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FX LIII-142 K 25 AIRFOIL (fxl142k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX LIII-142 K 25 AIRFOIL (fxl142k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 72.07 at α=11.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxl142k-il-1000000-n5.txt
Download as CSV file: xf-fxl142k-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX LIII-142 K 25 AIRFOIL                        
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1442   0.13020   0.12711   0.0172   1.0000   0.0026
 -19.500  -1.1767   0.12018   0.11695   0.0120   1.0000   0.0027
 -19.250  -1.2049   0.11114   0.10776   0.0074   1.0000   0.0026
 -19.000  -1.2266   0.10354   0.10002   0.0037   1.0000   0.0026
 -18.750  -1.2508   0.09566   0.09199  -0.0001   1.0000   0.0026
 -18.500  -1.2700   0.08882   0.08502  -0.0034   1.0000   0.0026
 -18.250  -1.2848   0.08288   0.07897  -0.0061   1.0000   0.0027
 -18.000  -1.2990   0.07712   0.07308  -0.0087   1.0000   0.0026
 -17.750  -1.3127   0.07161   0.06747  -0.0111   1.0000   0.0027
 -17.500  -1.3175   0.06753   0.06328  -0.0127   1.0000   0.0027
 -17.250  -1.3276   0.06278   0.05843  -0.0146   1.0000   0.0027
 -17.000  -1.3311   0.05911   0.05467  -0.0160   1.0000   0.0027
 -16.750  -1.3389   0.05503   0.05049  -0.0173   1.0000   0.0029
 -16.500  -1.3420   0.05169   0.04706  -0.0183   1.0000   0.0029
 -16.250  -1.3443   0.04854   0.04383  -0.0191   1.0000   0.0030
 -16.000  -1.3446   0.04564   0.04084  -0.0199   1.0000   0.0030
 -15.750  -1.3449   0.04281   0.03792  -0.0204   1.0000   0.0031
 -15.500  -1.3422   0.04032   0.03535  -0.0210   1.0000   0.0031
 -15.250  -1.3397   0.03783   0.03278  -0.0214   1.0000   0.0033
 -15.000  -1.3351   0.03559   0.03046  -0.0217   1.0000   0.0033
 -14.750  -1.3295   0.03345   0.02825  -0.0220   1.0000   0.0035
 -14.500  -1.3221   0.03151   0.02624  -0.0223   1.0000   0.0035
 -14.250  -1.3140   0.02968   0.02434  -0.0225   1.0000   0.0037
 -14.000  -1.3073   0.02773   0.02232  -0.0226   1.0000   0.0041
 -13.750  -1.2989   0.02599   0.02051  -0.0226   1.0000   0.0045
 -13.500  -1.2867   0.02472   0.01919  -0.0224   1.0000   0.0044
 -13.250  -1.2777   0.02327   0.01766  -0.0220   1.0000   0.0051
 -13.000  -1.2681   0.02201   0.01634  -0.0212   1.0000   0.0058
 -12.750  -1.2571   0.02102   0.01530  -0.0201   1.0000   0.0062
 -12.500  -1.2475   0.02009   0.01433  -0.0184   1.0000   0.0071
 -12.250  -1.2421   0.01909   0.01332  -0.0157   1.0000   0.0098
 -12.000  -1.2326   0.01826   0.01250  -0.0134   1.0000   0.0134
 -11.750  -1.2182   0.01753   0.01178  -0.0118   1.0000   0.0168
 -11.500  -1.2003   0.01699   0.01123  -0.0106   1.0000   0.0185
 -11.250  -1.1823   0.01643   0.01069  -0.0094   1.0000   0.0214
 -10.750  -1.0934   0.01540   0.00949  -0.0179   0.8669   0.0288
 -10.500  -1.0744   0.01522   0.00915  -0.0164   0.8302   0.0297
 -10.250  -1.0536   0.01495   0.00879  -0.0154   0.8158   0.0303
 -10.000  -1.0330   0.01457   0.00836  -0.0143   0.8028   0.0318
  -9.750  -1.0130   0.01429   0.00795  -0.0130   0.7549   0.0334
  -9.500  -0.9915   0.01402   0.00760  -0.0121   0.7404   0.0351
  -9.250  -0.9685   0.01375   0.00727  -0.0113   0.7303   0.0362
  -9.000  -0.9447   0.01353   0.00699  -0.0108   0.7218   0.0375
  -8.750  -0.9205   0.01331   0.00671  -0.0102   0.7130   0.0383
  -8.500  -0.8954   0.01312   0.00649  -0.0098   0.7047   0.0390
  -8.250  -0.8716   0.01284   0.00613  -0.0092   0.6946   0.0395
  -8.000  -0.8475   0.01254   0.00579  -0.0086   0.6818   0.0414
  -7.500  -0.7985   0.01205   0.00519  -0.0075   0.6549   0.0443
  -7.250  -0.7736   0.01182   0.00492  -0.0070   0.6472   0.0459
  -7.000  -0.7484   0.01160   0.00467  -0.0066   0.6413   0.0474
  -6.750  -0.7229   0.01140   0.00443  -0.0061   0.6362   0.0492
  -6.500  -0.6977   0.01113   0.00418  -0.0057   0.6319   0.0548
  -6.250  -0.6717   0.01093   0.00397  -0.0054   0.6273   0.0597
  -6.000  -0.6460   0.01072   0.00374  -0.0050   0.6220   0.0657
  -5.750  -0.6198   0.01051   0.00354  -0.0047   0.6159   0.0721
  -5.500  -0.5939   0.01028   0.00334  -0.0044   0.6080   0.0816
  -5.250  -0.5682   0.01002   0.00314  -0.0040   0.6011   0.0976
  -5.000  -0.5411   0.00989   0.00298  -0.0038   0.5951   0.1027
  -4.750  -0.5146   0.00971   0.00281  -0.0036   0.5905   0.1106
  -4.500  -0.4875   0.00957   0.00267  -0.0034   0.5861   0.1176
  -4.250  -0.4608   0.00939   0.00252  -0.0032   0.5816   0.1280
  -4.000  -0.4342   0.00921   0.00237  -0.0029   0.5773   0.1413
  -3.750  -0.4073   0.00905   0.00223  -0.0027   0.5739   0.1532
  -3.500  -0.3805   0.00884   0.00209  -0.0025   0.5705   0.1702
  -3.250  -0.3553   0.00847   0.00189  -0.0021   0.5670   0.2134
  -3.000  -0.3295   0.00819   0.00173  -0.0018   0.5636   0.2510
  -2.750  -0.3034   0.00794   0.00160  -0.0015   0.5605   0.2833
  -2.500  -0.2770   0.00767   0.00147  -0.0012   0.5570   0.3211
  -2.250  -0.2506   0.00742   0.00137  -0.0009   0.5510   0.3603
  -2.000  -0.2239   0.00724   0.00128  -0.0007   0.5443   0.3915
  -1.750  -0.1964   0.00712   0.00122  -0.0005   0.5389   0.4114
  -1.500  -0.1688   0.00702   0.00117  -0.0004   0.5325   0.4296
  -1.250  -0.1409   0.00696   0.00114  -0.0003   0.5278   0.4437
  -1.000  -0.1132   0.00690   0.00113  -0.0002   0.5221   0.4668
  -0.750  -0.0851   0.00690   0.00113  -0.0001   0.5163   0.4843
  -0.500  -0.0568   0.00687   0.00113   0.0000   0.5124   0.4938
  -0.250  -0.0283   0.00688   0.00112   0.0000   0.5081   0.4990
   0.000   0.0000   0.00690   0.00112   0.0000   0.5030   0.5028
   0.250   0.0283   0.00688   0.00112   0.0000   0.4989   0.5081
   0.500   0.0568   0.00687   0.00113   0.0000   0.4937   0.5124
   0.750   0.0851   0.00690   0.00113   0.0001   0.4830   0.5163
   1.000   0.1132   0.00690   0.00113   0.0002   0.4648   0.5221
   1.250   0.1409   0.00696   0.00114   0.0003   0.4444   0.5277
   1.750   0.1962   0.00713   0.00122   0.0006   0.4090   0.5383
   2.000   0.2237   0.00727   0.00129   0.0007   0.3863   0.5443
   2.250   0.2505   0.00743   0.00137   0.0009   0.3577   0.5507
   2.500   0.2770   0.00766   0.00147   0.0012   0.3213   0.5567
   2.750   0.3033   0.00795   0.00160   0.0015   0.2821   0.5605
   3.000   0.3296   0.00819   0.00173   0.0018   0.2517   0.5636
   3.250   0.3554   0.00847   0.00189   0.0021   0.2145   0.5670
   3.500   0.3805   0.00884   0.00209   0.0025   0.1698   0.5705
   3.750   0.4072   0.00905   0.00223   0.0027   0.1522   0.5739
   4.000   0.4342   0.00922   0.00237   0.0029   0.1407   0.5772
   4.250   0.4608   0.00939   0.00252   0.0032   0.1277   0.5816
   4.500   0.4875   0.00957   0.00267   0.0034   0.1174   0.5861
   4.750   0.5145   0.00972   0.00281   0.0036   0.1103   0.5905
   5.000   0.5412   0.00988   0.00298   0.0038   0.1037   0.5952
   5.250   0.5682   0.01002   0.00314   0.0040   0.0980   0.6013
   5.500   0.5940   0.01027   0.00333   0.0044   0.0823   0.6079
   5.750   0.6198   0.01051   0.00354   0.0047   0.0720   0.6160
   6.000   0.6459   0.01072   0.00375   0.0050   0.0654   0.6220
   6.250   0.6717   0.01093   0.00397   0.0054   0.0598   0.6273
   6.500   0.6977   0.01113   0.00418   0.0057   0.0550   0.6319
   6.750   0.7229   0.01140   0.00443   0.0061   0.0492   0.6362
   7.000   0.7484   0.01160   0.00467   0.0066   0.0474   0.6413
   7.250   0.7737   0.01182   0.00492   0.0070   0.0459   0.6471
   7.500   0.7985   0.01205   0.00519   0.0075   0.0442   0.6548
   8.000   0.8476   0.01254   0.00579   0.0086   0.0416   0.6818
   8.250   0.8718   0.01282   0.00612   0.0091   0.0402   0.6948
   8.500   0.8956   0.01311   0.00648   0.0098   0.0392   0.7047
   8.750   0.9204   0.01331   0.00672   0.0102   0.0384   0.7131
   9.000   0.9446   0.01354   0.00700   0.0108   0.0378   0.7218
   9.250   0.9685   0.01376   0.00728   0.0114   0.0364   0.7299
   9.500   0.9915   0.01402   0.00760   0.0121   0.0349   0.7404
   9.750   1.0131   0.01429   0.00795   0.0131   0.0334   0.7551
  10.000   1.0331   0.01456   0.00836   0.0143   0.0319   0.8024
  10.250   1.0537   0.01494   0.00878   0.0153   0.0303   0.8160
  10.500   1.0745   0.01521   0.00914   0.0164   0.0296   0.8306
  10.750   1.0934   0.01539   0.00949   0.0179   0.0287   0.8681
  11.250   1.1827   0.01641   0.01068   0.0094   0.0219   1.0000
  11.500   1.2007   0.01697   0.01121   0.0106   0.0189   1.0000
  11.750   1.2182   0.01754   0.01179   0.0118   0.0165   1.0000
  12.000   1.2336   0.01820   0.01245   0.0133   0.0139   1.0000
  12.250   1.2424   0.01909   0.01332   0.0157   0.0098   1.0000
  12.500   1.2509   0.01992   0.01417   0.0180   0.0080   1.0000
  12.750   1.2593   0.02090   0.01519   0.0199   0.0066   1.0000
  13.000   1.2672   0.02212   0.01646   0.0212   0.0054   1.0000
  13.250   1.2789   0.02322   0.01761   0.0218   0.0052   1.0000
  13.500   1.2893   0.02456   0.01902   0.0223   0.0047   1.0000
  13.750   1.2991   0.02604   0.02056   0.0225   0.0043   1.0000
  14.000   1.3076   0.02779   0.02238   0.0224   0.0040   1.0000
  14.250   1.3167   0.02950   0.02416   0.0223   0.0039   1.0000
  14.500   1.3233   0.03149   0.02622   0.0221   0.0036   1.0000
  14.750   1.3315   0.03335   0.02814   0.0219   0.0035   1.0000
  15.000   1.3373   0.03549   0.03036   0.0215   0.0035   1.0000
  15.250   1.3424   0.03769   0.03263   0.0212   0.0033   1.0000
  15.500   1.3449   0.04018   0.03520   0.0207   0.0031   1.0000
  15.750   1.3469   0.04276   0.03787   0.0202   0.0031   1.0000
  16.000   1.3472   0.04553   0.04072   0.0196   0.0030   1.0000
  16.250   1.3468   0.04844   0.04371   0.0189   0.0029   1.0000
  16.500   1.3439   0.05169   0.04706   0.0180   0.0029   1.0000
  16.750   1.3399   0.05512   0.05058   0.0170   0.0028   1.0000
  17.000   1.3363   0.05870   0.05424   0.0158   0.0028   1.0000
  17.250   1.3303   0.06270   0.05835   0.0143   0.0028   1.0000
  17.500   1.3233   0.06700   0.06275   0.0126   0.0028   1.0000
  17.750   1.3131   0.07187   0.06773   0.0106   0.0027   1.0000
  18.000   1.3035   0.07678   0.07274   0.0085   0.0027   1.0000
  18.250   1.2882   0.08270   0.07878   0.0058   0.0026   1.0000
  18.500   1.2740   0.08857   0.08477   0.0031   0.0026   1.0000
  18.750   1.2544   0.09547   0.09181  -0.0002   0.0026   1.0000
  19.000   1.2363   0.10233   0.09878  -0.0035   0.0026   1.0000
  19.250   1.2135   0.11008   0.10667  -0.0073   0.0026   1.0000
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