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GOE 675 AIRFOIL (goe675-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 675 AIRFOIL (goe675-il)
Reynolds number: 500,000
Max Cl/Cd: 90.23 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe675-il-500000-n5.txt
Download as CSV file: xf-goe675-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 675 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.5187   0.07928   0.07592  -0.0958   0.9270   0.0291
 -14.000  -0.6046   0.06276   0.05911  -0.1075   0.9160   0.0291
 -13.750  -0.6955   0.04472   0.04070  -0.1234   0.9021   0.0290
 -13.500  -0.7266   0.03169   0.02718  -0.1403   0.8914   0.0290
 -13.250  -0.7172   0.02945   0.02477  -0.1415   0.8866   0.0292
 -13.000  -0.7029   0.02777   0.02296  -0.1421   0.8823   0.0294
 -12.750  -0.6862   0.02636   0.02144  -0.1424   0.8778   0.0296
 -12.500  -0.6679   0.02514   0.02010  -0.1425   0.8737   0.0298
 -12.250  -0.6482   0.02405   0.01888  -0.1425   0.8700   0.0300
 -12.000  -0.6273   0.02307   0.01777  -0.1425   0.8666   0.0303
 -11.750  -0.6053   0.02215   0.01676  -0.1425   0.8630   0.0305
 -11.500  -0.5827   0.02131   0.01582  -0.1424   0.8593   0.0308
 -11.250  -0.5594   0.02053   0.01494  -0.1423   0.8556   0.0311
 -11.000  -0.5356   0.01982   0.01411  -0.1422   0.8522   0.0313
 -10.750  -0.5112   0.01916   0.01333  -0.1421   0.8491   0.0316
 -10.500  -0.4862   0.01854   0.01262  -0.1420   0.8459   0.0319
 -10.250  -0.4609   0.01796   0.01196  -0.1419   0.8424   0.0322
 -10.000  -0.4355   0.01738   0.01130  -0.1418   0.8388   0.0325
  -9.750  -0.4101   0.01678   0.01064  -0.1417   0.8355   0.0329
  -9.500  -0.3842   0.01625   0.01004  -0.1417   0.8324   0.0334
  -9.250  -0.3577   0.01579   0.00950  -0.1416   0.8294   0.0338
  -9.000  -0.3310   0.01535   0.00902  -0.1416   0.8259   0.0344
  -8.750  -0.3040   0.01495   0.00856  -0.1416   0.8225   0.0350
  -8.500  -0.2768   0.01457   0.00812  -0.1415   0.8192   0.0357
  -8.250  -0.2494   0.01422   0.00770  -0.1415   0.8158   0.0363
  -8.000  -0.2220   0.01384   0.00726  -0.1415   0.8127   0.0370
  -7.750  -0.1945   0.01349   0.00687  -0.1415   0.8094   0.0380
  -7.500  -0.1668   0.01316   0.00652  -0.1415   0.8055   0.0390
  -7.250  -0.1390   0.01287   0.00617  -0.1414   0.8009   0.0403
  -7.000  -0.1112   0.01257   0.00582  -0.1414   0.7960   0.0419
  -6.750  -0.0833   0.01230   0.00552  -0.1414   0.7915   0.0444
  -6.500  -0.0553   0.01205   0.00529  -0.1414   0.7867   0.0477
  -6.250  -0.0270   0.01186   0.00511  -0.1414   0.7821   0.0523
  -6.000   0.0015   0.01173   0.00494  -0.1414   0.7775   0.0573
  -5.750   0.0301   0.01162   0.00480  -0.1414   0.7727   0.0618
  -5.500   0.0588   0.01153   0.00471  -0.1415   0.7678   0.0649
  -5.250   0.0874   0.01145   0.00457  -0.1415   0.7626   0.0679
  -5.000   0.1158   0.01134   0.00441  -0.1415   0.7576   0.0700
  -4.750   0.1443   0.01124   0.00432  -0.1415   0.7518   0.0721
  -4.500   0.1728   0.01115   0.00418  -0.1415   0.7457   0.0741
  -4.250   0.2012   0.01108   0.00403  -0.1414   0.7399   0.0758
  -4.000   0.2294   0.01094   0.00389  -0.1414   0.7332   0.0774
  -3.750   0.2576   0.01084   0.00377  -0.1414   0.7265   0.0793
  -3.500   0.2859   0.01078   0.00368  -0.1414   0.7207   0.0816
  -3.250   0.3144   0.01070   0.00359  -0.1414   0.7145   0.0836
  -3.000   0.3426   0.01064   0.00348  -0.1414   0.7081   0.0849
  -2.750   0.3706   0.01051   0.00334  -0.1413   0.7017   0.0867
  -2.500   0.3985   0.01043   0.00326  -0.1413   0.6937   0.0889
  -2.250   0.4263   0.01039   0.00318  -0.1411   0.6860   0.0912
  -2.000   0.4544   0.01033   0.00311  -0.1411   0.6780   0.0931
  -1.750   0.4819   0.01031   0.00302  -0.1409   0.6698   0.0944
  -1.500   0.5096   0.01024   0.00295  -0.1408   0.6605   0.0959
  -1.250   0.5366   0.01022   0.00289  -0.1405   0.6505   0.0979
  -1.000   0.5638   0.01019   0.00285  -0.1403   0.6393   0.1001
  -0.750   0.5908   0.01021   0.00283  -0.1401   0.6287   0.1027
  -0.500   0.6172   0.01025   0.00281  -0.1397   0.6166   0.1056
  -0.250   0.6436   0.01027   0.00282  -0.1394   0.6028   0.1102
   0.000   0.6693   0.01033   0.00284  -0.1389   0.5875   0.1156
   0.250   0.6945   0.01042   0.00288  -0.1383   0.5707   0.1228
   0.750   0.7433   0.01066   0.00303  -0.1369   0.5331   0.1438
   1.000   0.7663   0.01084   0.00314  -0.1360   0.5113   0.1566
   1.250   0.7888   0.01104   0.00327  -0.1350   0.4905   0.1729
   1.500   0.8116   0.01120   0.00343  -0.1341   0.4732   0.2009
   1.750   0.8354   0.01129   0.00360  -0.1334   0.4598   0.2481
   2.000   0.8591   0.01142   0.00376  -0.1327   0.4490   0.2854
   2.250   0.8824   0.01157   0.00394  -0.1319   0.4388   0.3168
   2.500   0.9066   0.01166   0.00410  -0.1313   0.4305   0.3566
   2.750   0.9303   0.01170   0.00430  -0.1307   0.4230   0.4301
   3.000   0.9534   0.01158   0.00454  -0.1301   0.4171   0.5831
   3.250   0.9761   0.01095   0.00480  -0.1287   0.4116   1.0000
   3.500   0.9992   0.01118   0.00497  -0.1279   0.4056   1.0000
   3.750   1.0209   0.01144   0.00517  -0.1268   0.4001   1.0000
   4.000   1.0441   0.01161   0.00534  -0.1259   0.3959   1.0000
   4.250   1.0665   0.01182   0.00552  -0.1249   0.3914   1.0000
   4.500   1.0880   0.01206   0.00573  -0.1238   0.3865   1.0000
   4.750   1.1086   0.01237   0.00599  -0.1225   0.3815   1.0000
   5.000   1.1316   0.01258   0.00620  -0.1217   0.3768   1.0000
   5.250   1.1537   0.01283   0.00644  -0.1208   0.3712   1.0000
   5.500   1.1739   0.01317   0.00673  -0.1195   0.3649   1.0000
   5.750   1.1957   0.01345   0.00700  -0.1186   0.3591   1.0000
   6.000   1.2170   0.01375   0.00729  -0.1176   0.3523   1.0000
   6.250   1.2364   0.01415   0.00764  -0.1163   0.3457   1.0000
   6.500   1.2585   0.01444   0.00794  -0.1155   0.3407   1.0000
   6.750   1.2797   0.01477   0.00826  -0.1146   0.3354   1.0000
   7.000   1.2995   0.01517   0.00865  -0.1135   0.3300   1.0000
   7.250   1.3199   0.01555   0.00903  -0.1125   0.3249   1.0000
   7.500   1.3408   0.01592   0.00940  -0.1116   0.3193   1.0000
   7.750   1.3597   0.01638   0.00985  -0.1104   0.3131   1.0000
   8.000   1.3789   0.01684   0.01030  -0.1093   0.3060   1.0000
   8.250   1.3967   0.01738   0.01081  -0.1081   0.2971   1.0000
   8.500   1.4149   0.01792   0.01133  -0.1069   0.2896   1.0000
   8.750   1.4323   0.01849   0.01190  -0.1057   0.2814   1.0000
   9.000   1.4496   0.01909   0.01248  -0.1045   0.2742   1.0000
   9.250   1.4656   0.01977   0.01314  -0.1031   0.2649   1.0000
   9.500   1.4818   0.02045   0.01381  -0.1018   0.2560   1.0000
   9.750   1.4953   0.02130   0.01462  -0.1002   0.2452   1.0000
  10.000   1.5072   0.02227   0.01552  -0.0985   0.2310   1.0000
  10.250   1.5178   0.02334   0.01652  -0.0967   0.2160   1.0000
  10.500   1.5276   0.02449   0.01760  -0.0949   0.2008   1.0000
  10.750   1.5358   0.02575   0.01880  -0.0930   0.1856   1.0000
  11.000   1.5437   0.02707   0.02006  -0.0911   0.1714   1.0000
  11.250   1.5507   0.02849   0.02142  -0.0892   0.1585   1.0000
  11.500   1.5574   0.02995   0.02283  -0.0873   0.1460   1.0000
  11.750   1.5614   0.03166   0.02448  -0.0853   0.1302   1.0000
  12.000   1.5616   0.03373   0.02646  -0.0831   0.1114   1.0000
  12.250   1.5594   0.03608   0.02870  -0.0809   0.0923   1.0000
  12.500   1.5579   0.03845   0.03101  -0.0789   0.0785   1.0000
  12.750   1.5573   0.04083   0.03336  -0.0772   0.0661   1.0000
  13.000   1.5465   0.04426   0.03669  -0.0750   0.0452   1.0000
  13.250   1.5457   0.04687   0.03931  -0.0736   0.0398   1.0000
  13.500   1.5480   0.04925   0.04172  -0.0725   0.0375   1.0000
  13.750   1.5501   0.05171   0.04424  -0.0716   0.0358   1.0000
  14.000   1.5537   0.05407   0.04667  -0.0708   0.0347   1.0000
  14.250   1.5563   0.05658   0.04925  -0.0700   0.0339   1.0000
  14.500   1.5577   0.05927   0.05201  -0.0693   0.0332   1.0000
  14.750   1.5584   0.06210   0.05492  -0.0688   0.0326   1.0000
  15.000   1.5580   0.06512   0.05801  -0.0683   0.0321   1.0000
  15.250   1.5560   0.06840   0.06137  -0.0679   0.0316   1.0000
  15.500   1.5528   0.07185   0.06491  -0.0676   0.0312   1.0000
  15.750   1.5513   0.07517   0.06832  -0.0674   0.0309   1.0000
  16.000   1.5489   0.07866   0.07192  -0.0674   0.0306   1.0000
  16.250   1.5455   0.08233   0.07568  -0.0675   0.0303   1.0000
  16.500   1.5415   0.08613   0.07958  -0.0677   0.0300   1.0000
  16.750   1.5366   0.09008   0.08362  -0.0679   0.0297   1.0000
  17.000   1.5311   0.09415   0.08779  -0.0684   0.0294   1.0000
  17.250   1.5250   0.09835   0.09208  -0.0689   0.0291   1.0000
  17.500   1.5186   0.10264   0.09647  -0.0696   0.0288   1.0000
  17.750   1.5118   0.10702   0.10094  -0.0703   0.0285   1.0000
  18.000   1.5048   0.11143   0.10544  -0.0712   0.0283   1.0000
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