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FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX 84-W-175 (fx84w175-il)
Reynolds number: 200,000
Max Cl/Cd: 68.36 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx84w175-il-200000.txt
Download as CSV file: xf-fx84w175-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-175                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.1149   0.10670   0.10287  -0.1074   0.9455   0.0818
 -12.000  -0.3351   0.05812   0.05390  -0.1391   0.9326   0.0543
 -11.750  -0.3607   0.05325   0.04887  -0.1410   0.9222   0.0540
 -11.500  -0.3865   0.04953   0.04495  -0.1409   0.9119   0.0538
 -11.250  -0.4130   0.04643   0.04165  -0.1392   0.9007   0.0536
 -11.000  -0.4393   0.04394   0.03889  -0.1357   0.8915   0.0536
 -10.750  -0.4608   0.04182   0.03649  -0.1317   0.8822   0.0537
 -10.500  -0.4756   0.03963   0.03389  -0.1279   0.8758   0.0541
 -10.250  -0.4807   0.03737   0.03131  -0.1253   0.8678   0.0548
 -10.000  -0.4657   0.03593   0.02985  -0.1243   0.8630   0.0559
  -9.750  -0.4485   0.03503   0.02891  -0.1231   0.8595   0.0571
  -9.500  -0.4379   0.03377   0.02750  -0.1217   0.8526   0.0582
  -9.250  -0.4271   0.03220   0.02564  -0.1200   0.8472   0.0593
  -9.000  -0.4143   0.03066   0.02374  -0.1181   0.8433   0.0607
  -8.750  -0.4017   0.02963   0.02235  -0.1164   0.8377   0.0621
  -8.500  -0.3807   0.02836   0.02115  -0.1160   0.8326   0.0640
  -8.250  -0.3593   0.02758   0.02028  -0.1152   0.8285   0.0659
  -8.000  -0.3374   0.02663   0.01914  -0.1143   0.8253   0.0681
  -7.750  -0.3181   0.02599   0.01825  -0.1132   0.8201   0.0703
  -7.500  -0.2961   0.02493   0.01725  -0.1127   0.8149   0.0729
  -7.250  -0.2724   0.02435   0.01662  -0.1122   0.8110   0.0759
  -7.000  -0.2478   0.02366   0.01575  -0.1116   0.8079   0.0791
  -6.750  -0.2248   0.02283   0.01489  -0.1110   0.8039   0.0824
  -6.500  -0.2033   0.02249   0.01460  -0.1103   0.7980   0.0863
  -6.250  -0.1788   0.02207   0.01402  -0.1097   0.7940   0.0908
  -6.000  -0.1537   0.02122   0.01324  -0.1093   0.7910   0.0959
  -5.750  -0.1273   0.02079   0.01270  -0.1089   0.7884   0.1020
  -5.500  -0.1087   0.02042   0.01244  -0.1079   0.7816   0.1078
  -5.250  -0.0843   0.02011   0.01208  -0.1074   0.7774   0.1154
  -5.000  -0.0593   0.01950   0.01152  -0.1069   0.7742   0.1241
  -4.750  -0.0329   0.01898   0.01097  -0.1066   0.7716   0.1348
  -4.500  -0.0125   0.01892   0.01093  -0.1057   0.7656   0.1460
  -4.250   0.0099   0.01856   0.01067  -0.1050   0.7610   0.1602
  -4.000   0.0356   0.01812   0.01026  -0.1047   0.7576   0.1786
  -3.750   0.0618   0.01757   0.00982  -0.1045   0.7549   0.2028
  -3.500   0.0833   0.01735   0.00973  -0.1037   0.7501   0.2336
  -3.250   0.1035   0.01703   0.00966  -0.1028   0.7447   0.2764
  -3.000   0.1270   0.01645   0.00939  -0.1023   0.7411   0.3486
  -2.750   0.1511   0.01576   0.00913  -0.1018   0.7383   0.4586
  -2.500   0.1746   0.01541   0.00915  -0.1008   0.7351   0.5621
  -2.250   0.1922   0.01558   0.00956  -0.0990   0.7286   0.6247
  -2.000   0.2176   0.01558   0.00963  -0.0981   0.7248   0.6722
  -1.750   0.2456   0.01554   0.00959  -0.0976   0.7219   0.7068
  -1.500   0.2748   0.01552   0.00954  -0.0972   0.7194   0.7344
  -1.250   0.2918   0.01593   0.01001  -0.0952   0.7130   0.7556
  -1.000   0.3156   0.01608   0.01015  -0.0940   0.7086   0.7752
  -0.750   0.3427   0.01609   0.01011  -0.0932   0.7054   0.7931
  -0.500   0.3710   0.01607   0.01002  -0.0926   0.7029   0.8096
  -0.250   0.3884   0.01641   0.01039  -0.0906   0.6973   0.8252
   0.000   0.4083   0.01659   0.01058  -0.0888   0.6923   0.8396
   0.250   0.4329   0.01658   0.01053  -0.0874   0.6889   0.8525
   0.500   0.4599   0.01650   0.01038  -0.0866   0.6862   0.8656
   0.750   0.4765   0.01673   0.01063  -0.0843   0.6813   0.8799
   1.000   0.4909   0.01692   0.01084  -0.0815   0.6758   0.8954
   1.250   0.5128   0.01686   0.01075  -0.0796   0.6723   0.9112
   1.500   0.5429   0.01672   0.01054  -0.0792   0.6695   0.9237
   1.750   0.5699   0.01683   0.01064  -0.0791   0.6653   0.9341
   2.000   0.5931   0.01703   0.01086  -0.0786   0.6594   0.9451
   2.250   0.6330   0.01695   0.01073  -0.0809   0.6557   0.9521
   2.500   0.6759   0.01681   0.01051  -0.0838   0.6528   0.9581
   2.750   0.7192   0.01691   0.01057  -0.0871   0.6488   0.9630
   3.000   0.7527   0.01714   0.01085  -0.0890   0.6427   0.9707
   3.250   0.8004   0.01707   0.01073  -0.0931   0.6387   0.9740
   3.500   0.8472   0.01693   0.01051  -0.0969   0.6356   0.9781
   3.750   0.8851   0.01712   0.01073  -0.0996   0.6303   0.9841
   4.000   0.9249   0.01724   0.01088  -0.1026   0.6247   0.9900
   4.250   0.9680   0.01713   0.01074  -0.1060   0.6207   0.9947
   4.500   1.0146   0.01697   0.01049  -0.1098   0.6174   0.9983
   4.750   1.0155   0.01742   0.01107  -0.1059   0.6106   1.0000
   5.000   1.0255   0.01750   0.01114  -0.1031   0.6058   1.0000
   5.250   1.0491   0.01740   0.01098  -0.1024   0.6021   1.0000
   5.500   1.0494   0.01770   0.01133  -0.0980   0.5968   1.0000
   5.750   1.0568   0.01795   0.01161  -0.0948   0.5910   1.0000
   6.000   1.0862   0.01791   0.01152  -0.0952   0.5867   1.0000
   6.250   1.1158   0.01798   0.01156  -0.0957   0.5824   1.0000
   6.500   1.1260   0.01840   0.01207  -0.0932   0.5753   1.0000
   6.750   1.1567   0.01836   0.01200  -0.0939   0.5703   1.0000
   7.000   1.1871   0.01842   0.01204  -0.0945   0.5655   1.0000
   7.250   1.1983   0.01883   0.01254  -0.0921   0.5583   1.0000
   7.500   1.2305   0.01878   0.01245  -0.0929   0.5531   1.0000
   7.750   1.2523   0.01902   0.01272  -0.0922   0.5471   1.0000
   8.000   1.2683   0.01930   0.01307  -0.0905   0.5402   1.0000
   8.250   1.3042   0.01921   0.01292  -0.0919   0.5350   1.0000
   8.500   1.3118   0.01969   0.01351  -0.0890   0.5277   1.0000
   8.750   1.3360   0.01977   0.01361  -0.0885   0.5210   1.0000
   9.000   1.3586   0.01996   0.01380  -0.0879   0.5145   1.0000
   9.250   1.3656   0.02027   0.01417  -0.0846   0.5064   1.0000
   9.500   1.3871   0.02029   0.01417  -0.0836   0.4982   1.0000
   9.750   1.3894   0.02065   0.01458  -0.0797   0.4887   1.0000
  10.000   1.3986   0.02099   0.01493  -0.0771   0.4792   1.0000
  10.250   1.4116   0.02126   0.01519  -0.0750   0.4698   1.0000
  10.500   1.4126   0.02200   0.01601  -0.0716   0.4601   1.0000
  10.750   1.4324   0.02221   0.01616  -0.0706   0.4508   1.0000
  11.000   1.4269   0.02330   0.01736  -0.0666   0.4406   1.0000
  11.250   1.4361   0.02397   0.01804  -0.0646   0.4306   1.0000
  11.500   1.4442   0.02470   0.01876  -0.0625   0.4199   1.0000
  11.750   1.4427   0.02596   0.02011  -0.0595   0.4086   1.0000
  12.000   1.4472   0.02702   0.02118  -0.0573   0.3970   1.0000
  12.250   1.4521   0.02810   0.02223  -0.0552   0.3847   1.0000
  12.500   1.4522   0.02954   0.02370  -0.0529   0.3717   1.0000
  12.750   1.4504   0.03119   0.02538  -0.0506   0.3579   1.0000
  13.000   1.4494   0.03293   0.02713  -0.0485   0.3439   1.0000
  13.250   1.4478   0.03481   0.02900  -0.0466   0.3292   1.0000
  13.500   1.4455   0.03686   0.03104  -0.0448   0.3139   1.0000
  13.750   1.4420   0.03913   0.03328  -0.0431   0.2979   1.0000
  14.000   1.4373   0.04161   0.03573  -0.0415   0.2813   1.0000
  14.250   1.4317   0.04430   0.03838  -0.0400   0.2644   1.0000
  14.500   1.4248   0.04724   0.04126  -0.0387   0.2472   1.0000
  14.750   1.4171   0.05038   0.04434  -0.0376   0.2303   1.0000
  15.000   1.4081   0.05379   0.04769  -0.0367   0.2133   1.0000
  15.250   1.3995   0.05732   0.05117  -0.0359   0.1964   1.0000
  15.500   1.3905   0.06101   0.05482  -0.0354   0.1794   1.0000
  15.750   1.3807   0.06493   0.05868  -0.0350   0.1630   1.0000
  16.000   1.3708   0.06899   0.06268  -0.0349   0.1476   1.0000
  16.250   1.3612   0.07312   0.06675  -0.0349   0.1341   1.0000
  16.500   1.3527   0.07723   0.07081  -0.0350   0.1223   1.0000
  16.750   1.3447   0.08135   0.07487  -0.0353   0.1126   1.0000
  17.000   1.3388   0.08529   0.07879  -0.0357   0.1037   1.0000
  17.250   1.3356   0.08895   0.08248  -0.0361   0.0960   1.0000
  17.500   1.3307   0.09279   0.08625  -0.0367   0.0898   1.0000
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