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FX 84-W-097 (fx84w097-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-097 (fx84w097-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.12 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w097-il-1000000-n5.txt
Download as CSV file: xf-fx84w097-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-097                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.9340   0.03928   0.03725  -0.0535   1.0000   0.0056
 -12.000  -0.9462   0.03377   0.03141  -0.0543   1.0000   0.0056
 -11.750  -0.9429   0.03037   0.02774  -0.0542   1.0000   0.0057
 -11.500  -0.9302   0.02770   0.02481  -0.0545   0.9795   0.0057
 -11.250  -0.9111   0.02571   0.02256  -0.0551   0.9450   0.0058
 -11.000  -0.8973   0.02413   0.02072  -0.0539   0.9229   0.0058
 -10.750  -0.8804   0.02278   0.01913  -0.0530   0.9072   0.0059
 -10.500  -0.8634   0.02123   0.01733  -0.0521   0.8939   0.0059
 -10.250  -0.8454   0.01964   0.01548  -0.0514   0.8822   0.0061
  -9.750  -0.8015   0.01765   0.01315  -0.0504   0.8611   0.0065
  -9.500  -0.7776   0.01693   0.01230  -0.0501   0.8519   0.0067
  -9.250  -0.7533   0.01628   0.01152  -0.0498   0.8430   0.0068
  -9.000  -0.7284   0.01567   0.01078  -0.0495   0.8345   0.0070
  -8.750  -0.7033   0.01509   0.01007  -0.0493   0.8266   0.0072
  -8.500  -0.6778   0.01451   0.00939  -0.0490   0.8185   0.0075
  -8.250  -0.6520   0.01401   0.00878  -0.0488   0.8112   0.0078
  -8.000  -0.6259   0.01355   0.00821  -0.0487   0.8035   0.0081
  -7.750  -0.5995   0.01315   0.00771  -0.0485   0.7964   0.0083
  -7.500  -0.5728   0.01278   0.00723  -0.0484   0.7890   0.0085
  -7.250  -0.5471   0.01212   0.00647  -0.0482   0.7822   0.0091
  -7.000  -0.5203   0.01172   0.00600  -0.0481   0.7748   0.0095
  -6.750  -0.4934   0.01140   0.00561  -0.0480   0.7681   0.0100
  -6.500  -0.4662   0.01108   0.00524  -0.0479   0.7611   0.0105
  -6.250  -0.4390   0.01079   0.00486  -0.0479   0.7541   0.0111
  -6.000  -0.4115   0.01052   0.00452  -0.0478   0.7466   0.0116
  -5.750  -0.3842   0.01024   0.00417  -0.0477   0.7394   0.0121
  -5.500  -0.3567   0.00992   0.00380  -0.0477   0.7319   0.0131
  -5.250  -0.3291   0.00969   0.00353  -0.0477   0.7250   0.0141
  -5.000  -0.3013   0.00949   0.00329  -0.0477   0.7181   0.0152
  -4.500  -0.2456   0.00907   0.00278  -0.0477   0.7047   0.0178
  -4.250  -0.2178   0.00889   0.00257  -0.0477   0.6979   0.0195
  -4.000  -0.1897   0.00874   0.00238  -0.0477   0.6914   0.0211
  -3.750  -0.1617   0.00857   0.00218  -0.0477   0.6844   0.0237
  -3.500  -0.1337   0.00841   0.00201  -0.0477   0.6779   0.0267
  -3.250  -0.1055   0.00830   0.00185  -0.0478   0.6705   0.0289
  -3.000  -0.0774   0.00814   0.00170  -0.0478   0.6636   0.0344
  -2.750  -0.0492   0.00803   0.00157  -0.0479   0.6560   0.0397
  -2.500  -0.0211   0.00791   0.00145  -0.0479   0.6489   0.0475
  -2.250   0.0071   0.00779   0.00134  -0.0480   0.6413   0.0574
  -2.000   0.0353   0.00767   0.00125  -0.0481   0.6344   0.0702
  -1.750   0.0635   0.00757   0.00116  -0.0482   0.6270   0.0847
  -1.500   0.0917   0.00745   0.00108  -0.0482   0.6205   0.1054
  -1.250   0.1199   0.00733   0.00102  -0.0483   0.6135   0.1289
  -1.000   0.1480   0.00720   0.00097  -0.0484   0.6070   0.1623
  -0.750   0.1761   0.00706   0.00092  -0.0486   0.5998   0.2007
  -0.500   0.2041   0.00689   0.00088  -0.0487   0.5933   0.2519
  -0.250   0.2319   0.00668   0.00086  -0.0488   0.5861   0.3211
   0.000   0.2596   0.00645   0.00084  -0.0489   0.5788   0.4011
   0.250   0.2870   0.00616   0.00083  -0.0490   0.5706   0.5054
   0.500   0.3139   0.00585   0.00084  -0.0490   0.5626   0.6248
   0.750   0.3407   0.00562   0.00087  -0.0488   0.5542   0.7220
   1.000   0.3677   0.00551   0.00092  -0.0486   0.5464   0.7806
   1.250   0.3945   0.00546   0.00097  -0.0483   0.5385   0.8251
   1.500   0.4207   0.00541   0.00102  -0.0478   0.5311   0.8662
   1.750   0.4467   0.00542   0.00108  -0.0473   0.5232   0.8964
   2.000   0.4718   0.00542   0.00114  -0.0465   0.5136   0.9277
   2.250   0.4984   0.00544   0.00118  -0.0459   0.5029   0.9663
   2.500   0.5349   0.00551   0.00122  -0.0478   0.4908   0.9864
   2.750   0.5688   0.00561   0.00128  -0.0492   0.4804   0.9945
   3.000   0.6011   0.00570   0.00133  -0.0503   0.4685   1.0000
   3.250   0.6278   0.00582   0.00141  -0.0501   0.4563   1.0000
   3.500   0.6547   0.00594   0.00151  -0.0500   0.4446   1.0000
   3.750   0.6817   0.00608   0.00160  -0.0499   0.4314   1.0000
   4.000   0.7079   0.00634   0.00174  -0.0497   0.4009   1.0000
   4.250   0.7333   0.00673   0.00192  -0.0495   0.3569   1.0000
   4.500   0.7588   0.00712   0.00214  -0.0493   0.3164   1.0000
   4.750   0.7845   0.00748   0.00235  -0.0491   0.2830   1.0000
   5.000   0.8093   0.00796   0.00263  -0.0488   0.2394   1.0000
   5.250   0.8335   0.00852   0.00296  -0.0485   0.1916   1.0000
   5.500   0.8571   0.00913   0.00334  -0.0482   0.1433   1.0000
   5.750   0.8804   0.00977   0.00375  -0.0477   0.0978   1.0000
   6.000   0.9045   0.01029   0.00412  -0.0474   0.0686   1.0000
   6.250   0.9290   0.01073   0.00447  -0.0471   0.0497   1.0000
   6.500   0.9538   0.01113   0.00481  -0.0468   0.0375   1.0000
   6.750   0.9787   0.01149   0.00514  -0.0465   0.0299   1.0000
   7.000   1.0035   0.01186   0.00548  -0.0462   0.0246   1.0000
   7.250   1.0284   0.01219   0.00581  -0.0459   0.0210   1.0000
   7.500   1.0526   0.01259   0.00620  -0.0455   0.0173   1.0000
   7.750   1.0771   0.01294   0.00656  -0.0452   0.0153   1.0000
   8.000   1.1008   0.01335   0.00697  -0.0447   0.0132   1.0000
   8.250   1.1244   0.01376   0.00739  -0.0443   0.0117   1.0000
   8.500   1.1478   0.01415   0.00781  -0.0438   0.0106   1.0000
   8.750   1.1705   0.01459   0.00828  -0.0432   0.0098   1.0000
   9.000   1.1921   0.01511   0.00882  -0.0425   0.0089   1.0000
   9.250   1.2137   0.01561   0.00936  -0.0418   0.0084   1.0000
   9.500   1.2350   0.01609   0.00989  -0.0411   0.0080   1.0000
   9.750   1.2558   0.01658   0.01042  -0.0403   0.0076   1.0000
  10.000   1.2756   0.01712   0.01100  -0.0393   0.0073   1.0000
  10.250   1.2947   0.01767   0.01159  -0.0383   0.0068   1.0000
  10.500   1.3120   0.01830   0.01226  -0.0371   0.0065   1.0000
  10.750   1.3267   0.01904   0.01305  -0.0355   0.0061   1.0000
  11.000   1.3364   0.01982   0.01390  -0.0331   0.0059   1.0000
  11.250   1.3486   0.02046   0.01460  -0.0311   0.0058   1.0000
  11.500   1.3583   0.02130   0.01551  -0.0291   0.0057   1.0000
  11.750   1.3693   0.02213   0.01641  -0.0274   0.0055   1.0000
  12.000   1.3794   0.02308   0.01743  -0.0257   0.0054   1.0000
  12.250   1.3880   0.02420   0.01863  -0.0241   0.0053   1.0000
  12.500   1.3976   0.02531   0.01982  -0.0228   0.0051   1.0000
  12.750   1.4055   0.02660   0.02118  -0.0214   0.0050   1.0000
  13.000   1.4138   0.02792   0.02258  -0.0203   0.0048   1.0000
  13.250   1.4218   0.02933   0.02406  -0.0193   0.0047   1.0000
  13.500   1.4292   0.03084   0.02564  -0.0184   0.0045   1.0000
  13.750   1.4359   0.03248   0.02735  -0.0176   0.0044   1.0000
  14.000   1.4405   0.03437   0.02931  -0.0168   0.0043   1.0000
  14.250   1.4427   0.03658   0.03162  -0.0162   0.0043   1.0000
  14.500   1.4434   0.03901   0.03414  -0.0157   0.0040   1.0000
  14.750   1.4408   0.04189   0.03714  -0.0154   0.0039   1.0000
  15.000   1.4410   0.04459   0.03994  -0.0153   0.0039   1.0000
  15.250   1.4432   0.04713   0.04258  -0.0154   0.0038   1.0000
  15.500   1.4414   0.05025   0.04582  -0.0157   0.0038   1.0000
  15.750   1.4418   0.05322   0.04889  -0.0162   0.0037   1.0000
  16.000   1.4424   0.05626   0.05203  -0.0168   0.0037   1.0000
  16.250   1.4381   0.06012   0.05601  -0.0178   0.0036   1.0000
  16.500   1.4337   0.06413   0.06014  -0.0190   0.0036   1.0000
  16.750   1.4286   0.06839   0.06452  -0.0204   0.0036   1.0000
  17.000   1.4224   0.07300   0.06924  -0.0222   0.0035   1.0000
  17.250   1.4160   0.07781   0.07417  -0.0241   0.0034   1.0000
  17.500   1.4047   0.08354   0.08004  -0.0266   0.0035   1.0000
  17.750   1.3987   0.08860   0.08521  -0.0290   0.0034   1.0000
  18.000   1.3844   0.09528   0.09204  -0.0322   0.0034   1.0000
  18.250   1.3729   0.10167   0.09855  -0.0355   0.0034   1.0000
  18.500   1.3588   0.10876   0.10577  -0.0392   0.0034   1.0000
  18.750   1.3441   0.11618   0.11333  -0.0433   0.0033   1.0000
  19.000   1.3301   0.12359   0.12087  -0.0474   0.0033   1.0000
  19.250   1.3132   0.13186   0.12927  -0.0522   0.0033   1.0000
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