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WORTMANN FX 63-137 AIRFOIL (fx63137-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 63-137 AIRFOIL (fx63137-il)
Reynolds number: 500,000
Max Cl/Cd: 103.57 at α=1.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63137-il-500000-n5.txt
Download as CSV file: xf-fx63137-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.5402   0.04129   0.03799  -0.1209   0.9491   0.0065
 -11.750  -0.5411   0.03471   0.03116  -0.1304   0.9350   0.0064
 -11.500  -0.5168   0.02925   0.02542  -0.1423   0.9248   0.0065
 -11.250  -0.4778   0.02514   0.02102  -0.1542   0.9161   0.0067
 -11.000  -0.4311   0.02252   0.01814  -0.1639   0.9091   0.0068
 -10.750  -0.3891   0.02067   0.01606  -0.1705   0.9000   0.0069
 -10.500  -0.3505   0.01927   0.01444  -0.1752   0.8901   0.0072
 -10.000  -0.2838   0.01734   0.01219  -0.1807   0.8690   0.0076
  -9.750  -0.2533   0.01667   0.01140  -0.1823   0.8594   0.0080
  -9.500  -0.2240   0.01637   0.01108  -0.1832   0.8500   0.0088
  -9.250  -0.1950   0.01637   0.01111  -0.1836   0.8417   0.0094
  -9.000  -0.1663   0.01577   0.01034  -0.1845   0.8333   0.0118
  -8.750  -0.1376   0.01522   0.00962  -0.1854   0.8259   0.0132
  -8.500  -0.1091   0.01483   0.00909  -0.1859   0.8181   0.0144
  -8.250  -0.0804   0.01457   0.00869  -0.1864   0.8112   0.0151
  -8.000  -0.0517   0.01418   0.00824  -0.1870   0.8043   0.0156
  -7.750  -0.0227   0.01386   0.00782  -0.1877   0.7978   0.0161
  -7.500   0.0064   0.01355   0.00743  -0.1882   0.7917   0.0167
  -7.250   0.0354   0.01326   0.00705  -0.1888   0.7851   0.0172
  -7.000   0.0647   0.01301   0.00670  -0.1893   0.7787   0.0177
  -6.750   0.0935   0.01281   0.00642  -0.1896   0.7723   0.0183
  -6.500   0.1238   0.01237   0.00593  -0.1906   0.7665   0.0191
  -6.250   0.1539   0.01209   0.00559  -0.1913   0.7617   0.0199
  -6.000   0.1839   0.01182   0.00529  -0.1920   0.7566   0.0206
  -5.750   0.2138   0.01159   0.00499  -0.1926   0.7510   0.0212
  -5.500   0.2438   0.01139   0.00470  -0.1932   0.7455   0.0215
  -5.250   0.2741   0.01115   0.00442  -0.1938   0.7397   0.0218
  -5.000   0.3044   0.01093   0.00416  -0.1944   0.7337   0.0223
  -4.750   0.3346   0.01076   0.00392  -0.1950   0.7284   0.0227
  -4.500   0.3649   0.01058   0.00372  -0.1956   0.7230   0.0235
  -4.250   0.3949   0.01044   0.00354  -0.1961   0.7168   0.0246
  -4.000   0.4248   0.01032   0.00338  -0.1966   0.7104   0.0259
  -3.750   0.4546   0.01019   0.00325  -0.1970   0.7028   0.0271
  -3.500   0.4840   0.01011   0.00312  -0.1974   0.6952   0.0285
  -3.250   0.5136   0.01002   0.00301  -0.1977   0.6873   0.0323
  -3.000   0.5425   0.00998   0.00290  -0.1979   0.6791   0.0362
  -2.750   0.5717   0.00993   0.00280  -0.1981   0.6703   0.0397
  -2.500   0.6008   0.00989   0.00270  -0.1984   0.6616   0.0438
  -2.250   0.6300   0.00984   0.00264  -0.1986   0.6510   0.0483
  -2.000   0.6592   0.00979   0.00258  -0.1989   0.6402   0.0618
  -1.750   0.6875   0.00981   0.00254  -0.1990   0.6286   0.0703
  -1.500   0.7173   0.00973   0.00250  -0.1995   0.6189   0.0944
  -1.250   0.7476   0.00964   0.00247  -0.2002   0.6109   0.1418
  -1.000   0.7787   0.00950   0.00246  -0.2010   0.6032   0.2010
  -0.750   0.8098   0.00937   0.00247  -0.2020   0.5955   0.2733
  -0.500   0.8413   0.00923   0.00253  -0.2030   0.5867   0.3539
  -0.250   0.8709   0.00922   0.00263  -0.2034   0.5780   0.4114
   0.000   0.8997   0.00926   0.00272  -0.2036   0.5680   0.4475
   0.250   0.9275   0.00936   0.00281  -0.2036   0.5586   0.4673
   0.500   0.9549   0.00948   0.00291  -0.2034   0.5494   0.4816
   0.750   0.9823   0.00961   0.00301  -0.2033   0.5407   0.4940
   1.000   1.0087   0.00979   0.00313  -0.2030   0.5285   0.5053
   1.250   1.0347   0.00999   0.00327  -0.2026   0.5079   0.5150
   1.500   1.0590   0.01029   0.00344  -0.2019   0.4833   0.5258
   1.750   1.0835   0.01059   0.00364  -0.2013   0.4634   0.5377
   2.000   1.1091   0.01083   0.00383  -0.2009   0.4430   0.5496
   2.250   1.1339   0.01111   0.00403  -0.2003   0.4242   0.5596
   2.500   1.1591   0.01137   0.00423  -0.1998   0.4119   0.5674
   2.750   1.1846   0.01160   0.00443  -0.1994   0.4003   0.5743
   3.000   1.2100   0.01184   0.00463  -0.1990   0.3866   0.5804
   3.250   1.2341   0.01216   0.00489  -0.1983   0.3668   0.5873
   3.500   1.2578   0.01250   0.00514  -0.1976   0.3521   0.5939
   3.750   1.2820   0.01280   0.00540  -0.1970   0.3390   0.5996
   4.000   1.3057   0.01312   0.00569  -0.1963   0.3214   0.6058
   4.250   1.3265   0.01364   0.00606  -0.1952   0.2946   0.6119
   4.500   1.3485   0.01407   0.00641  -0.1942   0.2777   0.6179
   4.750   1.3692   0.01456   0.00682  -0.1930   0.2514   0.6245
   5.000   1.3887   0.01513   0.00726  -0.1916   0.2319   0.6310
   5.250   1.4100   0.01554   0.00765  -0.1906   0.2214   0.6381
   5.500   1.4308   0.01596   0.00806  -0.1894   0.2060   0.6462
   5.750   1.4469   0.01657   0.00858  -0.1875   0.1850   0.6547
   6.250   1.4818   0.01755   0.00954  -0.1839   0.1662   0.6746
   6.500   1.4999   0.01800   0.01001  -0.1823   0.1515   0.6845
   6.750   1.5123   0.01880   0.01071  -0.1799   0.1342   0.6942
   7.000   1.5271   0.01945   0.01135  -0.1778   0.1256   0.7044
   7.500   1.5575   0.02074   0.01269  -0.1740   0.1009   0.7303
   7.750   1.5695   0.02161   0.01353  -0.1717   0.0933   0.7449
   8.000   1.5842   0.02232   0.01429  -0.1699   0.0880   0.7607
   8.250   1.5982   0.02308   0.01513  -0.1680   0.0831   0.7786
   8.500   1.6116   0.02391   0.01602  -0.1661   0.0788   0.8004
   8.750   1.6252   0.02470   0.01690  -0.1643   0.0687   0.8295
   9.000   1.6261   0.02552   0.01784  -0.1602   0.0645   0.9308
   9.250   1.6343   0.02673   0.01904  -0.1580   0.0593   1.0000
   9.500   1.6457   0.02788   0.02022  -0.1563   0.0573   1.0000
   9.750   1.6564   0.02912   0.02149  -0.1546   0.0555   1.0000
  10.000   1.6668   0.03042   0.02282  -0.1529   0.0541   1.0000
  10.250   1.6765   0.03182   0.02427  -0.1513   0.0526   1.0000
  10.500   1.6853   0.03334   0.02584  -0.1497   0.0509   1.0000
  10.750   1.6968   0.03466   0.02722  -0.1485   0.0498   1.0000
  11.000   1.7079   0.03605   0.02869  -0.1473   0.0489   1.0000
  11.250   1.7181   0.03755   0.03026  -0.1461   0.0478   1.0000
  11.500   1.7275   0.03917   0.03195  -0.1449   0.0466   1.0000
  11.750   1.7354   0.04097   0.03381  -0.1437   0.0451   1.0000
  12.000   1.7421   0.04295   0.03585  -0.1425   0.0438   1.0000
  12.250   1.7462   0.04526   0.03821  -0.1413   0.0420   1.0000
  12.500   1.7565   0.04695   0.03997  -0.1405   0.0409   1.0000
  12.750   1.7656   0.04880   0.04190  -0.1397   0.0397   1.0000
  13.000   1.7734   0.05084   0.04400  -0.1389   0.0377   1.0000
  13.250   1.7790   0.05318   0.04637  -0.1382   0.0350   1.0000
  13.500   1.7849   0.05553   0.04878  -0.1375   0.0326   1.0000
  13.750   1.7832   0.05889   0.05205  -0.1368   0.0227   1.0000
  14.000   1.7730   0.06351   0.05665  -0.1361   0.0139   1.0000
  14.250   1.7582   0.06895   0.06213  -0.1357   0.0054   1.0000
  14.500   1.7536   0.07318   0.06646  -0.1356   0.0041   1.0000
  14.750   1.7525   0.07699   0.07037  -0.1357   0.0037   1.0000
  15.000   1.7523   0.08074   0.07423  -0.1359   0.0035   1.0000
  15.250   1.7507   0.08476   0.07837  -0.1362   0.0033   1.0000
  15.500   1.7500   0.08871   0.08244  -0.1366   0.0031   1.0000
  15.750   1.7488   0.09282   0.08667  -0.1372   0.0030   1.0000
  16.000   1.7476   0.09695   0.09092  -0.1380   0.0029   1.0000
  16.250   1.7455   0.10129   0.09538  -0.1388   0.0028   1.0000
  16.500   1.7431   0.10572   0.09992  -0.1399   0.0028   1.0000
  16.750   1.7393   0.11042   0.10475  -0.1411   0.0026   1.0000
  17.000   1.7355   0.11515   0.10960  -0.1424   0.0025   1.0000
  17.250   1.7319   0.11989   0.11448  -0.1440   0.0025   1.0000
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