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FX 84-W-150 (fx84w150-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX 84-W-150 (fx84w150-il)
Reynolds number: 200,000
Max Cl/Cd: 77.34 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx84w150-il-200000.txt
Download as CSV file: xf-fx84w150-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-150                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.1975   0.10660   0.10309  -0.0782   0.9734   0.0653
 -11.000  -0.2095   0.09966   0.09617  -0.0909   0.9662   0.0690
 -10.750  -0.1997   0.09373   0.09024  -0.0946   0.9614   0.0700
 -10.500  -0.1655   0.09228   0.08873  -0.0933   0.9584   0.0722
 -10.250  -0.1513   0.08922   0.08565  -0.0955   0.9506   0.0748
 -10.000  -0.1485   0.08452   0.08093  -0.1009   0.9426   0.0787
  -9.750  -0.2082   0.07465   0.07106  -0.1161   0.9216   0.0808
  -9.500  -0.1939   0.07089   0.06734  -0.1138   0.9165   0.0820
  -9.250  -0.3361   0.04755   0.04322  -0.1198   0.8944   0.0496
  -9.000  -0.3427   0.04412   0.03959  -0.1182   0.8859   0.0490
  -8.750  -0.3495   0.04041   0.03553  -0.1162   0.8789   0.0486
  -8.500  -0.3519   0.03681   0.03151  -0.1143   0.8709   0.0485
  -8.250  -0.3480   0.03371   0.02790  -0.1121   0.8658   0.0490
  -8.000  -0.3386   0.03191   0.02555  -0.1103   0.8583   0.0502
  -7.750  -0.3230   0.02941   0.02292  -0.1094   0.8531   0.0518
  -7.500  -0.3022   0.02822   0.02161  -0.1085   0.8494   0.0534
  -7.250  -0.2827   0.02699   0.02018  -0.1077   0.8429   0.0551
  -7.000  -0.2618   0.02574   0.01862  -0.1067   0.8376   0.0574
  -6.750  -0.2398   0.02433   0.01689  -0.1058   0.8339   0.0600
  -6.500  -0.2166   0.02348   0.01604  -0.1054   0.8290   0.0627
  -6.250  -0.1930   0.02276   0.01521  -0.1048   0.8233   0.0656
  -6.000  -0.1678   0.02218   0.01438  -0.1041   0.8191   0.0691
  -5.750  -0.1429   0.02095   0.01314  -0.1037   0.8160   0.0730
  -5.500  -0.1193   0.02052   0.01269  -0.1033   0.8096   0.0770
  -5.250  -0.0939   0.01991   0.01194  -0.1027   0.8049   0.0818
  -5.000  -0.0684   0.01915   0.01122  -0.1023   0.8014   0.0873
  -4.750  -0.0428   0.01884   0.01079  -0.1019   0.7969   0.0935
  -4.500  -0.0197   0.01822   0.01028  -0.1013   0.7910   0.1009
  -4.250   0.0060   0.01769   0.00970  -0.1008   0.7869   0.1101
  -4.000   0.0327   0.01724   0.00922  -0.1005   0.7837   0.1219
  -3.750   0.0555   0.01691   0.00898  -0.0999   0.7775   0.1361
  -3.500   0.0803   0.01647   0.00862  -0.0995   0.7726   0.1560
  -3.250   0.1063   0.01597   0.00821  -0.0992   0.7691   0.1853
  -3.000   0.1310   0.01548   0.00793  -0.0989   0.7653   0.2306
  -2.750   0.1525   0.01501   0.00786  -0.0983   0.7589   0.3103
  -2.500   0.1740   0.01418   0.00768  -0.0974   0.7547   0.4705
  -2.250   0.1963   0.01365   0.00768  -0.0959   0.7516   0.6275
  -2.000   0.2172   0.01371   0.00798  -0.0942   0.7460   0.7048
  -1.750   0.2401   0.01378   0.00811  -0.0927   0.7409   0.7531
  -1.500   0.2650   0.01378   0.00810  -0.0914   0.7372   0.7887
  -1.250   0.2905   0.01381   0.00806  -0.0901   0.7344   0.8172
  -1.000   0.3086   0.01409   0.00840  -0.0880   0.7276   0.8403
  -0.750   0.3312   0.01414   0.00840  -0.0863   0.7232   0.8621
  -0.500   0.3550   0.01412   0.00830  -0.0847   0.7199   0.8814
  -0.250   0.3746   0.01427   0.00845  -0.0826   0.7147   0.8991
   0.000   0.3963   0.01436   0.00852  -0.0809   0.7094   0.9165
   0.250   0.4259   0.01430   0.00840  -0.0806   0.7056   0.9328
   0.500   0.4656   0.01425   0.00822  -0.0823   0.7027   0.9475
   0.750   0.5157   0.01446   0.00843  -0.0867   0.6965   0.9627
   1.000   0.5703   0.01443   0.00833  -0.0920   0.6919   0.9723
   1.250   0.6195   0.01428   0.00807  -0.0963   0.6882   0.9779
   1.500   0.6616   0.01431   0.00807  -0.0996   0.6832   0.9849
   1.750   0.7041   0.01431   0.00806  -0.1030   0.6775   0.9914
   2.000   0.7475   0.01419   0.00787  -0.1065   0.6733   0.9971
   2.250   0.7792   0.01418   0.00780  -0.1077   0.6690   1.0000
   2.500   0.7927   0.01438   0.00804  -0.1057   0.6625   1.0000
   2.750   0.8120   0.01440   0.00804  -0.1044   0.6580   1.0000
   3.000   0.8347   0.01440   0.00796  -0.1036   0.6544   1.0000
   3.250   0.8435   0.01470   0.00834  -0.1007   0.6473   1.0000
   3.500   0.8625   0.01474   0.00835  -0.0993   0.6425   1.0000
   3.750   0.8878   0.01474   0.00827  -0.0988   0.6389   1.0000
   4.000   0.8975   0.01508   0.00868  -0.0960   0.6316   1.0000
   4.250   0.9215   0.01512   0.00870  -0.0954   0.6265   1.0000
   4.500   0.9498   0.01517   0.00869  -0.0955   0.6223   1.0000
   4.750   0.9678   0.01547   0.00908  -0.0942   0.6150   1.0000
   5.000   0.9958   0.01552   0.00909  -0.0943   0.6100   1.0000
   5.250   1.0222   0.01568   0.00926  -0.0942   0.6048   1.0000
   5.500   1.0441   0.01593   0.00957  -0.0934   0.5980   1.0000
   5.750   1.0739   0.01596   0.00957  -0.0938   0.5931   1.0000
   6.000   1.0962   0.01621   0.00989  -0.0931   0.5861   1.0000
   6.250   1.1224   0.01626   0.00995  -0.0929   0.5792   1.0000
   6.500   1.1487   0.01637   0.01007  -0.0927   0.5726   1.0000
   6.750   1.1715   0.01656   0.01033  -0.0920   0.5651   1.0000
   7.000   1.2029   0.01659   0.01031  -0.0927   0.5597   1.0000
   7.250   1.2202   0.01690   0.01076  -0.0911   0.5511   1.0000
   7.500   1.2507   0.01692   0.01074  -0.0916   0.5447   1.0000
   7.750   1.2675   0.01710   0.01103  -0.0899   0.5340   1.0000
   8.000   1.2872   0.01707   0.01101  -0.0884   0.5213   1.0000
   8.250   1.3063   0.01708   0.01101  -0.0869   0.5083   1.0000
   8.500   1.3271   0.01716   0.01108  -0.0857   0.4966   1.0000
   8.750   1.3396   0.01742   0.01142  -0.0833   0.4841   1.0000
   9.000   1.3520   0.01771   0.01176  -0.0808   0.4712   1.0000
   9.250   1.3625   0.01801   0.01209  -0.0781   0.4585   1.0000
   9.500   1.3713   0.01840   0.01250  -0.0751   0.4456   1.0000
   9.750   1.3789   0.01889   0.01299  -0.0722   0.4317   1.0000
  10.000   1.3849   0.01951   0.01362  -0.0692   0.4169   1.0000
  10.250   1.3892   0.02027   0.01440  -0.0662   0.4008   1.0000
  10.500   1.3919   0.02119   0.01532  -0.0631   0.3829   1.0000
  10.750   1.3930   0.02230   0.01640  -0.0602   0.3630   1.0000
  11.000   1.3920   0.02363   0.01767  -0.0572   0.3420   1.0000
  11.250   1.3897   0.02519   0.01919  -0.0543   0.3177   1.0000
  11.500   1.3835   0.02711   0.02101  -0.0514   0.2911   1.0000
  11.750   1.3747   0.02939   0.02315  -0.0486   0.2637   1.0000
  12.000   1.3640   0.03199   0.02561  -0.0459   0.2344   1.0000
  12.250   1.3507   0.03498   0.02843  -0.0435   0.2047   1.0000
  12.500   1.3372   0.03826   0.03155  -0.0415   0.1753   1.0000
  12.750   1.3231   0.04183   0.03494  -0.0397   0.1463   1.0000
  13.000   1.3096   0.04557   0.03852  -0.0383   0.1228   1.0000
  13.250   1.2992   0.04919   0.04203  -0.0372   0.1054   1.0000
  13.500   1.2910   0.05274   0.04552  -0.0364   0.0935   1.0000
  13.750   1.2834   0.05636   0.04908  -0.0358   0.0846   1.0000
  14.000   1.2821   0.05937   0.05214  -0.0354   0.0773   1.0000
  14.250   1.2766   0.06289   0.05560  -0.0350   0.0721   1.0000
  14.500   1.2794   0.06558   0.05838  -0.0349   0.0672   1.0000
  14.750   1.2778   0.06877   0.06153  -0.0347   0.0632   1.0000
  15.000   1.2813   0.07137   0.06420  -0.0345   0.0598   1.0000
  15.250   1.2855   0.07397   0.06686  -0.0345   0.0567   1.0000
  15.500   1.2889   0.07657   0.06944  -0.0343   0.0539   1.0000
  15.750   1.2958   0.07873   0.07165  -0.0340   0.0514   1.0000
  16.000   1.3018   0.08119   0.07421  -0.0341   0.0490   1.0000
  16.250   1.3089   0.08343   0.07649  -0.0341   0.0471   1.0000
  16.500   1.3214   0.08464   0.07759  -0.0334   0.0447   1.0000
  16.750   1.3287   0.08701   0.08011  -0.0334   0.0433   1.0000
  17.000   1.3342   0.08961   0.08286  -0.0337   0.0416   1.0000
  17.250   1.3413   0.09197   0.08529  -0.0340   0.0401   1.0000
  17.500   1.3509   0.09388   0.08721  -0.0340   0.0387   1.0000
  17.750   1.3687   0.09461   0.08792  -0.0330   0.0371   1.0000
  18.000   1.3701   0.09792   0.09145  -0.0337   0.0363   1.0000
  18.250   1.3714   0.10124   0.09497  -0.0345   0.0354   1.0000
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