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FX 84-W-127 (fx84w127-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-127 (fx84w127-il)
Reynolds number: 1,000,000
Max Cl/Cd: 131.7 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w127-il-1000000-n5.txt
Download as CSV file: xf-fx84w127-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-127                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.9816   0.03208   0.02891  -0.0949   0.9405   0.0074
 -14.250  -0.9957   0.02983   0.02643  -0.0928   0.9097   0.0074
 -14.000  -1.0025   0.02835   0.02478  -0.0899   0.8923   0.0075
 -13.750  -1.0009   0.02710   0.02338  -0.0875   0.8806   0.0076
 -13.500  -0.9934   0.02578   0.02191  -0.0860   0.8706   0.0077
 -13.250  -0.9802   0.02475   0.02077  -0.0849   0.8626   0.0079
 -13.000  -0.9657   0.02374   0.01963  -0.0839   0.8550   0.0080
 -12.750  -0.9488   0.02283   0.01861  -0.0831   0.8485   0.0082
 -12.500  -0.9305   0.02199   0.01765  -0.0824   0.8416   0.0084
 -12.250  -0.9116   0.02117   0.01670  -0.0817   0.8355   0.0085
 -12.000  -0.8916   0.02037   0.01579  -0.0811   0.8293   0.0087
 -11.750  -0.8709   0.01962   0.01492  -0.0805   0.8234   0.0089
 -11.500  -0.8492   0.01891   0.01410  -0.0800   0.8179   0.0090
 -11.250  -0.8269   0.01825   0.01332  -0.0796   0.8118   0.0092
 -10.750  -0.7803   0.01708   0.01193  -0.0789   0.8006   0.0095
 -10.500  -0.7577   0.01632   0.01107  -0.0785   0.7947   0.0099
 -10.250  -0.7337   0.01576   0.01042  -0.0782   0.7894   0.0102
 -10.000  -0.7087   0.01526   0.00987  -0.0780   0.7840   0.0105
  -9.750  -0.6835   0.01482   0.00935  -0.0778   0.7783   0.0108
  -9.500  -0.6580   0.01440   0.00885  -0.0776   0.7734   0.0112
  -9.250  -0.6322   0.01399   0.00836  -0.0775   0.7682   0.0115
  -9.000  -0.6062   0.01360   0.00790  -0.0774   0.7629   0.0119
  -8.750  -0.5799   0.01325   0.00747  -0.0773   0.7580   0.0122
  -8.500  -0.5537   0.01284   0.00700  -0.0772   0.7530   0.0126
  -8.250  -0.5273   0.01247   0.00657  -0.0771   0.7480   0.0133
  -8.000  -0.5006   0.01217   0.00623  -0.0770   0.7433   0.0139
  -7.750  -0.4735   0.01187   0.00589  -0.0770   0.7384   0.0146
  -7.500  -0.4463   0.01160   0.00555  -0.0770   0.7331   0.0151
  -7.250  -0.4191   0.01135   0.00523  -0.0770   0.7286   0.0155
  -7.000  -0.3920   0.01102   0.00487  -0.0770   0.7242   0.0165
  -6.750  -0.3646   0.01076   0.00458  -0.0770   0.7192   0.0173
  -6.500  -0.3371   0.01054   0.00432  -0.0770   0.7142   0.0183
  -6.250  -0.3093   0.01034   0.00408  -0.0771   0.7095   0.0193
  -6.000  -0.2816   0.01010   0.00381  -0.0771   0.7044   0.0206
  -5.750  -0.2540   0.00990   0.00358  -0.0772   0.6992   0.0219
  -5.500  -0.2259   0.00972   0.00336  -0.0773   0.6943   0.0233
  -5.250  -0.1979   0.00954   0.00315  -0.0773   0.6890   0.0247
  -5.000  -0.1701   0.00936   0.00296  -0.0774   0.6838   0.0269
  -4.750  -0.1418   0.00921   0.00278  -0.0775   0.6790   0.0289
  -4.500  -0.1137   0.00905   0.00261  -0.0776   0.6738   0.0311
  -4.250  -0.0856   0.00891   0.00245  -0.0777   0.6688   0.0339
  -4.000  -0.0572   0.00879   0.00231  -0.0779   0.6642   0.0365
  -3.750  -0.0290   0.00864   0.00216  -0.0780   0.6589   0.0409
  -3.500  -0.0007   0.00854   0.00204  -0.0781   0.6539   0.0444
  -3.250   0.0276   0.00840   0.00192  -0.0783   0.6494   0.0508
  -3.000   0.0561   0.00829   0.00181  -0.0784   0.6441   0.0566
  -2.750   0.0844   0.00819   0.00172  -0.0785   0.6389   0.0643
  -2.500   0.1128   0.00808   0.00163  -0.0787   0.6343   0.0746
  -2.250   0.1412   0.00797   0.00155  -0.0789   0.6291   0.0857
  -2.000   0.1695   0.00788   0.00148  -0.0790   0.6237   0.0999
  -1.750   0.1979   0.00778   0.00141  -0.0792   0.6186   0.1166
  -1.500   0.2263   0.00768   0.00136  -0.0794   0.6128   0.1376
  -1.000   0.2828   0.00746   0.00127  -0.0798   0.6012   0.1950
  -0.750   0.3110   0.00733   0.00124  -0.0800   0.5955   0.2338
  -0.500   0.3390   0.00717   0.00121  -0.0802   0.5904   0.2864
  -0.250   0.3671   0.00696   0.00120  -0.0804   0.5855   0.3545
   0.000   0.3948   0.00672   0.00119  -0.0806   0.5800   0.4401
   0.250   0.4224   0.00649   0.00119  -0.0808   0.5749   0.5300
   0.500   0.4502   0.00630   0.00122  -0.0809   0.5692   0.6077
   0.750   0.4779   0.00619   0.00126  -0.0810   0.5637   0.6686
   1.000   0.5058   0.00613   0.00131  -0.0810   0.5588   0.7134
   1.250   0.5337   0.00610   0.00136  -0.0810   0.5530   0.7507
   1.500   0.5613   0.00612   0.00142  -0.0810   0.5465   0.7772
   1.750   0.5892   0.00613   0.00148  -0.0810   0.5402   0.8000
   2.000   0.6162   0.00615   0.00156  -0.0808   0.5332   0.8286
   2.250   0.6429   0.00617   0.00164  -0.0805   0.5274   0.8574
   2.500   0.6698   0.00621   0.00172  -0.0803   0.5209   0.8755
   2.750   0.6969   0.00628   0.00179  -0.0802   0.5149   0.8866
   3.000   0.7244   0.00634   0.00186  -0.0801   0.5087   0.8971
   3.250   0.7508   0.00642   0.00194  -0.0798   0.5020   0.9076
   3.500   0.7775   0.00649   0.00203  -0.0796   0.4940   0.9174
   3.750   0.8035   0.00660   0.00212  -0.0793   0.4840   0.9275
   4.000   0.8291   0.00669   0.00221  -0.0789   0.4740   0.9381
   4.250   0.8549   0.00678   0.00231  -0.0785   0.4660   0.9496
   4.500   0.8817   0.00689   0.00241  -0.0784   0.4569   0.9626
   4.750   0.9118   0.00700   0.00252  -0.0790   0.4479   0.9757
   5.000   0.9443   0.00717   0.00265  -0.0802   0.4362   0.9899
   5.250   0.9726   0.00740   0.00281  -0.0806   0.4175   1.0000
   5.500   0.9955   0.00783   0.00306  -0.0800   0.3820   1.0000
   5.750   1.0179   0.00829   0.00334  -0.0794   0.3458   1.0000
   6.000   1.0406   0.00872   0.00363  -0.0788   0.3158   1.0000
   6.250   1.0615   0.00927   0.00399  -0.0779   0.2793   1.0000
   6.500   1.0821   0.00980   0.00436  -0.0770   0.2473   1.0000
   6.750   1.1010   0.01042   0.00480  -0.0758   0.2101   1.0000
   7.000   1.1189   0.01107   0.00526  -0.0745   0.1770   1.0000
   7.250   1.1355   0.01174   0.00576  -0.0730   0.1433   1.0000
   7.500   1.1517   0.01239   0.00625  -0.0713   0.1152   1.0000
   7.750   1.1666   0.01305   0.00678  -0.0695   0.0908   1.0000
   8.000   1.1796   0.01366   0.00729  -0.0673   0.0723   1.0000
   8.250   1.1914   0.01422   0.00779  -0.0649   0.0598   1.0000
   8.500   1.2047   0.01475   0.00829  -0.0628   0.0513   1.0000
   8.750   1.2180   0.01532   0.00883  -0.0608   0.0438   1.0000
   9.000   1.2315   0.01592   0.00942  -0.0590   0.0381   1.0000
   9.250   1.2451   0.01654   0.01003  -0.0573   0.0335   1.0000
   9.500   1.2594   0.01716   0.01065  -0.0557   0.0303   1.0000
   9.750   1.2724   0.01787   0.01136  -0.0541   0.0268   1.0000
  10.000   1.2864   0.01856   0.01207  -0.0527   0.0246   1.0000
  10.250   1.3000   0.01931   0.01283  -0.0513   0.0226   1.0000
  10.500   1.3124   0.02015   0.01368  -0.0498   0.0207   1.0000
  10.750   1.3260   0.02093   0.01450  -0.0485   0.0197   1.0000
  11.000   1.3387   0.02180   0.01540  -0.0472   0.0184   1.0000
  11.250   1.3503   0.02278   0.01639  -0.0459   0.0172   1.0000
  11.500   1.3614   0.02381   0.01746  -0.0446   0.0160   1.0000
  11.750   1.3738   0.02480   0.01849  -0.0435   0.0153   1.0000
  12.000   1.3851   0.02587   0.01960  -0.0424   0.0145   1.0000
  12.250   1.3952   0.02707   0.02083  -0.0413   0.0137   1.0000
  12.500   1.4046   0.02836   0.02215  -0.0402   0.0130   1.0000
  12.750   1.4141   0.02967   0.02350  -0.0391   0.0124   1.0000
  13.000   1.4239   0.03098   0.02488  -0.0382   0.0120   1.0000
  13.250   1.4331   0.03238   0.02633  -0.0373   0.0115   1.0000
  13.500   1.4417   0.03386   0.02785  -0.0365   0.0109   1.0000
  13.750   1.4490   0.03549   0.02952  -0.0357   0.0104   1.0000
  14.000   1.4552   0.03728   0.03136  -0.0349   0.0099   1.0000
  14.250   1.4618   0.03909   0.03323  -0.0343   0.0096   1.0000
  14.500   1.4694   0.04085   0.03505  -0.0337   0.0094   1.0000
  14.750   1.4761   0.04273   0.03701  -0.0332   0.0092   1.0000
  15.000   1.4824   0.04471   0.03905  -0.0329   0.0088   1.0000
  15.250   1.4876   0.04687   0.04127  -0.0325   0.0085   1.0000
  15.500   1.4925   0.04909   0.04355  -0.0323   0.0083   1.0000
  15.750   1.4970   0.05140   0.04592  -0.0321   0.0080   1.0000
  16.000   1.5000   0.05395   0.04853  -0.0321   0.0077   1.0000
  16.250   1.5026   0.05662   0.05127  -0.0321   0.0075   1.0000
  16.500   1.5037   0.05953   0.05426  -0.0323   0.0074   1.0000
  16.750   1.5068   0.06223   0.05703  -0.0325   0.0072   1.0000
  17.000   1.5085   0.06519   0.06009  -0.0329   0.0071   1.0000
  17.250   1.5109   0.06813   0.06310  -0.0333   0.0069   1.0000
  17.500   1.5120   0.07128   0.06634  -0.0339   0.0068   1.0000
  17.750   1.5141   0.07434   0.06947  -0.0345   0.0065   1.0000
  18.000   1.5137   0.07782   0.07304  -0.0354   0.0064   1.0000
  18.250   1.5124   0.08150   0.07681  -0.0363   0.0063   1.0000
  18.500   1.5110   0.08524   0.08064  -0.0374   0.0062   1.0000
  18.750   1.5095   0.08908   0.08456  -0.0386   0.0061   1.0000
  19.000   1.5068   0.09314   0.08870  -0.0400   0.0059   1.0000
  19.250   1.5035   0.09737   0.09302  -0.0415   0.0058   1.0000
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