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FX 84-W-150 (fx84w150-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-150 (fx84w150-il)
Reynolds number: 500,000
Max Cl/Cd: 110.99 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w150-il-500000-n5.txt
Download as CSV file: xf-fx84w150-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.6528   0.07215   0.06918  -0.0844   0.9575   0.0138
 -14.750  -0.7183   0.05346   0.05010  -0.1004   0.9359   0.0135
 -14.250  -0.7660   0.03910   0.03516  -0.1114   0.8983   0.0136
 -14.000  -0.7774   0.03564   0.03151  -0.1126   0.8856   0.0136
 -13.750  -0.7846   0.03303   0.02871  -0.1126   0.8749   0.0138
 -13.500  -0.7904   0.03088   0.02638  -0.1118   0.8651   0.0139
 -13.250  -0.7911   0.02921   0.02455  -0.1107   0.8564   0.0141
 -12.750  -0.7887   0.02656   0.02157  -0.1068   0.8415   0.0145
 -12.500  -0.7845   0.02558   0.02042  -0.1044   0.8348   0.0147
 -12.250  -0.7756   0.02454   0.01926  -0.1028   0.8289   0.0149
 -12.000  -0.7630   0.02359   0.01822  -0.1015   0.8230   0.0152
 -11.750  -0.7469   0.02283   0.01737  -0.1005   0.8179   0.0156
 -11.500  -0.7286   0.02216   0.01660  -0.0997   0.8130   0.0160
 -11.250  -0.7098   0.02145   0.01579  -0.0989   0.8078   0.0164
 -11.000  -0.6905   0.02075   0.01496  -0.0981   0.8027   0.0168
 -10.750  -0.6706   0.02005   0.01413  -0.0974   0.7982   0.0172
 -10.500  -0.6493   0.01940   0.01337  -0.0969   0.7932   0.0176
 -10.250  -0.6279   0.01875   0.01260  -0.0963   0.7883   0.0181
 -10.000  -0.6063   0.01813   0.01190  -0.0957   0.7839   0.0186
  -9.750  -0.5829   0.01763   0.01134  -0.0953   0.7794   0.0192
  -9.500  -0.5589   0.01717   0.01081  -0.0950   0.7746   0.0199
  -9.250  -0.5347   0.01673   0.01027  -0.0947   0.7701   0.0207
  -9.000  -0.5103   0.01630   0.00972  -0.0944   0.7661   0.0214
  -8.750  -0.4860   0.01578   0.00917  -0.0941   0.7615   0.0222
  -8.500  -0.4609   0.01537   0.00871  -0.0939   0.7570   0.0231
  -8.250  -0.4356   0.01501   0.00827  -0.0937   0.7528   0.0240
  -8.000  -0.4100   0.01465   0.00783  -0.0935   0.7488   0.0250
  -7.750  -0.3840   0.01429   0.00741  -0.0933   0.7442   0.0260
  -7.500  -0.3583   0.01392   0.00702  -0.0932   0.7398   0.0274
  -7.250  -0.3320   0.01364   0.00667  -0.0931   0.7359   0.0287
  -7.000  -0.3054   0.01336   0.00632  -0.0930   0.7320   0.0301
  -6.750  -0.2791   0.01302   0.00596  -0.0929   0.7275   0.0314
  -6.500  -0.2525   0.01274   0.00565  -0.0928   0.7231   0.0331
  -6.250  -0.2256   0.01252   0.00536  -0.0928   0.7191   0.0349
  -6.000  -0.1986   0.01226   0.00507  -0.0928   0.7151   0.0369
  -5.750  -0.1716   0.01201   0.00481  -0.0928   0.7107   0.0392
  -5.500  -0.1443   0.01181   0.00456  -0.0928   0.7063   0.0415
  -5.250  -0.1173   0.01160   0.00430  -0.0927   0.7022   0.0443
  -5.000  -0.0898   0.01138   0.00410  -0.0928   0.6978   0.0475
  -4.750  -0.0622   0.01121   0.00389  -0.0928   0.6931   0.0507
  -4.500  -0.0349   0.01102   0.00368  -0.0928   0.6886   0.0553
  -4.250  -0.0072   0.01087   0.00350  -0.0929   0.6844   0.0596
  -4.000   0.0204   0.01068   0.00334  -0.0930   0.6798   0.0659
  -3.750   0.0481   0.01053   0.00318  -0.0930   0.6754   0.0726
  -3.500   0.0758   0.01040   0.00303  -0.0931   0.6712   0.0804
  -3.250   0.1036   0.01024   0.00291  -0.0932   0.6669   0.0910
  -3.000   0.1315   0.01010   0.00279  -0.0933   0.6625   0.1028
  -2.750   0.1592   0.00997   0.00268  -0.0934   0.6581   0.1166
  -2.500   0.1869   0.00984   0.00258  -0.0935   0.6540   0.1344
  -2.250   0.2148   0.00969   0.00250  -0.0937   0.6494   0.1561
  -2.000   0.2425   0.00953   0.00242  -0.0938   0.6449   0.1841
  -1.750   0.2700   0.00938   0.00235  -0.0939   0.6407   0.2194
  -1.500   0.2974   0.00918   0.00229  -0.0941   0.6366   0.2654
  -1.250   0.3247   0.00892   0.00223  -0.0942   0.6319   0.3284
  -1.000   0.3515   0.00863   0.00218  -0.0943   0.6273   0.4126
  -0.500   0.4048   0.00811   0.00218  -0.0943   0.6187   0.5876
  -0.250   0.4319   0.00799   0.00222  -0.0942   0.6137   0.6450
   0.000   0.4590   0.00795   0.00227  -0.0941   0.6089   0.6856
   0.250   0.4865   0.00795   0.00231  -0.0940   0.6042   0.7149
   0.500   0.5139   0.00795   0.00237  -0.0940   0.5990   0.7410
   1.000   0.5685   0.00803   0.00248  -0.0937   0.5899   0.7814
   1.250   0.5954   0.00805   0.00257  -0.0935   0.5851   0.8025
   1.500   0.6214   0.00810   0.00266  -0.0931   0.5800   0.8258
   1.750   0.6475   0.00817   0.00273  -0.0927   0.5755   0.8413
   2.000   0.6749   0.00822   0.00280  -0.0926   0.5709   0.8510
   2.250   0.7017   0.00828   0.00287  -0.0925   0.5660   0.8602
   2.500   0.7281   0.00837   0.00294  -0.0922   0.5611   0.8682
   2.750   0.7547   0.00844   0.00302  -0.0921   0.5562   0.8766
   3.000   0.7810   0.00851   0.00311  -0.0918   0.5508   0.8844
   3.250   0.8066   0.00861   0.00319  -0.0914   0.5454   0.8930
   3.500   0.8323   0.00868   0.00329  -0.0911   0.5399   0.9011
   3.750   0.8575   0.00877   0.00339  -0.0906   0.5339   0.9102
   4.000   0.8816   0.00888   0.00349  -0.0900   0.5284   0.9193
   4.250   0.9067   0.00895   0.00360  -0.0895   0.5227   0.9294
   4.500   0.9310   0.00904   0.00371  -0.0889   0.5170   0.9406
   4.750   0.9566   0.00916   0.00383  -0.0886   0.5118   0.9530
   5.000   0.9858   0.00926   0.00396  -0.0891   0.5052   0.9655
   5.250   1.0172   0.00943   0.00411  -0.0902   0.4974   0.9806
   5.500   1.0486   0.00956   0.00426  -0.0913   0.4887   1.0000
   5.750   1.0726   0.00977   0.00444  -0.0908   0.4809   1.0000
   6.000   1.0978   0.00992   0.00462  -0.0906   0.4738   1.0000
   6.500   1.1454   0.01032   0.00502  -0.0897   0.4584   1.0000
   6.750   1.1672   0.01058   0.00525  -0.0889   0.4498   1.0000
   7.000   1.1862   0.01090   0.00552  -0.0876   0.4342   1.0000
   7.250   1.2013   0.01131   0.00585  -0.0857   0.4113   1.0000
   7.500   1.2117   0.01177   0.00622  -0.0828   0.3902   1.0000
   7.750   1.2223   0.01228   0.00666  -0.0802   0.3710   1.0000
   8.000   1.2317   0.01290   0.00719  -0.0775   0.3489   1.0000
   8.250   1.2408   0.01360   0.00779  -0.0749   0.3283   1.0000
   8.500   1.2500   0.01434   0.00846  -0.0725   0.3077   1.0000
   8.750   1.2569   0.01525   0.00927  -0.0699   0.2846   1.0000
   9.000   1.2629   0.01627   0.01018  -0.0673   0.2618   1.0000
   9.250   1.2669   0.01745   0.01125  -0.0647   0.2367   1.0000
   9.500   1.2702   0.01875   0.01242  -0.0621   0.2109   1.0000
   9.750   1.2727   0.02016   0.01372  -0.0596   0.1868   1.0000
  10.000   1.2769   0.02155   0.01501  -0.0575   0.1659   1.0000
  10.250   1.2801   0.02306   0.01642  -0.0554   0.1450   1.0000
  10.500   1.2819   0.02472   0.01798  -0.0533   0.1235   1.0000
  10.750   1.2843   0.02641   0.01958  -0.0514   0.1052   1.0000
  11.000   1.2873   0.02811   0.02122  -0.0496   0.0895   1.0000
  11.250   1.2926   0.02971   0.02278  -0.0482   0.0787   1.0000
  11.500   1.2979   0.03137   0.02442  -0.0469   0.0693   1.0000
  11.750   1.3036   0.03305   0.02609  -0.0457   0.0615   1.0000
  12.000   1.3097   0.03475   0.02779  -0.0446   0.0546   1.0000
  12.250   1.3166   0.03642   0.02948  -0.0437   0.0498   1.0000
  12.500   1.3220   0.03829   0.03135  -0.0428   0.0447   1.0000
  12.750   1.3295   0.04002   0.03311  -0.0420   0.0410   1.0000
  13.000   1.3352   0.04195   0.03506  -0.0413   0.0379   1.0000
  13.250   1.3424   0.04379   0.03695  -0.0407   0.0352   1.0000
  13.500   1.3486   0.04577   0.03896  -0.0402   0.0328   1.0000
  13.750   1.3539   0.04789   0.04112  -0.0397   0.0308   1.0000
  14.000   1.3608   0.04987   0.04316  -0.0393   0.0293   1.0000
  14.250   1.3662   0.05206   0.04540  -0.0389   0.0278   1.0000
  14.500   1.3702   0.05443   0.04781  -0.0386   0.0262   1.0000
  14.750   1.3758   0.05669   0.05014  -0.0385   0.0251   1.0000
  15.000   1.3809   0.05904   0.05256  -0.0383   0.0241   1.0000
  15.250   1.3854   0.06151   0.05509  -0.0383   0.0230   1.0000
  15.500   1.3886   0.06417   0.05780  -0.0383   0.0222   1.0000
  15.750   1.3903   0.06707   0.06076  -0.0384   0.0214   1.0000
  16.000   1.3951   0.06963   0.06341  -0.0386   0.0207   1.0000
  16.250   1.3983   0.07243   0.06630  -0.0389   0.0202   1.0000
  16.500   1.4015   0.07525   0.06919  -0.0392   0.0194   1.0000
  16.750   1.4035   0.07829   0.07229  -0.0397   0.0187   1.0000
  17.000   1.4042   0.08156   0.07563  -0.0402   0.0182   1.0000
  17.250   1.4035   0.08509   0.07922  -0.0409   0.0176   1.0000
  17.500   1.4058   0.08822   0.08245  -0.0416   0.0172   1.0000
  17.750   1.4074   0.09148   0.08580  -0.0424   0.0167   1.0000
  18.000   1.4081   0.09490   0.08932  -0.0432   0.0163   1.0000
  18.250   1.4089   0.09836   0.09287  -0.0442   0.0158   1.0000
  18.500   1.4088   0.10200   0.09658  -0.0453   0.0154   1.0000
  18.750   1.4084   0.10569   0.10036  -0.0464   0.0151   1.0000
  19.000   1.4063   0.10970   0.10443  -0.0478   0.0147   1.0000
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