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GOE 500 AIRFOIL (goe500-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 500 AIRFOIL (goe500-il)
Reynolds number: 1,000,000
Max Cl/Cd: 159.15 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe500-il-1000000.txt
Download as CSV file: xf-goe500-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 500 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.2586   0.12614   0.12440  -0.0575   0.9916   0.0158
 -12.000  -0.2548   0.11986   0.11811  -0.0623   0.9893   0.0174
 -11.750  -0.5566   0.02424   0.02146  -0.1581   0.9534   0.0156
 -11.500  -0.5350   0.02260   0.01969  -0.1599   0.9480   0.0160
 -11.250  -0.5120   0.02121   0.01814  -0.1614   0.9437   0.0165
 -11.000  -0.4880   0.02003   0.01679  -0.1625   0.9397   0.0170
 -10.750  -0.4637   0.01931   0.01595  -0.1629   0.9360   0.0174
 -10.500  -0.4425   0.01757   0.01401  -0.1639   0.9317   0.0182
 -10.250  -0.4164   0.01716   0.01357  -0.1641   0.9285   0.0188
 -10.000  -0.3897   0.01677   0.01311  -0.1644   0.9253   0.0194
  -9.750  -0.3638   0.01629   0.01256  -0.1645   0.9223   0.0201
  -9.500  -0.3378   0.01578   0.01195  -0.1647   0.9189   0.0208
  -9.250  -0.3111   0.01537   0.01143  -0.1648   0.9157   0.0214
  -9.000  -0.2863   0.01425   0.01013  -0.1651   0.9123   0.0222
  -8.750  -0.2596   0.01376   0.00959  -0.1653   0.9091   0.0230
  -8.500  -0.2326   0.01350   0.00930  -0.1654   0.9061   0.0238
  -8.250  -0.2054   0.01321   0.00896  -0.1654   0.9027   0.0247
  -8.000  -0.1782   0.01285   0.00851  -0.1654   0.8994   0.0255
  -7.750  -0.1507   0.01256   0.00813  -0.1654   0.8963   0.0261
  -7.500  -0.1241   0.01178   0.00721  -0.1656   0.8928   0.0270
  -7.250  -0.0973   0.01125   0.00664  -0.1657   0.8893   0.0282
  -7.000  -0.0698   0.01095   0.00631  -0.1657   0.8856   0.0291
  -6.750  -0.0422   0.01062   0.00591  -0.1657   0.8821   0.0300
  -6.500  -0.0142   0.01037   0.00557  -0.1657   0.8782   0.0309
  -6.250   0.0133   0.01014   0.00530  -0.1656   0.8737   0.0317
  -6.000   0.0409   0.00983   0.00493  -0.1655   0.8686   0.0323
  -5.750   0.0682   0.00917   0.00415  -0.1655   0.8637   0.0338
  -5.500   0.0958   0.00888   0.00384  -0.1655   0.8585   0.0351
  -5.250   0.1236   0.00864   0.00355  -0.1654   0.8528   0.0363
  -5.000   0.1516   0.00843   0.00327  -0.1654   0.8473   0.0374
  -4.750   0.1794   0.00822   0.00302  -0.1653   0.8407   0.0384
  -4.500   0.2074   0.00801   0.00274  -0.1652   0.8344   0.0396
  -4.250   0.2354   0.00771   0.00241  -0.1652   0.8283   0.0425
  -4.000   0.2634   0.00754   0.00220  -0.1651   0.8217   0.0448
  -3.750   0.2915   0.00741   0.00202  -0.1651   0.8153   0.0470
  -3.500   0.3195   0.00719   0.00180  -0.1650   0.8074   0.0541
  -3.250   0.3473   0.00701   0.00166  -0.1649   0.7997   0.0700
  -3.000   0.3751   0.00693   0.00163  -0.1648   0.7910   0.0883
  -2.750   0.4030   0.00691   0.00157  -0.1647   0.7828   0.0954
  -2.500   0.4307   0.00688   0.00152  -0.1646   0.7739   0.1021
  -2.250   0.4586   0.00688   0.00148  -0.1645   0.7652   0.1061
  -2.000   0.4861   0.00687   0.00141  -0.1643   0.7564   0.1102
  -1.750   0.5138   0.00682   0.00135  -0.1642   0.7472   0.1157
  -1.500   0.5413   0.00682   0.00132  -0.1640   0.7383   0.1201
  -1.250   0.5688   0.00684   0.00128  -0.1638   0.7294   0.1227
  -1.000   0.5965   0.00679   0.00124  -0.1637   0.7213   0.1301
  -0.750   0.6238   0.00679   0.00123  -0.1635   0.7130   0.1393
  -0.500   0.6515   0.00673   0.00121  -0.1634   0.7051   0.1582
  -0.250   0.6786   0.00662   0.00124  -0.1633   0.6970   0.2174
   0.000   0.7062   0.00656   0.00128  -0.1632   0.6890   0.2621
   0.250   0.7332   0.00658   0.00132  -0.1630   0.6805   0.2899
   0.500   0.7607   0.00658   0.00135  -0.1629   0.6719   0.3125
   0.750   0.7877   0.00661   0.00140  -0.1627   0.6636   0.3352
   1.000   0.8150   0.00662   0.00145  -0.1625   0.6550   0.3594
   1.250   0.8420   0.00664   0.00152  -0.1623   0.6465   0.3879
   1.750   0.8957   0.00666   0.00169  -0.1618   0.6278   0.4684
   2.000   0.9219   0.00669   0.00179  -0.1615   0.6164   0.5196
   2.250   0.9477   0.00674   0.00190  -0.1610   0.6035   0.5651
   2.500   0.9737   0.00678   0.00201  -0.1606   0.5904   0.6136
   2.750   0.9989   0.00679   0.00213  -0.1601   0.5754   0.6813
   3.000   1.0233   0.00643   0.00227  -0.1594   0.5572   1.0000
   3.250   1.0486   0.00662   0.00238  -0.1588   0.5393   1.0000
   3.500   1.0733   0.00685   0.00251  -0.1582   0.5179   1.0000
   3.750   1.0971   0.00713   0.00267  -0.1574   0.4957   1.0000
   4.000   1.1219   0.00735   0.00282  -0.1568   0.4794   1.0000
   4.250   1.1466   0.00758   0.00299  -0.1562   0.4652   1.0000
   4.500   1.1709   0.00783   0.00317  -0.1555   0.4492   1.0000
   4.750   1.1949   0.00809   0.00336  -0.1548   0.4319   1.0000
   5.000   1.2191   0.00834   0.00355  -0.1541   0.4190   1.0000
   5.250   1.2434   0.00857   0.00374  -0.1535   0.4052   1.0000
   5.500   1.2668   0.00885   0.00395  -0.1527   0.3884   1.0000
   5.750   1.2901   0.00914   0.00417  -0.1518   0.3675   1.0000
   6.000   1.3100   0.00963   0.00448  -0.1505   0.3297   1.0000
   6.250   1.3223   0.01061   0.00505  -0.1478   0.2573   1.0000
   6.500   1.3331   0.01168   0.00575  -0.1450   0.1950   1.0000
   6.750   1.3406   0.01291   0.00655  -0.1416   0.1233   1.0000
   7.000   1.3464   0.01406   0.00736  -0.1379   0.0669   1.0000
   7.250   1.3576   0.01479   0.00796  -0.1350   0.0466   1.0000
   7.500   1.3735   0.01528   0.00843  -0.1329   0.0406   1.0000
   7.750   1.3897   0.01575   0.00891  -0.1309   0.0374   1.0000
   8.000   1.4038   0.01635   0.00951  -0.1286   0.0338   1.0000
   8.250   1.4216   0.01675   0.00995  -0.1270   0.0326   1.0000
   8.500   1.4379   0.01723   0.01046  -0.1252   0.0309   1.0000
   8.750   1.4522   0.01785   0.01107  -0.1231   0.0289   1.0000
   9.000   1.4643   0.01861   0.01187  -0.1207   0.0269   1.0000
   9.250   1.4811   0.01909   0.01239  -0.1192   0.0259   1.0000
   9.500   1.4966   0.01966   0.01300  -0.1175   0.0246   1.0000
   9.750   1.5103   0.02036   0.01370  -0.1155   0.0231   1.0000
  10.000   1.5192   0.02138   0.01477  -0.1130   0.0214   1.0000
  10.250   1.5347   0.02200   0.01542  -0.1115   0.0207   1.0000
  10.500   1.5489   0.02271   0.01618  -0.1098   0.0197   1.0000
  10.750   1.5617   0.02354   0.01703  -0.1080   0.0188   1.0000
  11.000   1.5709   0.02463   0.01814  -0.1059   0.0176   1.0000
  11.250   1.5785   0.02589   0.01947  -0.1036   0.0168   1.0000
  11.500   1.5920   0.02673   0.02035  -0.1021   0.0162   1.0000
  11.750   1.6031   0.02777   0.02144  -0.1005   0.0155   1.0000
  12.000   1.6138   0.02888   0.02259  -0.0988   0.0149   1.0000
  12.250   1.6224   0.03019   0.02394  -0.0971   0.0142   1.0000
  12.500   1.6221   0.03228   0.02611  -0.0947   0.0135   1.0000
  12.750   1.6306   0.03369   0.02759  -0.0932   0.0132   1.0000
  13.000   1.6387   0.03519   0.02916  -0.0917   0.0129   1.0000
  13.250   1.6459   0.03679   0.03083  -0.0903   0.0125   1.0000
  13.500   1.6524   0.03853   0.03264  -0.0890   0.0121   1.0000
  13.750   1.6584   0.04038   0.03456  -0.0878   0.0117   1.0000
  14.000   1.6632   0.04241   0.03665  -0.0867   0.0114   1.0000
  14.250   1.6659   0.04473   0.03904  -0.0856   0.0111   1.0000
  14.500   1.6622   0.04787   0.04225  -0.0844   0.0107   1.0000
  14.750   1.6583   0.05116   0.04566  -0.0835   0.0104   1.0000
  15.000   1.6642   0.05339   0.04797  -0.0830   0.0102   1.0000
  15.250   1.6675   0.05598   0.05065  -0.0825   0.0100   1.0000
  15.500   1.6695   0.05881   0.05357  -0.0821   0.0098   1.0000
  15.750   1.6708   0.06182   0.05668  -0.0819   0.0096   1.0000
  16.000   1.6720   0.06489   0.05984  -0.0819   0.0093   1.0000
  16.250   1.6717   0.06826   0.06330  -0.0819   0.0092   1.0000
  16.500   1.6715   0.07169   0.06681  -0.0822   0.0090   1.0000
  16.750   1.6707   0.07528   0.07049  -0.0825   0.0088   1.0000
  17.000   1.6685   0.07917   0.07447  -0.0831   0.0087   1.0000
  17.250   1.6646   0.08341   0.07880  -0.0839   0.0085   1.0000
  17.500   1.6585   0.08808   0.08357  -0.0849   0.0084   1.0000
  17.750   1.6493   0.09334   0.08894  -0.0862   0.0082   1.0000
  18.000   1.6371   0.09921   0.09494  -0.0878   0.0080   1.0000
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