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GOE 600 AIRFOIL (goe600-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 600 AIRFOIL (goe600-il)
Reynolds number: 200,000
Max Cl/Cd: 62.89 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe600-il-200000-n5.txt
Download as CSV file: xf-goe600-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 600 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.7802   0.09332   0.08944  -0.0274   1.0000   0.0157
 -14.000  -0.8286   0.07876   0.07463  -0.0368   1.0000   0.0153
 -13.750  -0.8584   0.06892   0.06455  -0.0436   1.0000   0.0151
 -13.500  -0.8794   0.06133   0.05675  -0.0490   1.0000   0.0151
 -13.250  -0.8947   0.05521   0.05042  -0.0532   1.0000   0.0152
 -13.000  -0.9058   0.05016   0.04516  -0.0564   1.0000   0.0153
 -12.750  -0.9140   0.04593   0.04073  -0.0587   1.0000   0.0155
 -12.500  -0.9198   0.04244   0.03703  -0.0598   1.0000   0.0157
 -12.250  -0.9234   0.03958   0.03397  -0.0599   1.0000   0.0160
 -12.000  -0.9252   0.03724   0.03142  -0.0590   1.0000   0.0164
 -11.750  -0.9255   0.03529   0.02925  -0.0573   1.0000   0.0168
 -11.500  -0.9216   0.03358   0.02731  -0.0554   1.0000   0.0173
 -11.250  -0.9153   0.03191   0.02556  -0.0538   1.0000   0.0179
 -11.000  -0.9046   0.03064   0.02421  -0.0525   1.0000   0.0185
 -10.750  -0.8922   0.02946   0.02293  -0.0511   1.0000   0.0192
 -10.500  -0.8792   0.02827   0.02161  -0.0496   1.0000   0.0199
 -10.250  -0.8662   0.02710   0.02031  -0.0480   1.0000   0.0208
 -10.000  -0.8534   0.02602   0.01907  -0.0461   1.0000   0.0217
  -9.750  -0.8417   0.02503   0.01800  -0.0440   1.0000   0.0227
  -9.500  -0.8291   0.02432   0.01727  -0.0420   1.0000   0.0239
  -9.250  -0.8086   0.02356   0.01642  -0.0415   0.9977   0.0257
  -9.000  -0.7780   0.02257   0.01526  -0.0428   0.9928   0.0279
  -8.750  -0.7483   0.02162   0.01427  -0.0442   0.9873   0.0302
  -8.500  -0.7168   0.02090   0.01344  -0.0456   0.9820   0.0337
  -8.250  -0.6868   0.02008   0.01256  -0.0468   0.9756   0.0371
  -8.000  -0.6563   0.01943   0.01182  -0.0479   0.9691   0.0411
  -7.750  -0.6265   0.01868   0.01098  -0.0489   0.9625   0.0453
  -7.500  -0.5975   0.01804   0.01027  -0.0496   0.9553   0.0499
  -7.250  -0.5673   0.01750   0.00961  -0.0504   0.9484   0.0542
  -7.000  -0.5403   0.01679   0.00889  -0.0508   0.9402   0.0598
  -6.500  -0.4854   0.01574   0.00780  -0.0512   0.9239   0.0746
  -6.250  -0.4580   0.01531   0.00742  -0.0513   0.9163   0.0873
  -6.000  -0.4314   0.01500   0.00709  -0.0511   0.9074   0.1033
  -5.750  -0.4042   0.01472   0.00674  -0.0510   0.8998   0.1172
  -5.500  -0.3783   0.01441   0.00642  -0.0508   0.8902   0.1285
  -5.250  -0.3519   0.01413   0.00609  -0.0505   0.8822   0.1389
  -5.000  -0.3253   0.01391   0.00579  -0.0503   0.8732   0.1490
  -4.750  -0.2992   0.01359   0.00547  -0.0501   0.8653   0.1596
  -4.500  -0.2728   0.01333   0.00517  -0.0498   0.8570   0.1697
  -4.250  -0.2466   0.01300   0.00489  -0.0497   0.8487   0.1869
  -4.000  -0.2207   0.01261   0.00461  -0.0494   0.8408   0.2179
  -3.750  -0.1950   0.01221   0.00440  -0.0493   0.8325   0.2733
  -3.500  -0.1688   0.01189   0.00422  -0.0491   0.8255   0.3238
  -3.250  -0.1424   0.01160   0.00408  -0.0489   0.8180   0.3749
  -3.000  -0.1160   0.01135   0.00397  -0.0487   0.8112   0.4217
  -2.750  -0.0889   0.01119   0.00389  -0.0485   0.8043   0.4566
  -2.500  -0.0615   0.01108   0.00380  -0.0484   0.7975   0.4835
  -2.250  -0.0340   0.01098   0.00374  -0.0483   0.7918   0.5112
  -2.000  -0.0062   0.01091   0.00369  -0.0483   0.7854   0.5358
  -1.750   0.0215   0.01084   0.00363  -0.0482   0.7799   0.5573
  -1.500   0.0493   0.01078   0.00359  -0.0481   0.7729   0.5787
  -1.250   0.0770   0.01073   0.00352  -0.0479   0.7655   0.5973
  -1.000   0.1045   0.01066   0.00348  -0.0478   0.7574   0.6160
  -0.750   0.1318   0.01060   0.00344  -0.0475   0.7495   0.6372
  -0.500   0.1591   0.01054   0.00342  -0.0473   0.7411   0.6586
  -0.250   0.1862   0.01048   0.00340  -0.0470   0.7335   0.6817
   0.000   0.2130   0.01041   0.00343  -0.0466   0.7263   0.7101
   0.250   0.2395   0.01034   0.00347  -0.0461   0.7198   0.7420
   0.500   0.2658   0.01030   0.00352  -0.0455   0.7137   0.7742
   0.750   0.2922   0.01026   0.00359  -0.0450   0.7066   0.8050
   1.000   0.3190   0.01026   0.00362  -0.0444   0.7006   0.8351
   1.250   0.3466   0.01026   0.00372  -0.0441   0.6929   0.8665
   1.500   0.3764   0.01029   0.00377  -0.0442   0.6859   0.8980
   1.750   0.4097   0.01033   0.00386  -0.0452   0.6775   0.9270
   2.000   0.4457   0.01038   0.00389  -0.0467   0.6693   0.9511
   2.250   0.4823   0.01043   0.00397  -0.0486   0.6588   0.9712
   2.500   0.5202   0.01049   0.00402  -0.0508   0.6472   0.9863
   2.750   0.5589   0.01054   0.00405  -0.0532   0.6328   0.9983
   3.000   0.5851   0.01060   0.00408  -0.0529   0.6173   1.0000
   3.250   0.6091   0.01068   0.00412  -0.0522   0.6002   1.0000
   3.500   0.6332   0.01077   0.00417  -0.0515   0.5808   1.0000
   3.750   0.6574   0.01089   0.00424  -0.0508   0.5594   1.0000
   4.000   0.6817   0.01104   0.00434  -0.0501   0.5353   1.0000
   4.250   0.7054   0.01125   0.00444  -0.0493   0.5048   1.0000
   4.500   0.7276   0.01157   0.00458  -0.0483   0.4664   1.0000
   4.750   0.7493   0.01199   0.00480  -0.0473   0.4316   1.0000
   5.000   0.7716   0.01240   0.00508  -0.0464   0.4045   1.0000
   5.250   0.7942   0.01282   0.00539  -0.0457   0.3802   1.0000
   5.500   0.8174   0.01320   0.00572  -0.0450   0.3584   1.0000
   5.750   0.8407   0.01357   0.00605  -0.0443   0.3387   1.0000
   6.000   0.8637   0.01397   0.00639  -0.0436   0.3192   1.0000
   6.250   0.8862   0.01440   0.00677  -0.0429   0.2957   1.0000
   6.500   0.9076   0.01490   0.00717  -0.0420   0.2697   1.0000
   6.750   0.9288   0.01541   0.00760  -0.0411   0.2440   1.0000
   7.000   0.9500   0.01592   0.00805  -0.0403   0.2228   1.0000
   7.250   0.9709   0.01646   0.00853  -0.0393   0.2022   1.0000
   7.500   0.9906   0.01707   0.00907  -0.0383   0.1813   1.0000
   7.750   1.0103   0.01768   0.00962  -0.0372   0.1610   1.0000
   8.000   1.0292   0.01832   0.01021  -0.0361   0.1423   1.0000
   8.250   1.0476   0.01900   0.01082  -0.0349   0.1241   1.0000
   8.500   1.0655   0.01969   0.01148  -0.0336   0.1079   1.0000
   8.750   1.0821   0.02044   0.01218  -0.0322   0.0940   1.0000
   9.000   1.0979   0.02123   0.01294  -0.0307   0.0830   1.0000
   9.250   1.1118   0.02207   0.01377  -0.0289   0.0727   1.0000
   9.500   1.1255   0.02283   0.01455  -0.0270   0.0616   1.0000
   9.750   1.1383   0.02368   0.01539  -0.0252   0.0498   1.0000
  10.250   1.1597   0.02579   0.01750  -0.0213   0.0377   1.0000
  10.500   1.1679   0.02709   0.01881  -0.0193   0.0343   1.0000
  10.750   1.1780   0.02828   0.02011  -0.0177   0.0318   1.0000
  11.000   1.1866   0.02962   0.02154  -0.0160   0.0297   1.0000
  11.250   1.1923   0.03124   0.02323  -0.0144   0.0279   1.0000
  11.500   1.1973   0.03297   0.02506  -0.0128   0.0264   1.0000
  11.750   1.2050   0.03453   0.02675  -0.0116   0.0250   1.0000
  12.000   1.2115   0.03626   0.02861  -0.0104   0.0236   1.0000
  12.250   1.2161   0.03819   0.03064  -0.0094   0.0225   1.0000
  12.500   1.2176   0.04048   0.03301  -0.0084   0.0216   1.0000
  12.750   1.2174   0.04302   0.03564  -0.0075   0.0209   1.0000
  13.000   1.2216   0.04520   0.03797  -0.0068   0.0202   1.0000
  13.250   1.2244   0.04758   0.04050  -0.0063   0.0194   1.0000
  13.500   1.2261   0.05013   0.04317  -0.0059   0.0186   1.0000
  13.750   1.2271   0.05280   0.04596  -0.0056   0.0179   1.0000
  14.000   1.2270   0.05567   0.04894  -0.0056   0.0174   1.0000
  14.250   1.2254   0.05878   0.05215  -0.0058   0.0169   1.0000
  14.500   1.2216   0.06224   0.05572  -0.0061   0.0164   1.0000
  14.750   1.2171   0.06592   0.05949  -0.0065   0.0161   1.0000
  15.000   1.2147   0.06950   0.06324  -0.0071   0.0157   1.0000
  15.250   1.2111   0.07333   0.06724  -0.0079   0.0154   1.0000
  15.500   1.2067   0.07742   0.07148  -0.0089   0.0151   1.0000
  15.750   1.2017   0.08172   0.07594  -0.0101   0.0148   1.0000
  16.000   1.1957   0.08627   0.08064  -0.0116   0.0146   1.0000
  16.250   1.1892   0.09107   0.08559  -0.0134   0.0143   1.0000
  16.500   1.1820   0.09611   0.09078  -0.0154   0.0141   1.0000
  16.750   1.1742   0.10139   0.09621  -0.0177   0.0139   1.0000
  17.000   1.1657   0.10690   0.10186  -0.0202   0.0137   1.0000
  17.250   1.1568   0.11261   0.10771  -0.0230   0.0135   1.0000
  17.500   1.1474   0.11855   0.11378  -0.0260   0.0133   1.0000
  17.750   1.1378   0.12469   0.12006  -0.0293   0.0132   1.0000
  18.000   1.1278   0.13101   0.12650  -0.0328   0.0130   1.0000
  18.250   1.1173   0.13760   0.13323  -0.0365   0.0129   1.0000
  18.500   1.1065   0.14448   0.14023  -0.0405   0.0128   1.0000
  18.750   1.0947   0.15185   0.14772  -0.0450   0.0127   1.0000
  19.000   1.0801   0.16028   0.15630  -0.0502   0.0127   1.0000
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