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GOE 628 AIRFOIL (goe628-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 628 AIRFOIL (goe628-il)
Reynolds number: 500,000
Max Cl/Cd: 88.62 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe628-il-500000.txt
Download as CSV file: xf-goe628-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 628 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.2159   0.14591   0.14359  -0.0459   1.0000   0.0380
 -15.500  -0.6940   0.07051   0.06723  -0.0875   1.0000   0.0429
 -15.250  -0.7455   0.06109   0.05762  -0.0941   1.0000   0.0431
 -15.000  -0.7446   0.05896   0.05553  -0.0943   1.0000   0.0436
 -14.750  -0.7465   0.05658   0.05316  -0.0949   1.0000   0.0439
 -14.500  -0.7560   0.05348   0.05005  -0.0961   1.0000   0.0443
 -14.250  -0.7829   0.04889   0.04537  -0.0981   1.0000   0.0445
 -14.000  -0.8101   0.04523   0.04164  -0.0987   1.0000   0.0447
 -13.750  -0.8245   0.04181   0.03815  -0.1013   0.9990   0.0450
 -13.500  -0.8048   0.03826   0.03444  -0.1101   0.9937   0.0457
 -13.250  -0.7910   0.03586   0.03185  -0.1140   0.9865   0.0466
 -13.000  -0.7680   0.03347   0.02918  -0.1186   0.9814   0.0476
 -12.750  -0.7502   0.03172   0.02713  -0.1207   0.9745   0.0484
 -12.500  -0.7221   0.02986   0.02531  -0.1225   0.9710   0.0493
 -12.250  -0.6883   0.02901   0.02447  -0.1247   0.9685   0.0502
 -12.000  -0.6534   0.02803   0.02346  -0.1271   0.9665   0.0512
 -11.750  -0.6289   0.02699   0.02231  -0.1278   0.9595   0.0521
 -11.500  -0.5982   0.02590   0.02104  -0.1297   0.9547   0.0531
 -11.250  -0.5646   0.02512   0.02003  -0.1319   0.9507   0.0539
 -11.000  -0.5444   0.02340   0.01821  -0.1317   0.9403   0.0548
 -10.750  -0.5112   0.02233   0.01717  -0.1333   0.9345   0.0559
 -10.500  -0.4876   0.02172   0.01652  -0.1328   0.9227   0.0569
 -10.250  -0.4605   0.02117   0.01591  -0.1330   0.9120   0.0581
 -10.000  -0.4355   0.02051   0.01511  -0.1327   0.8998   0.0589
  -9.750  -0.4133   0.01986   0.01432  -0.1318   0.8856   0.0594
  -9.500  -0.3901   0.01925   0.01357  -0.1310   0.8711   0.0598
  -9.250  -0.3665   0.01875   0.01292  -0.1302   0.8562   0.0602
  -9.000  -0.3434   0.01811   0.01213  -0.1293   0.8412   0.0607
  -8.750  -0.3214   0.01712   0.01107  -0.1284   0.8258   0.0613
  -8.500  -0.2986   0.01647   0.01035  -0.1274   0.8108   0.0618
  -8.250  -0.2753   0.01594   0.00975  -0.1266   0.7974   0.0624
  -8.000  -0.2515   0.01550   0.00922  -0.1257   0.7854   0.0629
  -7.750  -0.2276   0.01509   0.00874  -0.1249   0.7737   0.0634
  -7.500  -0.2033   0.01472   0.00829  -0.1241   0.7636   0.0640
  -7.250  -0.1788   0.01438   0.00787  -0.1234   0.7538   0.0647
  -7.000  -0.1539   0.01408   0.00749  -0.1227   0.7453   0.0655
  -6.750  -0.1289   0.01378   0.00712  -0.1220   0.7366   0.0661
  -6.500  -0.1037   0.01352   0.00676  -0.1213   0.7283   0.0667
  -6.250  -0.0785   0.01324   0.00644  -0.1206   0.7193   0.0672
  -6.000  -0.0536   0.01300   0.00607  -0.1198   0.7099   0.0678
  -5.750  -0.0295   0.01258   0.00565  -0.1190   0.7007   0.0688
  -5.500  -0.0044   0.01231   0.00531  -0.1183   0.6927   0.0699
  -5.250   0.0215   0.01206   0.00504  -0.1178   0.6860   0.0710
  -5.000   0.0476   0.01184   0.00479  -0.1172   0.6789   0.0722
  -4.750   0.0739   0.01170   0.00455  -0.1167   0.6721   0.0737
  -4.500   0.1006   0.01152   0.00435  -0.1162   0.6653   0.0753
  -4.250   0.1267   0.01128   0.00410  -0.1157   0.6584   0.0780
  -4.000   0.1533   0.01115   0.00391  -0.1152   0.6520   0.0811
  -3.750   0.1799   0.01094   0.00374  -0.1147   0.6454   0.0866
  -3.500   0.2059   0.01070   0.00355  -0.1142   0.6382   0.1027
  -3.250   0.2310   0.01033   0.00335  -0.1136   0.6316   0.1513
  -3.000   0.2571   0.01009   0.00327  -0.1131   0.6243   0.1943
  -2.750   0.2838   0.01004   0.00323  -0.1127   0.6174   0.2180
  -2.500   0.3109   0.01001   0.00321  -0.1123   0.6108   0.2353
  -2.250   0.3379   0.00998   0.00321  -0.1119   0.6031   0.2496
  -1.750   0.3918   0.01000   0.00318  -0.1110   0.5877   0.2703
  -1.500   0.4182   0.01001   0.00318  -0.1104   0.5799   0.2796
  -1.250   0.4452   0.01005   0.00318  -0.1100   0.5725   0.2884
  -1.000   0.4716   0.01005   0.00319  -0.1095   0.5642   0.2965
  -0.750   0.4980   0.01011   0.00320  -0.1090   0.5563   0.3048
  -0.500   0.5244   0.01013   0.00321  -0.1084   0.5472   0.3126
  -0.250   0.5502   0.01019   0.00324  -0.1078   0.5385   0.3206
   0.000   0.5766   0.01025   0.00327  -0.1073   0.5290   0.3284
   0.250   0.6018   0.01030   0.00331  -0.1066   0.5200   0.3375
   0.500   0.6279   0.01038   0.00336  -0.1060   0.5102   0.3461
   0.750   0.6528   0.01043   0.00341  -0.1053   0.5007   0.3542
   1.000   0.6780   0.01052   0.00347  -0.1046   0.4899   0.3629
   1.250   0.7028   0.01059   0.00352  -0.1038   0.4793   0.3712
   1.750   0.7512   0.01082   0.00367  -0.1021   0.4558   0.3876
   2.000   0.7746   0.01091   0.00375  -0.1011   0.4446   0.3955
   2.250   0.7975   0.01107   0.00385  -0.1000   0.4327   0.4034
   2.500   0.8211   0.01117   0.00395  -0.0991   0.4215   0.4118
   2.750   0.8435   0.01134   0.00408  -0.0980   0.4108   0.4216
   3.000   0.8657   0.01148   0.00421  -0.0968   0.4001   0.4316
   3.250   0.8881   0.01164   0.00435  -0.0957   0.3909   0.4429
   3.500   0.9095   0.01179   0.00450  -0.0944   0.3822   0.4554
   3.750   0.9313   0.01193   0.00467  -0.0932   0.3750   0.4712
   4.000   0.9528   0.01205   0.00484  -0.0920   0.3681   0.4921
   4.250   0.9716   0.01222   0.00504  -0.0903   0.3617   0.5227
   4.500   0.9899   0.01212   0.00525  -0.0884   0.3568   0.6134
   4.750   1.0519   0.01187   0.00569  -0.0958   0.3489   1.0000
   5.000   1.0699   0.01219   0.00593  -0.0939   0.3436   1.0000
   5.250   1.0911   0.01236   0.00610  -0.0926   0.3399   1.0000
   5.500   1.1108   0.01257   0.00630  -0.0910   0.3358   1.0000
   5.750   1.1294   0.01284   0.00653  -0.0893   0.3319   1.0000
   6.000   1.1469   0.01317   0.00680  -0.0874   0.3278   1.0000
   6.250   1.1668   0.01344   0.00706  -0.0860   0.3244   1.0000
   6.500   1.1872   0.01365   0.00730  -0.0847   0.3211   1.0000
   6.750   1.2067   0.01392   0.00756  -0.0832   0.3176   1.0000
   7.000   1.2256   0.01423   0.00784  -0.0817   0.3143   1.0000
   7.250   1.2437   0.01462   0.00819  -0.0801   0.3110   1.0000
   7.500   1.2633   0.01497   0.00854  -0.0788   0.3080   1.0000
   7.750   1.2833   0.01523   0.00884  -0.0776   0.3054   1.0000
   8.000   1.3025   0.01553   0.00916  -0.0763   0.3024   1.0000
   8.250   1.3214   0.01586   0.00950  -0.0750   0.2995   1.0000
   8.500   1.3395   0.01625   0.00988  -0.0736   0.2967   1.0000
   8.750   1.3575   0.01674   0.01033  -0.0722   0.2934   1.0000
   9.000   1.3761   0.01712   0.01074  -0.0710   0.2905   1.0000
   9.250   1.3938   0.01746   0.01114  -0.0696   0.2875   1.0000
   9.500   1.4112   0.01785   0.01156  -0.0683   0.2841   1.0000
   9.750   1.4279   0.01831   0.01202  -0.0669   0.2810   1.0000
  10.000   1.4441   0.01885   0.01254  -0.0655   0.2779   1.0000
  10.250   1.4617   0.01941   0.01309  -0.0643   0.2749   1.0000
  10.500   1.4788   0.01986   0.01363  -0.0632   0.2729   1.0000
  10.750   1.4957   0.02035   0.01418  -0.0620   0.2704   1.0000
  11.000   1.5119   0.02090   0.01477  -0.0608   0.2677   1.0000
  11.250   1.5273   0.02150   0.01540  -0.0596   0.2649   1.0000
  11.500   1.5418   0.02219   0.01608  -0.0583   0.2620   1.0000
  11.750   1.5576   0.02290   0.01678  -0.0572   0.2589   1.0000
  12.000   1.5724   0.02356   0.01753  -0.0561   0.2569   1.0000
  12.250   1.5871   0.02427   0.01832  -0.0550   0.2543   1.0000
  12.500   1.6008   0.02505   0.01916  -0.0539   0.2514   1.0000
  12.750   1.6137   0.02590   0.02004  -0.0529   0.2485   1.0000
  13.000   1.6256   0.02686   0.02099  -0.0517   0.2455   1.0000
  13.250   1.6382   0.02780   0.02197  -0.0507   0.2424   1.0000
  13.500   1.6497   0.02883   0.02311  -0.0498   0.2393   1.0000
  13.750   1.6605   0.02995   0.02430  -0.0489   0.2356   1.0000
  14.000   1.6691   0.03125   0.02562  -0.0480   0.2317   1.0000
  14.250   1.6767   0.03266   0.02703  -0.0469   0.2274   1.0000
  14.500   1.6871   0.03397   0.02845  -0.0463   0.2239   1.0000
  14.750   1.6959   0.03540   0.02995  -0.0457   0.2200   1.0000
  15.000   1.7015   0.03712   0.03167  -0.0449   0.2159   1.0000
  15.250   1.7070   0.03887   0.03347  -0.0442   0.2118   1.0000
  15.500   1.7147   0.04054   0.03524  -0.0437   0.2073   1.0000
  15.750   1.7189   0.04251   0.03725  -0.0431   0.2029   1.0000
  16.000   1.7191   0.04485   0.03958  -0.0425   0.1985   1.0000
  16.250   1.7251   0.04677   0.04162  -0.0421   0.1938   1.0000
  16.500   1.7266   0.04913   0.04402  -0.0417   0.1892   1.0000
  16.750   1.7230   0.05201   0.04691  -0.0413   0.1844   1.0000
  17.000   1.7260   0.05432   0.04932  -0.0411   0.1796   1.0000
  17.250   1.7219   0.05739   0.05242  -0.0409   0.1745   1.0000
  17.500   1.7166   0.06064   0.05572  -0.0407   0.1695   1.0000
  17.750   1.7142   0.06364   0.05879  -0.0407   0.1645   1.0000
  18.000   1.7020   0.06777   0.06293  -0.0408   0.1590   1.0000
  18.250   1.6978   0.07106   0.06629  -0.0409   0.1543   1.0000
  18.500   1.6883   0.07502   0.07032  -0.0412   0.1496   1.0000
  18.750   1.6740   0.07962   0.07493  -0.0417   0.1450   1.0000
  19.000   1.6663   0.08347   0.07887  -0.0422   0.1404   1.0000
  19.250   1.6520   0.08821   0.08365  -0.0429   0.1360   1.0000
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