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WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)
Reynolds number: 50,000
Max Cl/Cd: 29.01 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx62k131-il-50000-n5.txt
Download as CSV file: xf-fx62k131-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 62-K-131 AIRFOIL                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -7.750  -0.4030   0.09444   0.08850  -0.0637   0.9731   0.0508
  -7.500  -0.3907   0.09128   0.08533  -0.0618   0.9697   0.0493
  -7.250  -0.3866   0.08720   0.08124  -0.0642   0.9646   0.0481
  -7.000  -0.3841   0.08263   0.07665  -0.0680   0.9593   0.0468
  -6.750  -0.3840   0.07820   0.07215  -0.0711   0.9528   0.0456
  -6.500  -0.3757   0.07295   0.06672  -0.0762   0.9480   0.0439
  -6.250  -0.3743   0.06865   0.06223  -0.0783   0.9415   0.0425
  -6.000  -0.3590   0.06295   0.05607  -0.0833   0.9368   0.0401
  -5.750  -0.3353   0.05884   0.05109  -0.0873   0.9321   0.0377
  -5.500  -0.3161   0.05494   0.04692  -0.0890   0.9279   0.0373
  -5.250  -0.2877   0.05106   0.04261  -0.0921   0.9246   0.0369
  -5.000  -0.2530   0.04742   0.03843  -0.0956   0.9221   0.0368
  -4.750  -0.2221   0.04455   0.03503  -0.0976   0.9189   0.0370
  -4.500  -0.1922   0.04233   0.03221  -0.0988   0.9150   0.0377
  -4.250  -0.1614   0.03990   0.02964  -0.1007   0.9120   0.0412
  -4.000  -0.1281   0.03832   0.02777  -0.1019   0.9093   0.0449
  -3.750  -0.0971   0.03695   0.02610  -0.1017   0.9067   0.0471
  -3.500  -0.0786   0.03614   0.02508  -0.0995   0.9016   0.0492
  -3.250  -0.0534   0.03519   0.02406  -0.0987   0.8978   0.0543
  -3.000  -0.0213   0.03443   0.02309  -0.0996   0.8947   0.0644
  -2.750   0.0085   0.03352   0.02205  -0.1007   0.8906   0.0766
  -2.250   0.0495   0.03136   0.02299  -0.0971   0.8825   0.6909
  -2.000   0.0395   0.03283   0.02446  -0.0862   0.8757   0.7740
  -1.750   0.0232   0.03344   0.02507  -0.0743   0.8687   0.8249
  -1.500   0.0207   0.03348   0.02496  -0.0665   0.8631   0.8624
  -1.250   0.0393   0.03346   0.02462  -0.0652   0.8569   0.8752
  -1.000   0.0681   0.03342   0.02419  -0.0658   0.8528   0.8866
  -0.750   0.0871   0.03347   0.02400  -0.0649   0.8465   0.8976
  -0.500   0.1105   0.03342   0.02372  -0.0646   0.8411   0.9079
  -0.250   0.1422   0.03339   0.02343  -0.0657   0.8374   0.9172
   0.000   0.1577   0.03354   0.02344  -0.0646   0.8296   0.9268
   0.250   0.1883   0.03357   0.02324  -0.0658   0.8251   0.9352
   0.500   0.2099   0.03373   0.02327  -0.0657   0.8183   0.9436
   0.750   0.2387   0.03388   0.02328  -0.0667   0.8127   0.9514
   1.000   0.2701   0.03401   0.02326  -0.0682   0.8078   0.9588
   1.250   0.2936   0.03431   0.02348  -0.0687   0.8002   0.9668
   1.500   0.3310   0.03445   0.02352  -0.0711   0.7961   0.9740
   1.750   0.3529   0.03488   0.02391  -0.0716   0.7874   0.9834
   2.250   0.4081   0.03554   0.02449  -0.0739   0.7732   0.9999
   2.500   0.4455   0.03584   0.02475  -0.0764   0.7687   0.9999
   2.750   0.4673   0.03653   0.02545  -0.0770   0.7596   0.9999
   3.000   0.5048   0.03681   0.02573  -0.0794   0.7549   0.9999
   3.250   0.5267   0.03754   0.02649  -0.0799   0.7454   0.9999
   3.500   0.5651   0.03775   0.02672  -0.0823   0.7407   0.9999
   3.750   0.5864   0.03853   0.02756  -0.0827   0.7305   0.9999
   4.000   0.6262   0.03860   0.02773  -0.0851   0.7262   0.9999
   4.250   0.6467   0.03943   0.02864  -0.0854   0.7153   0.9999
   4.500   0.6720   0.04008   0.02939  -0.0862   0.7060   0.9999
   4.750   0.7083   0.04022   0.02969  -0.0880   0.7000   0.9999
   5.000   0.7299   0.04104   0.03063  -0.0884   0.6892   0.9999
   5.500   0.7901   0.04177   0.03166  -0.0905   0.6730   0.9999
   5.750   0.8126   0.04255   0.03266  -0.0909   0.6620   0.9999
   6.250   0.8736   0.04299   0.03351  -0.0926   0.6449   0.9999
   6.500   0.8957   0.04372   0.03444  -0.0927   0.6331   0.9999
   6.750   0.9199   0.04426   0.03521  -0.0929   0.6219   0.9999
   7.000   0.9595   0.04346   0.03475  -0.0937   0.6159   0.9999
   7.250   0.9823   0.04391   0.03545  -0.0935   0.6031   0.9999
   7.500   1.0072   0.04404   0.03586  -0.0932   0.5903   0.9999
   7.750   1.0355   0.04365   0.03576  -0.0928   0.5768   0.9999
   8.000   1.0689   0.04251   0.03500  -0.0922   0.5618   0.9999
   8.250   1.0976   0.04163   0.03442  -0.0912   0.5427   0.9999
   8.500   1.1244   0.04085   0.03392  -0.0899   0.5201   0.9999
   8.750   1.1463   0.04061   0.03394  -0.0885   0.4934   0.9999
   9.000   1.1678   0.04030   0.03380  -0.0868   0.4593   0.9999
   9.250   1.1815   0.04073   0.03430  -0.0847   0.4152   0.9999
   9.500   1.1895   0.04168   0.03506  -0.0822   0.3572   0.9999
   9.750   1.1889   0.04369   0.03678  -0.0796   0.2934   0.9999
  10.000   1.1827   0.04659   0.03931  -0.0774   0.2328   0.9999
  10.250   1.1749   0.04996   0.04232  -0.0756   0.1845   0.9999
  10.500   1.1673   0.05354   0.04562  -0.0741   0.1475   0.9999
  10.750   1.1609   0.05721   0.04909  -0.0729   0.1194   0.9999
  11.000   1.1558   0.06087   0.05261  -0.0717   0.1009   0.9999
  11.250   1.1535   0.06436   0.05609  -0.0707   0.0847   0.9999
  11.500   1.1521   0.06781   0.05954  -0.0698   0.0707   0.9999
  11.750   1.1528   0.07108   0.06284  -0.0689   0.0607   0.9999
  12.000   1.1524   0.07447   0.06621  -0.0683   0.0515   0.9999
  12.250   1.1557   0.07761   0.06953  -0.0678   0.0434   0.9999
  12.500   1.1609   0.08058   0.07267  -0.0671   0.0371   0.9999
  12.750   1.1664   0.08356   0.07581  -0.0666   0.0327   0.9999
  13.000   1.1730   0.08645   0.07879  -0.0659   0.0295   0.9999
  13.250   1.1829   0.08943   0.08219  -0.0650   0.0269   0.9999
  13.500   1.1891   0.09299   0.08608  -0.0645   0.0255   0.9999
  13.750   1.1899   0.09725   0.09066  -0.0647   0.0246   0.9999
  14.000   1.1862   0.10203   0.09575  -0.0656   0.0241   0.9999
  14.250   1.1794   0.10742   0.10143  -0.0671   0.0237   0.9999
  14.500   1.1701   0.11332   0.10762  -0.0694   0.0235   0.9999
  14.750   1.1584   0.11995   0.11452  -0.0726   0.0235   0.9999
  15.000   1.1446   0.12745   0.12228  -0.0768   0.0235   0.9999
  15.250   1.1287   0.13585   0.13093  -0.0821   0.0238   0.9999
  15.500   1.1116   0.14553   0.14083  -0.0886   0.0242   0.9999
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