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FX 73-CL1-152 (fx73cl1152-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 73-CL1-152 (fx73cl1152-il)
Reynolds number: 500,000
Max Cl/Cd: 100.82 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx73cl1152-il-500000.txt
Download as CSV file: xf-fx73cl1152-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-CL1-152                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.0429   0.09916   0.09471  -0.0701   0.5414   0.0412
  -9.750  -0.0337   0.09690   0.09240  -0.0709   0.5338   0.0421
  -9.500  -0.0578   0.09030   0.08585  -0.0770   0.5336   0.0448
  -9.250  -0.0458   0.08805   0.08358  -0.0770   0.5264   0.0450
  -9.000  -0.0308   0.08649   0.08198  -0.0766   0.5191   0.0453
  -8.750  -0.0180   0.08472   0.08014  -0.0766   0.5124   0.0456
  -8.500  -0.2796   0.03080   0.02570  -0.1175   0.5468   0.0397
  -8.250  -0.2730   0.02655   0.02093  -0.1189   0.5394   0.0400
  -8.000  -0.2539   0.02486   0.01903  -0.1188   0.5311   0.0404
  -7.750  -0.2309   0.02385   0.01793  -0.1187   0.5236   0.0409
  -7.500  -0.2071   0.02312   0.01708  -0.1184   0.5161   0.0414
  -7.250  -0.1832   0.02224   0.01605  -0.1182   0.5098   0.0419
  -7.000  -0.1592   0.02117   0.01478  -0.1180   0.5038   0.0426
  -6.750  -0.1349   0.02017   0.01354  -0.1177   0.4982   0.0434
  -6.500  -0.1100   0.01938   0.01247  -0.1174   0.4928   0.0442
  -6.250  -0.0843   0.01848   0.01135  -0.1172   0.4883   0.0449
  -6.000  -0.0589   0.01758   0.01040  -0.1169   0.4835   0.0456
  -5.750  -0.0324   0.01716   0.00990  -0.1166   0.4788   0.0464
  -5.500  -0.0059   0.01680   0.00942  -0.1162   0.4743   0.0472
  -5.250   0.0213   0.01633   0.00888  -0.1159   0.4711   0.0481
  -5.000   0.0486   0.01589   0.00834  -0.1156   0.4676   0.0491
  -4.750   0.0762   0.01561   0.00791  -0.1153   0.4641   0.0500
  -4.500   0.1026   0.01499   0.00726  -0.1150   0.4608   0.0512
  -4.250   0.1298   0.01480   0.00701  -0.1147   0.4572   0.0524
  -4.000   0.1574   0.01455   0.00672  -0.1144   0.4544   0.0537
  -3.750   0.1852   0.01428   0.00640  -0.1141   0.4516   0.0550
  -3.500   0.2131   0.01404   0.00609  -0.1137   0.4487   0.0562
  -3.250   0.2402   0.01362   0.00569  -0.1134   0.4460   0.0578
  -3.000   0.2680   0.01349   0.00553  -0.1132   0.4434   0.0597
  -2.750   0.2958   0.01340   0.00536  -0.1128   0.4407   0.0617
  -2.500   0.3230   0.01325   0.00515  -0.1125   0.4375   0.0638
  -2.250   0.3509   0.01305   0.00499  -0.1123   0.4356   0.0661
  -2.000   0.3790   0.01292   0.00485  -0.1120   0.4333   0.0689
  -1.750   0.4067   0.01271   0.00465  -0.1117   0.4310   0.0722
  -1.500   0.4346   0.01262   0.00456  -0.1115   0.4286   0.0762
  -1.250   0.4624   0.01247   0.00440  -0.1112   0.4261   0.0808
  -1.000   0.4902   0.01242   0.00433  -0.1109   0.4237   0.0862
  -0.750   0.5178   0.01239   0.00429  -0.1106   0.4210   0.0937
  -0.500   0.5455   0.01237   0.00429  -0.1104   0.4185   0.1028
  -0.250   0.5734   0.01226   0.00424  -0.1101   0.4167   0.1148
   0.000   0.6011   0.01216   0.00422  -0.1099   0.4147   0.1327
   0.250   0.6288   0.01208   0.00424  -0.1096   0.4126   0.1611
   0.500   0.6564   0.01203   0.00427  -0.1094   0.4102   0.1917
   0.750   0.6841   0.01201   0.00431  -0.1091   0.4080   0.2194
   1.250   0.7392   0.01211   0.00446  -0.1086   0.4037   0.2695
   1.500   0.7667   0.01225   0.00465  -0.1084   0.4012   0.3008
   1.750   0.7939   0.01218   0.00472  -0.1081   0.3998   0.3420
   2.000   0.8208   0.01209   0.00481  -0.1078   0.3978   0.3998
   2.250   0.8470   0.01193   0.00492  -0.1073   0.3957   0.4937
   2.500   0.8699   0.01156   0.00507  -0.1062   0.3935   0.6800
   2.750   0.9100   0.01110   0.00515  -0.1084   0.3912   1.0000
   3.000   0.9376   0.01123   0.00522  -0.1081   0.3892   1.0000
   3.250   0.9650   0.01141   0.00532  -0.1079   0.3872   1.0000
   3.500   0.9925   0.01171   0.00554  -0.1077   0.3846   1.0000
   3.750   1.0198   0.01186   0.00568  -0.1074   0.3829   1.0000
   4.000   1.0470   0.01196   0.00578  -0.1071   0.3811   1.0000
   4.250   1.0741   0.01207   0.00589  -0.1068   0.3789   1.0000
   4.500   1.1011   0.01219   0.00599  -0.1065   0.3766   1.0000
   4.750   1.1281   0.01232   0.00609  -0.1062   0.3743   1.0000
   5.000   1.1550   0.01245   0.00619  -0.1059   0.3721   1.0000
   5.250   1.1818   0.01265   0.00634  -0.1056   0.3700   1.0000
   5.500   1.2087   0.01301   0.00663  -0.1054   0.3672   1.0000
   5.750   1.2350   0.01312   0.00678  -0.1050   0.3656   1.0000
   6.000   1.2612   0.01324   0.00694  -0.1046   0.3635   1.0000
   6.250   1.2874   0.01338   0.00710  -0.1043   0.3613   1.0000
   6.500   1.3135   0.01353   0.00726  -0.1039   0.3589   1.0000
   6.750   1.3396   0.01368   0.00739  -0.1035   0.3566   1.0000
   7.000   1.3654   0.01385   0.00754  -0.1031   0.3543   1.0000
   7.250   1.3913   0.01415   0.00779  -0.1028   0.3515   1.0000
   7.500   1.4165   0.01436   0.00804  -0.1023   0.3494   1.0000
   7.750   1.4415   0.01452   0.00825  -0.1018   0.3472   1.0000
   8.000   1.4664   0.01469   0.00846  -0.1013   0.3447   1.0000
   8.250   1.4913   0.01487   0.00866  -0.1008   0.3424   1.0000
   8.500   1.5160   0.01505   0.00885  -0.1002   0.3401   1.0000
   8.750   1.5405   0.01528   0.00907  -0.0997   0.3377   1.0000
   9.000   1.5653   0.01568   0.00942  -0.0993   0.3348   1.0000
   9.250   1.5883   0.01585   0.00968  -0.0985   0.3327   1.0000
   9.500   1.6114   0.01606   0.00996  -0.0978   0.3303   1.0000
   9.750   1.6345   0.01629   0.01023  -0.0971   0.3279   1.0000
  10.000   1.6574   0.01652   0.01049  -0.0963   0.3255   1.0000
  10.250   1.6800   0.01678   0.01076  -0.0956   0.3233   1.0000
  10.500   1.7026   0.01713   0.01109  -0.0948   0.3208   1.0000
  10.750   1.7243   0.01750   0.01150  -0.0940   0.3184   1.0000
  11.000   1.7444   0.01777   0.01187  -0.0929   0.3161   1.0000
  11.250   1.7645   0.01807   0.01224  -0.0918   0.3138   1.0000
  11.500   1.7842   0.01838   0.01259  -0.0906   0.3115   1.0000
  11.750   1.8029   0.01868   0.01293  -0.0893   0.3091   1.0000
  12.000   1.8200   0.01903   0.01327  -0.0877   0.3065   1.0000
  12.250   1.8358   0.01947   0.01373  -0.0860   0.3034   1.0000
  12.500   1.8468   0.01980   0.01418  -0.0835   0.3005   1.0000
  12.750   1.8588   0.02018   0.01462  -0.0813   0.2971   1.0000
  13.000   1.8704   0.02062   0.01510  -0.0793   0.2936   1.0000
  13.250   1.8823   0.02124   0.01568  -0.0774   0.2897   1.0000
  13.500   1.8918   0.02190   0.01646  -0.0754   0.2869   1.0000
  13.750   1.9012   0.02264   0.01730  -0.0736   0.2834   1.0000
  14.000   1.9102   0.02351   0.01823  -0.0720   0.2800   1.0000
  14.250   1.9176   0.02458   0.01929  -0.0705   0.2765   1.0000
  14.500   1.9246   0.02580   0.02060  -0.0692   0.2729   1.0000
  14.750   1.9307   0.02721   0.02212  -0.0682   0.2690   1.0000
  15.000   1.9348   0.02887   0.02385  -0.0674   0.2647   1.0000
  15.250   1.9352   0.03095   0.02592  -0.0665   0.2600   1.0000
  15.500   1.9384   0.03305   0.02817  -0.0662   0.2561   1.0000
  15.750   1.9379   0.03553   0.03073  -0.0660   0.2516   1.0000
  16.000   1.9345   0.03830   0.03353  -0.0656   0.2478   1.0000
  16.250   1.9307   0.04119   0.03651  -0.0654   0.2442   1.0000
  16.500   1.9260   0.04430   0.03975  -0.0654   0.2403   1.0000
  16.750   1.9168   0.04784   0.04336  -0.0653   0.2361   1.0000
  17.000   1.9040   0.05173   0.04726  -0.0653   0.2320   1.0000
  17.250   1.8936   0.05569   0.05137  -0.0656   0.2278   1.0000
  17.500   1.8776   0.06029   0.05605  -0.0659   0.2227   1.0000
  17.750   1.8613   0.06490   0.06067  -0.0663   0.2181   1.0000
  18.000   1.8462   0.06960   0.06551  -0.0668   0.2133   1.0000
  18.250   1.8256   0.07496   0.07092  -0.0675   0.2073   1.0000
  18.500   1.8073   0.08013   0.07615  -0.0683   0.2014   1.0000
  18.750   1.7865   0.08571   0.08179  -0.0692   0.1948   1.0000
  19.000   1.7654   0.09140   0.08752  -0.0702   0.1879   1.0000
  19.250   1.7422   0.09749   0.09363  -0.0715   0.1801   1.0000
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