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GOE 798 AIRFOIL (goe798-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 798 AIRFOIL (goe798-il)
Reynolds number: 1,000,000
Max Cl/Cd: 119.99 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe798-il-1000000.txt
Download as CSV file: xf-goe798-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 798 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.6650   0.09501   0.09228  -0.1070   0.9943   0.0390
 -18.000  -0.7077   0.08398   0.08107  -0.1150   0.9931   0.0393
 -17.750  -0.7449   0.07441   0.07135  -0.1222   0.9910   0.0395
 -17.500  -0.7835   0.06534   0.06212  -0.1289   0.9859   0.0397
 -17.250  -0.8169   0.05668   0.05330  -0.1358   0.9808   0.0399
 -17.000  -0.8463   0.04894   0.04539  -0.1415   0.9731   0.0400
 -16.750  -0.8666   0.04234   0.03861  -0.1466   0.9648   0.0401
 -16.500  -0.8780   0.03723   0.03333  -0.1508   0.9560   0.0402
 -16.250  -0.8827   0.03353   0.02946  -0.1534   0.9478   0.0403
 -16.000  -0.8819   0.03084   0.02664  -0.1551   0.9398   0.0405
 -15.750  -0.8901   0.02795   0.02361  -0.1555   0.9313   0.0408
 -15.500  -0.8912   0.02597   0.02153  -0.1551   0.9237   0.0411
 -15.250  -0.8877   0.02458   0.02005  -0.1538   0.9162   0.0414
 -15.000  -0.8793   0.02353   0.01893  -0.1525   0.9096   0.0417
 -14.750  -0.8687   0.02268   0.01802  -0.1509   0.9023   0.0421
 -14.500  -0.8572   0.02198   0.01723  -0.1492   0.8952   0.0424
 -14.250  -0.8459   0.02139   0.01658  -0.1472   0.8875   0.0428
 -14.000  -0.8297   0.02080   0.01590  -0.1459   0.8798   0.0432
 -13.750  -0.8117   0.02022   0.01525  -0.1448   0.8725   0.0436
 -13.500  -0.7926   0.01969   0.01463  -0.1438   0.8639   0.0440
 -13.250  -0.7724   0.01920   0.01405  -0.1429   0.8556   0.0444
 -13.000  -0.7511   0.01876   0.01352  -0.1422   0.8455   0.0447
 -12.750  -0.7289   0.01838   0.01303  -0.1415   0.8351   0.0450
 -12.500  -0.7127   0.01758   0.01215  -0.1401   0.8221   0.0456
 -12.250  -0.6922   0.01704   0.01154  -0.1392   0.8090   0.0462
 -12.000  -0.6701   0.01664   0.01105  -0.1385   0.7961   0.0467
 -11.500  -0.6233   0.01595   0.01020  -0.1373   0.7738   0.0478
 -11.250  -0.5993   0.01567   0.00982  -0.1368   0.7642   0.0485
 -11.000  -0.5741   0.01538   0.00947  -0.1364   0.7570   0.0491
 -10.750  -0.5485   0.01515   0.00915  -0.1361   0.7500   0.0496
 -10.500  -0.5255   0.01473   0.00864  -0.1354   0.7430   0.0504
 -10.250  -0.5011   0.01430   0.00820  -0.1350   0.7382   0.0512
 -10.000  -0.4757   0.01399   0.00785  -0.1347   0.7328   0.0520
  -9.750  -0.4500   0.01374   0.00754  -0.1344   0.7276   0.0528
  -9.500  -0.4237   0.01352   0.00725  -0.1341   0.7227   0.0536
  -9.250  -0.3966   0.01328   0.00698  -0.1340   0.7195   0.0544
  -9.000  -0.3701   0.01299   0.00666  -0.1339   0.7158   0.0553
  -8.750  -0.3443   0.01267   0.00632  -0.1336   0.7120   0.0567
  -8.500  -0.3177   0.01245   0.00606  -0.1334   0.7081   0.0580
  -8.250  -0.2906   0.01229   0.00584  -0.1333   0.7034   0.0593
  -8.000  -0.2630   0.01206   0.00560  -0.1332   0.7009   0.0607
  -7.750  -0.2359   0.01178   0.00534  -0.1332   0.6980   0.0627
  -7.500  -0.2082   0.01159   0.00513  -0.1331   0.6950   0.0648
  -7.250  -0.1806   0.01140   0.00494  -0.1331   0.6919   0.0674
  -7.000  -0.1528   0.01126   0.00480  -0.1331   0.6887   0.0709
  -6.750  -0.1247   0.01118   0.00472  -0.1331   0.6848   0.0751
  -6.500  -0.0957   0.01111   0.00466  -0.1333   0.6821   0.0796
  -6.250  -0.0664   0.01107   0.00465  -0.1335   0.6797   0.0836
  -6.000  -0.0369   0.01105   0.00461  -0.1338   0.6771   0.0868
  -5.750  -0.0078   0.01100   0.00459  -0.1340   0.6745   0.0895
  -5.500   0.0215   0.01102   0.00459  -0.1342   0.6715   0.0920
  -5.250   0.0507   0.01108   0.00459  -0.1344   0.6677   0.0939
  -5.000   0.0788   0.01100   0.00449  -0.1344   0.6633   0.0961
  -4.750   0.1077   0.01092   0.00444  -0.1346   0.6609   0.0980
  -4.500   0.1367   0.01087   0.00440  -0.1348   0.6581   0.0997
  -4.250   0.1657   0.01084   0.00435  -0.1350   0.6552   0.1013
  -4.000   0.1946   0.01083   0.00431  -0.1352   0.6519   0.1025
  -3.750   0.2224   0.01072   0.00417  -0.1351   0.6484   0.1041
  -3.500   0.2501   0.01063   0.00406  -0.1352   0.6441   0.1059
  -3.250   0.2786   0.01053   0.00398  -0.1353   0.6420   0.1074
  -3.000   0.3072   0.01044   0.00391  -0.1354   0.6393   0.1087
  -2.750   0.3358   0.01037   0.00384  -0.1356   0.6364   0.1100
  -2.500   0.3642   0.01032   0.00377  -0.1357   0.6331   0.1113
  -2.250   0.3923   0.01030   0.00372  -0.1357   0.6294   0.1123
  -2.000   0.4201   0.01031   0.00367  -0.1357   0.6247   0.1131
  -1.750   0.4475   0.01011   0.00351  -0.1357   0.6220   0.1152
  -1.500   0.4756   0.01000   0.00343  -0.1357   0.6187   0.1170
  -1.250   0.5037   0.00994   0.00338  -0.1358   0.6155   0.1186
  -1.000   0.5316   0.00991   0.00334  -0.1358   0.6123   0.1201
  -0.750   0.5591   0.00990   0.00330  -0.1358   0.6089   0.1216
  -0.500   0.5868   0.00990   0.00328  -0.1358   0.6052   0.1225
  -0.250   0.6151   0.00985   0.00325  -0.1359   0.6027   0.1233
   0.000   0.6430   0.00978   0.00319  -0.1359   0.5996   0.1250
   0.250   0.6705   0.00972   0.00315  -0.1359   0.5961   0.1271
   0.500   0.6975   0.00970   0.00313  -0.1357   0.5923   0.1291
   0.750   0.7238   0.00972   0.00313  -0.1355   0.5881   0.1313
   1.000   0.7513   0.00971   0.00313  -0.1355   0.5847   0.1336
   1.250   0.7788   0.00968   0.00313  -0.1354   0.5807   0.1369
   1.500   0.8051   0.00965   0.00314  -0.1352   0.5761   0.1442
   1.750   0.8300   0.00963   0.00317  -0.1347   0.5712   0.1640
   2.000   0.8550   0.00952   0.00324  -0.1343   0.5668   0.2240
   2.250   0.8811   0.00940   0.00330  -0.1341   0.5623   0.2808
   2.500   0.9056   0.00928   0.00337  -0.1336   0.5569   0.3519
   2.750   0.9272   0.00909   0.00348  -0.1326   0.5510   0.4784
   3.000   0.9498   0.00875   0.00362  -0.1319   0.5459   0.6474
   3.250   0.9677   0.00843   0.00377  -0.1299   0.5396   0.8084
   3.500   0.9859   0.00844   0.00408  -0.1275   0.5323   0.9591
   3.750   1.0260   0.00864   0.00426  -0.1303   0.5244   0.9862
   4.250   1.1027   0.00919   0.00468  -0.1354   0.5012   1.0000
   4.500   1.1073   0.00938   0.00481  -0.1308   0.4894   1.0000
   4.750   1.1136   0.00967   0.00502  -0.1266   0.4752   1.0000
   5.000   1.1230   0.01004   0.00530  -0.1231   0.4588   1.0000
   5.250   1.1344   0.01048   0.00564  -0.1202   0.4411   1.0000
   5.500   1.1458   0.01099   0.00605  -0.1174   0.4229   1.0000
   5.750   1.1578   0.01155   0.00651  -0.1149   0.4056   1.0000
   6.000   1.1717   0.01208   0.00697  -0.1127   0.3909   1.0000
   6.250   1.1874   0.01259   0.00742  -0.1109   0.3794   1.0000
   6.500   1.2012   0.01320   0.00795  -0.1089   0.3691   1.0000
   6.750   1.2198   0.01364   0.00836  -0.1077   0.3620   1.0000
   7.000   1.2349   0.01423   0.00891  -0.1059   0.3550   1.0000
   7.250   1.2529   0.01473   0.00939  -0.1047   0.3498   1.0000
   7.500   1.2721   0.01518   0.00984  -0.1037   0.3457   1.0000
   7.750   1.2891   0.01575   0.01040  -0.1025   0.3413   1.0000
   8.000   1.3045   0.01641   0.01103  -0.1010   0.3363   1.0000
   8.250   1.3217   0.01699   0.01161  -0.0998   0.3326   1.0000
   8.500   1.3412   0.01748   0.01211  -0.0990   0.3298   1.0000
   8.750   1.3597   0.01803   0.01267  -0.0981   0.3269   1.0000
   9.000   1.3761   0.01870   0.01334  -0.0970   0.3240   1.0000
   9.250   1.3916   0.01944   0.01407  -0.0957   0.3210   1.0000
   9.500   1.4050   0.02030   0.01492  -0.0943   0.3174   1.0000
   9.750   1.4224   0.02096   0.01561  -0.0934   0.3152   1.0000
  10.000   1.4422   0.02150   0.01618  -0.0928   0.3132   1.0000
  10.250   1.4600   0.02217   0.01687  -0.0920   0.3105   1.0000
  10.500   1.4761   0.02296   0.01768  -0.0911   0.3079   1.0000
  10.750   1.4914   0.02381   0.01853  -0.0901   0.3052   1.0000
  11.000   1.5038   0.02487   0.01959  -0.0888   0.3022   1.0000
  11.250   1.5157   0.02595   0.02067  -0.0875   0.2988   1.0000
  11.500   1.5342   0.02665   0.02142  -0.0870   0.2975   1.0000
  11.750   1.5521   0.02739   0.02220  -0.0865   0.2956   1.0000
  12.000   1.5693   0.02817   0.02301  -0.0859   0.2933   1.0000
  12.250   1.5839   0.02916   0.02403  -0.0850   0.2905   1.0000
  12.500   1.5971   0.03025   0.02513  -0.0841   0.2876   1.0000
  12.750   1.6079   0.03154   0.02642  -0.0830   0.2844   1.0000
  13.000   1.6197   0.03273   0.02763  -0.0820   0.2815   1.0000
  13.250   1.6376   0.03350   0.02846  -0.0816   0.2794   1.0000
  13.500   1.6528   0.03449   0.02948  -0.0810   0.2765   1.0000
  13.750   1.6657   0.03566   0.03068  -0.0802   0.2729   1.0000
  14.000   1.6758   0.03704   0.03205  -0.0793   0.2689   1.0000
  14.250   1.6843   0.03858   0.03361  -0.0782   0.2650   1.0000
  14.500   1.7003   0.03951   0.03460  -0.0778   0.2616   1.0000
  14.750   1.7114   0.04084   0.03594  -0.0770   0.2560   1.0000
  15.000   1.7149   0.04283   0.03791  -0.0757   0.2493   1.0000
  15.250   1.7262   0.04415   0.03925  -0.0750   0.2413   1.0000
  15.500   1.7268   0.04643   0.04149  -0.0736   0.2304   1.0000
  15.750   1.7246   0.04895   0.04394  -0.0720   0.2149   1.0000
  16.000   1.7151   0.05215   0.04705  -0.0701   0.1979   1.0000
  16.250   1.7078   0.05521   0.05005  -0.0684   0.1859   1.0000
  16.500   1.7033   0.05805   0.05286  -0.0670   0.1773   1.0000
  16.750   1.7039   0.06051   0.05533  -0.0660   0.1721   1.0000
  17.000   1.7025   0.06315   0.05796  -0.0650   0.1672   1.0000
  17.250   1.7043   0.06551   0.06036  -0.0642   0.1635   1.0000
  17.500   1.7079   0.06773   0.06262  -0.0635   0.1605   1.0000
  17.750   1.7093   0.07016   0.06507  -0.0628   0.1573   1.0000
  18.000   1.7058   0.07319   0.06812  -0.0620   0.1539   1.0000
  18.250   1.7096   0.07543   0.07040  -0.0615   0.1515   1.0000
  18.500   1.7139   0.07764   0.07268  -0.0612   0.1497   1.0000
  18.750   1.7170   0.07998   0.07507  -0.0608   0.1474   1.0000
  19.000   1.7176   0.08260   0.07772  -0.0604   0.1450   1.0000
  19.250   1.7135   0.08581   0.08097  -0.0599   0.1423   1.0000
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