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FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 84-W-175 (fx84w175-il)
Reynolds number: 500,000
Max Cl/Cd: 108.63 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx84w175-il-500000.txt
Download as CSV file: xf-fx84w175-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.5795   0.08120   0.07828  -0.0961   0.9793   0.0274
 -15.750  -0.6334   0.06523   0.06194  -0.1108   0.9701   0.0273
 -15.500  -0.6543   0.05558   0.05198  -0.1217   0.9593   0.0274
 -15.250  -0.6671   0.04914   0.04524  -0.1287   0.9446   0.0275
 -15.000  -0.6835   0.04458   0.04042  -0.1315   0.9294   0.0276
 -14.750  -0.6939   0.04133   0.03701  -0.1321   0.9174   0.0279
 -14.500  -0.6995   0.03879   0.03432  -0.1321   0.9076   0.0280
 -14.250  -0.6991   0.03695   0.03241  -0.1318   0.8985   0.0284
 -14.000  -0.6989   0.03519   0.03054  -0.1313   0.8905   0.0286
 -13.750  -0.6976   0.03360   0.02886  -0.1306   0.8826   0.0289
 -13.500  -0.6959   0.03216   0.02729  -0.1296   0.8758   0.0293
 -13.250  -0.6938   0.03072   0.02573  -0.1286   0.8686   0.0296
 -13.000  -0.6907   0.02946   0.02433  -0.1271   0.8621   0.0299
 -12.750  -0.6864   0.02826   0.02300  -0.1256   0.8560   0.0304
 -12.500  -0.6812   0.02712   0.02172  -0.1240   0.8497   0.0308
 -12.250  -0.6754   0.02616   0.02060  -0.1220   0.8441   0.0313
 -12.000  -0.6684   0.02528   0.01957  -0.1200   0.8386   0.0316
 -11.750  -0.6609   0.02411   0.01828  -0.1179   0.8329   0.0322
 -11.500  -0.6497   0.02330   0.01742  -0.1161   0.8281   0.0327
 -11.250  -0.6353   0.02273   0.01679  -0.1146   0.8237   0.0334
 -11.000  -0.6185   0.02215   0.01618  -0.1135   0.8189   0.0341
 -10.750  -0.6009   0.02157   0.01552  -0.1125   0.8141   0.0349
 -10.500  -0.5826   0.02096   0.01477  -0.1114   0.8100   0.0356
 -10.250  -0.5631   0.02045   0.01411  -0.1105   0.8060   0.0364
 -10.000  -0.5445   0.01949   0.01312  -0.1096   0.8017   0.0372
  -9.750  -0.5241   0.01888   0.01251  -0.1089   0.7972   0.0382
  -9.500  -0.5025   0.01843   0.01200  -0.1082   0.7931   0.0392
  -9.250  -0.4801   0.01803   0.01151  -0.1076   0.7894   0.0404
  -9.000  -0.4568   0.01765   0.01104  -0.1071   0.7855   0.0415
  -8.750  -0.4358   0.01693   0.01031  -0.1064   0.7812   0.0429
  -8.500  -0.4128   0.01648   0.00984  -0.1059   0.7771   0.0442
  -8.250  -0.3890   0.01610   0.00940  -0.1054   0.7733   0.0456
  -8.000  -0.3643   0.01580   0.00901  -0.1051   0.7697   0.0472
  -7.750  -0.3416   0.01524   0.00845  -0.1045   0.7655   0.0491
  -7.500  -0.3170   0.01489   0.00810  -0.1042   0.7614   0.0511
  -7.250  -0.2915   0.01460   0.00775  -0.1040   0.7576   0.0533
  -7.000  -0.2672   0.01421   0.00728  -0.1036   0.7540   0.0556
  -6.750  -0.2423   0.01386   0.00697  -0.1033   0.7501   0.0582
  -6.500  -0.2161   0.01364   0.00671  -0.1031   0.7459   0.0613
  -6.250  -0.1914   0.01323   0.00630  -0.1028   0.7419   0.0648
  -6.000  -0.1649   0.01301   0.00604  -0.1027   0.7384   0.0687
  -5.750  -0.1392   0.01272   0.00573  -0.1025   0.7348   0.0730
  -5.500  -0.1129   0.01249   0.00551  -0.1024   0.7306   0.0781
  -5.250  -0.0867   0.01220   0.00524  -0.1022   0.7265   0.0840
  -5.000  -0.0597   0.01202   0.00502  -0.1022   0.7229   0.0903
  -4.750  -0.0331   0.01178   0.00478  -0.1021   0.7193   0.0986
  -4.500  -0.0065   0.01156   0.00460  -0.1021   0.7154   0.1076
  -4.250   0.0205   0.01137   0.00443  -0.1021   0.7112   0.1178
  -4.000   0.0476   0.01116   0.00425  -0.1021   0.7074   0.1308
  -3.750   0.0747   0.01096   0.00407  -0.1021   0.7038   0.1469
  -3.500   0.1016   0.01075   0.00394  -0.1021   0.7001   0.1675
  -3.250   0.1284   0.01053   0.00382  -0.1021   0.6959   0.1933
  -3.000   0.1552   0.01028   0.00369  -0.1022   0.6919   0.2260
  -2.750   0.1821   0.01003   0.00355  -0.1022   0.6882   0.2675
  -2.500   0.2088   0.00977   0.00344  -0.1023   0.6844   0.3238
  -2.250   0.2344   0.00939   0.00337  -0.1022   0.6804   0.3984
  -2.000   0.2600   0.00903   0.00330  -0.1021   0.6762   0.4835
  -1.750   0.2865   0.00879   0.00327  -0.1020   0.6723   0.5564
  -1.500   0.3140   0.00869   0.00327  -0.1020   0.6685   0.6092
  -1.250   0.3412   0.00864   0.00332  -0.1019   0.6646   0.6465
  -1.000   0.3689   0.00862   0.00336  -0.1019   0.6603   0.6752
  -0.750   0.3967   0.00861   0.00338  -0.1018   0.6563   0.6982
  -0.500   0.4250   0.00865   0.00340  -0.1018   0.6524   0.7175
  -0.250   0.4528   0.00871   0.00346  -0.1018   0.6484   0.7344
   0.000   0.4806   0.00874   0.00352  -0.1018   0.6442   0.7495
   0.250   0.5081   0.00878   0.00356  -0.1017   0.6400   0.7628
   0.500   0.5360   0.00884   0.00360  -0.1016   0.6360   0.7751
   0.750   0.5640   0.00893   0.00367  -0.1017   0.6320   0.7872
   1.000   0.5905   0.00897   0.00376  -0.1014   0.6277   0.7975
   1.250   0.6178   0.00903   0.00381  -0.1013   0.6233   0.8081
   1.500   0.6450   0.00912   0.00387  -0.1011   0.6193   0.8195
   1.750   0.6711   0.00921   0.00399  -0.1007   0.6151   0.8308
   2.000   0.6973   0.00929   0.00408  -0.1004   0.6106   0.8420
   2.250   0.7229   0.00933   0.00415  -0.0999   0.6061   0.8495
   2.500   0.7504   0.00943   0.00419  -0.0999   0.6019   0.8574
   2.750   0.7761   0.00949   0.00428  -0.0995   0.5976   0.8641
   3.000   0.8013   0.00954   0.00437  -0.0991   0.5928   0.8714
   3.250   0.8275   0.00961   0.00442  -0.0988   0.5883   0.8787
   3.500   0.8535   0.00972   0.00449  -0.0985   0.5839   0.8852
   3.750   0.8780   0.00978   0.00460  -0.0980   0.5792   0.8931
   4.000   0.9014   0.00982   0.00468  -0.0971   0.5744   0.9000
   4.250   0.9261   0.00990   0.00474  -0.0966   0.5698   0.9078
   4.500   0.9498   0.00999   0.00483  -0.0958   0.5653   0.9154
   4.750   0.9716   0.01005   0.00495  -0.0948   0.5604   0.9244
   5.000   0.9926   0.01009   0.00501  -0.0935   0.5555   0.9333
   5.250   1.0160   0.01021   0.00508  -0.0927   0.5508   0.9431
   5.500   1.0349   0.01024   0.00520  -0.0910   0.5457   0.9555
   5.750   1.0595   0.01030   0.00529  -0.0906   0.5399   0.9679
   6.000   1.0931   0.01047   0.00541  -0.0921   0.5342   0.9774
   6.250   1.1282   0.01061   0.00561  -0.0941   0.5282   0.9887
   6.500   1.1582   0.01075   0.00576  -0.0951   0.5220   1.0000
   6.750   1.1816   0.01094   0.00590  -0.0948   0.5163   1.0000
   7.000   1.2030   0.01108   0.00610  -0.0941   0.5102   1.0000
   7.250   1.2243   0.01127   0.00627  -0.0933   0.5042   1.0000
   7.500   1.2446   0.01149   0.00648  -0.0923   0.4984   1.0000
   7.750   1.2618   0.01170   0.00673  -0.0907   0.4918   1.0000
   8.000   1.2802   0.01197   0.00696  -0.0893   0.4854   1.0000
   8.250   1.2962   0.01224   0.00728  -0.0876   0.4783   1.0000
   8.500   1.3102   0.01260   0.00760  -0.0857   0.4696   1.0000
   8.750   1.3226   0.01298   0.00801  -0.0835   0.4594   1.0000
   9.000   1.3347   0.01346   0.00845  -0.0813   0.4498   1.0000
   9.250   1.3482   0.01392   0.00894  -0.0795   0.4403   1.0000
   9.500   1.3612   0.01445   0.00946  -0.0777   0.4316   1.0000
   9.750   1.3734   0.01503   0.01004  -0.0758   0.4219   1.0000
  10.000   1.3853   0.01566   0.01068  -0.0739   0.4121   1.0000
  10.250   1.3947   0.01643   0.01142  -0.0718   0.4021   1.0000
  10.500   1.4059   0.01717   0.01218  -0.0700   0.3907   1.0000
  10.750   1.4146   0.01805   0.01305  -0.0680   0.3789   1.0000
  11.000   1.4212   0.01908   0.01405  -0.0659   0.3665   1.0000
  11.250   1.4263   0.02024   0.01518  -0.0636   0.3533   1.0000
  11.500   1.4317   0.02144   0.01636  -0.0616   0.3390   1.0000
  11.750   1.4353   0.02281   0.01769  -0.0594   0.3239   1.0000
  12.000   1.4375   0.02432   0.01917  -0.0573   0.3083   1.0000
  12.250   1.4386   0.02600   0.02079  -0.0552   0.2923   1.0000
  12.500   1.4366   0.02797   0.02269  -0.0530   0.2746   1.0000
  12.750   1.4364   0.02990   0.02457  -0.0511   0.2583   1.0000
  13.000   1.4357   0.03195   0.02658  -0.0493   0.2417   1.0000
  13.250   1.4338   0.03418   0.02875  -0.0476   0.2250   1.0000
  13.500   1.4318   0.03651   0.03102  -0.0461   0.2090   1.0000
  13.750   1.4287   0.03903   0.03347  -0.0446   0.1921   1.0000
  14.000   1.4262   0.04157   0.03596  -0.0433   0.1769   1.0000
  14.250   1.4232   0.04423   0.03857  -0.0422   0.1614   1.0000
  14.500   1.4196   0.04705   0.04132  -0.0411   0.1459   1.0000
  14.750   1.4161   0.04995   0.04417  -0.0402   0.1319   1.0000
  15.000   1.4120   0.05298   0.04716  -0.0395   0.1185   1.0000
  15.250   1.4090   0.05600   0.05014  -0.0389   0.1066   1.0000
  15.500   1.4066   0.05903   0.05313  -0.0385   0.0962   1.0000
  15.750   1.4040   0.06214   0.05623  -0.0381   0.0875   1.0000
  16.250   1.4017   0.06828   0.06237  -0.0379   0.0736   1.0000
  16.500   1.4006   0.07145   0.06557  -0.0379   0.0683   1.0000
  16.750   1.3996   0.07465   0.06878  -0.0380   0.0634   1.0000
  17.000   1.3997   0.07778   0.07194  -0.0383   0.0592   1.0000
  17.250   1.3981   0.08117   0.07536  -0.0386   0.0555   1.0000
  17.500   1.3981   0.08442   0.07865  -0.0390   0.0522   1.0000
  17.750   1.3977   0.08778   0.08205  -0.0395   0.0492   1.0000
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