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GOE 459 AIRFOIL (goe459-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 459 AIRFOIL (goe459-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.59 at α=10.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe459-il-1000000.txt
Download as CSV file: xf-goe459-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 459 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.1544   0.08600   0.08258  -0.0319   1.0000   0.0098
 -18.000  -1.1773   0.07854   0.07498  -0.0357   1.0000   0.0099
 -17.750  -1.1963   0.07189   0.06820  -0.0390   1.0000   0.0099
 -17.500  -1.2134   0.06576   0.06194  -0.0419   1.0000   0.0099
 -17.250  -1.2240   0.06082   0.05688  -0.0442   1.0000   0.0100
 -17.000  -1.2402   0.05532   0.05125  -0.0466   1.0000   0.0099
 -16.750  -1.2503   0.05086   0.04667  -0.0483   1.0000   0.0100
 -16.500  -1.2606   0.04660   0.04229  -0.0496   1.0000   0.0102
 -16.250  -1.2713   0.04257   0.03812  -0.0506   1.0000   0.0102
 -16.000  -1.2824   0.03878   0.03422  -0.0511   1.0000   0.0104
 -15.750  -1.2890   0.03572   0.03104  -0.0509   1.0000   0.0106
 -15.500  -1.2904   0.03336   0.02859  -0.0504   1.0000   0.0107
 -15.250  -1.2907   0.03125   0.02639  -0.0495   1.0000   0.0109
 -15.000  -1.2909   0.02931   0.02436  -0.0482   1.0000   0.0113
 -14.750  -1.2870   0.02780   0.02278  -0.0467   1.0000   0.0115
 -14.500  -1.2818   0.02650   0.02139  -0.0451   1.0000   0.0117
 -14.250  -1.2770   0.02525   0.02006  -0.0432   1.0000   0.0119
 -14.000  -1.2693   0.02426   0.01901  -0.0413   1.0000   0.0122
 -13.750  -1.2630   0.02326   0.01792  -0.0390   1.0000   0.0125
 -13.500  -1.2561   0.02237   0.01695  -0.0366   1.0000   0.0128
 -13.250  -1.2522   0.02137   0.01588  -0.0336   1.0000   0.0132
 -13.000  -1.2474   0.02050   0.01495  -0.0304   1.0000   0.0138
 -12.750  -1.2413   0.01975   0.01416  -0.0272   1.0000   0.0145
 -12.500  -1.2332   0.01917   0.01353  -0.0241   1.0000   0.0149
 -12.250  -1.2260   0.01864   0.01292  -0.0207   1.0000   0.0155
 -12.000  -1.2205   0.01813   0.01236  -0.0168   1.0000   0.0161
 -11.750  -1.2174   0.01755   0.01176  -0.0124   1.0000   0.0172
 -11.500  -1.2078   0.01703   0.01121  -0.0092   1.0000   0.0183
 -11.250  -1.1976   0.01645   0.01062  -0.0062   1.0000   0.0206
 -11.000  -1.1865   0.01591   0.01012  -0.0032   1.0000   0.0248
 -10.750  -1.1720   0.01552   0.00979  -0.0009   1.0000   0.0307
 -10.500  -1.1539   0.01534   0.00961   0.0009   1.0000   0.0340
 -10.250  -1.1374   0.01507   0.00937   0.0030   1.0000   0.0367
 -10.000  -1.1186   0.01493   0.00924   0.0046   1.0000   0.0388
  -9.750  -1.0992   0.01483   0.00912   0.0062   1.0000   0.0403
  -9.500  -1.0791   0.01479   0.00905   0.0077   1.0000   0.0411
  -9.250  -1.0673   0.01431   0.00854   0.0106   1.0000   0.0428
  -9.000  -1.0516   0.01405   0.00829   0.0128   1.0000   0.0443
  -8.750  -1.0230   0.01383   0.00806   0.0124   0.9991   0.0457
  -8.500  -0.9899   0.01363   0.00785   0.0110   0.9977   0.0472
  -8.250  -0.9564   0.01344   0.00764   0.0096   0.9961   0.0483
  -8.000  -0.9217   0.01330   0.00749   0.0080   0.9947   0.0492
  -7.750  -0.8897   0.01285   0.00700   0.0068   0.9929   0.0504
  -7.500  -0.8593   0.01237   0.00650   0.0059   0.9900   0.0527
  -7.250  -0.8255   0.01203   0.00616   0.0045   0.9875   0.0543
  -7.000  -0.7904   0.01173   0.00586   0.0027   0.9854   0.0559
  -6.750  -0.7547   0.01148   0.00559   0.0009   0.9839   0.0577
  -6.500  -0.7193   0.01124   0.00533  -0.0009   0.9828   0.0588
  -6.250  -0.6937   0.01093   0.00501  -0.0005   0.9777   0.0598
  -6.000  -0.6627   0.01056   0.00462  -0.0012   0.9748   0.0624
  -5.750  -0.6297   0.01023   0.00430  -0.0025   0.9727   0.0652
  -5.500  -0.5954   0.00995   0.00403  -0.0039   0.9711   0.0678
  -5.250  -0.5681   0.00970   0.00377  -0.0038   0.9658   0.0705
  -5.000  -0.5390   0.00930   0.00346  -0.0042   0.9615   0.0834
  -4.750  -0.5095   0.00866   0.00311  -0.0048   0.9583   0.1375
  -4.500  -0.4800   0.00831   0.00287  -0.0053   0.9531   0.1631
  -4.250  -0.4491   0.00798   0.00266  -0.0060   0.9469   0.1870
  -4.000  -0.4114   0.00761   0.00244  -0.0084   0.9431   0.2222
  -3.750  -0.3791   0.00731   0.00226  -0.0095   0.9350   0.2565
  -3.500  -0.3418   0.00700   0.00208  -0.0117   0.9278   0.2892
  -3.250  -0.3087   0.00675   0.00190  -0.0129   0.9152   0.3190
  -3.000  -0.2791   0.00646   0.00174  -0.0133   0.9003   0.3582
  -2.750  -0.2542   0.00618   0.00161  -0.0127   0.8848   0.4103
  -2.500  -0.2302   0.00599   0.00153  -0.0119   0.8694   0.4545
  -2.250  -0.2063   0.00587   0.00146  -0.0109   0.8535   0.4860
  -2.000  -0.1820   0.00579   0.00140  -0.0100   0.8371   0.5087
  -1.750  -0.1585   0.00573   0.00134  -0.0089   0.8193   0.5290
  -1.500  -0.1357   0.00566   0.00129  -0.0077   0.8005   0.5523
  -1.250  -0.1128   0.00563   0.00125  -0.0065   0.7804   0.5725
  -1.000  -0.0905   0.00558   0.00122  -0.0051   0.7606   0.5953
  -0.750  -0.0679   0.00555   0.00120  -0.0038   0.7419   0.6196
  -0.500  -0.0451   0.00553   0.00118  -0.0026   0.7242   0.6413
  -0.250  -0.0227   0.00549   0.00118  -0.0013   0.7072   0.6682
   0.000   0.0000   0.00548   0.00118   0.0000   0.6898   0.6895
   0.250   0.0227   0.00550   0.00118   0.0013   0.6676   0.7071
   0.500   0.0454   0.00552   0.00118   0.0025   0.6427   0.7239
   0.750   0.0680   0.00555   0.00119   0.0038   0.6188   0.7409
   1.000   0.0902   0.00559   0.00121   0.0052   0.5938   0.7607
   1.250   0.1127   0.00563   0.00125   0.0065   0.5722   0.7810
   1.500   0.1357   0.00567   0.00129   0.0077   0.5515   0.8004
   1.750   0.1585   0.00572   0.00134   0.0089   0.5295   0.8196
   2.000   0.1820   0.00579   0.00140   0.0100   0.5085   0.8373
   2.250   0.2061   0.00587   0.00146   0.0110   0.4844   0.8536
   2.500   0.2303   0.00599   0.00153   0.0118   0.4549   0.8687
   2.750   0.2542   0.00618   0.00161   0.0127   0.4107   0.8843
   3.000   0.2793   0.00646   0.00174   0.0133   0.3584   0.9007
   3.250   0.3087   0.00675   0.00191   0.0129   0.3179   0.9153
   3.500   0.3415   0.00700   0.00207   0.0117   0.2893   0.9277
   3.750   0.3791   0.00731   0.00226   0.0095   0.2565   0.9350
   4.000   0.4113   0.00761   0.00244   0.0084   0.2218   0.9431
   4.250   0.4491   0.00798   0.00266   0.0060   0.1870   0.9469
   4.500   0.4799   0.00831   0.00287   0.0053   0.1625   0.9531
   4.750   0.5094   0.00868   0.00311   0.0048   0.1360   0.9583
   5.000   0.5390   0.00931   0.00346   0.0042   0.0830   0.9615
   5.250   0.5682   0.00970   0.00377   0.0038   0.0706   0.9658
   5.500   0.5953   0.00994   0.00402   0.0040   0.0678   0.9711
   5.750   0.6297   0.01024   0.00431   0.0025   0.0649   0.9727
   6.000   0.6628   0.01056   0.00461   0.0012   0.0625   0.9748
   6.250   0.6938   0.01093   0.00500   0.0004   0.0598   0.9777
   6.500   0.7193   0.01123   0.00532   0.0009   0.0587   0.9828
   6.750   0.7548   0.01147   0.00558  -0.0009   0.0577   0.9839
   7.000   0.7905   0.01175   0.00588  -0.0027   0.0562   0.9855
   7.250   0.8257   0.01203   0.00616  -0.0045   0.0544   0.9875
   7.500   0.8594   0.01236   0.00650  -0.0059   0.0528   0.9900
   7.750   0.8900   0.01282   0.00696  -0.0068   0.0508   0.9928
   8.000   0.9218   0.01331   0.00751  -0.0080   0.0492   0.9947
   8.250   0.9566   0.01344   0.00765  -0.0096   0.0484   0.9961
   8.500   0.9901   0.01362   0.00784  -0.0111   0.0471   0.9977
   8.750   1.0230   0.01383   0.00807  -0.0124   0.0457   0.9991
   9.000   1.0516   0.01404   0.00828  -0.0128   0.0443   1.0000
   9.250   1.0673   0.01430   0.00853  -0.0106   0.0430   1.0000
   9.500   1.0791   0.01478   0.00904  -0.0077   0.0411   1.0000
   9.750   1.0993   0.01483   0.00912  -0.0062   0.0403   1.0000
  10.000   1.1190   0.01491   0.00921  -0.0047   0.0387   1.0000
  10.250   1.1377   0.01505   0.00935  -0.0030   0.0366   1.0000
  10.500   1.1542   0.01532   0.00959  -0.0010   0.0339   1.0000
  10.750   1.1721   0.01552   0.00978   0.0009   0.0304   1.0000
  11.000   1.1866   0.01590   0.01011   0.0032   0.0251   1.0000
  11.250   1.1979   0.01644   0.01061   0.0061   0.0208   1.0000
  11.500   1.2085   0.01699   0.01117   0.0091   0.0187   1.0000
  11.750   1.2173   0.01757   0.01178   0.0124   0.0172   1.0000
  12.000   1.2204   0.01814   0.01238   0.0168   0.0161   1.0000
  12.250   1.2265   0.01863   0.01291   0.0206   0.0154   1.0000
  12.500   1.2342   0.01914   0.01349   0.0240   0.0149   1.0000
  12.750   1.2416   0.01975   0.01416   0.0272   0.0143   1.0000
  13.000   1.2486   0.02045   0.01490   0.0302   0.0138   1.0000
  13.250   1.2548   0.02125   0.01575   0.0332   0.0134   1.0000
  13.500   1.2556   0.02242   0.01700   0.0366   0.0127   1.0000
  13.750   1.2630   0.02329   0.01794   0.0390   0.0126   1.0000
  14.000   1.2715   0.02416   0.01889   0.0410   0.0123   1.0000
  14.250   1.2772   0.02527   0.02008   0.0431   0.0120   1.0000
  14.500   1.2836   0.02642   0.02131   0.0449   0.0117   1.0000
  14.750   1.2882   0.02776   0.02274   0.0466   0.0115   1.0000
  15.000   1.2933   0.02917   0.02422   0.0479   0.0112   1.0000
  15.250   1.2937   0.03106   0.02620   0.0492   0.0110   1.0000
  15.500   1.2937   0.03314   0.02836   0.0502   0.0108   1.0000
  15.750   1.2920   0.03551   0.03083   0.0507   0.0106   1.0000
  16.000   1.2846   0.03866   0.03409   0.0509   0.0104   1.0000
  16.250   1.2764   0.04213   0.03767   0.0505   0.0103   1.0000
  16.500   1.2549   0.04746   0.04317   0.0491   0.0101   1.0000
  16.750   1.2478   0.05136   0.04718   0.0478   0.0100   1.0000
  17.000   1.2386   0.05572   0.05166   0.0461   0.0100   1.0000
  17.250   1.2363   0.05932   0.05535   0.0446   0.0099   1.0000
  17.500   1.2188   0.06521   0.06138   0.0419   0.0099   1.0000
  17.750   1.1989   0.07176   0.06807   0.0387   0.0099   1.0000
  18.000   1.1840   0.07778   0.07421   0.0357   0.0098   1.0000
  18.250   1.1626   0.08500   0.08156   0.0321   0.0098   1.0000
  18.500   1.1356   0.09321   0.08991   0.0280   0.0098   1.0000
  18.750   1.1118   0.10105   0.09786   0.0241   0.0098   1.0000
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