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GOE 628 AIRFOIL (goe628-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 628 AIRFOIL (goe628-il)
Reynolds number: 500,000
Max Cl/Cd: 84.49 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe628-il-500000-n5.txt
Download as CSV file: xf-goe628-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7169   0.08021   0.07687  -0.0791   1.0000   0.0355
 -16.250  -0.7420   0.07334   0.06987  -0.0832   1.0000   0.0359
 -16.000  -0.7626   0.06750   0.06391  -0.0865   1.0000   0.0364
 -15.750  -0.7835   0.06217   0.05846  -0.0894   1.0000   0.0368
 -15.500  -0.8036   0.05738   0.05356  -0.0917   1.0000   0.0371
 -15.250  -0.8231   0.05299   0.04905  -0.0935   1.0000   0.0374
 -15.000  -0.8396   0.04938   0.04540  -0.0944   1.0000   0.0376
 -14.500  -0.8332   0.04199   0.03791  -0.1027   0.9938   0.0382
 -14.250  -0.8242   0.03834   0.03419  -0.1078   0.9864   0.0386
 -14.000  -0.8080   0.03469   0.03044  -0.1142   0.9803   0.0391
 -13.750  -0.7938   0.03040   0.02600  -0.1223   0.9703   0.0395
 -13.500  -0.7732   0.02832   0.02377  -0.1261   0.9624   0.0401
 -13.250  -0.7468   0.02679   0.02210  -0.1291   0.9559   0.0408
 -13.000  -0.7187   0.02549   0.02064  -0.1317   0.9495   0.0415
 -12.750  -0.6920   0.02439   0.01936  -0.1335   0.9408   0.0420
 -12.500  -0.6641   0.02340   0.01831  -0.1350   0.9324   0.0425
 -12.250  -0.6379   0.02264   0.01750  -0.1359   0.9217   0.0430
 -12.000  -0.6129   0.02207   0.01687  -0.1362   0.9104   0.0436
 -11.750  -0.5882   0.02151   0.01622  -0.1363   0.8982   0.0442
 -11.500  -0.5666   0.02100   0.01560  -0.1357   0.8843   0.0448
 -11.250  -0.5453   0.02051   0.01500  -0.1350   0.8700   0.0455
 -11.000  -0.5238   0.02007   0.01441  -0.1342   0.8546   0.0462
 -10.750  -0.5020   0.01970   0.01387  -0.1334   0.8382   0.0468
 -10.500  -0.4804   0.01932   0.01333  -0.1324   0.8209   0.0472
 -10.250  -0.4606   0.01866   0.01258  -0.1313   0.8029   0.0476
 -10.000  -0.4401   0.01813   0.01194  -0.1301   0.7858   0.0479
  -9.750  -0.4188   0.01767   0.01138  -0.1291   0.7707   0.0482
  -9.500  -0.3967   0.01724   0.01087  -0.1281   0.7581   0.0485
  -9.250  -0.3744   0.01685   0.01039  -0.1272   0.7465   0.0488
  -9.000  -0.3512   0.01648   0.00995  -0.1264   0.7361   0.0492
  -8.750  -0.3277   0.01614   0.00952  -0.1256   0.7276   0.0496
  -8.500  -0.3037   0.01579   0.00910  -0.1249   0.7193   0.0500
  -8.250  -0.2798   0.01546   0.00869  -0.1241   0.7113   0.0504
  -8.000  -0.2552   0.01513   0.00829  -0.1235   0.7045   0.0508
  -7.750  -0.2305   0.01481   0.00792  -0.1228   0.6975   0.0511
  -7.250  -0.1803   0.01424   0.00721  -0.1216   0.6847   0.0519
  -7.000  -0.1548   0.01398   0.00689  -0.1210   0.6782   0.0523
  -6.750  -0.1293   0.01376   0.00659  -0.1204   0.6719   0.0526
  -6.500  -0.1034   0.01352   0.00630  -0.1199   0.6652   0.0529
  -6.250  -0.0786   0.01322   0.00595  -0.1192   0.6565   0.0534
  -6.000  -0.0537   0.01294   0.00561  -0.1185   0.6476   0.0539
  -5.750  -0.0283   0.01269   0.00532  -0.1179   0.6377   0.0546
  -5.500  -0.0027   0.01250   0.00506  -0.1173   0.6297   0.0553
  -5.250   0.0238   0.01229   0.00483  -0.1169   0.6226   0.0560
  -5.000   0.0499   0.01213   0.00461  -0.1164   0.6154   0.0567
  -4.750   0.0765   0.01197   0.00440  -0.1159   0.6093   0.0574
  -4.500   0.1033   0.01182   0.00421  -0.1155   0.6021   0.0581
  -4.250   0.1295   0.01171   0.00403  -0.1149   0.5946   0.0588
  -4.000   0.1563   0.01157   0.00386  -0.1145   0.5874   0.0597
  -3.750   0.1827   0.01143   0.00368  -0.1140   0.5800   0.0609
  -3.500   0.2091   0.01132   0.00352  -0.1136   0.5735   0.0623
  -3.250   0.2360   0.01121   0.00339  -0.1131   0.5658   0.0640
  -3.000   0.2622   0.01115   0.00327  -0.1126   0.5577   0.0661
  -2.750   0.2888   0.01103   0.00315  -0.1121   0.5496   0.0709
  -2.500   0.3141   0.01080   0.00301  -0.1116   0.5414   0.0984
  -2.250   0.3398   0.01061   0.00291  -0.1111   0.5342   0.1306
  -2.000   0.3657   0.01044   0.00284  -0.1106   0.5261   0.1647
  -1.750   0.3914   0.01039   0.00282  -0.1100   0.5181   0.1873
  -1.500   0.4178   0.01035   0.00281  -0.1095   0.5090   0.2050
  -1.250   0.4434   0.01038   0.00282  -0.1089   0.4997   0.2193
  -1.000   0.4697   0.01039   0.00283  -0.1084   0.4898   0.2338
  -0.750   0.4952   0.01043   0.00286  -0.1078   0.4809   0.2466
  -0.500   0.5213   0.01047   0.00289  -0.1072   0.4712   0.2571
  -0.250   0.5468   0.01054   0.00294  -0.1066   0.4620   0.2670
   0.000   0.5723   0.01061   0.00298  -0.1060   0.4515   0.2752
   0.250   0.5974   0.01070   0.00304  -0.1053   0.4406   0.2856
   0.750   0.6468   0.01092   0.00320  -0.1038   0.4180   0.3071
   1.000   0.6711   0.01103   0.00329  -0.1029   0.4081   0.3142
   1.250   0.6956   0.01115   0.00337  -0.1021   0.3978   0.3211
   1.750   0.7435   0.01141   0.00359  -0.1004   0.3793   0.3375
   2.000   0.7673   0.01156   0.00370  -0.0995   0.3711   0.3458
   2.250   0.7907   0.01169   0.00382  -0.0986   0.3626   0.3528
   2.500   0.8137   0.01185   0.00395  -0.0976   0.3551   0.3599
   2.750   0.8373   0.01199   0.00407  -0.0967   0.3486   0.3668
   3.000   0.8597   0.01214   0.00422  -0.0956   0.3426   0.3738
   3.250   0.8825   0.01228   0.00436  -0.0946   0.3378   0.3811
   3.500   0.9055   0.01241   0.00450  -0.0936   0.3329   0.3887
   3.750   0.9266   0.01256   0.00466  -0.0922   0.3278   0.3974
   4.250   0.9669   0.01286   0.00498  -0.0892   0.3193   0.4155
   4.750   1.0077   0.01316   0.00534  -0.0863   0.3119   0.4381
   5.000   1.0269   0.01335   0.00556  -0.0847   0.3084   0.4525
   5.250   1.0454   0.01357   0.00582  -0.0831   0.3050   0.4699
   5.500   1.0662   0.01370   0.00603  -0.0818   0.3025   0.4933
   5.750   1.0859   0.01381   0.00628  -0.0803   0.2994   0.5327
   6.000   1.0935   0.01334   0.00660  -0.0764   0.2966   0.8250
   6.500   1.1787   0.01395   0.00731  -0.0833   0.2891   1.0000
   6.750   1.1979   0.01424   0.00759  -0.0819   0.2868   1.0000
   7.000   1.2185   0.01448   0.00786  -0.0808   0.2846   1.0000
   7.250   1.2385   0.01476   0.00815  -0.0795   0.2821   1.0000
   7.500   1.2577   0.01506   0.00846  -0.0782   0.2793   1.0000
   7.750   1.2760   0.01541   0.00880  -0.0768   0.2765   1.0000
   8.000   1.2937   0.01580   0.00919  -0.0753   0.2739   1.0000
   8.250   1.3107   0.01623   0.00961  -0.0738   0.2715   1.0000
   8.500   1.3293   0.01660   0.01000  -0.0726   0.2694   1.0000
   8.750   1.3488   0.01695   0.01039  -0.0715   0.2670   1.0000
   9.000   1.3671   0.01735   0.01082  -0.0703   0.2642   1.0000
   9.250   1.3846   0.01780   0.01128  -0.0691   0.2612   1.0000
   9.500   1.4000   0.01835   0.01182  -0.0676   0.2573   1.0000
   9.750   1.4146   0.01897   0.01243  -0.0661   0.2537   1.0000
  10.000   1.4330   0.01942   0.01294  -0.0651   0.2514   1.0000
  10.250   1.4505   0.01994   0.01349  -0.0641   0.2490   1.0000
  10.500   1.4671   0.02051   0.01411  -0.0630   0.2464   1.0000
  10.750   1.4823   0.02118   0.01479  -0.0618   0.2435   1.0000
  11.000   1.4963   0.02193   0.01555  -0.0605   0.2407   1.0000
  11.250   1.5094   0.02276   0.01640  -0.0593   0.2382   1.0000
  11.500   1.5260   0.02341   0.01711  -0.0584   0.2363   1.0000
  11.750   1.5419   0.02412   0.01788  -0.0575   0.2339   1.0000
  12.000   1.5565   0.02492   0.01873  -0.0565   0.2312   1.0000
  12.250   1.5699   0.02583   0.01967  -0.0556   0.2284   1.0000
  12.500   1.5809   0.02692   0.02078  -0.0545   0.2252   1.0000
  12.750   1.5916   0.02807   0.02196  -0.0534   0.2223   1.0000
  13.000   1.6061   0.02897   0.02293  -0.0527   0.2200   1.0000
  13.250   1.6189   0.03002   0.02405  -0.0519   0.2172   1.0000
  13.500   1.6297   0.03123   0.02530  -0.0511   0.2136   1.0000
  13.750   1.6370   0.03276   0.02684  -0.0502   0.2096   1.0000
  14.000   1.6461   0.03418   0.02831  -0.0494   0.2053   1.0000
  14.250   1.6552   0.03563   0.02981  -0.0488   0.2002   1.0000
  14.500   1.6596   0.03751   0.03171  -0.0479   0.1954   1.0000
  14.750   1.6658   0.03927   0.03351  -0.0473   0.1914   1.0000
  15.000   1.6725   0.04100   0.03529  -0.0467   0.1863   1.0000
  15.250   1.6710   0.04356   0.03786  -0.0459   0.1800   1.0000
  15.500   1.6760   0.04553   0.03988  -0.0454   0.1754   1.0000
  15.750   1.6754   0.04808   0.04246  -0.0449   0.1693   1.0000
  16.000   1.6743   0.05073   0.04514  -0.0444   0.1642   1.0000
  16.250   1.6742   0.05334   0.04780  -0.0441   0.1588   1.0000
  16.500   1.6666   0.05679   0.05127  -0.0438   0.1530   1.0000
  16.750   1.6631   0.05986   0.05439  -0.0436   0.1469   1.0000
  17.000   1.6573   0.06326   0.05783  -0.0435   0.1426   1.0000
  17.250   1.6490   0.06699   0.06161  -0.0435   0.1370   1.0000
  17.500   1.6399   0.07087   0.06553  -0.0436   0.1318   1.0000
  17.750   1.6295   0.07499   0.06970  -0.0439   0.1281   1.0000
  18.000   1.6218   0.07885   0.07363  -0.0442   0.1240   1.0000
  18.250   1.6109   0.08315   0.07798  -0.0447   0.1203   1.0000
  18.500   1.5966   0.08796   0.08285  -0.0454   0.1169   1.0000
  18.750   1.5904   0.09177   0.08674  -0.0460   0.1140   1.0000
  19.000   1.5795   0.09628   0.09131  -0.0469   0.1105   1.0000
  19.250   1.5643   0.10141   0.09650  -0.0480   0.1072   1.0000
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