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GOE 625 AIRFOIL (goe625-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 625 AIRFOIL (goe625-il)
Reynolds number: 200,000
Max Cl/Cd: 57.43 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe625-il-200000-n5.txt
Download as CSV file: xf-goe625-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 625 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.5345   0.04022   0.03492  -0.1411   0.9127   0.0620
 -12.500  -0.5596   0.03674   0.03105  -0.1398   0.9009   0.0629
 -12.250  -0.5715   0.03437   0.02828  -0.1376   0.8914   0.0640
 -12.000  -0.5535   0.03382   0.02775  -0.1367   0.8841   0.0646
 -11.750  -0.5359   0.03318   0.02705  -0.1358   0.8776   0.0655
 -11.500  -0.5217   0.03240   0.02619  -0.1346   0.8694   0.0664
 -11.250  -0.5075   0.03136   0.02496  -0.1336   0.8626   0.0677
 -11.000  -0.4949   0.03010   0.02343  -0.1324   0.8559   0.0691
 -10.750  -0.4831   0.02880   0.02175  -0.1310   0.8482   0.0705
 -10.500  -0.4605   0.02814   0.02109  -0.1304   0.8421   0.0713
 -10.250  -0.4388   0.02762   0.02056  -0.1297   0.8345   0.0723
 -10.000  -0.4176   0.02702   0.01988  -0.1289   0.8262   0.0735
  -9.750  -0.3958   0.02630   0.01897  -0.1283   0.8197   0.0750
  -9.500  -0.3757   0.02555   0.01803  -0.1274   0.8121   0.0764
  -9.250  -0.3543   0.02481   0.01701  -0.1267   0.8063   0.0778
  -9.000  -0.3292   0.02416   0.01636  -0.1264   0.8015   0.0790
  -8.750  -0.3055   0.02371   0.01593  -0.1259   0.7947   0.0802
  -8.500  -0.2811   0.02324   0.01540  -0.1255   0.7880   0.0816
  -8.250  -0.2559   0.02270   0.01471  -0.1251   0.7823   0.0831
  -8.000  -0.2322   0.02218   0.01405  -0.1246   0.7748   0.0847
  -7.750  -0.2073   0.02165   0.01334  -0.1241   0.7678   0.0860
  -7.500  -0.1814   0.02109   0.01277  -0.1239   0.7618   0.0872
  -7.250  -0.1564   0.02069   0.01238  -0.1234   0.7540   0.0884
  -7.000  -0.1303   0.02029   0.01191  -0.1231   0.7469   0.0898
  -6.750  -0.1044   0.01988   0.01143  -0.1228   0.7396   0.0912
  -6.500  -0.0787   0.01948   0.01093  -0.1224   0.7312   0.0925
  -6.250  -0.0522   0.01909   0.01041  -0.1221   0.7233   0.0938
  -6.000  -0.0267   0.01871   0.00997  -0.1216   0.7134   0.0951
  -5.750  -0.0006   0.01835   0.00958  -0.1213   0.7040   0.0964
  -5.500   0.0251   0.01805   0.00924  -0.1208   0.6929   0.0976
  -5.250   0.0512   0.01777   0.00890  -0.1204   0.6820   0.0990
  -5.000   0.0772   0.01752   0.00857  -0.1200   0.6701   0.1007
  -4.750   0.1030   0.01729   0.00826  -0.1196   0.6576   0.1025
  -4.500   0.1288   0.01708   0.00794  -0.1191   0.6445   0.1041
  -4.250   0.1540   0.01687   0.00768  -0.1185   0.6305   0.1058
  -4.000   0.1791   0.01672   0.00748  -0.1180   0.6151   0.1077
  -3.750   0.2042   0.01661   0.00728  -0.1174   0.5997   0.1099
  -3.500   0.2290   0.01652   0.00708  -0.1168   0.5844   0.1126
  -3.250   0.2534   0.01645   0.00692  -0.1161   0.5695   0.1156
  -3.000   0.2775   0.01644   0.00683  -0.1153   0.5552   0.1191
  -2.750   0.3020   0.01642   0.00673  -0.1147   0.5419   0.1237
  -2.500   0.3265   0.01641   0.00666  -0.1140   0.5306   0.1284
  -2.250   0.3509   0.01644   0.00662  -0.1134   0.5207   0.1344
  -2.000   0.3759   0.01645   0.00659  -0.1129   0.5124   0.1411
  -1.750   0.4009   0.01649   0.00658  -0.1123   0.5046   0.1488
  -1.500   0.4256   0.01655   0.00658  -0.1118   0.4983   0.1564
  -1.250   0.4514   0.01659   0.00660  -0.1114   0.4923   0.1647
  -1.000   0.4767   0.01663   0.00661  -0.1110   0.4867   0.1721
  -0.750   0.5018   0.01671   0.00664  -0.1106   0.4819   0.1797
  -0.500   0.5276   0.01679   0.00667  -0.1102   0.4777   0.1866
  -0.250   0.5532   0.01680   0.00672  -0.1099   0.4732   0.1939
   0.000   0.5787   0.01688   0.00676  -0.1096   0.4688   0.2016
   0.250   0.6040   0.01695   0.00682  -0.1092   0.4649   0.2100
   0.500   0.6296   0.01706   0.00690  -0.1089   0.4616   0.2211
   0.750   0.6556   0.01710   0.00699  -0.1087   0.4587   0.2341
   1.000   0.6815   0.01713   0.00709  -0.1085   0.4557   0.2507
   1.250   0.7070   0.01713   0.00722  -0.1083   0.4527   0.2813
   1.500   0.7319   0.01702   0.00737  -0.1080   0.4499   0.3563
   1.750   0.7556   0.01682   0.00755  -0.1075   0.4470   0.4793
   2.000   0.7765   0.01649   0.00779  -0.1063   0.4443   0.6586
   2.250   0.7960   0.01634   0.00810  -0.1039   0.4418   0.8438
   2.500   0.8401   0.01651   0.00838  -0.1070   0.4392   0.9663
   2.750   0.8771   0.01674   0.00857  -0.1092   0.4366   1.0000
   3.000   0.8993   0.01694   0.00873  -0.1083   0.4338   1.0000
   3.250   0.9210   0.01715   0.00889  -0.1073   0.4305   1.0000
   3.500   0.9431   0.01739   0.00904  -0.1064   0.4270   1.0000
   3.750   0.9664   0.01766   0.00920  -0.1058   0.4234   1.0000
   4.000   0.9878   0.01791   0.00941  -0.1048   0.4200   1.0000
   4.250   1.0074   0.01813   0.00964  -0.1035   0.4163   1.0000
   4.500   1.0275   0.01837   0.00986  -0.1023   0.4132   1.0000
   4.750   1.0483   0.01863   0.01009  -0.1012   0.4103   1.0000
   5.000   1.0698   0.01891   0.01032  -0.1003   0.4077   1.0000
   5.250   1.0928   0.01921   0.01056  -0.0997   0.4051   1.0000
   5.500   1.1175   0.01953   0.01081  -0.0995   0.4027   1.0000
   5.750   1.1367   0.01983   0.01116  -0.0982   0.4004   1.0000
   6.000   1.1564   0.02015   0.01151  -0.0972   0.3978   1.0000
   6.250   1.1762   0.02048   0.01187  -0.0961   0.3950   1.0000
   6.500   1.1957   0.02083   0.01222  -0.0950   0.3921   1.0000
   6.750   1.2157   0.02118   0.01256  -0.0941   0.3892   1.0000
   7.000   1.2369   0.02154   0.01288  -0.0934   0.3865   1.0000
   7.250   1.2587   0.02192   0.01322  -0.0928   0.3838   1.0000
   7.500   1.2754   0.02237   0.01375  -0.0914   0.3810   1.0000
   7.750   1.2928   0.02282   0.01426  -0.0902   0.3779   1.0000
   8.000   1.3102   0.02329   0.01477  -0.0891   0.3748   1.0000
   8.250   1.3278   0.02376   0.01526  -0.0880   0.3717   1.0000
   8.500   1.3465   0.02422   0.01570  -0.0871   0.3689   1.0000
   8.750   1.3655   0.02470   0.01616  -0.0862   0.3660   1.0000
   9.000   1.3788   0.02536   0.01693  -0.0847   0.3623   1.0000
   9.250   1.3927   0.02602   0.01767  -0.0834   0.3584   1.0000
   9.500   1.4070   0.02667   0.01835  -0.0821   0.3545   1.0000
   9.750   1.4222   0.02731   0.01897  -0.0809   0.3511   1.0000
  10.000   1.4362   0.02805   0.01976  -0.0797   0.3474   1.0000
  10.250   1.4473   0.02895   0.02078  -0.0783   0.3427   1.0000
  10.500   1.4586   0.02985   0.02171  -0.0770   0.3379   1.0000
  10.750   1.4703   0.03072   0.02257  -0.0757   0.3336   1.0000
  11.000   1.4799   0.03184   0.02379  -0.0743   0.3283   1.0000
  11.250   1.4886   0.03301   0.02502  -0.0730   0.3227   1.0000
  11.500   1.4973   0.03417   0.02618  -0.0716   0.3179   1.0000
  11.750   1.5053   0.03552   0.02761  -0.0704   0.3125   1.0000
  12.000   1.5123   0.03695   0.02910  -0.0692   0.3067   1.0000
  12.250   1.5187   0.03844   0.03057  -0.0679   0.3017   1.0000
  12.500   1.5248   0.04009   0.03232  -0.0669   0.2961   1.0000
  12.750   1.5296   0.04186   0.03412  -0.0657   0.2905   1.0000
  13.000   1.5341   0.04368   0.03593  -0.0647   0.2858   1.0000
  13.250   1.5387   0.04563   0.03797  -0.0638   0.2809   1.0000
  13.500   1.5424   0.04766   0.04004  -0.0629   0.2761   1.0000
  13.750   1.5455   0.04975   0.04213  -0.0620   0.2720   1.0000
  14.000   1.5486   0.05195   0.04441  -0.0612   0.2679   1.0000
  14.250   1.5505   0.05434   0.04686  -0.0605   0.2634   1.0000
  14.500   1.5518   0.05678   0.04932  -0.0599   0.2592   1.0000
  14.750   1.5552   0.05895   0.05147  -0.0593   0.2556   1.0000
  15.000   1.5557   0.06164   0.05428  -0.0588   0.2520   1.0000
  15.250   1.5557   0.06439   0.05712  -0.0584   0.2484   1.0000
  15.500   1.5566   0.06703   0.05980  -0.0580   0.2449   1.0000
  15.750   1.5597   0.06938   0.06213  -0.0577   0.2416   1.0000
  16.000   1.5591   0.07226   0.06508  -0.0575   0.2383   1.0000
  16.250   1.5557   0.07559   0.06854  -0.0574   0.2348   1.0000
  16.500   1.5537   0.07872   0.07174  -0.0573   0.2313   1.0000
  16.750   1.5551   0.08140   0.07444  -0.0573   0.2280   1.0000
  17.000   1.5611   0.08344   0.07645  -0.0572   0.2249   1.0000
  17.250   1.5529   0.08752   0.08070  -0.0575   0.2219   1.0000
  17.500   1.5465   0.09137   0.08468  -0.0578   0.2186   1.0000
  17.750   1.5444   0.09463   0.08800  -0.0581   0.2154   1.0000
  18.000   1.5481   0.09705   0.09043  -0.0583   0.2122   1.0000
  18.250   1.5479   0.10006   0.09347  -0.0587   0.2089   1.0000
  18.500   1.5341   0.10510   0.09869  -0.0595   0.2053   1.0000
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