088   0.8199
   9.000   1.0376   0.02703   0.01823  -0.0203   0.1975   0.8239
   9.250   1.0505   0.02787   0.01911  -0.0188   0.1864   0.8284
   9.500   1.0653   0.02876   0.02006  -0.0178   0.1755   0.8334
   9.750   1.0767   0.02970   0.02106  -0.0163   0.1663   0.8385
  10.000   1.0883   0.03071   0.02217  -0.0150   0.1569   0.8449
  10.250   1.1003   0.03175   0.02331  -0.0139   0.1482   0.8520
  10.500   1.1086   0.03294   0.02456  -0.0125   0.1406   0.8605
  10.750   1.1191   0.03403   0.02582  -0.0113   0.1323   0.8708
  11.000   1.1247   0.03535   0.02718  -0.0097   0.1261   0.8852
  11.250   1.1309   0.03639   0.02845  -0.0077   0.1191   0.9124
  11.500   1.1350   0.03776   0.02988  -0.0065   0.1134   1.0000
  11.750   1.1472   0.03937   0.03158  -0.0066   0.1066   1.0000
  12.000   1.1559   0.04120   0.03343  -0.0065   0.1010   1.0000
  12.250   1.1653   0.04302   0.03533  -0.0064   0.0956   1.0000
  12.500   1.1730   0.04495   0.03735  -0.0062   0.0906   1.0000
  12.750   1.1782   0.04707   0.03945  -0.0060   0.0868   1.0000
  13.000   1.1858   0.04909   0.04164  -0.0058   0.0824   1.0000
  13.250   1.1904   0.05132   0.04394  -0.0057   0.0788   1.0000
  13.750   1.1980   0.05607   0.04887  -0.0054   0.0727   1.0000
  14.000   1.2007   0.05860   0.05152  -0.0053   0.0698   1.0000
  14.250   1.2018   0.06129   0.05429  -0.0055   0.0674   1.0000
  14.500   1.2029   0.06397   0.05695  -0.0055   0.0653   1.0000
  14.750   1.2028   0.06705   0.06028  -0.0058   0.0631   1.0000
  15.000   1.2017   0.07029   0.06370  -0.0062   0.0610   1.0000
  15.250   1.2000   0.07365   0.06718  -0.0068   0.0592   1.0000
  15.500   1.1983   0.07704   0.07066  -0.0076   0.0576   1.0000
  15.750   1.1980   0.08022   0.07384  -0.0083   0.0561   1.0000
  16.000   1.1910   0.08473   0.07859  -0.0097   0.0547   1.0000
  16.250   1.1823   0.08966   0.08376  -0.0115   0.0534   1.0000
  16.500   1.1729   0.09482   0.08913  -0.0136   0.0522   1.0000
  16.750   1.1628   0.10022   0.09470  -0.0160   0.0511   1.0000
  17.000   1.1530   0.10571   0.10035  -0.0187   0.0501   1.0000
  17.250   1.1449   0.11099   0.10573  -0.0213   0.0491   1.0000
  17.500   1.1431   0.11505   0.10984  -0.0233   0.0481   1.0000
  17.750   1.1312   0.12129   0.11620  -0.0266   0.0473   1.0000
  18.000   1.1025   0.13152   0.12669  -0.0329   0.0470   1.0000
  18.250   1.0578   0.14630   0.14174  -0.0424   0.0469   1.0000
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