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WORTMANN FX 63-137 AIRFOIL (fx63137-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 63-137 AIRFOIL (fx63137-il)
Reynolds number: 50,000
Max Cl/Cd: 31.61 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63137-il-50000-n5.txt
Download as CSV file: xf-fx63137-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 63-137 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.2813   0.13470   0.12831  -0.0348   1.0000   0.1078
  -9.750  -0.2909   0.13347   0.12717  -0.0333   1.0000   0.1101
  -9.500  -0.2920   0.13081   0.12455  -0.0401   0.9940   0.1131
  -9.250  -0.2863   0.12719   0.12095  -0.0448   0.9878   0.1134
  -9.000  -0.2675   0.11788   0.11154  -0.0487   0.9840   0.0771
  -8.750  -0.2599   0.11373   0.10741  -0.0521   0.9774   0.0771
  -8.500  -0.2503   0.10942   0.10310  -0.0563   0.9718   0.0772
  -8.250  -0.2428   0.10561   0.09930  -0.0584   0.9645   0.0766
  -8.000  -0.2325   0.10140   0.09509  -0.0620   0.9589   0.0760
  -7.750  -0.2313   0.09784   0.09156  -0.0641   0.9502   0.0759
  -7.500  -0.2237   0.09351   0.08723  -0.0682   0.9440   0.0755
  -7.250  -0.2257   0.09018   0.08393  -0.0693   0.9338   0.0743
  -7.000  -0.2245   0.08578   0.07955  -0.0729   0.9253   0.0729
  -6.750  -0.2388   0.07078   0.06436  -0.0947   0.9129   0.0680
  -6.500  -0.2356   0.06585   0.05929  -0.0996   0.9030   0.0677
  -6.250  -0.2098   0.05811   0.05104  -0.1122   0.8976   0.0677
  -6.000  -0.1912   0.05451   0.04721  -0.1161   0.8906   0.0690
  -5.750  -0.1615   0.05110   0.04351  -0.1210   0.8853   0.0708
  -5.500  -0.1177   0.04662   0.03843  -0.1291   0.8820   0.0716
  -5.250  -0.0776   0.04342   0.03467  -0.1345   0.8780   0.0725
  -5.000  -0.0469   0.04130   0.03213  -0.1371   0.8717   0.0736
  -4.750  -0.0072   0.03923   0.02960  -0.1406   0.8676   0.0754
  -4.500   0.0347   0.03752   0.02748  -0.1438   0.8644   0.0784
  -4.250   0.0584   0.03676   0.02669  -0.1438   0.8570   0.0815
  -4.000   0.0915   0.03578   0.02553  -0.1449   0.8515   0.0857
  -3.750   0.1293   0.03470   0.02430  -0.1464   0.8477   0.0903
  -3.500   0.1521   0.03426   0.02380  -0.1460   0.8401   0.0954
  -3.250   0.1852   0.03357   0.02307  -0.1474   0.8349   0.1056
  -3.000   0.2269   0.03275   0.02224  -0.1505   0.8315   0.1269
  -2.750   0.2645   0.03203   0.02167  -0.1534   0.8264   0.1568
  -2.500   0.3120   0.03084   0.02127  -0.1591   0.8213   0.2702
  -2.250   0.3467   0.03091   0.02181  -0.1599   0.8164   0.4243
  -2.000   0.3817   0.03129   0.02217  -0.1598   0.8127   0.5006
  -1.750   0.3921   0.03215   0.02303  -0.1565   0.8019   0.5368
  -1.500   0.4220   0.03242   0.02323  -0.1553   0.7973   0.5786
  -1.250   0.4319   0.03306   0.02386  -0.1517   0.7871   0.6011
  -1.000   0.4630   0.03304   0.02372  -0.1513   0.7819   0.6244
  -0.750   0.4857   0.03334   0.02390  -0.1505   0.7743   0.6387
  -0.500   0.5126   0.03354   0.02398  -0.1505   0.7676   0.6527
  -0.250   0.5501   0.03340   0.02369  -0.1519   0.7638   0.6679
   0.000   0.5663   0.03404   0.02426  -0.1507   0.7540   0.6806
   0.250   0.5994   0.03391   0.02403  -0.1512   0.7488   0.6925
   0.750   0.6557   0.03425   0.02420  -0.1517   0.7336   0.7163
   1.000   0.6953   0.03382   0.02369  -0.1530   0.7298   0.7291
   1.250   0.7060   0.03456   0.02445  -0.1508   0.7179   0.7398
   1.500   0.7458   0.03421   0.02402  -0.1523   0.7138   0.7534
   1.750   0.7567   0.03510   0.02493  -0.1504   0.7026   0.7648
   2.000   0.7915   0.03489   0.02469  -0.1512   0.6980   0.7772
   2.250   0.8038   0.03579   0.02562  -0.1495   0.6878   0.7891
   2.500   0.8366   0.03568   0.02551  -0.1501   0.6825   0.8033
   3.000   0.8818   0.03616   0.02606  -0.1486   0.6665   0.8347
   3.500   0.9201   0.03648   0.02649  -0.1457   0.6497   0.8772
   4.000   0.9646   0.03689   0.02701  -0.1444   0.6326   1.0000
   4.500   1.0309   0.03773   0.02783  -0.1474   0.6163   1.0000
   5.000   1.0905   0.03868   0.02881  -0.1490   0.5996   1.0000
   5.500   1.1460   0.03953   0.02972  -0.1495   0.5822   1.0000
   5.750   1.1590   0.04084   0.03107  -0.1483   0.5706   1.0000
   6.000   1.2023   0.04005   0.03030  -0.1496   0.5645   1.0000
   6.250   1.2122   0.04144   0.03178  -0.1480   0.5523   1.0000
   6.500   1.2637   0.03998   0.03033  -0.1498   0.5467   1.0000
   6.750   1.2677   0.04166   0.03210  -0.1475   0.5336   1.0000
   7.000   1.2836   0.04259   0.03312  -0.1462   0.5225   1.0000
   7.250   1.3214   0.04193   0.03250  -0.1467   0.5141   1.0000
   7.500   1.3247   0.04374   0.03442  -0.1444   0.5014   1.0000
   7.750   1.3463   0.04424   0.03502  -0.1436   0.4912   1.0000
   8.000   1.3795   0.04378   0.03461  -0.1434   0.4816   1.0000
   8.250   1.3851   0.04538   0.03633  -0.1414   0.4686   1.0000
   8.500   1.3992   0.04626   0.03728  -0.1398   0.4556   1.0000
   8.750   1.4142   0.04691   0.03801  -0.1382   0.4415   1.0000
   9.000   1.4286   0.04753   0.03867  -0.1365   0.4264   1.0000
   9.250   1.4445   0.04802   0.03917  -0.1350   0.4110   1.0000
   9.500   1.4555   0.04905   0.04022  -0.1333   0.3955   1.0000
   9.750   1.4597   0.05085   0.04212  -0.1314   0.3802   1.0000
  10.000   1.4632   0.05283   0.04421  -0.1298   0.3656   1.0000
  10.250   1.4688   0.05467   0.04612  -0.1283   0.3512   1.0000
  10.500   1.4718   0.05684   0.04836  -0.1269   0.3360   1.0000
  10.750   1.4707   0.05956   0.05119  -0.1256   0.3201   1.0000
  11.000   1.4716   0.06211   0.05383  -0.1244   0.3045   1.0000
  11.250   1.4756   0.06434   0.05608  -0.1234   0.2896   1.0000
  11.500   1.4773   0.06700   0.05881  -0.1225   0.2751   1.0000
  11.750   1.4758   0.07020   0.06210  -0.1218   0.2601   1.0000
  12.000   1.4757   0.07326   0.06522  -0.1212   0.2457   1.0000
  12.250   1.4778   0.07604   0.06801  -0.1205   0.2324   1.0000
  12.500   1.4787   0.07908   0.07105  -0.1200   0.2192   1.0000
  12.750   1.4763   0.08279   0.07482  -0.1199   0.2056   1.0000
  13.000   1.4742   0.08648   0.07855  -0.1199   0.1929   1.0000
  13.250   1.4743   0.08982   0.08185  -0.1198   0.1818   1.0000
  13.500   1.4726   0.09369   0.08576  -0.1200   0.1708   1.0000
  13.750   1.4718   0.09749   0.08962  -0.1204   0.1610   1.0000
  14.000   1.4730   0.10091   0.09302  -0.1207   0.1525   1.0000
  14.250   1.4724   0.10494   0.09723  -0.1214   0.1449   1.0000
  14.500   1.4797   0.10738   0.09958  -0.1213   0.1394   1.0000
  14.750   1.4817   0.11110   0.10351  -0.1220   0.1342   1.0000
  15.000   1.4893   0.11368   0.10613  -0.1222   0.1298   1.0000
  15.250   1.5034   0.11509   0.10750  -0.1217   0.1261   1.0000
  15.500   1.4995   0.12009   0.11285  -0.1234   0.1228   1.0000
  15.750   1.4971   0.12476   0.11776  -0.1250   0.1195   1.0000
  16.000   1.5011   0.12811   0.12123  -0.1260   0.1165   1.0000
  16.250   1.5150   0.12950   0.12260  -0.1258   0.1135   1.0000
  16.500   1.4939   0.13808   0.13158  -0.1304   0.1116   1.0000
  16.750   1.4655   0.14870   0.14255  -0.1366   0.1098   1.0000
  17.000   1.4080   0.16764   0.16179  -0.1491   0.1079   1.0000
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