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FX 84-W-140 (fx84w140-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-140 (fx84w140-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.43 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w140-il-1000000-n5.txt
Download as CSV file: xf-fx84w140-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-140                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6262   0.09679   0.09465  -0.0633   0.9689   0.0092
 -15.500  -0.8984   0.04115   0.03806  -0.1064   0.9260   0.0085
 -15.250  -0.9266   0.03531   0.03193  -0.1096   0.9007   0.0084
 -15.000  -0.9398   0.03216   0.02859  -0.1100   0.8852   0.0085
 -14.750  -0.9483   0.02982   0.02609  -0.1093   0.8729   0.0085
 -14.500  -0.9536   0.02800   0.02412  -0.1078   0.8627   0.0086
 -14.250  -0.9554   0.02660   0.02260  -0.1058   0.8532   0.0087
 -14.000  -0.9554   0.02546   0.02135  -0.1032   0.8455   0.0088
 -13.750  -0.9492   0.02450   0.02026  -0.1011   0.8381   0.0089
 -13.500  -0.9377   0.02353   0.01918  -0.0998   0.8320   0.0090
 -13.250  -0.9229   0.02267   0.01822  -0.0987   0.8260   0.0092
 -13.000  -0.9072   0.02183   0.01726  -0.0977   0.8205   0.0093
 -12.750  -0.8894   0.02107   0.01639  -0.0969   0.8157   0.0095
 -12.500  -0.8706   0.02032   0.01555  -0.0962   0.8103   0.0097
 -12.250  -0.8509   0.01963   0.01475  -0.0955   0.8048   0.0099
 -12.000  -0.8301   0.01898   0.01399  -0.0949   0.8002   0.0101
 -11.750  -0.8081   0.01841   0.01333  -0.0945   0.7953   0.0102
 -11.500  -0.7858   0.01785   0.01267  -0.0940   0.7903   0.0104
 -11.250  -0.7645   0.01712   0.01185  -0.0935   0.7856   0.0108
 -11.000  -0.7413   0.01655   0.01121  -0.0932   0.7808   0.0111
 -10.750  -0.7174   0.01605   0.01065  -0.0929   0.7759   0.0114
 -10.250  -0.6684   0.01514   0.00959  -0.0924   0.7669   0.0120
 -10.000  -0.6433   0.01471   0.00909  -0.0922   0.7621   0.0124
  -9.750  -0.6180   0.01432   0.00862  -0.0920   0.7575   0.0127
  -9.500  -0.5924   0.01395   0.00817  -0.0919   0.7533   0.0130
  -9.250  -0.5667   0.01353   0.00769  -0.0918   0.7489   0.0134
  -9.000  -0.5409   0.01313   0.00724  -0.0916   0.7441   0.0140
  -8.500  -0.4881   0.01248   0.00651  -0.0915   0.7360   0.0151
  -8.250  -0.4612   0.01221   0.00618  -0.0915   0.7314   0.0158
  -8.000  -0.4342   0.01195   0.00586  -0.0915   0.7268   0.0163
  -7.750  -0.4076   0.01163   0.00550  -0.0914   0.7227   0.0172
  -7.500  -0.3804   0.01135   0.00521  -0.0915   0.7187   0.0180
  -7.250  -0.3530   0.01112   0.00493  -0.0915   0.7145   0.0189
  -7.000  -0.3256   0.01091   0.00466  -0.0915   0.7100   0.0197
  -6.750  -0.2982   0.01066   0.00439  -0.0916   0.7060   0.0209
  -6.500  -0.2705   0.01044   0.00416  -0.0917   0.7015   0.0223
  -6.250  -0.2427   0.01026   0.00394  -0.0918   0.6971   0.0235
  -5.750  -0.1872   0.00987   0.00350  -0.0919   0.6884   0.0264
  -5.500  -0.1592   0.00971   0.00331  -0.0920   0.6835   0.0280
  -5.250  -0.1312   0.00957   0.00313  -0.0921   0.6786   0.0296
  -5.000  -0.1032   0.00939   0.00295  -0.0923   0.6742   0.0320
  -4.750  -0.0750   0.00925   0.00279  -0.0924   0.6695   0.0341
  -4.500  -0.0468   0.00911   0.00263  -0.0925   0.6649   0.0364
  -4.250  -0.0188   0.00898   0.00249  -0.0927   0.6608   0.0396
  -4.000   0.0097   0.00886   0.00236  -0.0929   0.6564   0.0430
  -3.750   0.0379   0.00873   0.00224  -0.0930   0.6515   0.0475
  -3.500   0.0662   0.00863   0.00212  -0.0932   0.6471   0.0521
  -3.250   0.0946   0.00851   0.00202  -0.0934   0.6432   0.0579
  -3.000   0.1230   0.00840   0.00192  -0.0936   0.6385   0.0651
  -2.750   0.1514   0.00832   0.00184  -0.0937   0.6337   0.0720
  -2.500   0.1797   0.00822   0.00176  -0.0939   0.6295   0.0821
  -2.250   0.2082   0.00812   0.00169  -0.0941   0.6252   0.0941
  -2.000   0.2366   0.00803   0.00163  -0.0943   0.6204   0.1070
  -1.750   0.2648   0.00795   0.00157  -0.0945   0.6156   0.1236
  -1.500   0.2933   0.00785   0.00152  -0.0947   0.6115   0.1432
  -1.250   0.3216   0.00773   0.00148  -0.0950   0.6066   0.1702
  -1.000   0.3497   0.00763   0.00145  -0.0952   0.6014   0.2036
  -0.750   0.3779   0.00750   0.00143  -0.0954   0.5968   0.2424
  -0.500   0.4060   0.00733   0.00140  -0.0956   0.5915   0.2954
  -0.250   0.4337   0.00714   0.00139  -0.0959   0.5863   0.3659
   0.000   0.4614   0.00691   0.00139  -0.0961   0.5819   0.4495
   0.250   0.4892   0.00668   0.00140  -0.0963   0.5773   0.5363
   0.500   0.5169   0.00653   0.00143  -0.0965   0.5722   0.6071
   0.750   0.5447   0.00646   0.00148  -0.0966   0.5673   0.6572
   1.000   0.5729   0.00642   0.00153  -0.0967   0.5624   0.6958
   1.250   0.6008   0.00641   0.00158  -0.0968   0.5574   0.7259
   1.500   0.6286   0.00644   0.00165  -0.0969   0.5527   0.7517
   1.750   0.6566   0.00645   0.00171  -0.0969   0.5479   0.7733
   2.000   0.6840   0.00647   0.00179  -0.0969   0.5423   0.8016
   2.250   0.7107   0.00651   0.00189  -0.0967   0.5370   0.8271
   2.500   0.7384   0.00656   0.00196  -0.0967   0.5313   0.8404
   3.000   0.7931   0.00671   0.00211  -0.0967   0.5192   0.8580
   3.250   0.8207   0.00679   0.00219  -0.0967   0.5129   0.8662
   3.500   0.8472   0.00689   0.00229  -0.0965   0.5069   0.8745
   3.750   0.8747   0.00696   0.00237  -0.0966   0.5016   0.8825
   4.000   0.9011   0.00705   0.00248  -0.0964   0.4949   0.8906
   4.250   0.9274   0.00716   0.00258  -0.0962   0.4872   0.8990
   4.500   0.9526   0.00728   0.00270  -0.0958   0.4780   0.9081
   4.750   0.9781   0.00738   0.00282  -0.0954   0.4701   0.9174
   5.000   1.0026   0.00752   0.00295  -0.0949   0.4619   0.9282
   5.250   1.0269   0.00761   0.00307  -0.0942   0.4545   0.9402
   5.500   1.0502   0.00776   0.00322  -0.0935   0.4456   0.9550
   5.750   1.0778   0.00790   0.00336  -0.0936   0.4356   0.9724
   6.000   1.1071   0.00821   0.00358  -0.0944   0.4144   1.0000
   6.250   1.1273   0.00866   0.00387  -0.0934   0.3821   1.0000
   6.500   1.1462   0.00917   0.00421  -0.0921   0.3501   1.0000
   6.750   1.1631   0.00973   0.00460  -0.0906   0.3156   1.0000
   7.000   1.1795   0.01028   0.00500  -0.0889   0.2865   1.0000
   7.250   1.1948   0.01083   0.00542  -0.0871   0.2611   1.0000
   7.500   1.2039   0.01145   0.00589  -0.0840   0.2326   1.0000
   7.750   1.2115   0.01213   0.00644  -0.0809   0.2064   1.0000
   8.000   1.2209   0.01280   0.00700  -0.0782   0.1838   1.0000
   8.250   1.2285   0.01360   0.00768  -0.0754   0.1598   1.0000
   8.500   1.2336   0.01456   0.00850  -0.0724   0.1326   1.0000
   8.750   1.2407   0.01550   0.00933  -0.0698   0.1105   1.0000
   9.000   1.2487   0.01645   0.01019  -0.0675   0.0925   1.0000
   9.250   1.2582   0.01737   0.01105  -0.0654   0.0786   1.0000
   9.500   1.2673   0.01836   0.01198  -0.0635   0.0658   1.0000
   9.750   1.2774   0.01932   0.01291  -0.0617   0.0563   1.0000
  10.000   1.2881   0.02029   0.01385  -0.0601   0.0489   1.0000
  10.500   1.3100   0.02228   0.01582  -0.0572   0.0379   1.0000
  10.750   1.3211   0.02331   0.01686  -0.0558   0.0342   1.0000
  11.000   1.3325   0.02436   0.01791  -0.0546   0.0310   1.0000
  11.250   1.3430   0.02548   0.01904  -0.0533   0.0284   1.0000
  11.500   1.3538   0.02662   0.02019  -0.0521   0.0258   1.0000
  11.750   1.3638   0.02784   0.02143  -0.0510   0.0239   1.0000
  12.000   1.3745   0.02903   0.02266  -0.0500   0.0226   1.0000
  12.250   1.3850   0.03027   0.02393  -0.0490   0.0215   1.0000
  12.500   1.3945   0.03163   0.02532  -0.0480   0.0203   1.0000
  12.750   1.4028   0.03313   0.02684  -0.0470   0.0190   1.0000
  13.000   1.4131   0.03448   0.02824  -0.0462   0.0183   1.0000
  13.250   1.4225   0.03596   0.02976  -0.0454   0.0177   1.0000
  13.500   1.4310   0.03755   0.03139  -0.0447   0.0168   1.0000
  13.750   1.4390   0.03923   0.03311  -0.0439   0.0160   1.0000
  14.000   1.4453   0.04109   0.03501  -0.0433   0.0153   1.0000
  14.250   1.4543   0.04274   0.03672  -0.0427   0.0148   1.0000
  14.500   1.4621   0.04456   0.03859  -0.0422   0.0144   1.0000
  14.750   1.4692   0.04648   0.04056  -0.0418   0.0138   1.0000
  15.000   1.4760   0.04846   0.04259  -0.0414   0.0132   1.0000
  15.250   1.4812   0.05064   0.04481  -0.0411   0.0126   1.0000
  15.500   1.4858   0.05296   0.04719  -0.0408   0.0122   1.0000
  15.750   1.4925   0.05506   0.04935  -0.0406   0.0118   1.0000
  16.000   1.4978   0.05737   0.05173  -0.0405   0.0115   1.0000
  16.250   1.5029   0.05975   0.05417  -0.0405   0.0111   1.0000
  16.500   1.5070   0.06227   0.05675  -0.0405   0.0107   1.0000
  16.750   1.5109   0.06487   0.05941  -0.0407   0.0104   1.0000
  17.000   1.5141   0.06758   0.06218  -0.0409   0.0100   1.0000
  17.250   1.5155   0.07060   0.06526  -0.0412   0.0097   1.0000
  17.500   1.5173   0.07362   0.06834  -0.0416   0.0094   1.0000
  17.750   1.5203   0.07649   0.07130  -0.0420   0.0092   1.0000
  18.000   1.5225   0.07954   0.07442  -0.0426   0.0090   1.0000
  18.250   1.5236   0.08278   0.07774  -0.0432   0.0087   1.0000
  18.500   1.5252   0.08600   0.08103  -0.0439   0.0086   1.0000
  18.750   1.5253   0.08947   0.08458  -0.0448   0.0082   1.0000
  19.000   1.5251   0.09301   0.08820  -0.0458   0.0081   1.0000
  19.250   1.5244   0.09668   0.09194  -0.0468   0.0078   1.0000
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