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AS5048 (18%) (as5048-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: AS5048 (18%) (as5048-il)
Reynolds number: 100,000
Max Cl/Cd: 41.21 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-as5048-il-100000.txt
Download as CSV file: xf-as5048-il-100000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.4325   0.09082   0.08631  -0.0592   1.0000   0.0954
 -11.750  -0.4982   0.07878   0.07420  -0.0648   1.0000   0.0939
 -11.500  -0.5512   0.07098   0.06630  -0.0666   1.0000   0.0934
 -11.250  -0.6055   0.06488   0.06006  -0.0662   1.0000   0.0923
 -11.000  -0.6622   0.06079   0.05580  -0.0632   1.0000   0.0910
 -10.750  -0.7059   0.05914   0.05413  -0.0577   1.0000   0.0906
 -10.500  -0.7229   0.06001   0.05525  -0.0513   1.0000   0.0918
 -10.250  -0.8069   0.06412   0.05869  -0.0467   1.0000   0.0925
 -10.000  -0.8731   0.06739   0.06141  -0.0360   0.9953   0.0887
  -9.750  -0.8631   0.05696   0.05008  -0.0356   0.9894   0.0645
  -9.500  -0.8405   0.05227   0.04517  -0.0372   0.9845   0.0628
  -9.250  -0.8205   0.04839   0.04091  -0.0378   0.9780   0.0608
  -9.000  -0.8035   0.04466   0.03640  -0.0372   0.9711   0.0571
  -8.750  -0.7772   0.04313   0.03428  -0.0374   0.9652   0.0555
  -8.500  -0.7461   0.04024   0.03118  -0.0384   0.9613   0.0552
  -8.250  -0.7153   0.03807   0.02878  -0.0392   0.9570   0.0552
  -8.000  -0.6748   0.03554   0.02621  -0.0413   0.9549   0.0566
  -7.750  -0.6343   0.03376   0.02451  -0.0438   0.9529   0.0599
  -7.500  -0.5950   0.03238   0.02309  -0.0455   0.9503   0.0626
  -7.250  -0.5634   0.03134   0.02201  -0.0459   0.9459   0.0648
  -7.000  -0.5334   0.02991   0.02079  -0.0467   0.9425   0.0690
  -6.750  -0.5060   0.02884   0.01970  -0.0475   0.9392   0.0754
  -6.500  -0.4981   0.02791   0.01881  -0.0452   0.9333   0.0802
  -6.250  -0.4826   0.02701   0.01786  -0.0440   0.9280   0.0885
  -6.000  -0.4652   0.02541   0.01652  -0.0437   0.9242   0.1155
  -5.750  -0.4825   0.02374   0.01575  -0.0379   0.9170   0.2278
  -5.500  -0.4914   0.02376   0.01785  -0.0299   0.9119   0.5783
  -5.250  -0.4534   0.02745   0.02140  -0.0271   0.9091   0.6395
  -5.000  -0.3999   0.03154   0.02539  -0.0253   0.9079   0.6715
  -4.750  -0.2805   0.03761   0.03125  -0.0292   0.9112   0.6955
  -4.500  -0.2426   0.03738   0.03083  -0.0312   0.9090   0.7079
  -4.250  -0.2686   0.03730   0.03074  -0.0234   0.9010   0.7219
  -4.000  -0.1801   0.03762   0.03081  -0.0321   0.9022   0.7279
  -3.750  -0.1797   0.03733   0.03046  -0.0285   0.8963   0.7402
  -3.500  -0.1174   0.03723   0.03019  -0.0342   0.8954   0.7477
  -3.250  -0.0888   0.03671   0.02955  -0.0353   0.8923   0.7579
  -3.000  -0.0278   0.03628   0.02897  -0.0414   0.8912   0.7655
  -2.750  -0.0896   0.03688   0.02966  -0.0270   0.8804   0.7751
  -2.500  -0.0345   0.03655   0.02919  -0.0322   0.8784   0.7819
  -2.250  -0.0233   0.03601   0.02858  -0.0307   0.8745   0.7906
  -2.000  -0.0442   0.03668   0.02928  -0.0227   0.8664   0.7965
  -1.750  -0.0882   0.03630   0.02890  -0.0123   0.8587   0.8063
  -1.500  -0.0052   0.03602   0.02849  -0.0220   0.8580   0.8095
  -1.250  -0.0860   0.03665   0.02921  -0.0046   0.8465   0.8172
  -1.000  -0.0781   0.03608   0.02857  -0.0027   0.8415   0.8238
  -0.750  -0.0047   0.03585   0.02825  -0.0107   0.8397   0.8265
  -0.500  -0.0647   0.03634   0.02879   0.0028   0.8287   0.8333
  -0.250  -0.0397   0.03590   0.02827   0.0020   0.8238   0.8384
   0.000  -0.0368   0.03599   0.02835   0.0052   0.8166   0.8426
   0.250  -0.0205   0.03606   0.02840   0.0063   0.8094   0.8463
   0.500   0.0300   0.03579   0.02808   0.0021   0.8054   0.8494
   0.750   0.0081   0.03600   0.02828   0.0084   0.7947   0.8547
   1.000   0.0460   0.03570   0.02793   0.0060   0.7891   0.8577
   1.250   0.1077   0.03538   0.02758   0.0006   0.7860   0.8595
   1.500   0.0888   0.03594   0.02817   0.0067   0.7732   0.8633
   1.750   0.1486   0.03549   0.02771   0.0016   0.7698   0.8653
   2.000   0.1337   0.03606   0.02829   0.0068   0.7565   0.8701
   2.250   0.1901   0.03549   0.02771   0.0023   0.7529   0.8720
   2.500   0.1849   0.03606   0.02830   0.0059   0.7395   0.8755
   2.750   0.2427   0.03544   0.02770   0.0018   0.7360   0.8774
   3.000   0.2411   0.03606   0.02835   0.0053   0.7222   0.8812
   3.250   0.3025   0.03528   0.02759   0.0007   0.7190   0.8828
   3.500   0.3020   0.03578   0.02813   0.0039   0.7048   0.8866
   3.750   0.3657   0.03481   0.02719  -0.0009   0.7018   0.8886
   4.000   0.3689   0.03515   0.02757   0.0021   0.6875   0.8925
   4.250   0.4365   0.03376   0.02623  -0.0026   0.6844   0.8939
   4.500   0.4476   0.03387   0.02641  -0.0004   0.6702   0.8971
   4.750   0.4779   0.03337   0.02597  -0.0004   0.6601   0.9002
   5.000   0.5226   0.03227   0.02493  -0.0021   0.6527   0.9032
   5.250   0.5770   0.03084   0.02354  -0.0051   0.6480   0.9059
   5.500   0.5970   0.03044   0.02324  -0.0038   0.6353   0.9095
   5.750   0.6188   0.03005   0.02294  -0.0026   0.6228   0.9129
   6.000   0.6767   0.02831   0.02127  -0.0060   0.6173   0.9150
   6.250   0.6955   0.02778   0.02084  -0.0043   0.6036   0.9198
   6.500   0.7209   0.02697   0.02013  -0.0035   0.5906   0.9246
   6.750   0.7582   0.02585   0.01911  -0.0041   0.5777   0.9283
   7.000   0.7941   0.02473   0.01806  -0.0047   0.5625   0.9326
   7.250   0.8244   0.02377   0.01713  -0.0044   0.5439   0.9377
   7.500   0.8663   0.02272   0.01603  -0.0059   0.5209   0.9413
   7.750   0.8912   0.02242   0.01567  -0.0052   0.4915   0.9471
   8.000   0.9154   0.02240   0.01551  -0.0046   0.4595   0.9539
   8.250   0.9366   0.02273   0.01566  -0.0038   0.4272   0.9622
   8.500   0.9584   0.02331   0.01605  -0.0035   0.3961   0.9707
   8.750   0.9821   0.02405   0.01661  -0.0038   0.3678   0.9794
   9.000   1.0065   0.02489   0.01734  -0.0046   0.3419   0.9887
   9.250   1.0343   0.02582   0.01814  -0.0061   0.3185   0.9973
   9.500   1.0343   0.02617   0.01839  -0.0025   0.3055   1.0000
   9.750   1.0415   0.02684   0.01904  -0.0006   0.2906   1.0000
  10.000   1.0568   0.02774   0.01990   0.0000   0.2750   1.0000
  10.250   1.0727   0.02874   0.02086   0.0004   0.2602   1.0000
  10.500   1.0886   0.02981   0.02190   0.0009   0.2463   1.0000
  10.750   1.1045   0.03093   0.02300   0.0014   0.2331   1.0000
  11.000   1.1219   0.03208   0.02405   0.0017   0.2207   1.0000
  11.250   1.1388   0.03322   0.02510   0.0022   0.2085   1.0000
  11.500   1.1464   0.03455   0.02656   0.0037   0.1977   1.0000
  11.750   1.1606   0.03591   0.02790   0.0044   0.1872   1.0000
  12.000   1.1817   0.03716   0.02897   0.0044   0.1762   1.0000
  12.250   1.1823   0.03874   0.03081   0.0064   0.1680   1.0000
  12.500   1.2000   0.04016   0.03214   0.0068   0.1590   1.0000
  12.750   1.2038   0.04179   0.03392   0.0083   0.1515   1.0000
  13.000   1.2202   0.04335   0.03543   0.0088   0.1439   1.0000
  13.250   1.2218   0.04521   0.03750   0.0103   0.1377   1.0000
  13.500   1.2427   0.04667   0.03881   0.0104   0.1306   1.0000
  13.750   1.2369   0.04897   0.04143   0.0121   0.1262   1.0000
  14.000   1.2458   0.05063   0.04313   0.0129   0.1210   1.0000
  14.250   1.2571   0.05270   0.04522   0.0135   0.1161   1.0000
  14.500   1.2488   0.05546   0.04828   0.0149   0.1127   1.0000
  14.750   1.2488   0.05778   0.05074   0.0158   0.1090   1.0000
  15.000   1.2722   0.05935   0.05216   0.0158   0.1042   1.0000
  15.250   1.2533   0.06297   0.05615   0.0171   0.1025   1.0000
  15.500   1.2363   0.06680   0.06028   0.0179   0.1006   1.0000
  15.750   1.2224   0.07060   0.06432   0.0183   0.0985   1.0000
  16.000   1.2113   0.07430   0.06820   0.0185   0.0965   1.0000
  16.250   1.2424   0.07513   0.06879   0.0187   0.0922   1.0000
  16.500   1.2119   0.08050   0.07449   0.0185   0.0917   1.0000
  16.750   1.1781   0.08680   0.08110   0.0174   0.0915   1.0000
  17.000   1.1406   0.09424   0.08882   0.0152   0.0915   1.0000
  17.250   1.0971   0.10343   0.09828   0.0115   0.0918   1.0000
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