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WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 75-141 (fx75141-il)
Reynolds number: 100,000
Max Cl/Cd: 53.45 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75141-il-100000-n5.txt
Download as CSV file: xf-fx75141-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 75-141                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.3944   0.09460   0.08963  -0.0668   0.9763   0.0360
 -11.000  -0.4032   0.08508   0.08010  -0.0739   0.9660   0.0359
 -10.750  -0.4254   0.07195   0.06689  -0.0858   0.9566   0.0355
 -10.500  -0.4524   0.06025   0.05491  -0.0995   0.9465   0.0351
 -10.250  -0.4702   0.05245   0.04671  -0.1093   0.9367   0.0352
 -10.000  -0.4809   0.04723   0.04104  -0.1144   0.9264   0.0354
  -9.750  -0.4843   0.04294   0.03621  -0.1168   0.9186   0.0358
  -9.500  -0.4776   0.03973   0.03257  -0.1178   0.9127   0.0363
  -9.250  -0.4592   0.03764   0.03031  -0.1190   0.9092   0.0372
  -9.000  -0.4423   0.03611   0.02861  -0.1193   0.9051   0.0384
  -8.750  -0.4266   0.03463   0.02689  -0.1191   0.9003   0.0402
  -8.500  -0.4078   0.03271   0.02456  -0.1194   0.8963   0.0422
  -8.250  -0.3853   0.03075   0.02221  -0.1198   0.8933   0.0438
  -8.000  -0.3615   0.02944   0.02084  -0.1203   0.8907   0.0454
  -7.750  -0.3433   0.02861   0.01992  -0.1194   0.8865   0.0476
  -7.500  -0.3215   0.02761   0.01870  -0.1191   0.8828   0.0507
  -7.250  -0.2974   0.02649   0.01742  -0.1190   0.8799   0.0534
  -7.000  -0.2717   0.02560   0.01652  -0.1194   0.8773   0.0563
  -6.750  -0.2462   0.02487   0.01564  -0.1195   0.8746   0.0608
  -6.500  -0.2289   0.02422   0.01495  -0.1180   0.8702   0.0643
  -6.250  -0.2075   0.02362   0.01436  -0.1174   0.8665   0.0685
  -6.000  -0.1824   0.02305   0.01368  -0.1173   0.8633   0.0748
  -5.750  -0.1568   0.02239   0.01306  -0.1175   0.8607   0.0816
  -5.500  -0.1349   0.02193   0.01256  -0.1169   0.8572   0.0900
  -5.250  -0.1164   0.02159   0.01221  -0.1156   0.8527   0.0994
  -5.000  -0.0934   0.02112   0.01178  -0.1153   0.8490   0.1131
  -4.750  -0.0671   0.02061   0.01131  -0.1155   0.8459   0.1328
  -4.500  -0.0392   0.02004   0.01087  -0.1161   0.8434   0.1650
  -4.250  -0.0226   0.01970   0.01073  -0.1147   0.8383   0.2068
  -4.000  -0.0011   0.01918   0.01050  -0.1143   0.8341   0.2748
  -3.750   0.0233   0.01857   0.01038  -0.1143   0.8307   0.3813
  -3.500   0.0505   0.01835   0.01046  -0.1141   0.8280   0.4775
  -3.250   0.0694   0.01852   0.01075  -0.1123   0.8232   0.5284
  -3.000   0.0904   0.01876   0.01105  -0.1107   0.8184   0.5670
  -2.750   0.1162   0.01900   0.01129  -0.1098   0.8149   0.5982
  -2.500   0.1449   0.01922   0.01145  -0.1094   0.8122   0.6231
  -2.250   0.1641   0.01961   0.01179  -0.1076   0.8070   0.6424
  -2.000   0.1858   0.01993   0.01206  -0.1062   0.8019   0.6606
  -1.750   0.2127   0.02015   0.01220  -0.1056   0.7984   0.6767
  -1.500   0.2421   0.02028   0.01225  -0.1055   0.7958   0.6904
  -1.250   0.2570   0.02065   0.01261  -0.1031   0.7889   0.7031
  -1.000   0.2814   0.02082   0.01272  -0.1023   0.7844   0.7165
  -0.750   0.3093   0.02086   0.01272  -0.1019   0.7812   0.7261
  -0.500   0.3310   0.02102   0.01283  -0.1009   0.7759   0.7345
  -0.250   0.3511   0.02117   0.01297  -0.0995   0.7698   0.7420
   0.000   0.3805   0.02114   0.01287  -0.0998   0.7662   0.7496
   0.250   0.4114   0.02105   0.01274  -0.1001   0.7636   0.7560
   0.500   0.4239   0.02141   0.01312  -0.0978   0.7548   0.7639
   0.750   0.4507   0.02137   0.01307  -0.0974   0.7507   0.7698
   1.000   0.4834   0.02126   0.01291  -0.0982   0.7480   0.7769
   1.250   0.4937   0.02161   0.01332  -0.0954   0.7389   0.7830
   1.500   0.5216   0.02156   0.01326  -0.0953   0.7347   0.7896
   1.750   0.5541   0.02140   0.01309  -0.0960   0.7319   0.7958
   2.000   0.5634   0.02179   0.01355  -0.0930   0.7221   0.8022
   2.250   0.5938   0.02169   0.01345  -0.0934   0.7183   0.8089
   2.750   0.6344   0.02193   0.01377  -0.0909   0.7050   0.8212
   3.000   0.6665   0.02172   0.01360  -0.0915   0.7017   0.8271
   3.250   0.6783   0.02209   0.01404  -0.0890   0.6923   0.8337
   3.500   0.7084   0.02194   0.01393  -0.0893   0.6879   0.8402
   3.750   0.7269   0.02208   0.01414  -0.0877   0.6806   0.8464
   4.000   0.7512   0.02205   0.01418  -0.0871   0.6742   0.8532
   4.250   0.7856   0.02166   0.01385  -0.0878   0.6707   0.8593
   4.500   0.7972   0.02198   0.01426  -0.0852   0.6601   0.8673
   4.750   0.8333   0.02144   0.01379  -0.0861   0.6557   0.8739
   5.000   0.8485   0.02149   0.01393  -0.0839   0.6440   0.8829
   5.250   0.8719   0.02119   0.01371  -0.0827   0.6329   0.8918
   5.500   0.9050   0.02060   0.01319  -0.0829   0.6232   0.9013
   5.750   0.9293   0.02044   0.01313  -0.0821   0.6120   0.9135
   6.000   0.9555   0.02038   0.01319  -0.0818   0.6005   0.9303
   6.250   0.9877   0.02013   0.01304  -0.0824   0.5890   1.0000
   6.500   1.0204   0.02002   0.01297  -0.0832   0.5767   1.0000
   6.750   1.0488   0.02004   0.01303  -0.0832   0.5622   1.0000
   7.000   1.0720   0.02023   0.01324  -0.0826   0.5455   1.0000
   7.250   1.0907   0.02052   0.01356  -0.0812   0.5255   1.0000
   7.500   1.1102   0.02077   0.01376  -0.0798   0.5006   1.0000
   7.750   1.1232   0.02126   0.01418  -0.0775   0.4714   1.0000
   8.000   1.1350   0.02185   0.01466  -0.0752   0.4385   1.0000
   8.250   1.1440   0.02264   0.01531  -0.0727   0.4018   1.0000
   8.500   1.1502   0.02364   0.01611  -0.0701   0.3617   1.0000
   8.750   1.1539   0.02489   0.01712  -0.0674   0.3224   1.0000
   9.000   1.1565   0.02633   0.01833  -0.0648   0.2866   1.0000
   9.250   1.1594   0.02787   0.01968  -0.0625   0.2550   1.0000
   9.500   1.1631   0.02944   0.02111  -0.0604   0.2277   1.0000
   9.750   1.1668   0.03109   0.02264  -0.0585   0.2035   1.0000
  10.000   1.1721   0.03269   0.02415  -0.0568   0.1813   1.0000
  10.250   1.1771   0.03436   0.02575  -0.0551   0.1614   1.0000
  10.500   1.1815   0.03613   0.02744  -0.0536   0.1429   1.0000
  10.750   1.1873   0.03785   0.02912  -0.0522   0.1258   1.0000
  11.000   1.1923   0.03967   0.03090  -0.0508   0.1115   1.0000
  11.250   1.1966   0.04160   0.03280  -0.0495   0.0996   1.0000
  11.500   1.2010   0.04358   0.03476  -0.0483   0.0900   1.0000
  11.750   1.2065   0.04551   0.03673  -0.0472   0.0823   1.0000
  12.000   1.2091   0.04772   0.03891  -0.0461   0.0768   1.0000
  12.250   1.2156   0.04966   0.04095  -0.0452   0.0714   1.0000
  12.500   1.2193   0.05189   0.04321  -0.0443   0.0669   1.0000
  12.750   1.2235   0.05415   0.04553  -0.0435   0.0633   1.0000
  13.000   1.2299   0.05625   0.04775  -0.0428   0.0598   1.0000
  13.250   1.2343   0.05858   0.05014  -0.0422   0.0568   1.0000
  13.500   1.2377   0.06107   0.05262  -0.0417   0.0543   1.0000
  13.750   1.2452   0.06323   0.05496  -0.0412   0.0518   1.0000
  14.000   1.2508   0.06562   0.05746  -0.0408   0.0492   1.0000
  14.250   1.2554   0.06813   0.06004  -0.0406   0.0473   1.0000
  14.500   1.2600   0.07067   0.06257  -0.0403   0.0455   1.0000
  14.750   1.2665   0.07316   0.06529  -0.0400   0.0438   1.0000
  15.000   1.2718   0.07582   0.06813  -0.0399   0.0421   1.0000
  15.250   1.2758   0.07863   0.07108  -0.0400   0.0406   1.0000
  15.500   1.2787   0.08158   0.07410  -0.0402   0.0392   1.0000
  15.750   1.2825   0.08439   0.07693  -0.0405   0.0379   1.0000
  16.000   1.2839   0.08774   0.08047  -0.0409   0.0368   1.0000
  16.250   1.2827   0.09157   0.08457  -0.0415   0.0358   1.0000
  16.500   1.2803   0.09560   0.08885  -0.0425   0.0349   1.0000
  16.750   1.2763   0.09992   0.09338  -0.0437   0.0340   1.0000
  17.000   1.2715   0.10438   0.09803  -0.0453   0.0332   1.0000
  17.250   1.2668   0.10885   0.10265  -0.0470   0.0325   1.0000
  17.500   1.2628   0.11326   0.10718  -0.0489   0.0318   1.0000
  17.750   1.2609   0.11731   0.11130  -0.0506   0.0311   1.0000
  18.000   1.2538   0.12249   0.11661  -0.0531   0.0306   1.0000
  18.250   1.2365   0.12991   0.12431  -0.0573   0.0304   1.0000
  18.500   1.2171   0.13813   0.13281  -0.0623   0.0302   1.0000
  18.750   1.1944   0.14757   0.14250  -0.0684   0.0301   1.0000
  19.000   1.1663   0.15903   0.15420  -0.0762   0.0302   1.0000
  19.250   1.1265   0.17497   0.17033  -0.0871   0.0305   1.0000
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