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FX 63-147 AIRFOIL (fx63147-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 63-147 AIRFOIL (fx63147-il)
Reynolds number: 500,000
Max Cl/Cd: 84.5 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63147-il-500000-n5.txt
Download as CSV file: xf-fx63147-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-147 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.4131   0.05720   0.05478  -0.0822   0.9883   0.0064
  -9.500  -0.4234   0.05211   0.04954  -0.0865   0.9828   0.0063
  -9.250  -0.4371   0.04701   0.04425  -0.0883   0.9744   0.0063
  -8.750  -0.4622   0.03772   0.03443  -0.0860   0.9483   0.0062
  -8.500  -0.4655   0.03323   0.02955  -0.0841   0.9355   0.0063
  -8.250  -0.4573   0.02978   0.02574  -0.0832   0.9249   0.0062
  -8.000  -0.4380   0.02654   0.02209  -0.0838   0.9174   0.0063
  -7.750  -0.4138   0.02402   0.01919  -0.0846   0.9081   0.0063
  -7.500  -0.3796   0.02188   0.01665  -0.0870   0.9006   0.0065
  -7.250  -0.3424   0.01959   0.01409  -0.0902   0.8907   0.0069
  -7.000  -0.2971   0.01802   0.01227  -0.0944   0.8784   0.0070
  -6.750  -0.2462   0.01664   0.01059  -0.0996   0.8625   0.0068
  -6.500  -0.2076   0.01576   0.00949  -0.1022   0.8398   0.0067
  -6.250  -0.1791   0.01513   0.00867  -0.1027   0.8158   0.0066
  -6.000  -0.1548   0.01461   0.00798  -0.1023   0.7954   0.0066
  -5.750  -0.1321   0.01416   0.00740  -0.1015   0.7760   0.0066
  -5.500  -0.1102   0.01371   0.00683  -0.1006   0.7584   0.0066
  -5.250  -0.0883   0.01329   0.00631  -0.0998   0.7426   0.0066
  -5.000  -0.0659   0.01292   0.00584  -0.0990   0.7279   0.0065
  -4.750  -0.0433   0.01256   0.00537  -0.0983   0.7139   0.0066
  -4.500  -0.0202   0.01224   0.00496  -0.0976   0.7004   0.0066
  -4.250   0.0034   0.01196   0.00458  -0.0971   0.6873   0.0066
  -4.000   0.0277   0.01172   0.00425  -0.0966   0.6747   0.0066
  -3.750   0.0527   0.01151   0.00395  -0.0963   0.6627   0.0067
  -3.500   0.0779   0.01133   0.00368  -0.0959   0.6508   0.0068
  -3.250   0.1035   0.01119   0.00344  -0.0957   0.6390   0.0069
  -3.000   0.1295   0.01107   0.00324  -0.0955   0.6282   0.0071
  -2.750   0.1563   0.01096   0.00306  -0.0955   0.6191   0.0074
  -2.500   0.1831   0.01087   0.00291  -0.0954   0.6108   0.0077
  -2.250   0.2106   0.01076   0.00278  -0.0956   0.6029   0.0088
  -2.000   0.2381   0.01070   0.00267  -0.0957   0.5950   0.0174
  -1.750   0.2660   0.01062   0.00258  -0.0959   0.5869   0.0220
  -1.500   0.2939   0.01047   0.00249  -0.0963   0.5793   0.0607
  -1.250   0.3328   0.00913   0.00222  -0.1006   0.5720   0.3878
  -1.000   0.3767   0.00843   0.00212  -0.1052   0.5644   0.5772
  -0.750   0.4115   0.00826   0.00223  -0.1070   0.5565   0.6624
  -0.500   0.4392   0.00835   0.00246  -0.1069   0.5488   0.7227
  -0.250   0.4677   0.00847   0.00258  -0.1071   0.5414   0.7453
   0.000   0.4949   0.00864   0.00272  -0.1069   0.5348   0.7599
   0.250   0.5215   0.00877   0.00284  -0.1066   0.5291   0.7673
   0.500   0.5499   0.00888   0.00291  -0.1068   0.5231   0.7732
   0.750   0.5790   0.00899   0.00297  -0.1072   0.5177   0.7782
   1.000   0.6051   0.00910   0.00309  -0.1069   0.5122   0.7816
   1.250   0.6323   0.00921   0.00318  -0.1068   0.5064   0.7849
   1.500   0.6607   0.00933   0.00326  -0.1070   0.5005   0.7890
   1.750   0.6906   0.00943   0.00334  -0.1077   0.4933   0.7930
   2.000   0.7158   0.00958   0.00346  -0.1072   0.4868   0.7952
   2.250   0.7425   0.00968   0.00357  -0.1070   0.4806   0.7974
   2.500   0.7687   0.00983   0.00368  -0.1068   0.4726   0.7999
   2.750   0.7951   0.00999   0.00379  -0.1067   0.4572   0.8025
   3.000   0.8219   0.01018   0.00387  -0.1068   0.4331   0.8050
   3.250   0.8495   0.01041   0.00397  -0.1071   0.4123   0.8076
   3.500   0.8744   0.01060   0.00412  -0.1067   0.3990   0.8092
   3.750   0.8993   0.01078   0.00431  -0.1062   0.3881   0.8111
   4.000   0.9240   0.01099   0.00448  -0.1058   0.3761   0.8132
   4.250   0.9489   0.01123   0.00467  -0.1054   0.3611   0.8155
   4.500   0.9732   0.01155   0.00490  -0.1050   0.3391   0.8177
   4.750   0.9970   0.01198   0.00517  -0.1047   0.3074   0.8200
   5.000   1.0204   0.01251   0.00550  -0.1044   0.2712   0.8223
   5.250   1.0400   0.01317   0.00593  -0.1033   0.2281   0.8239
   5.500   1.0533   0.01412   0.00656  -0.1011   0.1686   0.8255
   5.750   1.0677   0.01496   0.00717  -0.0991   0.1229   0.8272
   6.000   1.0837   0.01562   0.00771  -0.0973   0.0928   0.8290
   6.250   1.1024   0.01611   0.00815  -0.0959   0.0769   0.8310
   6.500   1.1218   0.01662   0.00861  -0.0948   0.0610   0.8332
   6.750   1.1435   0.01706   0.00904  -0.0941   0.0539   0.8355
   7.000   1.1640   0.01765   0.00959  -0.0934   0.0359   0.8377
   7.250   1.1837   0.01813   0.01007  -0.0924   0.0329   0.8392
   7.500   1.2019   0.01860   0.01056  -0.0910   0.0299   0.8405
   7.750   1.2206   0.01904   0.01106  -0.0898   0.0268   0.8418
   8.000   1.2349   0.01972   0.01175  -0.0879   0.0163   0.8435
   8.250   1.2491   0.02044   0.01246  -0.0861   0.0143   0.8454
   8.500   1.2657   0.02105   0.01312  -0.0848   0.0130   0.8472
   8.750   1.2828   0.02167   0.01380  -0.0836   0.0126   0.8490
   9.000   1.2997   0.02233   0.01452  -0.0825   0.0122   0.8508
   9.250   1.3161   0.02305   0.01531  -0.0814   0.0119   0.8525
   9.500   1.3311   0.02385   0.01618  -0.0802   0.0116   0.8540
   9.750   1.3433   0.02469   0.01711  -0.0785   0.0112   0.8552
  10.000   1.3546   0.02564   0.01816  -0.0768   0.0109   0.8567
  10.250   1.3650   0.02670   0.01931  -0.0752   0.0106   0.8583
  10.500   1.3737   0.02798   0.02068  -0.0736   0.0100   0.8599
  10.750   1.3818   0.02941   0.02220  -0.0722   0.0095   0.8614
  11.000   1.3940   0.03056   0.02342  -0.0713   0.0093   0.8630
  11.250   1.4058   0.03181   0.02475  -0.0706   0.0089   0.8645
  11.500   1.4165   0.03323   0.02626  -0.0699   0.0083   0.8662
  11.750   1.4266   0.03480   0.02791  -0.0693   0.0075   0.8678
  12.000   1.4344   0.03648   0.02966  -0.0686   0.0067   0.8691
  12.250   1.4433   0.03808   0.03137  -0.0679   0.0059   0.8703
  12.500   1.4486   0.04010   0.03345  -0.0673   0.0031   0.8715
  12.750   1.4510   0.04249   0.03590  -0.0667   0.0029   0.8727
  13.000   1.4521   0.04508   0.03857  -0.0662   0.0027   0.8740
  13.250   1.4527   0.04782   0.04142  -0.0659   0.0025   0.8755
  13.500   1.4532   0.05067   0.04437  -0.0657   0.0024   0.8769
  13.750   1.4533   0.05366   0.04745  -0.0656   0.0023   0.8782
  14.000   1.4530   0.05676   0.05066  -0.0657   0.0022   0.8793
  14.250   1.4519   0.06002   0.05402  -0.0659   0.0021   0.8804
  14.500   1.4504   0.06338   0.05749  -0.0662   0.0021   0.8815
  14.750   1.4486   0.06692   0.06114  -0.0667   0.0020   0.8824
  15.000   1.4455   0.07048   0.06482  -0.0671   0.0020   0.8832
  15.250   1.4414   0.07423   0.06869  -0.0675   0.0020   0.8841
  15.500   1.4371   0.07804   0.07262  -0.0680   0.0019   0.8851
  15.750   1.4325   0.08198   0.07669  -0.0687   0.0019   0.8860
  16.000   1.4274   0.08603   0.08085  -0.0694   0.0019   0.8870
  16.250   1.4216   0.09025   0.08520  -0.0703   0.0018   0.8880
  16.500   1.4161   0.09450   0.08958  -0.0713   0.0018   0.8888
  16.750   1.4100   0.09891   0.09410  -0.0724   0.0018   0.8897
  17.000   1.4041   0.10338   0.09869  -0.0737   0.0017   0.8905
  17.250   1.3978   0.10790   0.10333  -0.0751   0.0017   0.8913
  17.500   1.3915   0.11251   0.10805  -0.0766   0.0017   0.8922
  17.750   1.3852   0.11723   0.11289  -0.0784   0.0017   0.8930
  18.000   1.3786   0.12204   0.11782  -0.0802   0.0017   0.8938
  18.250   1.3719   0.12698   0.12288  -0.0823   0.0016   0.8945
  18.500   1.3658   0.13173   0.12774  -0.0844   0.0016   0.8953
  18.750   1.3589   0.13686   0.13298  -0.0868   0.0016   0.8961
  19.000   1.3523   0.14190   0.13813  -0.0893   0.0016   0.8970
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