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GOE 498 AIRFOIL (goe498-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 498 AIRFOIL (goe498-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.28 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe498-il-1000000-n5.txt
Download as CSV file: xf-goe498-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 498 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.8091   0.08787   0.08481  -0.0826   1.0000   0.0278
 -17.500  -0.8253   0.08274   0.07962  -0.0851   1.0000   0.0279
 -17.250  -0.8465   0.07704   0.07387  -0.0878   1.0000   0.0281
 -17.000  -0.8637   0.07100   0.06775  -0.0920   0.9997   0.0283
 -16.750  -0.8763   0.06445   0.06110  -0.0981   0.9987   0.0285
 -16.500  -0.8891   0.05794   0.05449  -0.1047   0.9971   0.0287
 -16.250  -0.9021   0.05165   0.04808  -0.1111   0.9943   0.0288
 -16.000  -0.9162   0.04583   0.04217  -0.1166   0.9901   0.0290
 -15.750  -0.9266   0.03996   0.03618  -0.1229   0.9850   0.0292
 -15.500  -0.9291   0.03477   0.03087  -0.1292   0.9792   0.0294
 -15.250  -0.9278   0.03008   0.02607  -0.1351   0.9708   0.0297
 -15.000  -0.9182   0.02564   0.02149  -0.1425   0.9612   0.0300
 -14.750  -0.8878   0.02223   0.01790  -0.1514   0.9561   0.0304
 -14.500  -0.8586   0.02088   0.01645  -0.1547   0.9517   0.0307
 -14.250  -0.8302   0.01983   0.01532  -0.1570   0.9460   0.0310
 -14.000  -0.8008   0.01873   0.01414  -0.1595   0.9406   0.0315
 -13.750  -0.7765   0.01789   0.01323  -0.1603   0.9333   0.0321
 -13.500  -0.7511   0.01719   0.01247  -0.1610   0.9264   0.0325
 -13.250  -0.7267   0.01662   0.01183  -0.1612   0.9205   0.0330
 -13.000  -0.7044   0.01610   0.01125  -0.1609   0.9139   0.0335
 -12.750  -0.6803   0.01562   0.01070  -0.1607   0.9077   0.0339
 -12.500  -0.6567   0.01519   0.01020  -0.1604   0.9021   0.0344
 -12.250  -0.6335   0.01480   0.00975  -0.1598   0.8962   0.0348
 -12.000  -0.6097   0.01437   0.00927  -0.1594   0.8898   0.0354
 -11.750  -0.5858   0.01396   0.00880  -0.1590   0.8839   0.0360
 -11.500  -0.5620   0.01359   0.00840  -0.1585   0.8770   0.0368
 -11.250  -0.5374   0.01326   0.00802  -0.1580   0.8694   0.0375
 -11.000  -0.5123   0.01295   0.00765  -0.1576   0.8628   0.0382
 -10.750  -0.4872   0.01266   0.00732  -0.1571   0.8551   0.0389
 -10.500  -0.4620   0.01238   0.00696  -0.1566   0.8471   0.0396
 -10.250  -0.4367   0.01207   0.00663  -0.1562   0.8389   0.0405
 -10.000  -0.4114   0.01182   0.00633  -0.1557   0.8288   0.0415
  -9.750  -0.3857   0.01158   0.00604  -0.1552   0.8175   0.0426
  -9.500  -0.3603   0.01140   0.00577  -0.1546   0.8041   0.0437
  -9.250  -0.3355   0.01119   0.00550  -0.1540   0.7893   0.0450
  -9.000  -0.3102   0.01101   0.00526  -0.1534   0.7743   0.0464
  -8.750  -0.2848   0.01086   0.00503  -0.1528   0.7603   0.0477
  -8.500  -0.2592   0.01073   0.00482  -0.1522   0.7479   0.0490
  -8.250  -0.2333   0.01057   0.00462  -0.1517   0.7370   0.0505
  -8.000  -0.2068   0.01043   0.00444  -0.1513   0.7288   0.0522
  -7.750  -0.1799   0.01031   0.00426  -0.1509   0.7206   0.0536
  -7.500  -0.1536   0.01018   0.00409  -0.1505   0.7129   0.0553
  -7.250  -0.1262   0.01004   0.00394  -0.1502   0.7060   0.0573
  -7.000  -0.0991   0.00994   0.00380  -0.1499   0.6990   0.0590
  -6.750  -0.0722   0.00984   0.00365  -0.1495   0.6929   0.0604
  -6.500  -0.0444   0.00970   0.00351  -0.1493   0.6880   0.0622
  -6.250  -0.0168   0.00959   0.00338  -0.1491   0.6818   0.0639
  -6.000   0.0104   0.00952   0.00326  -0.1487   0.6752   0.0654
  -5.750   0.0380   0.00942   0.00313  -0.1485   0.6698   0.0671
  -5.500   0.0658   0.00930   0.00301  -0.1483   0.6644   0.0691
  -5.250   0.0933   0.00921   0.00290  -0.1480   0.6583   0.0710
  -5.000   0.1205   0.00916   0.00280  -0.1477   0.6521   0.0725
  -4.750   0.1483   0.00907   0.00269  -0.1475   0.6451   0.0742
  -4.500   0.1753   0.00899   0.00258  -0.1471   0.6364   0.0766
  -4.250   0.2024   0.00892   0.00249  -0.1467   0.6274   0.0791
  -4.000   0.2291   0.00890   0.00241  -0.1463   0.6159   0.0812
  -3.750   0.2560   0.00882   0.00231  -0.1459   0.6059   0.0847
  -3.500   0.2829   0.00877   0.00223  -0.1455   0.5969   0.0887
  -3.250   0.3101   0.00868   0.00215  -0.1452   0.5898   0.0962
  -3.000   0.3366   0.00856   0.00208  -0.1448   0.5798   0.1178
  -2.750   0.3628   0.00850   0.00205  -0.1443   0.5676   0.1361
  -2.500   0.3888   0.00854   0.00203  -0.1438   0.5552   0.1450
  -2.250   0.4159   0.00850   0.00200  -0.1434   0.5458   0.1538
  -2.000   0.4426   0.00853   0.00200  -0.1430   0.5378   0.1598
  -1.750   0.4699   0.00850   0.00198  -0.1427   0.5313   0.1676
  -1.500   0.4968   0.00852   0.00198  -0.1423   0.5233   0.1739
  -1.250   0.5234   0.00854   0.00198  -0.1418   0.5158   0.1816
  -1.000   0.5504   0.00853   0.00199  -0.1415   0.5080   0.1923
  -0.500   0.6033   0.00853   0.00204  -0.1406   0.4925   0.2274
  -0.250   0.6295   0.00856   0.00208  -0.1401   0.4839   0.2432
   0.000   0.6558   0.00859   0.00212  -0.1397   0.4763   0.2580
   0.250   0.6822   0.00863   0.00217  -0.1392   0.4679   0.2705
   0.500   0.7080   0.00871   0.00223  -0.1386   0.4602   0.2817
   0.750   0.7345   0.00875   0.00228  -0.1382   0.4523   0.2906
   1.000   0.7595   0.00886   0.00236  -0.1375   0.4415   0.3004
   1.250   0.7848   0.00895   0.00244  -0.1368   0.4297   0.3104
   1.500   0.8097   0.00906   0.00252  -0.1361   0.4191   0.3204
   1.750   0.8339   0.00920   0.00262  -0.1353   0.4068   0.3291
   2.000   0.8587   0.00930   0.00272  -0.1345   0.3958   0.3403
   2.250   0.8827   0.00945   0.00283  -0.1337   0.3851   0.3487
   2.500   0.9065   0.00959   0.00295  -0.1328   0.3738   0.3598
   2.750   0.9302   0.00972   0.00307  -0.1318   0.3640   0.3716
   3.000   0.9531   0.00987   0.00321  -0.1308   0.3541   0.3867
   3.250   0.9759   0.00998   0.00334  -0.1297   0.3462   0.4027
   3.500   0.9975   0.01011   0.00348  -0.1284   0.3380   0.4184
   3.750   1.0192   0.01024   0.00361  -0.1271   0.3310   0.4330
   4.000   1.0412   0.01036   0.00376  -0.1259   0.3242   0.4503
   4.250   1.0617   0.01054   0.00395  -0.1244   0.3161   0.4717
   4.500   1.0833   0.01068   0.00413  -0.1231   0.3088   0.4989
   4.750   1.1038   0.01086   0.00435  -0.1217   0.3014   0.5276
   5.000   1.1251   0.01103   0.00455  -0.1204   0.2955   0.5446
   5.250   1.1465   0.01121   0.00474  -0.1191   0.2887   0.5601
   5.500   1.1657   0.01146   0.00499  -0.1174   0.2808   0.5738
   5.750   1.1853   0.01170   0.00522  -0.1159   0.2702   0.5879
   6.250   1.2188   0.01239   0.00584  -0.1119   0.2404   0.6205
   6.500   1.2283   0.01302   0.00633  -0.1088   0.2094   0.6385
   6.750   1.2355   0.01372   0.00693  -0.1054   0.1819   0.6614
   7.000   1.2494   0.01411   0.00738  -0.1031   0.1722   0.7059
   7.500   1.2900   0.01456   0.00829  -0.1011   0.1590   1.0000
   7.750   1.3076   0.01496   0.00868  -0.0996   0.1553   1.0000
   8.000   1.3241   0.01541   0.00912  -0.0979   0.1517   1.0000
   8.250   1.3412   0.01586   0.00956  -0.0963   0.1490   1.0000
   8.500   1.3578   0.01633   0.01003  -0.0947   0.1464   1.0000
   8.750   1.3760   0.01674   0.01046  -0.0934   0.1449   1.0000
   9.000   1.3943   0.01715   0.01089  -0.0921   0.1438   1.0000
   9.250   1.4116   0.01761   0.01137  -0.0907   0.1419   1.0000
   9.500   1.4288   0.01810   0.01187  -0.0894   0.1402   1.0000
   9.750   1.4447   0.01866   0.01245  -0.0879   0.1378   1.0000
  10.000   1.4599   0.01928   0.01307  -0.0864   0.1354   1.0000
  10.250   1.4745   0.01994   0.01373  -0.0848   0.1327   1.0000
  10.500   1.4902   0.02055   0.01437  -0.0835   0.1311   1.0000
  10.750   1.5062   0.02116   0.01501  -0.0822   0.1281   1.0000
  11.000   1.5197   0.02194   0.01578  -0.0807   0.1235   1.0000
  11.250   1.5317   0.02283   0.01665  -0.0791   0.1179   1.0000
  11.500   1.5403   0.02395   0.01772  -0.0773   0.1067   1.0000
  11.750   1.5346   0.02608   0.01968  -0.0743   0.0831   1.0000
  12.000   1.5384   0.02767   0.02125  -0.0724   0.0760   1.0000
  12.250   1.5445   0.02916   0.02275  -0.0707   0.0712   1.0000
  12.500   1.5513   0.03067   0.02427  -0.0693   0.0678   1.0000
  12.750   1.5589   0.03216   0.02580  -0.0680   0.0650   1.0000
  13.000   1.5660   0.03375   0.02740  -0.0668   0.0619   1.0000
  13.250   1.5724   0.03543   0.02910  -0.0656   0.0594   1.0000
  13.500   1.5794   0.03711   0.03081  -0.0646   0.0568   1.0000
  13.750   1.5851   0.03894   0.03268  -0.0636   0.0545   1.0000
  14.000   1.5913   0.04077   0.03454  -0.0627   0.0522   1.0000
  14.250   1.5968   0.04270   0.03650  -0.0619   0.0502   1.0000
  14.500   1.6011   0.04478   0.03861  -0.0611   0.0483   1.0000
  14.750   1.6059   0.04686   0.04073  -0.0604   0.0466   1.0000
  15.000   1.6101   0.04906   0.04296  -0.0598   0.0450   1.0000
  15.250   1.6126   0.05145   0.04538  -0.0592   0.0431   1.0000
  15.500   1.6157   0.05383   0.04782  -0.0588   0.0419   1.0000
  15.750   1.6189   0.05626   0.05029  -0.0584   0.0407   1.0000
  16.000   1.6213   0.05881   0.05289  -0.0581   0.0395   1.0000
  16.250   1.6222   0.06161   0.05574  -0.0579   0.0386   1.0000
  16.500   1.6236   0.06437   0.05855  -0.0578   0.0378   1.0000
  16.750   1.6255   0.06710   0.06135  -0.0578   0.0371   1.0000
  17.000   1.6264   0.07004   0.06435  -0.0579   0.0364   1.0000
  17.250   1.6273   0.07300   0.06736  -0.0580   0.0358   1.0000
  17.500   1.6263   0.07627   0.07070  -0.0583   0.0351   1.0000
  17.750   1.6246   0.07966   0.07415  -0.0587   0.0345   1.0000
  18.000   1.6230   0.08308   0.07763  -0.0591   0.0339   1.0000
  18.250   1.6209   0.08665   0.08128  -0.0597   0.0335   1.0000
  18.500   1.6207   0.08998   0.08467  -0.0604   0.0331   1.0000
  18.750   1.6190   0.09356   0.08833  -0.0611   0.0327   1.0000
  19.000   1.6166   0.09728   0.09212  -0.0620   0.0323   1.0000
  19.250   1.6151   0.10090   0.09581  -0.0630   0.0319   1.0000
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