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GOE 625 AIRFOIL (goe625-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 625 AIRFOIL (goe625-il)
Reynolds number: 500,000
Max Cl/Cd: 77.15 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe625-il-500000-n5.txt
Download as CSV file: xf-goe625-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.6533   0.08495   0.08165  -0.0939   0.9922   0.0411
 -16.500  -0.8508   0.05126   0.04738  -0.1195   0.9743   0.0411
 -16.250  -0.8974   0.03821   0.03394  -0.1329   0.9564   0.0413
 -16.000  -0.9063   0.03341   0.02891  -0.1375   0.9407   0.0418
 -15.750  -0.9084   0.03062   0.02593  -0.1388   0.9275   0.0423
 -15.500  -0.9069   0.02866   0.02382  -0.1387   0.9163   0.0428
 -15.250  -0.9014   0.02721   0.02227  -0.1381   0.9061   0.0434
 -15.000  -0.8931   0.02609   0.02105  -0.1369   0.8975   0.0441
 -14.750  -0.8829   0.02518   0.02006  -0.1355   0.8893   0.0450
 -14.500  -0.8724   0.02444   0.01921  -0.1337   0.8822   0.0458
 -14.250  -0.8567   0.02370   0.01835  -0.1327   0.8762   0.0468
 -14.000  -0.8395   0.02303   0.01760  -0.1317   0.8694   0.0477
 -13.750  -0.8203   0.02249   0.01699  -0.1308   0.8625   0.0485
 -13.500  -0.7998   0.02198   0.01642  -0.1301   0.8560   0.0495
 -13.250  -0.7785   0.02149   0.01585  -0.1294   0.8493   0.0506
 -13.000  -0.7571   0.02099   0.01523  -0.1287   0.8430   0.0517
 -12.750  -0.7348   0.02052   0.01468  -0.1280   0.8372   0.0527
 -12.500  -0.7112   0.02016   0.01428  -0.1276   0.8309   0.0536
 -12.250  -0.6871   0.01984   0.01390  -0.1271   0.8248   0.0547
 -12.000  -0.6627   0.01951   0.01347  -0.1266   0.8190   0.0559
 -11.750  -0.6382   0.01914   0.01301  -0.1262   0.8125   0.0571
 -11.500  -0.6137   0.01877   0.01254  -0.1258   0.8063   0.0581
 -11.250  -0.5889   0.01846   0.01218  -0.1254   0.8006   0.0589
 -11.000  -0.5633   0.01818   0.01187  -0.1251   0.7940   0.0598
 -10.750  -0.5377   0.01791   0.01153  -0.1247   0.7864   0.0607
 -10.500  -0.5120   0.01763   0.01116  -0.1244   0.7792   0.0617
 -10.250  -0.4860   0.01735   0.01079  -0.1241   0.7719   0.0628
 -10.000  -0.4596   0.01710   0.01042  -0.1238   0.7656   0.0637
  -9.750  -0.4339   0.01676   0.01005  -0.1235   0.7600   0.0646
  -9.500  -0.4075   0.01650   0.00976  -0.1233   0.7540   0.0655
  -9.250  -0.3809   0.01626   0.00947  -0.1231   0.7478   0.0663
  -9.000  -0.3542   0.01602   0.00917  -0.1229   0.7420   0.0672
  -8.750  -0.3272   0.01577   0.00886  -0.1227   0.7354   0.0681
  -8.500  -0.3003   0.01555   0.00856  -0.1225   0.7284   0.0691
  -8.250  -0.2730   0.01535   0.00827  -0.1223   0.7215   0.0700
  -8.000  -0.2460   0.01512   0.00797  -0.1222   0.7132   0.0707
  -7.750  -0.2201   0.01481   0.00762  -0.1218   0.7048   0.0717
  -7.500  -0.1931   0.01458   0.00737  -0.1217   0.6953   0.0727
  -7.250  -0.1662   0.01442   0.00714  -0.1214   0.6859   0.0738
  -7.000  -0.1389   0.01425   0.00692  -0.1213   0.6758   0.0750
  -6.750  -0.1120   0.01408   0.00667  -0.1210   0.6654   0.0759
  -6.500  -0.0851   0.01394   0.00644  -0.1208   0.6531   0.0768
  -6.250  -0.0582   0.01381   0.00622  -0.1205   0.6402   0.0775
  -6.000  -0.0319   0.01366   0.00598  -0.1202   0.6259   0.0780
  -5.750  -0.0065   0.01346   0.00572  -0.1197   0.6098   0.0790
  -5.500   0.0190   0.01334   0.00552  -0.1193   0.5922   0.0799
  -5.250   0.0445   0.01327   0.00535  -0.1188   0.5738   0.0809
  -5.000   0.0698   0.01323   0.00521  -0.1183   0.5548   0.0817
  -4.750   0.0951   0.01321   0.00508  -0.1177   0.5362   0.0825
  -4.500   0.1205   0.01320   0.00497  -0.1172   0.5193   0.0834
  -4.250   0.1463   0.01318   0.00487  -0.1168   0.5050   0.0843
  -4.000   0.1722   0.01317   0.00478  -0.1164   0.4937   0.0853
  -3.750   0.1982   0.01315   0.00469  -0.1160   0.4837   0.0863
  -3.500   0.2244   0.01309   0.00459  -0.1157   0.4759   0.0876
  -3.250   0.2508   0.01304   0.00452  -0.1154   0.4687   0.0889
  -2.750   0.3036   0.01300   0.00441  -0.1148   0.4572   0.0921
  -2.500   0.3305   0.01298   0.00437  -0.1146   0.4524   0.0939
  -2.250   0.3569   0.01297   0.00434  -0.1143   0.4478   0.0966
  -2.000   0.3829   0.01297   0.00433  -0.1140   0.4436   0.1007
  -1.750   0.4093   0.01296   0.00434  -0.1137   0.4402   0.1066
  -1.500   0.4363   0.01293   0.00435  -0.1136   0.4370   0.1158
  -1.250   0.4629   0.01294   0.00438  -0.1134   0.4337   0.1264
  -1.000   0.4892   0.01297   0.00442  -0.1131   0.4303   0.1361
  -0.750   0.5152   0.01302   0.00447  -0.1127   0.4271   0.1434
  -0.500   0.5409   0.01309   0.00452  -0.1124   0.4243   0.1501
  -0.250   0.5668   0.01316   0.00458  -0.1120   0.4218   0.1554
   0.000   0.5935   0.01318   0.00463  -0.1118   0.4200   0.1614
   0.250   0.6200   0.01322   0.00469  -0.1116   0.4181   0.1667
   0.500   0.6462   0.01326   0.00475  -0.1113   0.4161   0.1724
   0.750   0.6721   0.01331   0.00482  -0.1110   0.4140   0.1789
   1.000   0.6976   0.01339   0.00490  -0.1106   0.4117   0.1848
   1.250   0.7226   0.01346   0.00498  -0.1102   0.4093   0.1911
   1.500   0.7469   0.01356   0.00508  -0.1096   0.4067   0.1982
   2.000   0.7944   0.01373   0.00530  -0.1082   0.4017   0.2190
   2.250   0.8184   0.01374   0.00540  -0.1076   0.3996   0.2401
   2.500   0.8418   0.01372   0.00552  -0.1070   0.3972   0.2823
   2.750   0.8648   0.01363   0.00567  -0.1063   0.3945   0.3694
   3.000   0.8880   0.01358   0.00585  -0.1058   0.3915   0.4548
   3.250   0.9112   0.01348   0.00608  -0.1052   0.3885   0.5758
   3.500   0.9321   0.01325   0.00639  -0.1041   0.3858   0.7582
   3.750   0.9481   0.01313   0.00671  -0.1013   0.3838   0.9347
   4.000   0.9830   0.01326   0.00685  -0.1030   0.3822   1.0000
   4.250   1.0066   0.01343   0.00702  -0.1024   0.3804   1.0000
   4.500   1.0299   0.01363   0.00721  -0.1018   0.3782   1.0000
   4.750   1.0529   0.01384   0.00740  -0.1012   0.3758   1.0000
   5.000   1.0755   0.01408   0.00762  -0.1005   0.3733   1.0000
   5.250   1.0977   0.01434   0.00785  -0.0998   0.3710   1.0000
   5.500   1.1197   0.01462   0.00811  -0.0991   0.3689   1.0000
   5.750   1.1411   0.01495   0.00840  -0.0983   0.3667   1.0000
   6.000   1.1648   0.01518   0.00865  -0.0979   0.3649   1.0000
   6.250   1.1883   0.01542   0.00891  -0.0975   0.3629   1.0000
   6.500   1.2112   0.01570   0.00919  -0.0970   0.3606   1.0000
   6.750   1.2333   0.01600   0.00950  -0.0965   0.3579   1.0000
   7.000   1.2546   0.01634   0.00984  -0.0958   0.3550   1.0000
   7.250   1.2749   0.01673   0.01021  -0.0950   0.3520   1.0000
   7.500   1.2947   0.01716   0.01062  -0.0942   0.3489   1.0000
   7.750   1.3172   0.01748   0.01097  -0.0938   0.3456   1.0000
   8.000   1.3380   0.01787   0.01138  -0.0932   0.3411   1.0000
   8.250   1.3566   0.01837   0.01186  -0.0923   0.3364   1.0000
   8.500   1.3748   0.01891   0.01238  -0.0914   0.3323   1.0000
   8.750   1.3957   0.01933   0.01283  -0.0909   0.3283   1.0000
   9.000   1.4149   0.01984   0.01336  -0.0902   0.3236   1.0000
   9.250   1.4319   0.02048   0.01398  -0.0893   0.3188   1.0000
   9.500   1.4497   0.02109   0.01460  -0.0884   0.3141   1.0000
   9.750   1.4672   0.02172   0.01525  -0.0876   0.3079   1.0000
  10.000   1.4805   0.02261   0.01610  -0.0864   0.3014   1.0000
  10.250   1.4965   0.02336   0.01686  -0.0855   0.2942   1.0000
  10.750   1.5208   0.02539   0.01886  -0.0831   0.2788   1.0000
  11.000   1.5296   0.02666   0.02010  -0.0816   0.2713   1.0000
  11.250   1.5417   0.02773   0.02118  -0.0806   0.2647   1.0000
  11.500   1.5506   0.02907   0.02252  -0.0793   0.2583   1.0000
  11.750   1.5607   0.03036   0.02381  -0.0782   0.2533   1.0000
  12.000   1.5713   0.03164   0.02511  -0.0771   0.2485   1.0000
  12.250   1.5799   0.03309   0.02657  -0.0760   0.2439   1.0000
  12.500   1.5866   0.03473   0.02823  -0.0748   0.2398   1.0000
  12.750   1.5965   0.03615   0.02968  -0.0740   0.2355   1.0000
  13.000   1.6027   0.03791   0.03146  -0.0729   0.2306   1.0000
  13.250   1.6052   0.04002   0.03357  -0.0717   0.2261   1.0000
  13.500   1.6131   0.04170   0.03529  -0.0710   0.2224   1.0000
  13.750   1.6192   0.04359   0.03723  -0.0701   0.2185   1.0000
  14.000   1.6226   0.04576   0.03943  -0.0693   0.2147   1.0000
  14.250   1.6239   0.04816   0.04186  -0.0684   0.2114   1.0000
  14.500   1.6285   0.05030   0.04405  -0.0677   0.2087   1.0000
  14.750   1.6348   0.05228   0.04610  -0.0672   0.2060   1.0000
  15.000   1.6384   0.05458   0.04845  -0.0667   0.2033   1.0000
  15.250   1.6395   0.05717   0.05110  -0.0661   0.2005   1.0000
  15.500   1.6378   0.06010   0.05407  -0.0655   0.1976   1.0000
  15.750   1.6367   0.06297   0.05699  -0.0651   0.1950   1.0000
  16.000   1.6401   0.06541   0.05951  -0.0648   0.1925   1.0000
  16.250   1.6416   0.06808   0.06225  -0.0645   0.1896   1.0000
  16.500   1.6399   0.07114   0.06537  -0.0643   0.1867   1.0000
  16.750   1.6351   0.07460   0.06888  -0.0641   0.1839   1.0000
  17.000   1.6292   0.07818   0.07251  -0.0639   0.1812   1.0000
  17.250   1.6311   0.08087   0.07528  -0.0639   0.1784   1.0000
  17.500   1.6280   0.08420   0.07868  -0.0639   0.1747   1.0000
  17.750   1.6197   0.08820   0.08272  -0.0640   0.1704   1.0000
  18.000   1.6138   0.09190   0.08646  -0.0642   0.1668   1.0000
  18.250   1.6100   0.09535   0.08998  -0.0644   0.1623   1.0000
  18.500   1.6016   0.09940   0.09407  -0.0648   0.1571   1.0000
  18.750   1.5947   0.10331   0.09802  -0.0652   0.1525   1.0000
  19.000   1.5855   0.10754   0.10229  -0.0657   0.1458   1.0000
  19.250   1.5744   0.11203   0.10679  -0.0664   0.1377   1.0000
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