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FX 38-153 AIRFOIL (fx38153-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 38-153 AIRFOIL (fx38153-il)
Reynolds number: 500,000
Max Cl/Cd: 63.29 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx38153-il-500000.txt
Download as CSV file: xf-fx38153-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 38-153 AIRFOIL                               
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.3855   0.08931   0.08694  -0.0928   0.9788   0.0189
 -11.250  -0.4188   0.07663   0.07416  -0.1021   0.9755   0.0188
 -11.000  -0.4410   0.06977   0.06716  -0.1065   0.9732   0.0188
 -10.750  -0.4561   0.06472   0.06197  -0.1092   0.9714   0.0188
 -10.500  -0.4674   0.06059   0.05771  -0.1107   0.9700   0.0189
 -10.250  -0.4953   0.05894   0.05598  -0.1051   0.9641   0.0189
 -10.000  -0.5110   0.05645   0.05337  -0.1026   0.9597   0.0190
  -9.750  -0.5208   0.05389   0.05067  -0.1008   0.9569   0.0192
  -9.500  -0.5189   0.05077   0.04738  -0.1009   0.9550   0.0194
  -7.750  -0.5295   0.03016   0.02456  -0.0741   0.9272   0.0151
  -7.500  -0.5035   0.02687   0.02095  -0.0736   0.9267   0.0127
  -7.250  -0.4754   0.02454   0.01823  -0.0733   0.9263   0.0120
  -7.000  -0.4457   0.02344   0.01703  -0.0739   0.9258   0.0121
  -6.750  -0.4153   0.02252   0.01603  -0.0747   0.9253   0.0123
  -6.500  -0.4288   0.02238   0.01585  -0.0668   0.9167   0.0123
  -6.250  -0.4031   0.02160   0.01503  -0.0667   0.9149   0.0125
  -6.000  -0.3746   0.02091   0.01430  -0.0673   0.9135   0.0128
  -5.750  -0.3444   0.02036   0.01371  -0.0682   0.9124   0.0135
  -5.500  -0.3139   0.01976   0.01307  -0.0691   0.9116   0.0139
  -5.250  -0.2829   0.01909   0.01237  -0.0703   0.9108   0.0141
  -5.000  -0.2829   0.01895   0.01221  -0.0652   0.9041   0.0142
  -4.750  -0.2599   0.01847   0.01170  -0.0648   0.9010   0.0144
  -4.500  -0.2297   0.01780   0.01102  -0.0658   0.8992   0.0148
  -4.250  -0.1967   0.01725   0.01045  -0.0673   0.8980   0.0157
  -4.000  -0.1624   0.01681   0.00998  -0.0690   0.8971   0.0173
  -3.750  -0.1276   0.01633   0.00945  -0.0708   0.8964   0.0216
  -3.500  -0.0921   0.01592   0.00912  -0.0728   0.8957   0.0404
  -3.250  -0.0810   0.01580   0.00910  -0.0700   0.8890   0.0646
  -3.000  -0.0496   0.01536   0.00878  -0.0713   0.8861   0.1068
  -2.750  -0.0093   0.01421   0.00826  -0.0752   0.8850   0.2653
  -2.500   0.0573   0.01201   0.00762  -0.0863   0.8866   0.6427
  -2.250   0.0911   0.01189   0.00770  -0.0873   0.8849   0.7051
  -2.000   0.1257   0.01189   0.00773  -0.0884   0.8836   0.7346
  -1.750   0.1604   0.01189   0.00771  -0.0895   0.8826   0.7488
  -1.500   0.1929   0.01200   0.00783  -0.0899   0.8817   0.7603
  -1.250   0.2299   0.01195   0.00775  -0.0917   0.8810   0.7673
  -1.000   0.2643   0.01189   0.00768  -0.0926   0.8802   0.7724
  -0.750   0.2713   0.01215   0.00797  -0.0879   0.8714   0.7763
  -0.500   0.3115   0.01186   0.00766  -0.0899   0.8694   0.7833
  -0.250   0.3454   0.01169   0.00750  -0.0901   0.8673   0.7879
   0.000   0.3792   0.01160   0.00742  -0.0904   0.8654   0.7910
   0.250   0.3904   0.01173   0.00757  -0.0866   0.8570   0.7953
   0.500   0.4266   0.01153   0.00734  -0.0882   0.8534   0.8016
   0.750   0.4588   0.01144   0.00726  -0.0883   0.8504   0.8036
   1.000   0.4670   0.01144   0.00729  -0.0838   0.8400   0.8058
   1.250   0.4932   0.01121   0.00705  -0.0833   0.8313   0.8076
   1.500   0.5239   0.01095   0.00676  -0.0839   0.8210   0.8093
   1.750   0.5460   0.01077   0.00657  -0.0829   0.8076   0.8119
   2.000   0.5786   0.01058   0.00635  -0.0844   0.7939   0.8149
   2.250   0.6114   0.01044   0.00615  -0.0857   0.7787   0.8169
   2.500   0.6384   0.01038   0.00604  -0.0855   0.7603   0.8179
   2.750   0.6607   0.01044   0.00597  -0.0843   0.7287   0.8192
   3.000   0.6741   0.01068   0.00601  -0.0811   0.6819   0.8209
   3.250   0.6828   0.01106   0.00615  -0.0772   0.6321   0.8231
   3.500   0.6948   0.01146   0.00632  -0.0743   0.5886   0.8252
   3.750   0.7110   0.01188   0.00653  -0.0726   0.5444   0.8273
   4.000   0.7299   0.01234   0.00679  -0.0716   0.4989   0.8295
   4.250   0.7520   0.01287   0.00707  -0.0714   0.4525   0.8319
   4.750   0.7846   0.01371   0.00760  -0.0678   0.3791   0.8343
   5.000   0.8026   0.01416   0.00789  -0.0664   0.3449   0.8354
   5.250   0.8224   0.01455   0.00817  -0.0654   0.3159   0.8365
   5.500   0.8413   0.01500   0.00849  -0.0642   0.2857   0.8378
   5.750   0.8611   0.01544   0.00882  -0.0632   0.2561   0.8394
   6.000   0.8805   0.01598   0.00918  -0.0623   0.2238   0.8409
   6.500   0.9250   0.01688   0.00987  -0.0617   0.1770   0.8438
   6.750   0.9489   0.01730   0.01023  -0.0617   0.1608   0.8455
   7.250   0.9938   0.01825   0.01102  -0.0613   0.1262   0.8479
   7.500   1.0148   0.01857   0.01135  -0.0606   0.1167   0.8488
   7.750   1.0342   0.01903   0.01177  -0.0597   0.1021   0.8497
   8.000   1.0533   0.01951   0.01222  -0.0587   0.0916   0.8507
   8.250   1.0722   0.01999   0.01270  -0.0576   0.0844   0.8519
   8.500   1.0924   0.02042   0.01316  -0.0569   0.0746   0.8532
   8.750   1.1089   0.02114   0.01379  -0.0556   0.0593   0.8544
   9.000   1.1271   0.02177   0.01442  -0.0547   0.0514   0.8555
   9.250   1.1464   0.02235   0.01502  -0.0540   0.0411   0.8567
   9.500   1.1615   0.02324   0.01583  -0.0527   0.0324   0.8579
   9.750   1.1791   0.02399   0.01661  -0.0518   0.0291   0.8590
  10.000   1.1954   0.02485   0.01751  -0.0508   0.0263   0.8602
  10.250   1.2144   0.02551   0.01825  -0.0502   0.0250   0.8612
  10.500   1.2329   0.02624   0.01905  -0.0496   0.0238   0.8622
  10.750   1.2487   0.02697   0.01985  -0.0484   0.0225   0.8632
  11.000   1.2624   0.02779   0.02072  -0.0470   0.0213   0.8643
  11.250   1.2758   0.02865   0.02164  -0.0455   0.0203   0.8654
  11.500   1.2904   0.02944   0.02252  -0.0443   0.0195   0.8665
  11.750   1.3046   0.03032   0.02345  -0.0432   0.0187   0.8675
  12.000   1.3182   0.03126   0.02445  -0.0420   0.0181   0.8685
  12.250   1.3305   0.03230   0.02557  -0.0408   0.0175   0.8696
  12.500   1.3417   0.03347   0.02680  -0.0395   0.0169   0.8708
  12.750   1.3508   0.03483   0.02824  -0.0381   0.0164   0.8719
  13.000   1.3615   0.03611   0.02961  -0.0370   0.0161   0.8730
  13.250   1.3714   0.03749   0.03109  -0.0359   0.0158   0.8741
  13.500   1.3804   0.03898   0.03267  -0.0348   0.0154   0.8752
  13.750   1.3887   0.04059   0.03438  -0.0338   0.0151   0.8762
  14.000   1.3957   0.04238   0.03626  -0.0329   0.0146   0.8773
  14.250   1.3995   0.04434   0.03830  -0.0317   0.0141   0.8784
  14.500   1.4000   0.04666   0.04072  -0.0304   0.0136   0.8795
  14.750   1.3985   0.04930   0.04348  -0.0292   0.0132   0.8805
  15.000   1.3991   0.05187   0.04618  -0.0284   0.0129   0.8815
  15.250   1.4026   0.05422   0.04867  -0.0279   0.0126   0.8825
  15.500   1.4042   0.05689   0.05148  -0.0275   0.0123   0.8836
  15.750   1.4041   0.05985   0.05456  -0.0274   0.0119   0.8846
  16.000   1.4018   0.06320   0.05805  -0.0274   0.0115   0.8857
  16.250   1.3969   0.06700   0.06198  -0.0278   0.0111   0.8867
  16.500   1.3883   0.07146   0.06657  -0.0285   0.0107   0.8877
  16.750   1.3755   0.07663   0.07186  -0.0295   0.0104   0.8888
  17.000   1.3622   0.08204   0.07740  -0.0309   0.0102   0.8898
  17.250   1.3512   0.08732   0.08283  -0.0325   0.0100   0.8907
  17.500   1.3511   0.09125   0.08692  -0.0341   0.0096   0.8917
  17.750   1.3464   0.09587   0.09170  -0.0360   0.0093   0.8925
  18.000   1.3383   0.10096   0.09695  -0.0380   0.0089   0.8933
  18.250   1.3287   0.10635   0.10248  -0.0403   0.0085   0.8941
  18.500   1.3173   0.11216   0.10843  -0.0429   0.0082   0.8949
  18.750   1.3055   0.11813   0.11452  -0.0457   0.0081   0.8957
  19.000   1.2931   0.12432   0.12084  -0.0488   0.0079   0.8965
  19.250   1.2804   0.13064   0.12728  -0.0521   0.0077   0.8973
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