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GOE 646 AIRFOIL (goe646-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 646 AIRFOIL (goe646-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.4 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe646-il-1000000-n5.txt
Download as CSV file: xf-goe646-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 646 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.8848   0.08574   0.08221  -0.0811   1.0000   0.0304
 -18.000  -0.8959   0.08143   0.07785  -0.0828   1.0000   0.0306
 -17.750  -0.9079   0.07711   0.07347  -0.0845   1.0000   0.0309
 -17.500  -0.9152   0.07233   0.06862  -0.0878   0.9996   0.0310
 -17.250  -0.9186   0.06776   0.06398  -0.0915   0.9990   0.0314
 -17.000  -0.9233   0.06304   0.05918  -0.0954   0.9982   0.0316
 -16.750  -0.9297   0.05820   0.05424  -0.0996   0.9970   0.0317
 -16.500  -0.9344   0.05358   0.04953  -0.1037   0.9955   0.0320
 -16.250  -0.9388   0.04894   0.04480  -0.1081   0.9936   0.0321
 -16.000  -0.9445   0.04445   0.04022  -0.1119   0.9911   0.0323
 -15.750  -0.9519   0.03985   0.03552  -0.1156   0.9876   0.0325
 -15.500  -0.9554   0.03512   0.03070  -0.1204   0.9838   0.0329
 -15.000  -0.9515   0.02773   0.02312  -0.1276   0.9714   0.0335
 -14.750  -0.9443   0.02490   0.02021  -0.1305   0.9621   0.0339
 -14.500  -0.9250   0.02252   0.01774  -0.1347   0.9540   0.0344
 -14.250  -0.8976   0.02056   0.01567  -0.1396   0.9434   0.0349
 -14.000  -0.8575   0.01924   0.01427  -0.1450   0.9343   0.0357
 -13.750  -0.8112   0.01826   0.01319  -0.1507   0.9263   0.0364
 -13.500  -0.7724   0.01728   0.01213  -0.1550   0.9160   0.0372
 -13.250  -0.7438   0.01654   0.01130  -0.1567   0.9035   0.0382
 -13.000  -0.7292   0.01604   0.01071  -0.1553   0.8905   0.0391
 -12.750  -0.7123   0.01560   0.01019  -0.1541   0.8807   0.0399
 -12.500  -0.6955   0.01521   0.00974  -0.1527   0.8711   0.0406
 -12.250  -0.6783   0.01481   0.00927  -0.1513   0.8637   0.0417
 -12.000  -0.6609   0.01440   0.00884  -0.1498   0.8580   0.0430
 -11.750  -0.6418   0.01405   0.00845  -0.1486   0.8518   0.0443
 -11.500  -0.6213   0.01375   0.00809  -0.1475   0.8456   0.0457
 -11.250  -0.6014   0.01339   0.00772  -0.1463   0.8402   0.0475
 -11.000  -0.5803   0.01308   0.00738  -0.1453   0.8343   0.0497
 -10.750  -0.5585   0.01279   0.00706  -0.1444   0.8287   0.0517
 -10.500  -0.5363   0.01251   0.00676  -0.1435   0.8237   0.0543
 -10.250  -0.5133   0.01224   0.00648  -0.1427   0.8189   0.0570
 -10.000  -0.4903   0.01198   0.00621  -0.1418   0.8131   0.0600
  -9.750  -0.4667   0.01178   0.00596  -0.1411   0.8070   0.0625
  -9.500  -0.4432   0.01153   0.00570  -0.1403   0.8014   0.0652
  -9.250  -0.4189   0.01132   0.00548  -0.1396   0.7947   0.0677
  -9.000  -0.3948   0.01115   0.00526  -0.1389   0.7878   0.0698
  -8.750  -0.3704   0.01094   0.00503  -0.1382   0.7818   0.0724
  -8.500  -0.3456   0.01076   0.00483  -0.1376   0.7746   0.0747
  -8.250  -0.3211   0.01063   0.00465  -0.1369   0.7670   0.0766
  -8.000  -0.2964   0.01042   0.00443  -0.1362   0.7594   0.0794
  -7.750  -0.2720   0.01027   0.00425  -0.1354   0.7501   0.0821
  -7.500  -0.2470   0.01015   0.00408  -0.1348   0.7406   0.0842
  -7.250  -0.2237   0.01001   0.00389  -0.1338   0.7283   0.0873
  -7.000  -0.1995   0.00988   0.00372  -0.1330   0.7143   0.0903
  -6.750  -0.1757   0.00979   0.00358  -0.1320   0.6991   0.0933
  -6.500  -0.1526   0.00968   0.00342  -0.1310   0.6838   0.0977
  -6.000  -0.1058   0.00948   0.00314  -0.1290   0.6549   0.1104
  -5.750  -0.0820   0.00934   0.00300  -0.1282   0.6432   0.1213
  -5.500  -0.0586   0.00922   0.00288  -0.1272   0.6321   0.1335
  -5.250  -0.0337   0.00909   0.00277  -0.1265   0.6229   0.1444
  -4.750   0.0165   0.00893   0.00259  -0.1252   0.6070   0.1614
  -4.500   0.0417   0.00886   0.00252  -0.1245   0.5993   0.1689
  -4.250   0.0668   0.00882   0.00245  -0.1238   0.5923   0.1762
  -4.000   0.0928   0.00873   0.00238  -0.1233   0.5861   0.1851
  -3.750   0.1183   0.00870   0.00233  -0.1227   0.5791   0.1925
  -3.500   0.1432   0.00866   0.00229  -0.1219   0.5724   0.2011
  -3.250   0.1694   0.00862   0.00225  -0.1214   0.5656   0.2082
  -3.000   0.1946   0.00859   0.00221  -0.1207   0.5587   0.2164
  -2.750   0.2198   0.00858   0.00219  -0.1200   0.5530   0.2242
  -2.500   0.2463   0.00853   0.00216  -0.1196   0.5492   0.2319
  -2.250   0.2723   0.00851   0.00215  -0.1190   0.5437   0.2404
  -2.000   0.2973   0.00852   0.00214  -0.1183   0.5375   0.2470
  -1.750   0.3225   0.00851   0.00214  -0.1176   0.5322   0.2560
  -1.500   0.3489   0.00849   0.00213  -0.1171   0.5283   0.2632
  -1.250   0.3745   0.00849   0.00213  -0.1165   0.5231   0.2700
  -1.000   0.3993   0.00851   0.00214  -0.1157   0.5176   0.2765
  -0.750   0.4241   0.00853   0.00215  -0.1149   0.5128   0.2843
  -0.500   0.4500   0.00852   0.00217  -0.1144   0.5087   0.2904
  -0.250   0.4751   0.00853   0.00218  -0.1136   0.5047   0.2950
   0.000   0.4993   0.00856   0.00219  -0.1127   0.5008   0.2987
   0.250   0.5225   0.00857   0.00221  -0.1116   0.4968   0.3048
   0.500   0.5466   0.00859   0.00224  -0.1106   0.4933   0.3103
   0.750   0.5716   0.00861   0.00226  -0.1099   0.4894   0.3150
   1.000   0.5958   0.00864   0.00229  -0.1090   0.4843   0.3191
   1.250   0.6190   0.00867   0.00233  -0.1079   0.4795   0.3257
   1.500   0.6423   0.00873   0.00238  -0.1068   0.4749   0.3315
   1.750   0.6671   0.00877   0.00243  -0.1061   0.4695   0.3370
   2.000   0.6900   0.00882   0.00249  -0.1050   0.4626   0.3438
   2.250   0.7120   0.00892   0.00257  -0.1036   0.4556   0.3504
   2.500   0.7353   0.00900   0.00265  -0.1026   0.4471   0.3561
   2.750   0.7562   0.00913   0.00275  -0.1011   0.4371   0.3625
   3.000   0.7780   0.00924   0.00286  -0.0998   0.4253   0.3693
   3.250   0.7978   0.00943   0.00299  -0.0982   0.4089   0.3753
   3.500   0.8162   0.00966   0.00314  -0.0963   0.3903   0.3816
   3.750   0.8339   0.00989   0.00332  -0.0943   0.3730   0.3898
   4.000   0.8521   0.01014   0.00351  -0.0924   0.3576   0.3969
   4.250   0.8706   0.01038   0.00371  -0.0906   0.3443   0.4044
   4.750   0.9084   0.01080   0.00410  -0.0872   0.3241   0.4230
   5.000   0.9268   0.01102   0.00432  -0.0854   0.3158   0.4371
   5.250   0.9467   0.01118   0.00451  -0.0839   0.3093   0.4533
   5.500   0.9661   0.01134   0.00472  -0.0824   0.3033   0.4743
   5.750   0.9829   0.01158   0.00499  -0.0804   0.2957   0.5004
   6.000   1.0017   0.01173   0.00522  -0.0788   0.2888   0.5347
   6.250   1.0180   0.01200   0.00553  -0.0768   0.2802   0.5688
   6.500   1.0357   0.01221   0.00580  -0.0750   0.2737   0.5988
   6.750   1.0539   0.01244   0.00608  -0.0733   0.2679   0.6215
   7.000   1.0709   0.01273   0.00638  -0.0715   0.2620   0.6388
   7.250   1.0888   0.01300   0.00667  -0.0699   0.2564   0.6541
   7.500   1.1061   0.01328   0.00698  -0.0682   0.2502   0.6688
   7.750   1.1209   0.01365   0.00736  -0.0661   0.2426   0.6849
   8.000   1.1388   0.01391   0.00768  -0.0645   0.2389   0.7021
   8.250   1.1531   0.01430   0.00809  -0.0625   0.2302   0.7221
   8.500   1.1673   0.01462   0.00851  -0.0603   0.2249   0.7557
   9.000   1.2845   0.01558   0.00980  -0.0750   0.2018   1.0000
   9.250   1.3005   0.01619   0.01038  -0.0736   0.1937   1.0000
   9.500   1.3175   0.01678   0.01093  -0.0723   0.1865   1.0000
   9.750   1.3327   0.01746   0.01158  -0.0709   0.1798   1.0000
  10.000   1.3489   0.01811   0.01221  -0.0697   0.1733   1.0000
  10.250   1.3626   0.01890   0.01298  -0.0682   0.1668   1.0000
  10.500   1.3793   0.01955   0.01362  -0.0671   0.1625   1.0000
  10.750   1.3927   0.02039   0.01444  -0.0657   0.1565   1.0000
  11.000   1.4070   0.02119   0.01524  -0.0644   0.1520   1.0000
  11.250   1.4219   0.02198   0.01604  -0.0633   0.1476   1.0000
  11.500   1.4344   0.02294   0.01698  -0.0619   0.1428   1.0000
  11.750   1.4479   0.02385   0.01790  -0.0607   0.1388   1.0000
  12.000   1.4609   0.02480   0.01886  -0.0596   0.1340   1.0000
  12.250   1.4702   0.02603   0.02006  -0.0581   0.1274   1.0000
  12.500   1.4796   0.02729   0.02130  -0.0568   0.1190   1.0000
  12.750   1.4815   0.02911   0.02305  -0.0549   0.1053   1.0000
  13.000   1.4785   0.03138   0.02522  -0.0529   0.0887   1.0000
  13.250   1.4798   0.03341   0.02722  -0.0514   0.0806   1.0000
  13.500   1.4857   0.03514   0.02896  -0.0502   0.0765   1.0000
  13.750   1.4922   0.03687   0.03071  -0.0492   0.0738   1.0000
  14.000   1.4972   0.03876   0.03263  -0.0482   0.0711   1.0000
  14.250   1.5052   0.04043   0.03433  -0.0475   0.0691   1.0000
  14.500   1.5120   0.04227   0.03620  -0.0467   0.0676   1.0000
  14.750   1.5179   0.04420   0.03817  -0.0460   0.0662   1.0000
  15.000   1.5228   0.04624   0.04024  -0.0454   0.0648   1.0000
  15.250   1.5278   0.04832   0.04237  -0.0448   0.0636   1.0000
  15.500   1.5348   0.05022   0.04432  -0.0443   0.0628   1.0000
  15.750   1.5404   0.05229   0.04645  -0.0439   0.0620   1.0000
  16.000   1.5452   0.05446   0.04867  -0.0435   0.0611   1.0000
  16.250   1.5491   0.05673   0.05098  -0.0431   0.0602   1.0000
  16.500   1.5513   0.05920   0.05351  -0.0427   0.0594   1.0000
  16.750   1.5532   0.06172   0.05606  -0.0424   0.0583   1.0000
  17.000   1.5536   0.06446   0.05886  -0.0422   0.0574   1.0000
  17.250   1.5572   0.06684   0.06129  -0.0420   0.0566   1.0000
  17.500   1.5590   0.06945   0.06397  -0.0419   0.0560   1.0000
  17.750   1.5611   0.07202   0.06659  -0.0418   0.0552   1.0000
  18.000   1.5613   0.07487   0.06950  -0.0418   0.0543   1.0000
  18.250   1.5612   0.07775   0.07244  -0.0418   0.0536   1.0000
  18.500   1.5595   0.08087   0.07560  -0.0420   0.0527   1.0000
  18.750   1.5559   0.08421   0.07900  -0.0421   0.0517   1.0000
  19.000   1.5538   0.08740   0.08225  -0.0424   0.0512   1.0000
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