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FX 63-143 AIRFOIL (fx63143-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 63-143 AIRFOIL (fx63143-il)
Reynolds number: 100,000
Max Cl/Cd: 49.81 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63143-il-100000-n5.txt
Download as CSV file: xf-fx63143-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-143 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.3737   0.10363   0.09871  -0.0399   1.0000   0.0211
 -10.500  -0.3724   0.09988   0.09500  -0.0410   1.0000   0.0203
 -10.000  -0.3847   0.08828   0.08354  -0.0465   1.0000   0.0182
  -9.750  -0.3883   0.08373   0.07906  -0.0486   1.0000   0.0179
  -9.500  -0.3963   0.07774   0.07313  -0.0522   1.0000   0.0175
  -9.250  -0.4130   0.07107   0.06648  -0.0566   1.0000   0.0171
  -8.750  -0.4734   0.06109   0.05635  -0.0554   1.0000   0.0159
  -8.500  -0.4920   0.05901   0.05429  -0.0518   1.0000   0.0158
  -8.250  -0.4872   0.05462   0.04970  -0.0539   0.9716   0.0156
  -8.000  -0.4775   0.04990   0.04464  -0.0561   0.9419   0.0154
  -7.750  -0.4595   0.04516   0.03944  -0.0587   0.9202   0.0151
  -7.500  -0.4382   0.04061   0.03433  -0.0608   0.9007   0.0149
  -7.250  -0.4148   0.03665   0.02976  -0.0621   0.8810   0.0148
  -7.000  -0.3897   0.03336   0.02588  -0.0629   0.8619   0.0148
  -6.750  -0.3632   0.03074   0.02273  -0.0632   0.8439   0.0148
  -6.500  -0.3367   0.02854   0.02004  -0.0632   0.8264   0.0150
  -6.250  -0.3100   0.02673   0.01780  -0.0630   0.8100   0.0154
  -6.000  -0.2831   0.02523   0.01586  -0.0626   0.7947   0.0160
  -5.750  -0.2585   0.02404   0.01454  -0.0622   0.7804   0.0165
  -5.500  -0.2349   0.02296   0.01323  -0.0615   0.7670   0.0183
  -5.250  -0.2129   0.02197   0.01216  -0.0608   0.7550   0.0197
  -5.000  -0.1909   0.02106   0.01114  -0.0600   0.7447   0.0220
  -4.750  -0.1688   0.02042   0.01048  -0.0592   0.7343   0.0244
  -4.500  -0.1444   0.01999   0.00993  -0.0587   0.7259   0.0267
  -4.250  -0.1207   0.01962   0.00942  -0.0580   0.7164   0.0314
  -4.000  -0.0958   0.01930   0.00885  -0.0574   0.7086   0.0369
  -3.750  -0.0724   0.01892   0.00835  -0.0567   0.6996   0.0395
  -3.500  -0.0475   0.01864   0.00789  -0.0561   0.6924   0.0425
  -3.000   0.0013   0.01808   0.00729  -0.0551   0.6777   0.0591
  -2.750   0.0268   0.01798   0.00707  -0.0547   0.6710   0.0710
  -2.500   0.0511   0.01772   0.00686  -0.0543   0.6644   0.0963
  -2.250   0.0769   0.01755   0.00665  -0.0539   0.6589   0.1177
  -2.000   0.0985   0.01701   0.00652  -0.0532   0.6519   0.2434
  -1.750   0.1168   0.01614   0.00642  -0.0520   0.6458   0.4285
  -1.500   0.1338   0.01550   0.00655  -0.0496   0.6406   0.6048
  -1.250   0.1597   0.01563   0.00719  -0.0477   0.6337   0.7282
  -1.000   0.1885   0.01585   0.00733  -0.0472   0.6277   0.7648
  -0.750   0.2154   0.01608   0.00749  -0.0466   0.6222   0.7943
  -0.500   0.2406   0.01636   0.00772  -0.0457   0.6163   0.8201
  -0.250   0.2627   0.01661   0.00787  -0.0443   0.6115   0.8441
   0.000   0.2891   0.01696   0.00809  -0.0434   0.6075   0.8658
   0.250   0.3131   0.01729   0.00840  -0.0423   0.6018   0.8844
   0.500   0.3422   0.01760   0.00864  -0.0421   0.5964   0.9035
   0.750   0.3766   0.01780   0.00872  -0.0430   0.5917   0.9173
   1.000   0.4071   0.01796   0.00886  -0.0435   0.5854   0.9296
   1.250   0.4761   0.01807   0.00888  -0.0513   0.5784   0.9503
   1.500   0.5291   0.01804   0.00875  -0.0564   0.5726   0.9632
   1.750   0.5579   0.01808   0.00880  -0.0570   0.5661   0.9699
   2.000   0.5947   0.01802   0.00866  -0.0592   0.5606   0.9740
   2.250   0.6278   0.01800   0.00860  -0.0606   0.5540   0.9792
   2.500   0.6593   0.01798   0.00857  -0.0618   0.5467   0.9841
   2.750   0.6931   0.01791   0.00842  -0.0633   0.5396   0.9879
   3.000   0.7220   0.01792   0.00845  -0.0640   0.5305   0.9921
   3.250   0.7525   0.01787   0.00835  -0.0649   0.5219   0.9956
   3.500   0.7835   0.01784   0.00835  -0.0660   0.5111   0.9999
   3.750   0.8016   0.01793   0.00846  -0.0644   0.5028   1.0000
   4.000   0.8196   0.01802   0.00856  -0.0628   0.4948   1.0000
   4.250   0.8376   0.01813   0.00871  -0.0612   0.4878   1.0000
   4.500   0.8553   0.01831   0.00895  -0.0596   0.4813   1.0000
   4.750   0.8738   0.01843   0.00908  -0.0581   0.4757   1.0000
   5.000   0.8906   0.01863   0.00937  -0.0563   0.4691   1.0000
   5.250   0.9073   0.01883   0.00965  -0.0545   0.4628   1.0000
   5.500   0.9250   0.01899   0.00984  -0.0528   0.4575   1.0000
   5.750   0.9402   0.01925   0.01023  -0.0508   0.4511   1.0000
   6.000   0.9557   0.01947   0.01055  -0.0488   0.4449   1.0000
   6.250   0.9718   0.01966   0.01079  -0.0468   0.4393   1.0000
   6.500   0.9852   0.01994   0.01120  -0.0445   0.4323   1.0000
   6.750   0.9996   0.02013   0.01145  -0.0422   0.4259   1.0000
   7.000   1.0126   0.02039   0.01183  -0.0397   0.4192   1.0000
   7.250   1.0249   0.02065   0.01219  -0.0372   0.4126   1.0000
   7.500   1.0385   0.02085   0.01243  -0.0347   0.4070   1.0000
   7.750   1.0480   0.02122   0.01297  -0.0318   0.4001   1.0000
   8.000   1.0588   0.02152   0.01339  -0.0290   0.3935   1.0000
   8.250   1.0701   0.02185   0.01384  -0.0265   0.3864   1.0000
   8.500   1.0810   0.02223   0.01438  -0.0239   0.3780   1.0000
   8.750   1.0940   0.02260   0.01487  -0.0218   0.3701   1.0000
   9.000   1.1067   0.02298   0.01536  -0.0197   0.3608   1.0000
   9.250   1.1176   0.02342   0.01589  -0.0174   0.3503   1.0000
   9.500   1.1250   0.02394   0.01646  -0.0147   0.3361   1.0000
   9.750   1.1294   0.02471   0.01732  -0.0120   0.3163   1.0000
  10.000   1.1340   0.02557   0.01817  -0.0095   0.2975   1.0000
  10.250   1.1368   0.02668   0.01925  -0.0072   0.2805   1.0000
  10.500   1.1386   0.02811   0.02076  -0.0054   0.2577   1.0000
  10.750   1.1330   0.03009   0.02263  -0.0035   0.2354   1.0000
  11.000   1.1277   0.03239   0.02489  -0.0022   0.2160   1.0000
  11.250   1.1212   0.03508   0.02756  -0.0013   0.1871   1.0000
  11.500   1.1096   0.03838   0.03073  -0.0007   0.1708   1.0000
  11.750   1.1043   0.04137   0.03375  -0.0005   0.1441   1.0000
  12.000   1.0913   0.04519   0.03745  -0.0004   0.1328   1.0000
  12.250   1.0854   0.04847   0.04074  -0.0005   0.1217   1.0000
  12.500   1.0840   0.05138   0.04377  -0.0006   0.1031   1.0000
  12.750   1.0745   0.05522   0.04754  -0.0010   0.0956   1.0000
  13.000   1.0660   0.05908   0.05136  -0.0016   0.0900   1.0000
  13.250   1.0618   0.06259   0.05493  -0.0022   0.0842   1.0000
  13.500   1.0625   0.06564   0.05817  -0.0027   0.0747   1.0000
  13.750   1.0611   0.06905   0.06166  -0.0035   0.0657   1.0000
  14.000   1.0552   0.07310   0.06566  -0.0046   0.0612   1.0000
  14.250   1.0498   0.07716   0.06975  -0.0057   0.0577   1.0000
  14.500   1.0435   0.08136   0.07391  -0.0069   0.0549   1.0000
  14.750   1.0440   0.08466   0.07738  -0.0076   0.0510   1.0000
  15.000   1.0448   0.08784   0.08061  -0.0083   0.0476   1.0000
  15.250   1.0499   0.09053   0.08346  -0.0088   0.0442   1.0000
  15.500   1.0560   0.09309   0.08617  -0.0093   0.0410   1.0000
  15.750   1.0613   0.09576   0.08891  -0.0099   0.0390   1.0000
  16.000   1.0703   0.09785   0.09114  -0.0102   0.0372   1.0000
  16.250   1.0794   0.09998   0.09340  -0.0104   0.0357   1.0000
  16.500   1.0865   0.10249   0.09604  -0.0111   0.0343   1.0000
  16.750   1.0903   0.10565   0.09931  -0.0123   0.0329   1.0000
  17.000   1.0928   0.10903   0.10277  -0.0138   0.0317   1.0000
  17.250   1.0970   0.11206   0.10588  -0.0149   0.0304   1.0000
  17.500   1.0996   0.11560   0.10966  -0.0162   0.0293   1.0000
  17.750   1.0983   0.11995   0.11425  -0.0182   0.0281   1.0000
  18.000   1.0946   0.12478   0.11927  -0.0208   0.0269   1.0000
  18.250   1.0903   0.12980   0.12443  -0.0236   0.0258   1.0000
  18.500   1.0865   0.13473   0.12947  -0.0267   0.0247   1.0000
  18.750   1.0845   0.13927   0.13406  -0.0295   0.0236   1.0000
  19.000   1.0809   0.14412   0.13899  -0.0323   0.0226   1.0000
  19.250   1.0700   0.15114   0.14625  -0.0367   0.0222   1.0000
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