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FX 73-CL1-152 (fx73cl1152-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 73-CL1-152 (fx73cl1152-il)
Reynolds number: 500,000
Max Cl/Cd: 106.51 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73cl1152-il-500000-n5.txt
Download as CSV file: xf-fx73cl1152-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.1401   0.10763   0.10296  -0.0651   0.5276   0.0239
 -11.250  -0.5578   0.03045   0.02547  -0.1192   0.5965   0.0285
 -11.000  -0.5459   0.02841   0.02322  -0.1202   0.5835   0.0288
 -10.500  -0.5132   0.02541   0.01983  -0.1208   0.5594   0.0294
 -10.250  -0.4942   0.02417   0.01838  -0.1207   0.5492   0.0297
 -10.000  -0.4736   0.02305   0.01707  -0.1206   0.5393   0.0301
  -9.750  -0.4521   0.02205   0.01586  -0.1204   0.5304   0.0304
  -9.500  -0.4294   0.02114   0.01477  -0.1202   0.5219   0.0307
  -9.250  -0.4061   0.02036   0.01378  -0.1199   0.5136   0.0310
  -9.000  -0.3822   0.01960   0.01291  -0.1196   0.5066   0.0314
  -8.750  -0.3575   0.01902   0.01225  -0.1193   0.4989   0.0317
  -8.500  -0.3323   0.01854   0.01167  -0.1190   0.4921   0.0321
  -8.250  -0.3065   0.01810   0.01115  -0.1187   0.4855   0.0325
  -8.000  -0.2805   0.01769   0.01065  -0.1184   0.4789   0.0329
  -7.750  -0.2545   0.01729   0.01014  -0.1180   0.4735   0.0335
  -7.500  -0.2280   0.01687   0.00962  -0.1178   0.4688   0.0341
  -7.250  -0.2015   0.01645   0.00909  -0.1174   0.4640   0.0346
  -7.000  -0.1750   0.01607   0.00857  -0.1171   0.4593   0.0351
  -6.750  -0.1485   0.01567   0.00808  -0.1168   0.4553   0.0355
  -6.500  -0.1216   0.01529   0.00767  -0.1165   0.4518   0.0361
  -6.250  -0.0944   0.01500   0.00733  -0.1162   0.4481   0.0366
  -6.000  -0.0672   0.01473   0.00700  -0.1159   0.4442   0.0372
  -5.750  -0.0400   0.01449   0.00668  -0.1156   0.4403   0.0379
  -5.500  -0.0127   0.01427   0.00638  -0.1152   0.4368   0.0387
  -5.250   0.0150   0.01403   0.00608  -0.1150   0.4341   0.0395
  -5.000   0.0426   0.01376   0.00577  -0.1147   0.4313   0.0403
  -4.750   0.0701   0.01353   0.00552  -0.1144   0.4285   0.0411
  -4.500   0.0978   0.01335   0.00530  -0.1141   0.4257   0.0420
  -4.250   0.1254   0.01319   0.00508  -0.1138   0.4231   0.0429
  -4.000   0.1530   0.01305   0.00487  -0.1135   0.4205   0.0439
  -3.750   0.1809   0.01289   0.00467  -0.1132   0.4183   0.0449
  -3.500   0.2088   0.01271   0.00450  -0.1130   0.4161   0.0462
  -3.250   0.2368   0.01259   0.00435  -0.1127   0.4136   0.0477
  -3.000   0.2648   0.01248   0.00421  -0.1125   0.4112   0.0493
  -2.750   0.2927   0.01236   0.00406  -0.1122   0.4090   0.0507
  -2.500   0.3205   0.01225   0.00395  -0.1119   0.4069   0.0525
  -2.250   0.3484   0.01219   0.00385  -0.1116   0.4048   0.0546
  -2.000   0.3761   0.01214   0.00376  -0.1113   0.4025   0.0569
  -1.750   0.4040   0.01207   0.00370  -0.1110   0.4005   0.0598
  -1.500   0.4322   0.01200   0.00362  -0.1108   0.3987   0.0627
  -1.250   0.4602   0.01192   0.00356  -0.1106   0.3967   0.0663
  -1.000   0.4883   0.01188   0.00351  -0.1103   0.3945   0.0703
  -0.750   0.5161   0.01182   0.00347  -0.1101   0.3922   0.0757
  -0.500   0.5439   0.01179   0.00344  -0.1098   0.3899   0.0815
  -0.250   0.5716   0.01177   0.00341  -0.1095   0.3877   0.0883
   0.000   0.5991   0.01177   0.00341  -0.1092   0.3856   0.0973
   0.250   0.6266   0.01176   0.00343  -0.1089   0.3837   0.1090
   0.500   0.6546   0.01171   0.00344  -0.1087   0.3820   0.1239
   0.750   0.6823   0.01166   0.00347  -0.1085   0.3801   0.1455
   1.000   0.7101   0.01164   0.00352  -0.1082   0.3781   0.1690
   1.250   0.7377   0.01163   0.00357  -0.1080   0.3760   0.1911
   1.500   0.7651   0.01163   0.00363  -0.1077   0.3742   0.2135
   1.750   0.7925   0.01165   0.00369  -0.1074   0.3723   0.2354
   2.000   0.8197   0.01169   0.00376  -0.1071   0.3704   0.2561
   2.250   0.8467   0.01174   0.00384  -0.1068   0.3683   0.2794
   2.500   0.8738   0.01177   0.00394  -0.1065   0.3664   0.3083
   2.750   0.9011   0.01174   0.00404  -0.1062   0.3646   0.3503
   3.000   0.9279   0.01167   0.00416  -0.1059   0.3627   0.4176
   3.250   0.9535   0.01151   0.00431  -0.1054   0.3608   0.5363
   3.500   0.9734   0.01105   0.00449  -0.1036   0.3590   0.7769
   4.000   1.0436   0.01102   0.00469  -0.1063   0.3547   1.0000
   4.250   1.0703   0.01118   0.00480  -0.1059   0.3527   1.0000
   4.500   1.0968   0.01136   0.00493  -0.1056   0.3506   1.0000
   4.750   1.1241   0.01147   0.00505  -0.1053   0.3488   1.0000
   5.000   1.1512   0.01160   0.00518  -0.1050   0.3465   1.0000
   5.250   1.1780   0.01174   0.00531  -0.1047   0.3442   1.0000
   5.500   1.2045   0.01189   0.00546  -0.1044   0.3420   1.0000
   5.750   1.2308   0.01206   0.00560  -0.1040   0.3398   1.0000
   6.000   1.2568   0.01223   0.00575  -0.1036   0.3376   1.0000
   6.250   1.2823   0.01243   0.00592  -0.1031   0.3355   1.0000
   6.500   1.3084   0.01260   0.00611  -0.1028   0.3336   1.0000
   6.750   1.3346   0.01277   0.00630  -0.1024   0.3315   1.0000
   7.000   1.3605   0.01294   0.00648  -0.1020   0.3291   1.0000
   7.250   1.3859   0.01312   0.00668  -0.1016   0.3264   1.0000
   7.500   1.4109   0.01331   0.00687  -0.1011   0.3237   1.0000
   7.750   1.4353   0.01354   0.00708  -0.1005   0.3212   1.0000
   8.000   1.4596   0.01377   0.00731  -0.0999   0.3190   1.0000
   8.250   1.4847   0.01397   0.00755  -0.0994   0.3169   1.0000
   8.500   1.5092   0.01417   0.00779  -0.0989   0.3145   1.0000
   8.750   1.5333   0.01440   0.00805  -0.0983   0.3120   1.0000
   9.000   1.5567   0.01464   0.00831  -0.0976   0.3095   1.0000
   9.250   1.5793   0.01491   0.00858  -0.0968   0.3068   1.0000
   9.500   1.6010   0.01522   0.00888  -0.0958   0.3042   1.0000
   9.750   1.6242   0.01545   0.00918  -0.0951   0.3020   1.0000
  10.000   1.6466   0.01572   0.00949  -0.0943   0.2995   1.0000
  10.250   1.6681   0.01600   0.00982  -0.0934   0.2971   1.0000
  10.500   1.6886   0.01631   0.01016  -0.0923   0.2946   1.0000
  10.750   1.7078   0.01666   0.01052  -0.0910   0.2923   1.0000
  11.000   1.7239   0.01704   0.01091  -0.0893   0.2898   1.0000
  11.250   1.7418   0.01737   0.01130  -0.0878   0.2877   1.0000
  11.500   1.7593   0.01772   0.01172  -0.0862   0.2855   1.0000
  11.750   1.7755   0.01812   0.01217  -0.0846   0.2831   1.0000
  12.000   1.7905   0.01857   0.01266  -0.0829   0.2806   1.0000
  12.250   1.8030   0.01912   0.01323  -0.0809   0.2774   1.0000
  12.500   1.8141   0.01976   0.01390  -0.0789   0.2741   1.0000
  12.750   1.8280   0.02034   0.01455  -0.0774   0.2701   1.0000
  13.000   1.8380   0.02113   0.01539  -0.0756   0.2655   1.0000
  13.250   1.8440   0.02221   0.01648  -0.0737   0.2613   1.0000
  13.500   1.8542   0.02320   0.01754  -0.0724   0.2574   1.0000
  13.750   1.8628   0.02437   0.01879  -0.0712   0.2530   1.0000
  14.000   1.8672   0.02597   0.02042  -0.0700   0.2488   1.0000
  14.250   1.8709   0.02778   0.02229  -0.0691   0.2451   1.0000
  14.500   1.8782   0.02943   0.02403  -0.0686   0.2411   1.0000
  14.750   1.8802   0.03165   0.02632  -0.0682   0.2367   1.0000
  15.000   1.8750   0.03469   0.02939  -0.0679   0.2321   1.0000
  15.250   1.8748   0.03732   0.03212  -0.0677   0.2266   1.0000
  15.500   1.8663   0.04086   0.03573  -0.0676   0.2212   1.0000
  15.750   1.8530   0.04493   0.03986  -0.0676   0.2159   1.0000
  16.000   1.8402   0.04898   0.04400  -0.0676   0.2096   1.0000
  16.250   1.8173   0.05421   0.04928  -0.0677   0.2044   1.0000
  16.500   1.8038   0.05851   0.05366  -0.0679   0.1984   1.0000
  16.750   1.7809   0.06398   0.05918  -0.0683   0.1923   1.0000
  17.000   1.7598   0.06935   0.06461  -0.0688   0.1850   1.0000
  17.250   1.7338   0.07541   0.07070  -0.0695   0.1783   1.0000
  17.500   1.7153   0.08066   0.07600  -0.0702   0.1712   1.0000
  17.750   1.6900   0.08686   0.08222  -0.0711   0.1638   1.0000
  18.000   1.6655   0.09307   0.08844  -0.0722   0.1550   1.0000
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