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GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 776 AIRFOIL (goe776-il)
Reynolds number: 500,000
Max Cl/Cd: 50.01 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe776-il-500000.txt
Download as CSV file: xf-goe776-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 776 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2029   0.08721   0.08194  -0.0458   1.0000   0.1048
 -19.500  -1.2042   0.08398   0.07862  -0.0468   1.0000   0.1067
 -19.250  -1.2032   0.08112   0.07569  -0.0476   1.0000   0.1085
 -19.000  -1.2047   0.07809   0.07268  -0.0483   1.0000   0.1106
 -18.750  -1.2047   0.07516   0.06973  -0.0490   1.0000   0.1126
 -18.500  -1.2043   0.07226   0.06676  -0.0497   1.0000   0.1145
 -18.250  -1.2013   0.06965   0.06407  -0.0503   1.0000   0.1165
 -18.000  -1.2008   0.06692   0.06132  -0.0508   1.0000   0.1185
 -17.750  -1.2008   0.06416   0.05856  -0.0512   1.0000   0.1206
 -17.500  -1.1998   0.06145   0.05581  -0.0516   1.0000   0.1227
 -17.250  -1.1954   0.05913   0.05344  -0.0520   1.0000   0.1249
 -17.000  -1.1904   0.05685   0.05107  -0.0523   1.0000   0.1268
 -16.750  -1.1899   0.05435   0.04859  -0.0523   1.0000   0.1292
 -16.500  -1.1883   0.05187   0.04609  -0.0524   1.0000   0.1314
 -16.250  -1.1835   0.04973   0.04392  -0.0525   1.0000   0.1338
 -16.000  -1.1766   0.04781   0.04194  -0.0525   1.0000   0.1361
 -15.750  -1.1719   0.04579   0.03988  -0.0523   1.0000   0.1385
 -15.500  -1.1697   0.04358   0.03768  -0.0520   1.0000   0.1410
 -15.250  -1.1648   0.04162   0.03570  -0.0518   1.0000   0.1436
 -15.000  -1.1562   0.04003   0.03406  -0.0514   1.0000   0.1463
 -14.750  -1.1485   0.03842   0.03240  -0.0510   1.0000   0.1489
 -14.500  -1.1456   0.03652   0.03053  -0.0503   1.0000   0.1518
 -14.250  -1.1398   0.03490   0.02890  -0.0495   1.0000   0.1548
 -14.000  -1.1310   0.03358   0.02753  -0.0487   1.0000   0.1579
 -13.750  -1.1231   0.03230   0.02623  -0.0477   1.0000   0.1608
 -13.500  -1.1214   0.03076   0.02471  -0.0461   1.0000   0.1640
 -13.250  -1.1172   0.02957   0.02352  -0.0443   1.0000   0.1673
 -13.000  -1.1116   0.02861   0.02253  -0.0424   1.0000   0.1705
 -12.750  -1.1098   0.02763   0.02153  -0.0398   1.0000   0.1736
 -12.500  -1.1137   0.02659   0.02051  -0.0364   1.0000   0.1769
 -12.250  -1.1177   0.02578   0.01970  -0.0326   1.0000   0.1801
 -12.000  -1.1217   0.02515   0.01905  -0.0286   1.0000   0.1832
 -11.750  -1.1159   0.02441   0.01829  -0.0263   0.9992   0.1868
 -11.500  -1.0910   0.02330   0.01721  -0.0279   0.9966   0.1923
 -11.250  -1.0606   0.02256   0.01645  -0.0298   0.9941   0.1978
 -11.000  -1.0327   0.02161   0.01554  -0.0316   0.9918   0.2036
 -10.750  -1.0042   0.02083   0.01477  -0.0331   0.9889   0.2098
 -10.500  -0.9751   0.02015   0.01408  -0.0345   0.9848   0.2155
 -10.250  -0.9463   0.01932   0.01330  -0.0361   0.9813   0.2220
 -10.000  -0.9114   0.01876   0.01272  -0.0384   0.9789   0.2282
  -9.750  -0.8796   0.01798   0.01200  -0.0404   0.9765   0.2349
  -9.500  -0.8541   0.01741   0.01143  -0.0407   0.9695   0.2412
  -9.250  -0.8255   0.01688   0.01090  -0.0416   0.9634   0.2472
  -9.000  -0.8025   0.01627   0.01033  -0.0414   0.9559   0.2535
  -8.750  -0.7820   0.01585   0.00989  -0.0403   0.9454   0.2595
  -8.500  -0.7630   0.01541   0.00944  -0.0390   0.9351   0.2653
  -8.250  -0.7462   0.01496   0.00901  -0.0372   0.9236   0.2714
  -8.000  -0.7268   0.01466   0.00867  -0.0358   0.9117   0.2772
  -7.750  -0.7083   0.01428   0.00827  -0.0342   0.9005   0.2831
  -7.500  -0.6905   0.01395   0.00795  -0.0326   0.8874   0.2895
  -7.250  -0.6689   0.01372   0.00765  -0.0314   0.8759   0.2957
  -7.000  -0.6501   0.01340   0.00734  -0.0299   0.8624   0.3020
  -6.750  -0.6299   0.01314   0.00706  -0.0285   0.8502   0.3085
  -6.500  -0.6072   0.01297   0.00681  -0.0276   0.8369   0.3146
  -6.250  -0.5876   0.01269   0.00655  -0.0261   0.8240   0.3215
  -6.000  -0.5665   0.01250   0.00631  -0.0249   0.8108   0.3284
  -5.750  -0.5432   0.01238   0.00613  -0.0240   0.7977   0.3344
  -5.500  -0.5242   0.01216   0.00590  -0.0223   0.7847   0.3416
  -5.250  -0.5038   0.01203   0.00576  -0.0209   0.7716   0.3486
  -5.000  -0.4821   0.01196   0.00561  -0.0196   0.7591   0.3552
  -4.750  -0.4634   0.01180   0.00548  -0.0178   0.7461   0.3627
  -4.500  -0.4410   0.01173   0.00535  -0.0167   0.7343   0.3702
  -4.250  -0.4182   0.01163   0.00522  -0.0157   0.7217   0.3773
  -4.000  -0.3963   0.01152   0.00511  -0.0145   0.7102   0.3850
  -3.750  -0.3722   0.01146   0.00501  -0.0137   0.6985   0.3924
  -3.500  -0.3494   0.01137   0.00489  -0.0127   0.6873   0.3998
  -3.250  -0.3263   0.01127   0.00481  -0.0117   0.6758   0.4078
  -3.000  -0.3016   0.01127   0.00472  -0.0110   0.6649   0.4150
  -2.750  -0.2787   0.01113   0.00464  -0.0100   0.6542   0.4234
  -2.500  -0.2551   0.01111   0.00456  -0.0091   0.6430   0.4317
  -2.250  -0.2303   0.01104   0.00450  -0.0084   0.6326   0.4396
  -2.000  -0.2073   0.01098   0.00444  -0.0074   0.6218   0.4484
  -1.750  -0.1823   0.01095   0.00439  -0.0067   0.6116   0.4570
  -1.500  -0.1588   0.01089   0.00434  -0.0058   0.6005   0.4659
  -1.250  -0.1347   0.01086   0.00430  -0.0049   0.5904   0.4754
  -1.000  -0.1101   0.01083   0.00426  -0.0042   0.5795   0.4842
  -0.750  -0.0868   0.01081   0.00424  -0.0032   0.5691   0.4942
  -0.500  -0.0615   0.01079   0.00421  -0.0026   0.5584   0.5036
  -0.250  -0.0388   0.01078   0.00420  -0.0015   0.5478   0.5139
   0.000  -0.0134   0.01077   0.00419  -0.0009   0.5375   0.5240
   0.250   0.0096   0.01077   0.00419   0.0001   0.5269   0.5344
   0.500   0.0346   0.01077   0.00420   0.0008   0.5170   0.5451
   0.750   0.0580   0.01078   0.00421   0.0018   0.5067   0.5554
   1.000   0.0826   0.01080   0.00423   0.0025   0.4973   0.5664
   1.250   0.1066   0.01081   0.00425   0.0034   0.4873   0.5766
   1.500   0.1304   0.01086   0.00429   0.0042   0.4781   0.5876
   1.750   0.1552   0.01088   0.00432   0.0049   0.4689   0.5977
   2.000   0.1780   0.01095   0.00438   0.0060   0.4595   0.6087
   2.250   0.2035   0.01098   0.00442   0.0066   0.4513   0.6191
   2.500   0.2268   0.01101   0.00448   0.0075   0.4425   0.6299
   2.750   0.2509   0.01110   0.00455   0.0083   0.4344   0.6406
   3.000   0.2751   0.01111   0.00462   0.0092   0.4261   0.6514
   3.250   0.2979   0.01123   0.00470   0.0102   0.4178   0.6625
   3.500   0.3224   0.01126   0.00479   0.0109   0.4105   0.6732
   3.750   0.3460   0.01133   0.00487   0.0118   0.4026   0.6849
   4.000   0.3680   0.01146   0.00499   0.0130   0.3946   0.6959
   4.250   0.3925   0.01149   0.00508   0.0137   0.3877   0.7078
   4.500   0.4152   0.01159   0.00519   0.0147   0.3801   0.7192
   4.750   0.4369   0.01172   0.00533   0.0160   0.3727   0.7317
   5.000   0.4604   0.01177   0.00545   0.0169   0.3657   0.7436
   5.250   0.4802   0.01190   0.00557   0.0185   0.3582   0.7566
   5.500   0.5004   0.01201   0.00573   0.0200   0.3514   0.7690
   5.750   0.5216   0.01212   0.00587   0.0213   0.3445   0.7824
   6.000   0.5411   0.01229   0.00607   0.0229   0.3374   0.7952
   6.500   0.5851   0.01263   0.00650   0.0251   0.3243   0.8214
   6.750   0.6046   0.01290   0.00674   0.0265   0.3174   0.8347
   7.000   0.6268   0.01309   0.00700   0.0276   0.3112   0.8478
   7.250   0.6479   0.01332   0.00726   0.0288   0.3047   0.8602
   7.500   0.6659   0.01366   0.00759   0.0304   0.2980   0.8737
   7.750   0.6878   0.01389   0.00788   0.0315   0.2922   0.8853
   8.000   0.7067   0.01418   0.00819   0.0330   0.2857   0.8984
   8.250   0.7235   0.01462   0.00861   0.0349   0.2793   0.9098
   8.500   0.7437   0.01487   0.00891   0.0362   0.2739   0.9220
   8.750   0.7621   0.01528   0.00934   0.0377   0.2677   0.9328
   9.000   0.7783   0.01579   0.00981   0.0395   0.2616   0.9442
   9.250   0.8009   0.01616   0.01023   0.0402   0.2559   0.9539
   9.500   0.8230   0.01670   0.01074   0.0407   0.2497   0.9624
   9.750   0.8502   0.01731   0.01132   0.0400   0.2435   0.9686
  10.000   0.8758   0.01781   0.01184   0.0397   0.2374   0.9761
  10.250   0.9074   0.01859   0.01255   0.0377   0.2305   0.9787
  10.500   0.9424   0.01916   0.01314   0.0354   0.2244   0.9810
  10.750   0.9730   0.01990   0.01385   0.0336   0.2179   0.9842
  11.000   1.0007   0.02068   0.01462   0.0323   0.2120   0.9885
  11.250   1.0303   0.02137   0.01531   0.0308   0.2061   0.9915
  11.500   1.0572   0.02238   0.01626   0.0290   0.1999   0.9938
  11.750   1.0885   0.02307   0.01699   0.0270   0.1946   0.9963
  12.000   1.1154   0.02405   0.01794   0.0254   0.1892   0.9989
  12.250   1.1204   0.02500   0.01887   0.0274   0.1851   1.0000
  12.500   1.1179   0.02554   0.01946   0.0314   0.1822   1.0000
  12.750   1.1155   0.02626   0.02019   0.0350   0.1789   1.0000
  13.000   1.1131   0.02720   0.02111   0.0383   0.1757   1.0000
  13.250   1.1101   0.02840   0.02229   0.0413   0.1723   1.0000
  13.500   1.1178   0.02923   0.02316   0.0432   0.1693   1.0000
  13.750   1.1233   0.03034   0.02429   0.0449   0.1659   1.0000
  14.000   1.1270   0.03174   0.02568   0.0464   0.1627   1.0000
  14.250   1.1312   0.03325   0.02718   0.0476   0.1594   1.0000
  14.500   1.1415   0.03447   0.02845   0.0483   0.1565   1.0000
  14.750   1.1490   0.03595   0.02995   0.0490   0.1534   1.0000
  15.000   1.1533   0.03775   0.03175   0.0497   0.1505   1.0000
  15.250   1.1575   0.03961   0.03361   0.0503   0.1477   1.0000
  15.500   1.1675   0.04109   0.03516   0.0506   0.1450   1.0000
  15.750   1.1736   0.04295   0.03705   0.0508   0.1423   1.0000
  16.000   1.1774   0.04502   0.03912   0.0511   0.1397   1.0000
  16.250   1.1789   0.04732   0.04141   0.0513   0.1371   1.0000
  16.500   1.1871   0.04912   0.04329   0.0513   0.1349   1.0000
  16.750   1.1925   0.05122   0.04543   0.0512   0.1324   1.0000
  17.000   1.1951   0.05359   0.04783   0.0511   0.1301   1.0000
  17.250   1.1954   0.05617   0.05039   0.0510   0.1278   1.0000
  17.500   1.1993   0.05849   0.05278   0.0508   0.1257   1.0000
  17.750   1.2041   0.06078   0.05513   0.0504   0.1235   1.0000
  18.000   1.2057   0.06342   0.05781   0.0500   0.1213   1.0000
  18.250   1.2061   0.06617   0.06056   0.0496   0.1192   1.0000
  18.500   1.2057   0.06898   0.06338   0.0492   0.1170   1.0000
  18.750   1.2089   0.07156   0.06604   0.0486   0.1152   1.0000
  19.000   1.2096   0.07444   0.06899   0.0479   0.1131   1.0000
  19.250   1.2100   0.07733   0.07190   0.0472   0.1111   1.0000
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