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FX 84-W-150 (fx84w150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 84-W-150 (fx84w150-il)
Reynolds number: 1,000,000
Max Cl/Cd: 146.26 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx84w150-il-1000000.txt
Download as CSV file: xf-fx84w150-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7115   0.07661   0.07438  -0.0772   1.0000   0.0136
 -15.500  -0.7944   0.05883   0.05632  -0.0889   1.0000   0.0133
 -15.250  -0.8376   0.04724   0.04449  -0.0978   0.9949   0.0132
 -15.000  -0.8341   0.03928   0.03627  -0.1101   0.9634   0.0133
 -14.750  -0.8299   0.03532   0.03209  -0.1150   0.9363   0.0134
 -14.500  -0.8406   0.03238   0.02892  -0.1152   0.9148   0.0135
 -14.250  -0.8454   0.03028   0.02666  -0.1146   0.9006   0.0137
 -14.000  -0.8489   0.02846   0.02470  -0.1135   0.8891   0.0137
 -13.750  -0.8494   0.02701   0.02309  -0.1119   0.8793   0.0139
 -13.500  -0.8500   0.02565   0.02160  -0.1099   0.8699   0.0141
 -13.250  -0.8463   0.02467   0.02048  -0.1077   0.8620   0.0143
 -13.000  -0.8416   0.02382   0.01953  -0.1052   0.8545   0.0144
 -12.750  -0.8327   0.02302   0.01858  -0.1032   0.8482   0.0146
 -12.500  -0.8177   0.02227   0.01772  -0.1020   0.8425   0.0147
 -12.250  -0.8116   0.02077   0.01606  -0.1000   0.8362   0.0151
 -12.000  -0.7972   0.01981   0.01499  -0.0987   0.8308   0.0154
 -11.750  -0.7779   0.01914   0.01427  -0.0979   0.8257   0.0157
 -11.500  -0.7569   0.01861   0.01367  -0.0973   0.8205   0.0161
 -11.250  -0.7355   0.01810   0.01306  -0.0966   0.8155   0.0165
 -11.000  -0.7132   0.01755   0.01245  -0.0962   0.8109   0.0169
 -10.750  -0.6906   0.01701   0.01182  -0.0957   0.8061   0.0173
 -10.500  -0.6669   0.01661   0.01131  -0.0952   0.8014   0.0177
 -10.250  -0.6442   0.01602   0.01063  -0.0948   0.7970   0.0181
 -10.000  -0.6226   0.01526   0.00983  -0.0942   0.7924   0.0189
  -9.750  -0.5978   0.01489   0.00941  -0.0939   0.7878   0.0195
  -9.500  -0.5729   0.01454   0.00899  -0.0937   0.7834   0.0201
  -9.250  -0.5472   0.01416   0.00857  -0.0935   0.7794   0.0208
  -9.000  -0.5213   0.01383   0.00816  -0.0934   0.7749   0.0214
  -8.750  -0.4970   0.01330   0.00755  -0.0930   0.7705   0.0221
  -8.500  -0.4718   0.01288   0.00709  -0.0928   0.7662   0.0232
  -8.250  -0.4450   0.01260   0.00680  -0.0928   0.7624   0.0241
  -8.000  -0.4180   0.01235   0.00650  -0.0927   0.7581   0.0251
  -7.750  -0.3912   0.01209   0.00617  -0.0927   0.7538   0.0260
  -7.500  -0.3657   0.01165   0.00570  -0.0925   0.7495   0.0276
  -7.250  -0.3383   0.01140   0.00544  -0.0925   0.7454   0.0289
  -7.000  -0.3109   0.01119   0.00519  -0.0925   0.7412   0.0301
  -6.750  -0.2843   0.01087   0.00481  -0.0924   0.7370   0.0317
  -6.500  -0.2571   0.01063   0.00456  -0.0924   0.7328   0.0336
  -6.250  -0.2292   0.01045   0.00436  -0.0925   0.7285   0.0353
  -6.000  -0.2018   0.01020   0.00407  -0.0926   0.7241   0.0371
  -5.750  -0.1746   0.00998   0.00382  -0.0925   0.7195   0.0395
  -5.500  -0.1465   0.00981   0.00364  -0.0927   0.7153   0.0417
  -5.250  -0.1186   0.00959   0.00340  -0.0928   0.7109   0.0445
  -5.000  -0.0908   0.00941   0.00322  -0.0928   0.7065   0.0478
  -4.750  -0.0627   0.00932   0.00307  -0.0929   0.7021   0.0504
  -4.500  -0.0348   0.00907   0.00287  -0.0931   0.6981   0.0559
  -4.250  -0.0065   0.00893   0.00272  -0.0932   0.6938   0.0604
  -4.000   0.0215   0.00877   0.00256  -0.0933   0.6896   0.0676
  -3.750   0.0495   0.00863   0.00243  -0.0935   0.6853   0.0760
  -3.500   0.0780   0.00847   0.00231  -0.0937   0.6812   0.0858
  -3.250   0.1062   0.00833   0.00220  -0.0938   0.6767   0.0985
  -3.000   0.1343   0.00821   0.00210  -0.0940   0.6724   0.1137
  -2.750   0.1626   0.00806   0.00201  -0.0942   0.6684   0.1328
  -2.500   0.1910   0.00791   0.00193  -0.0944   0.6641   0.1565
  -2.250   0.2191   0.00775   0.00186  -0.0946   0.6595   0.1859
  -2.000   0.2469   0.00760   0.00179  -0.0948   0.6550   0.2247
  -1.750   0.2749   0.00736   0.00173  -0.0950   0.6511   0.2780
  -1.500   0.3026   0.00706   0.00167  -0.0953   0.6465   0.3567
  -1.250   0.3296   0.00672   0.00162  -0.0954   0.6418   0.4585
  -1.000   0.3567   0.00644   0.00161  -0.0955   0.6372   0.5571
  -0.750   0.3846   0.00624   0.00162  -0.0957   0.6325   0.6286
  -0.500   0.4126   0.00617   0.00164  -0.0957   0.6276   0.6750
  -0.250   0.4405   0.00616   0.00168  -0.0958   0.6229   0.7081
   0.000   0.4691   0.00613   0.00171  -0.0960   0.6189   0.7334
   0.250   0.4975   0.00613   0.00175  -0.0961   0.6141   0.7545
   0.500   0.5256   0.00617   0.00178  -0.0961   0.6093   0.7717
   0.750   0.5539   0.00620   0.00183  -0.0963   0.6049   0.7862
   1.000   0.5824   0.00622   0.00188  -0.0964   0.6005   0.8007
   1.500   0.6380   0.00634   0.00199  -0.0964   0.5910   0.8258
   1.750   0.6661   0.00635   0.00204  -0.0965   0.5865   0.8380
   2.000   0.6933   0.00640   0.00212  -0.0964   0.5814   0.8533
   2.250   0.7200   0.00649   0.00219  -0.0961   0.5763   0.8666
   2.500   0.7476   0.00652   0.00226  -0.0961   0.5714   0.8757
   2.750   0.7749   0.00658   0.00232  -0.0961   0.5657   0.8838
   3.000   0.8012   0.00667   0.00240  -0.0958   0.5601   0.8921
   3.250   0.8287   0.00671   0.00246  -0.0958   0.5551   0.8996
   3.500   0.8551   0.00677   0.00254  -0.0956   0.5496   0.9075
   3.750   0.8808   0.00688   0.00263  -0.0953   0.5443   0.9155
   4.000   0.9069   0.00692   0.00271  -0.0950   0.5394   0.9241
   4.250   0.9319   0.00699   0.00279  -0.0944   0.5332   0.9329
   4.500   0.9561   0.00709   0.00288  -0.0938   0.5267   0.9432
   4.750   0.9795   0.00713   0.00296  -0.0929   0.5202   0.9546
   5.000   1.0034   0.00724   0.00305  -0.0922   0.5135   0.9683
   5.250   1.0350   0.00730   0.00315  -0.0932   0.5074   0.9806
   5.500   1.0700   0.00743   0.00327  -0.0950   0.5004   0.9928
   5.750   1.0996   0.00757   0.00340  -0.0958   0.4938   1.0000
   6.000   1.1262   0.00770   0.00353  -0.0959   0.4863   1.0000
   6.250   1.1516   0.00788   0.00368  -0.0957   0.4751   1.0000
   6.500   1.1752   0.00812   0.00386  -0.0952   0.4586   1.0000
   6.750   1.1984   0.00837   0.00406  -0.0947   0.4438   1.0000
   7.000   1.2209   0.00864   0.00427  -0.0940   0.4295   1.0000
   7.250   1.2429   0.00892   0.00450  -0.0932   0.4165   1.0000
   7.500   1.2638   0.00922   0.00476  -0.0923   0.4024   1.0000
   7.750   1.2836   0.00953   0.00503  -0.0911   0.3878   1.0000
   8.000   1.3004   0.00989   0.00533  -0.0894   0.3707   1.0000
   8.250   1.3133   0.01031   0.00568  -0.0870   0.3530   1.0000
   8.500   1.3243   0.01081   0.00611  -0.0843   0.3333   1.0000
   8.750   1.3328   0.01145   0.00664  -0.0815   0.3115   1.0000
   9.000   1.3384   0.01226   0.00732  -0.0783   0.2835   1.0000
   9.250   1.3443   0.01312   0.00806  -0.0753   0.2587   1.0000
   9.500   1.3481   0.01414   0.00896  -0.0722   0.2325   1.0000
   9.750   1.3503   0.01532   0.00998  -0.0691   0.2059   1.0000
  10.000   1.3540   0.01649   0.01104  -0.0663   0.1820   1.0000
  10.250   1.3553   0.01786   0.01228  -0.0635   0.1566   1.0000
  10.500   1.3561   0.01934   0.01363  -0.0607   0.1331   1.0000
  10.750   1.3561   0.02094   0.01510  -0.0581   0.1104   1.0000
  11.000   1.3588   0.02246   0.01654  -0.0559   0.0932   1.0000
  11.250   1.3619   0.02402   0.01803  -0.0539   0.0784   1.0000
  11.500   1.3660   0.02557   0.01952  -0.0521   0.0668   1.0000
  11.750   1.3718   0.02705   0.02098  -0.0506   0.0586   1.0000
  12.000   1.3772   0.02861   0.02252  -0.0491   0.0513   1.0000
  12.250   1.3820   0.03028   0.02416  -0.0477   0.0448   1.0000
  12.500   1.3904   0.03172   0.02563  -0.0467   0.0410   1.0000
  12.750   1.3957   0.03347   0.02737  -0.0455   0.0370   1.0000
  13.000   1.4042   0.03499   0.02893  -0.0446   0.0344   1.0000
  13.250   1.4090   0.03688   0.03082  -0.0436   0.0316   1.0000
  13.500   1.4175   0.03849   0.03248  -0.0429   0.0301   1.0000
  13.750   1.4247   0.04025   0.03427  -0.0422   0.0285   1.0000
  14.000   1.4293   0.04228   0.03633  -0.0414   0.0267   1.0000
  14.250   1.4348   0.04430   0.03840  -0.0408   0.0255   1.0000
  14.500   1.4427   0.04612   0.04027  -0.0404   0.0246   1.0000
  14.750   1.4486   0.04819   0.04238  -0.0399   0.0236   1.0000
  15.000   1.4529   0.05045   0.04468  -0.0395   0.0226   1.0000
  15.250   1.4527   0.05325   0.04754  -0.0391   0.0214   1.0000
  15.500   1.4600   0.05529   0.04965  -0.0390   0.0209   1.0000
  15.750   1.4663   0.05748   0.05190  -0.0388   0.0203   1.0000
  16.000   1.4710   0.05988   0.05436  -0.0388   0.0196   1.0000
  16.250   1.4745   0.06247   0.05700  -0.0388   0.0190   1.0000
  16.500   1.4757   0.06537   0.05994  -0.0389   0.0183   1.0000
  16.750   1.4704   0.06918   0.06383  -0.0391   0.0176   1.0000
  17.000   1.4764   0.07160   0.06632  -0.0394   0.0173   1.0000
  17.250   1.4815   0.07416   0.06896  -0.0397   0.0168   1.0000
  17.500   1.4840   0.07710   0.07197  -0.0401   0.0163   1.0000
  17.750   1.4859   0.08017   0.07510  -0.0406   0.0159   1.0000
  18.000   1.4870   0.08338   0.07838  -0.0413   0.0155   1.0000
  18.250   1.4862   0.08693   0.08199  -0.0420   0.0151   1.0000
  18.500   1.4806   0.09120   0.08633  -0.0430   0.0146   1.0000
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