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FX 84-W-150 (fx84w150-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 84-W-150 (fx84w150-il)
Reynolds number: 500,000
Max Cl/Cd: 116.02 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx84w150-il-500000.txt
Download as CSV file: xf-fx84w150-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.5402   0.05156   0.04872  -0.1090   0.9470   0.0209
 -12.750  -0.5741   0.04355   0.04038  -0.1157   0.9247   0.0207
 -12.500  -0.6011   0.03903   0.03557  -0.1170   0.9083   0.0206
 -12.250  -0.6212   0.03593   0.03221  -0.1162   0.8955   0.0207
 -12.000  -0.6381   0.03337   0.02939  -0.1140   0.8842   0.0208
 -11.750  -0.6496   0.03152   0.02731  -0.1109   0.8746   0.0210
 -11.500  -0.6526   0.03004   0.02554  -0.1081   0.8670   0.0213
 -11.250  -0.6485   0.02851   0.02374  -0.1062   0.8601   0.0216
 -11.000  -0.6422   0.02645   0.02152  -0.1047   0.8538   0.0222
 -10.500  -0.6075   0.02495   0.01988  -0.1029   0.8431   0.0232
 -10.250  -0.5897   0.02406   0.01885  -0.1020   0.8377   0.0238
 -10.000  -0.5721   0.02301   0.01759  -0.1011   0.8330   0.0245
  -9.750  -0.5525   0.02202   0.01642  -0.1003   0.8279   0.0251
  -9.500  -0.5314   0.02125   0.01544  -0.0996   0.8228   0.0257
  -9.250  -0.5128   0.01976   0.01382  -0.0989   0.8183   0.0266
  -9.000  -0.4898   0.01919   0.01321  -0.0985   0.8139   0.0274
  -8.750  -0.4657   0.01873   0.01269  -0.0982   0.8089   0.0284
  -8.500  -0.4416   0.01818   0.01203  -0.0978   0.8044   0.0296
  -8.250  -0.4169   0.01775   0.01141  -0.0973   0.8003   0.0305
  -8.000  -0.3947   0.01664   0.01027  -0.0969   0.7957   0.0318
  -7.750  -0.3696   0.01619   0.00981  -0.0967   0.7910   0.0331
  -7.500  -0.3442   0.01578   0.00931  -0.0964   0.7868   0.0346
  -7.250  -0.3179   0.01551   0.00890  -0.0962   0.7830   0.0360
  -7.000  -0.2941   0.01471   0.00812  -0.0958   0.7783   0.0380
  -6.750  -0.2679   0.01438   0.00776  -0.0957   0.7736   0.0399
  -6.500  -0.2414   0.01406   0.00735  -0.0955   0.7696   0.0418
  -6.250  -0.2163   0.01352   0.00675  -0.0952   0.7656   0.0440
  -6.000  -0.1898   0.01320   0.00645  -0.0952   0.7611   0.0466
  -5.750  -0.1627   0.01296   0.00615  -0.0951   0.7565   0.0493
  -5.500  -0.1370   0.01250   0.00563  -0.0949   0.7524   0.0523
  -5.250  -0.1101   0.01225   0.00538  -0.0948   0.7482   0.0558
  -5.000  -0.0824   0.01208   0.00516  -0.0949   0.7434   0.0590
  -4.750  -0.0564   0.01164   0.00474  -0.0947   0.7389   0.0643
  -4.500  -0.0287   0.01150   0.00452  -0.0947   0.7349   0.0691
  -4.250  -0.0020   0.01116   0.00423  -0.0946   0.7304   0.0765
  -4.000   0.0253   0.01091   0.00399  -0.0947   0.7258   0.0848
  -3.750   0.0529   0.01072   0.00378  -0.0947   0.7216   0.0949
  -3.500   0.0804   0.01052   0.00359  -0.0947   0.7176   0.1086
  -3.250   0.1077   0.01027   0.00343  -0.0948   0.7129   0.1275
  -3.000   0.1352   0.01005   0.00329  -0.0949   0.7085   0.1520
  -2.750   0.1626   0.00983   0.00314  -0.0950   0.7045   0.1845
  -2.500   0.1898   0.00958   0.00304  -0.0951   0.7002   0.2295
  -2.250   0.2166   0.00924   0.00294  -0.0952   0.6955   0.2948
  -2.000   0.2428   0.00880   0.00283  -0.0952   0.6912   0.3956
  -1.750   0.2685   0.00835   0.00276  -0.0951   0.6872   0.5237
  -1.500   0.2944   0.00807   0.00280  -0.0949   0.6826   0.6213
  -1.250   0.3212   0.00794   0.00283  -0.0946   0.6779   0.6811
  -1.000   0.3485   0.00790   0.00285  -0.0944   0.6737   0.7211
  -0.750   0.3761   0.00792   0.00289  -0.0942   0.6695   0.7503
  -0.500   0.4033   0.00792   0.00294  -0.0940   0.6646   0.7736
  -0.250   0.4308   0.00794   0.00296  -0.0938   0.6598   0.7931
   0.000   0.4583   0.00800   0.00298  -0.0936   0.6555   0.8099
   0.250   0.4852   0.00803   0.00304  -0.0934   0.6505   0.8246
   0.500   0.5120   0.00806   0.00309  -0.0931   0.6456   0.8387
   0.750   0.5388   0.00812   0.00312  -0.0927   0.6412   0.8521
   1.000   0.5656   0.00819   0.00318  -0.0925   0.6368   0.8651
   1.250   0.5908   0.00823   0.00325  -0.0918   0.6318   0.8793
   1.500   0.6144   0.00828   0.00332  -0.0907   0.6270   0.8957
   1.750   0.6378   0.00837   0.00337  -0.0895   0.6227   0.9093
   2.000   0.6617   0.00838   0.00343  -0.0886   0.6180   0.9192
   2.250   0.6863   0.00841   0.00347  -0.0879   0.6131   0.9296
   2.500   0.7105   0.00846   0.00348  -0.0871   0.6085   0.9393
   2.750   0.7351   0.00849   0.00353  -0.0864   0.6036   0.9491
   3.000   0.7611   0.00851   0.00357  -0.0861   0.5984   0.9595
   3.250   0.7911   0.00857   0.00359  -0.0866   0.5933   0.9686
   3.500   0.8254   0.00864   0.00367  -0.0881   0.5879   0.9757
   3.750   0.8602   0.00870   0.00374  -0.0898   0.5820   0.9832
   4.000   0.8987   0.00881   0.00380  -0.0923   0.5766   0.9877
   4.250   0.9360   0.00890   0.00392  -0.0946   0.5707   0.9933
   4.500   0.9743   0.00899   0.00401  -0.0971   0.5649   0.9988
   4.750   0.9960   0.00913   0.00410  -0.0963   0.5597   1.0000
   5.000   1.0160   0.00920   0.00422  -0.0951   0.5533   1.0000
   5.250   1.0402   0.00933   0.00432  -0.0947   0.5466   1.0000
   5.500   1.0653   0.00947   0.00447  -0.0944   0.5399   1.0000
   5.750   1.0907   0.00960   0.00461  -0.0942   0.5330   1.0000
   6.000   1.1164   0.00979   0.00477  -0.0941   0.5271   1.0000
   6.250   1.1414   0.00992   0.00495  -0.0939   0.5199   1.0000
   6.500   1.1664   0.01012   0.00511  -0.0936   0.5133   1.0000
   6.750   1.1904   0.01026   0.00532  -0.0931   0.5049   1.0000
   7.000   1.2118   0.01045   0.00549  -0.0922   0.4921   1.0000
   7.250   1.2320   0.01068   0.00568  -0.0910   0.4779   1.0000
   7.500   1.2517   0.01094   0.00592  -0.0898   0.4654   1.0000
   7.750   1.2710   0.01120   0.00618  -0.0886   0.4525   1.0000
   8.000   1.2896   0.01149   0.00646  -0.0872   0.4401   1.0000
   8.250   1.3048   0.01180   0.00677  -0.0852   0.4279   1.0000
   8.500   1.3179   0.01219   0.00714  -0.0829   0.4153   1.0000
   8.750   1.3298   0.01264   0.00756  -0.0805   0.4009   1.0000
   9.000   1.3410   0.01317   0.00806  -0.0780   0.3851   1.0000
   9.250   1.3504   0.01380   0.00866  -0.0755   0.3667   1.0000
   9.500   1.3574   0.01460   0.00939  -0.0728   0.3467   1.0000
   9.750   1.3625   0.01555   0.01026  -0.0700   0.3258   1.0000
  10.000   1.3663   0.01664   0.01126  -0.0672   0.3005   1.0000
  10.250   1.3668   0.01800   0.01249  -0.0641   0.2741   1.0000
  10.500   1.3657   0.01954   0.01390  -0.0612   0.2471   1.0000
  10.750   1.3635   0.02126   0.01547  -0.0583   0.2192   1.0000
  11.000   1.3608   0.02312   0.01720  -0.0557   0.1932   1.0000
  11.250   1.3587   0.02504   0.01899  -0.0532   0.1676   1.0000
  11.500   1.3551   0.02716   0.02098  -0.0509   0.1420   1.0000
  11.750   1.3503   0.02945   0.02314  -0.0487   0.1176   1.0000
  12.000   1.3463   0.03182   0.02539  -0.0467   0.0972   1.0000
  12.250   1.3452   0.03406   0.02756  -0.0452   0.0822   1.0000
  12.500   1.3452   0.03632   0.02977  -0.0438   0.0703   1.0000
  12.750   1.3457   0.03861   0.03203  -0.0426   0.0614   1.0000
  13.000   1.3481   0.04082   0.03424  -0.0417   0.0549   1.0000
  13.250   1.3511   0.04302   0.03647  -0.0408   0.0498   1.0000
  13.500   1.3525   0.04546   0.03891  -0.0401   0.0460   1.0000
  13.750   1.3554   0.04783   0.04134  -0.0395   0.0429   1.0000
  14.000   1.3595   0.05011   0.04367  -0.0390   0.0404   1.0000
  14.250   1.3588   0.05296   0.04654  -0.0385   0.0381   1.0000
  14.500   1.3621   0.05546   0.04912  -0.0382   0.0362   1.0000
  14.750   1.3669   0.05785   0.05158  -0.0380   0.0345   1.0000
  15.000   1.3690   0.06058   0.05436  -0.0379   0.0331   1.0000
  15.250   1.3662   0.06395   0.05778  -0.0379   0.0317   1.0000
  15.500   1.3669   0.06698   0.06089  -0.0379   0.0306   1.0000
  15.750   1.3710   0.06963   0.06362  -0.0381   0.0296   1.0000
  16.000   1.3742   0.07245   0.06652  -0.0383   0.0285   1.0000
  16.250   1.3757   0.07550   0.06964  -0.0387   0.0277   1.0000
  16.500   1.3744   0.07897   0.07314  -0.0391   0.0267   1.0000
  16.750   1.3699   0.08292   0.07715  -0.0397   0.0258   1.0000
  17.000   1.3738   0.08582   0.08016  -0.0402   0.0251   1.0000
  17.250   1.3765   0.08891   0.08334  -0.0409   0.0244   1.0000
  17.500   1.3779   0.09220   0.08671  -0.0416   0.0237   1.0000
  17.750   1.3798   0.09547   0.09004  -0.0424   0.0230   1.0000
  18.000   1.3796   0.09905   0.09368  -0.0434   0.0225   1.0000
  18.250   1.3781   0.10276   0.09742  -0.0444   0.0219   1.0000
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