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AS5048 (18%) (as5048-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: AS5048 (18%) (as5048-il)
Reynolds number: 200,000
Max Cl/Cd: 59.93 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-as5048-il-200000.txt
Download as CSV file: xf-as5048-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.3498   0.12618   0.12287  -0.0444   1.0000   0.0684
 -13.500  -0.3476   0.12353   0.12025  -0.0448   1.0000   0.0705
 -13.250  -0.5328   0.11494   0.11137  -0.0481   1.0000   0.0667
 -13.000  -0.5145   0.11540   0.11184  -0.0453   1.0000   0.0680
 -12.750  -0.5113   0.11211   0.10857  -0.0459   1.0000   0.0697
 -12.500  -0.5295   0.10340   0.09990  -0.0510   1.0000   0.0721
 -12.250  -0.5784   0.09078   0.08724  -0.0592   1.0000   0.0724
 -12.000  -0.6185   0.08294   0.07932  -0.0629   1.0000   0.0722
 -11.750  -0.6533   0.07716   0.07344  -0.0643   1.0000   0.0722
 -11.500  -0.6849   0.07263   0.06882  -0.0642   1.0000   0.0726
 -11.250  -0.7154   0.06908   0.06516  -0.0628   1.0000   0.0731
 -11.000  -0.7467   0.06654   0.06253  -0.0596   1.0000   0.0737
 -10.750  -0.7838   0.06520   0.06094  -0.0559   0.9928   0.0753
  -9.750  -0.7268   0.03589   0.02868  -0.0588   0.9167   0.0320
  -9.500  -0.6816   0.03271   0.02517  -0.0628   0.9095   0.0314
  -9.250  -0.6355   0.03037   0.02254  -0.0667   0.9013   0.0318
  -9.000  -0.5942   0.02883   0.02065  -0.0700   0.8918   0.0331
  -8.750  -0.5412   0.02680   0.01854  -0.0740   0.8858   0.0340
  -8.500  -0.4969   0.02551   0.01729  -0.0763   0.8793   0.0352
  -8.250  -0.4642   0.02459   0.01635  -0.0773   0.8725   0.0366
  -8.000  -0.4399   0.02379   0.01551  -0.0771   0.8658   0.0382
  -7.750  -0.4191   0.02292   0.01457  -0.0767   0.8599   0.0404
  -7.500  -0.4030   0.02192   0.01359  -0.0760   0.8548   0.0428
  -7.250  -0.3884   0.02105   0.01269  -0.0749   0.8494   0.0451
  -7.000  -0.3754   0.02023   0.01179  -0.0734   0.8442   0.0473
  -6.750  -0.3680   0.01940   0.01092  -0.0711   0.8398   0.0508
  -6.500  -0.3549   0.01875   0.01022  -0.0694   0.8362   0.0567
  -6.250  -0.3433   0.01797   0.00948  -0.0674   0.8325   0.0680
  -6.000  -0.3507   0.01606   0.00835  -0.0631   0.8285   0.1938
  -5.750  -0.3676   0.01366   0.00742  -0.0571   0.8244   0.4549
  -5.500  -0.3465   0.01441   0.00865  -0.0548   0.8215   0.5894
  -5.250  -0.3209   0.01532   0.00949  -0.0536   0.8188   0.6201
  -5.000  -0.2927   0.01639   0.01054  -0.0527   0.8162   0.6374
  -4.750  -0.2643   0.01751   0.01163  -0.0517   0.8134   0.6527
  -4.500  -0.2293   0.01928   0.01348  -0.0504   0.8106   0.6630
  -4.250  -0.2009   0.02003   0.01417  -0.0495   0.8080   0.6737
  -4.000  -0.1695   0.02073   0.01482  -0.0491   0.8058   0.6793
  -3.750  -0.1470   0.02060   0.01455  -0.0489   0.8032   0.6886
  -3.500  -0.1194   0.02093   0.01489  -0.0482   0.8004   0.6916
  -3.250  -0.0934   0.02111   0.01503  -0.0477   0.7976   0.6962
  -3.000  -0.0731   0.02076   0.01457  -0.0475   0.7944   0.7050
  -2.750  -0.0451   0.02094   0.01473  -0.0471   0.7915   0.7075
  -2.500  -0.0175   0.02107   0.01482  -0.0468   0.7889   0.7109
  -2.250   0.0083   0.02106   0.01472  -0.0469   0.7864   0.7163
  -2.000   0.0284   0.02077   0.01440  -0.0465   0.7830   0.7222
  -1.750   0.0532   0.02085   0.01449  -0.0458   0.7796   0.7247
  -1.500   0.0786   0.02088   0.01450  -0.0454   0.7762   0.7279
  -1.250   0.1043   0.02082   0.01438  -0.0455   0.7730   0.7322
  -1.000   0.1306   0.02061   0.01405  -0.0463   0.7699   0.7379
  -0.750   0.1532   0.02063   0.01412  -0.0454   0.7661   0.7401
  -0.500   0.1762   0.02067   0.01418  -0.0446   0.7616   0.7427
  -0.250   0.2022   0.02063   0.01413  -0.0444   0.7574   0.7456
   0.000   0.2305   0.02055   0.01399  -0.0449   0.7536   0.7490
   0.250   0.2546   0.02049   0.01389  -0.0450   0.7488   0.7528
   0.500   0.2784   0.02036   0.01377  -0.0448   0.7432   0.7555
   0.750   0.3056   0.02027   0.01367  -0.0447   0.7387   0.7576
   1.000   0.3354   0.02025   0.01361  -0.0451   0.7351   0.7596
   1.250   0.3555   0.02028   0.01371  -0.0441   0.7288   0.7619
   1.500   0.3826   0.02020   0.01363  -0.0442   0.7235   0.7646
   1.750   0.4133   0.02007   0.01345  -0.0450   0.7193   0.7673
   2.000   0.4379   0.02006   0.01346  -0.0450   0.7132   0.7698
   2.250   0.4655   0.01992   0.01332  -0.0454   0.7069   0.7719
   2.500   0.4961   0.01967   0.01305  -0.0457   0.7020   0.7738
   2.750   0.5187   0.01956   0.01301  -0.0448   0.6938   0.7760
   3.000   0.5490   0.01920   0.01264  -0.0451   0.6866   0.7780
   3.250   0.5771   0.01898   0.01242  -0.0452   0.6797   0.7800
   3.500   0.6036   0.01875   0.01223  -0.0451   0.6718   0.7821
   3.750   0.6374   0.01842   0.01185  -0.0462   0.6667   0.7846
   4.000   0.6602   0.01830   0.01183  -0.0456   0.6575   0.7872
   4.250   0.6921   0.01793   0.01143  -0.0464   0.6512   0.7891
   4.500   0.7157   0.01768   0.01128  -0.0456   0.6421   0.7909
   4.750   0.7450   0.01726   0.01089  -0.0457   0.6345   0.7927
   5.000   0.7686   0.01702   0.01075  -0.0449   0.6242   0.7949
   5.250   0.7977   0.01660   0.01034  -0.0450   0.6154   0.7975
   5.500   0.8216   0.01630   0.01011  -0.0442   0.6022   0.8002
   5.750   0.8464   0.01602   0.00989  -0.0437   0.5872   0.8026
   6.000   0.8721   0.01575   0.00963  -0.0433   0.5698   0.8049
   6.250   0.8945   0.01555   0.00943  -0.0423   0.5471   0.8070
   6.500   0.9153   0.01544   0.00923  -0.0408   0.5201   0.8091
   6.750   0.9331   0.01557   0.00923  -0.0389   0.4880   0.8119
   7.000   0.9488   0.01589   0.00940  -0.0368   0.4549   0.8150
   7.250   0.9630   0.01634   0.00969  -0.0346   0.4224   0.8180
   7.500   0.9762   0.01687   0.01009  -0.0323   0.3914   0.8209
   7.750   0.9879   0.01744   0.01054  -0.0299   0.3630   0.8237
   8.000   0.9950   0.01801   0.01100  -0.0265   0.3390   0.8266
   8.250   1.0030   0.01859   0.01154  -0.0234   0.3164   0.8299
   8.500   1.0131   0.01929   0.01218  -0.0210   0.2954   0.8337
   8.750   1.0241   0.02007   0.01288  -0.0189   0.2768   0.8379
   9.000   1.0347   0.02083   0.01361  -0.0168   0.2606   0.8420
   9.250   1.0450   0.02159   0.01438  -0.0147   0.2466   0.8465
   9.500   1.0559   0.02242   0.01521  -0.0129   0.2340   0.8513
   9.750   1.0667   0.02337   0.01610  -0.0113   0.2227   0.8566
  10.000   1.0770   0.02416   0.01698  -0.0095   0.2118   0.8622
  10.250   1.0875   0.02507   0.01794  -0.0079   0.2018   0.8692
  10.500   1.0959   0.02613   0.01897  -0.0061   0.1926   0.8773
  10.750   1.1048   0.02699   0.01999  -0.0043   0.1834   0.8888
  11.250   1.1051   0.02854   0.02175   0.0027   0.1689   1.0000
  11.500   1.1186   0.02993   0.02305   0.0027   0.1600   1.0000
  11.750   1.1325   0.03125   0.02444   0.0025   0.1509   1.0000
  12.000   1.1443   0.03268   0.02585   0.0028   0.1428   1.0000
  12.250   1.1550   0.03414   0.02733   0.0030   0.1348   1.0000
  12.500   1.1653   0.03565   0.02885   0.0035   0.1274   1.0000
  12.750   1.1740   0.03722   0.03042   0.0039   0.1205   1.0000
  13.000   1.1829   0.03881   0.03204   0.0045   0.1141   1.0000
  13.250   1.1906   0.04047   0.03374   0.0050   0.1081   1.0000
  13.500   1.1979   0.04218   0.03542   0.0057   0.1028   1.0000
  13.750   1.2053   0.04391   0.03724   0.0062   0.0977   1.0000
  14.000   1.2113   0.04571   0.03898   0.0068   0.0932   1.0000
  14.250   1.2182   0.04755   0.04093   0.0074   0.0890   1.0000
  14.500   1.2240   0.04947   0.04292   0.0078   0.0851   1.0000
  14.750   1.2303   0.05131   0.04469   0.0084   0.0815   1.0000
  15.000   1.2359   0.05335   0.04686   0.0089   0.0784   1.0000
  15.250   1.2404   0.05551   0.04913   0.0091   0.0752   1.0000
  15.500   1.2450   0.05765   0.05130   0.0093   0.0725   1.0000
  15.750   1.2541   0.05933   0.05291   0.0101   0.0695   1.0000
  16.000   1.2545   0.06205   0.05584   0.0101   0.0675   1.0000
  16.250   1.2564   0.06463   0.05856   0.0100   0.0652   1.0000
  16.500   1.2597   0.06707   0.06104   0.0099   0.0631   1.0000
  16.750   1.2675   0.06894   0.06287   0.0103   0.0609   1.0000
  17.000   1.2686   0.07172   0.06580   0.0104   0.0592   1.0000
  17.250   1.2643   0.07526   0.06955   0.0098   0.0577   1.0000
  17.500   1.2618   0.07864   0.07308   0.0091   0.0561   1.0000
  17.750   1.2613   0.08179   0.07632   0.0084   0.0546   1.0000
  18.000   1.2647   0.08437   0.07891   0.0080   0.0531   1.0000
  18.250   1.2714   0.08641   0.08093   0.0085   0.0514   1.0000
  18.500   1.2601   0.09123   0.08600   0.0069   0.0507   1.0000
  18.750   1.2484   0.09628   0.09128   0.0050   0.0499   1.0000
  19.000   1.2366   0.10148   0.09670   0.0028   0.0491   1.0000
  19.250   1.2241   0.10695   0.10237   0.0004   0.0482   1.0000
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