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GOE 798 AIRFOIL (goe798-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 798 AIRFOIL (goe798-il)
Reynolds number: 500,000
Max Cl/Cd: 83.79 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe798-il-500000-n5.txt
Download as CSV file: xf-goe798-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.5638   0.08575   0.08202  -0.1168   0.9559   0.0406
 -16.500  -0.6254   0.07353   0.06955  -0.1243   0.9499   0.0409
 -16.250  -0.6736   0.06376   0.05958  -0.1304   0.9420   0.0411
 -16.000  -0.7158   0.05472   0.05032  -0.1362   0.9340   0.0412
 -15.750  -0.7469   0.04660   0.04198  -0.1422   0.9251   0.0413
 -15.500  -0.7659   0.04003   0.03521  -0.1478   0.9166   0.0415
 -15.250  -0.7760   0.03521   0.03022  -0.1520   0.9071   0.0417
 -15.000  -0.7801   0.03203   0.02688  -0.1540   0.8985   0.0419
 -14.750  -0.7797   0.02979   0.02453  -0.1546   0.8893   0.0421
 -14.500  -0.7763   0.02815   0.02277  -0.1541   0.8809   0.0424
 -14.250  -0.7698   0.02685   0.02137  -0.1532   0.8717   0.0427
 -14.000  -0.7618   0.02579   0.02018  -0.1518   0.8627   0.0430
 -13.750  -0.7526   0.02487   0.01917  -0.1502   0.8522   0.0433
 -13.500  -0.7441   0.02415   0.01833  -0.1480   0.8416   0.0437
 -13.250  -0.7301   0.02344   0.01750  -0.1466   0.8298   0.0441
 -13.000  -0.7141   0.02278   0.01673  -0.1454   0.8186   0.0445
 -12.750  -0.6966   0.02219   0.01600  -0.1443   0.8070   0.0450
 -12.500  -0.6778   0.02163   0.01532  -0.1433   0.7958   0.0455
 -12.250  -0.6580   0.02114   0.01468  -0.1424   0.7855   0.0459
 -12.000  -0.6400   0.02050   0.01397  -0.1413   0.7754   0.0464
 -11.750  -0.6204   0.01997   0.01335  -0.1404   0.7666   0.0469
 -11.500  -0.5993   0.01948   0.01279  -0.1396   0.7582   0.0474
 -11.000  -0.5548   0.01864   0.01177  -0.1383   0.7444   0.0486
 -10.750  -0.5316   0.01824   0.01130  -0.1377   0.7386   0.0492
 -10.500  -0.5080   0.01788   0.01084  -0.1372   0.7332   0.0499
 -10.250  -0.4839   0.01755   0.01041  -0.1367   0.7285   0.0505
 -10.000  -0.4596   0.01716   0.00997  -0.1363   0.7244   0.0512
  -9.750  -0.4356   0.01675   0.00954  -0.1359   0.7199   0.0521
  -9.500  -0.4110   0.01641   0.00916  -0.1355   0.7154   0.0530
  -9.250  -0.3859   0.01612   0.00879  -0.1351   0.7111   0.0539
  -9.000  -0.3603   0.01583   0.00845  -0.1348   0.7074   0.0549
  -8.750  -0.3342   0.01555   0.00812  -0.1346   0.7042   0.0558
  -8.500  -0.3083   0.01525   0.00779  -0.1343   0.7008   0.0568
  -8.250  -0.2823   0.01496   0.00749  -0.1341   0.6975   0.0581
  -8.000  -0.2559   0.01472   0.00720  -0.1339   0.6942   0.0596
  -7.750  -0.2294   0.01450   0.00693  -0.1337   0.6910   0.0612
  -7.500  -0.2027   0.01429   0.00670  -0.1336   0.6878   0.0633
  -7.250  -0.1755   0.01407   0.00649  -0.1335   0.6850   0.0658
  -7.000  -0.1481   0.01389   0.00631  -0.1335   0.6819   0.0686
  -6.750  -0.1204   0.01375   0.00619  -0.1335   0.6790   0.0720
  -6.500  -0.0924   0.01365   0.00609  -0.1335   0.6761   0.0756
  -6.250  -0.0644   0.01358   0.00599  -0.1335   0.6733   0.0797
  -6.000  -0.0362   0.01354   0.00592  -0.1336   0.6705   0.0829
  -5.750  -0.0079   0.01351   0.00584  -0.1336   0.6676   0.0862
  -5.500   0.0204   0.01342   0.00574  -0.1337   0.6651   0.0887
  -5.250   0.0487   0.01335   0.00567  -0.1338   0.6625   0.0907
  -5.000   0.0770   0.01329   0.00560  -0.1339   0.6598   0.0928
  -4.750   0.1053   0.01323   0.00551  -0.1339   0.6571   0.0949
  -4.500   0.1334   0.01319   0.00541  -0.1339   0.6538   0.0966
  -4.250   0.1606   0.01308   0.00528  -0.1338   0.6502   0.0983
  -4.000   0.1883   0.01302   0.00520  -0.1338   0.6467   0.0999
  -3.750   0.2162   0.01292   0.00512  -0.1338   0.6434   0.1015
  -3.500   0.2440   0.01284   0.00503  -0.1338   0.6399   0.1030
  -3.250   0.2717   0.01279   0.00494  -0.1338   0.6362   0.1044
  -3.000   0.2995   0.01276   0.00485  -0.1337   0.6328   0.1055
  -2.750   0.3263   0.01263   0.00471  -0.1336   0.6296   0.1070
  -2.500   0.3536   0.01253   0.00463  -0.1335   0.6263   0.1086
  -2.250   0.3811   0.01244   0.00457  -0.1335   0.6224   0.1103
  -2.000   0.4083   0.01238   0.00450  -0.1334   0.6184   0.1120
  -1.750   0.4354   0.01233   0.00443  -0.1332   0.6146   0.1133
  -1.500   0.4623   0.01231   0.00437  -0.1330   0.6107   0.1147
  -1.250   0.4894   0.01228   0.00433  -0.1329   0.6067   0.1158
  -1.000   0.5160   0.01217   0.00425  -0.1327   0.6023   0.1175
  -0.750   0.5425   0.01211   0.00420  -0.1325   0.5981   0.1189
  -0.500   0.5688   0.01207   0.00415  -0.1322   0.5941   0.1201
  -0.250   0.5949   0.01206   0.00412  -0.1319   0.5903   0.1212
   0.000   0.6217   0.01202   0.00411  -0.1317   0.5864   0.1225
   0.250   0.6482   0.01200   0.00410  -0.1315   0.5821   0.1239
   0.500   0.6741   0.01200   0.00409  -0.1312   0.5779   0.1253
   0.750   0.6995   0.01203   0.00409  -0.1307   0.5736   0.1268
   1.000   0.7251   0.01203   0.00411  -0.1303   0.5696   0.1291
   1.250   0.7508   0.01202   0.00414  -0.1300   0.5650   0.1323
   1.500   0.7755   0.01204   0.00417  -0.1294   0.5598   0.1364
   1.750   0.7989   0.01208   0.00422  -0.1286   0.5546   0.1431
   2.000   0.8231   0.01207   0.00428  -0.1280   0.5496   0.1587
   2.250   0.8463   0.01203   0.00437  -0.1272   0.5434   0.1952
   2.500   0.8657   0.01204   0.00446  -0.1257   0.5369   0.2297
   2.750   0.8858   0.01205   0.00456  -0.1243   0.5302   0.2637
   3.000   0.9045   0.01209   0.00469  -0.1226   0.5217   0.3009
   3.250   0.9237   0.01214   0.00486  -0.1212   0.5131   0.3566
   3.500   0.9432   0.01212   0.00510  -0.1199   0.5028   0.4617
   3.750   0.9620   0.01199   0.00540  -0.1185   0.4928   0.6211
   4.000   0.9763   0.01190   0.00576  -0.1161   0.4815   0.7846
   4.250   1.0105   0.01206   0.00624  -0.1174   0.4676   0.9947
   4.500   1.0263   0.01244   0.00654  -0.1154   0.4546   1.0000
   4.750   1.0383   0.01289   0.00691  -0.1127   0.4413   1.0000
   5.250   1.0644   0.01390   0.00777  -0.1080   0.4146   1.0000
   5.500   1.0771   0.01449   0.00828  -0.1058   0.4023   1.0000
   5.750   1.0890   0.01515   0.00886  -0.1035   0.3904   1.0000
   6.000   1.1040   0.01574   0.00939  -0.1017   0.3800   1.0000
   6.250   1.1170   0.01644   0.01003  -0.0997   0.3709   1.0000
   6.500   1.1327   0.01705   0.01060  -0.0982   0.3629   1.0000
   6.750   1.1459   0.01779   0.01129  -0.0964   0.3555   1.0000
   7.000   1.1626   0.01840   0.01188  -0.0951   0.3500   1.0000
   7.250   1.1794   0.01902   0.01249  -0.0939   0.3449   1.0000
   7.500   1.1943   0.01975   0.01320  -0.0925   0.3403   1.0000
   7.750   1.2085   0.02055   0.01397  -0.0911   0.3359   1.0000
   8.000   1.2267   0.02114   0.01457  -0.0902   0.3328   1.0000
   8.250   1.2437   0.02181   0.01525  -0.0892   0.3295   1.0000
   8.500   1.2600   0.02254   0.01598  -0.0881   0.3260   1.0000
   8.750   1.2745   0.02339   0.01682  -0.0869   0.3224   1.0000
   9.000   1.2884   0.02430   0.01772  -0.0857   0.3189   1.0000
   9.250   1.3043   0.02511   0.01854  -0.0847   0.3163   1.0000
   9.500   1.3220   0.02582   0.01929  -0.0840   0.3143   1.0000
   9.750   1.3392   0.02657   0.02006  -0.0832   0.3120   1.0000
  10.000   1.3551   0.02742   0.02093  -0.0824   0.3093   1.0000
  10.250   1.3701   0.02834   0.02186  -0.0814   0.3065   1.0000
  10.500   1.3840   0.02935   0.02287  -0.0805   0.3036   1.0000
  10.750   1.3960   0.03052   0.02403  -0.0793   0.3002   1.0000
  11.000   1.4120   0.03140   0.02495  -0.0786   0.2976   1.0000
  11.250   1.4283   0.03228   0.02588  -0.0780   0.2954   1.0000
  11.500   1.4440   0.03321   0.02685  -0.0773   0.2930   1.0000
  11.750   1.4587   0.03421   0.02787  -0.0766   0.2900   1.0000
  12.000   1.4714   0.03539   0.02907  -0.0757   0.2869   1.0000
  12.250   1.4831   0.03665   0.03033  -0.0748   0.2838   1.0000
  12.500   1.4959   0.03782   0.03152  -0.0740   0.2810   1.0000
  12.750   1.5112   0.03884   0.03260  -0.0734   0.2785   1.0000
  13.000   1.5254   0.03992   0.03373  -0.0728   0.2756   1.0000
  13.250   1.5386   0.04109   0.03493  -0.0721   0.2723   1.0000
  13.500   1.5488   0.04252   0.03638  -0.0712   0.2686   1.0000
  13.750   1.5574   0.04410   0.03796  -0.0703   0.2649   1.0000
  14.000   1.5718   0.04520   0.03913  -0.0698   0.2612   1.0000
  14.250   1.5826   0.04664   0.04061  -0.0691   0.2564   1.0000
  14.500   1.5902   0.04836   0.04234  -0.0683   0.2515   1.0000
  14.750   1.5997   0.04991   0.04391  -0.0675   0.2469   1.0000
  15.000   1.6080   0.05159   0.04564  -0.0668   0.2404   1.0000
  15.250   1.6115   0.05375   0.04779  -0.0658   0.2331   1.0000
  15.500   1.6162   0.05581   0.04987  -0.0650   0.2236   1.0000
  15.750   1.6163   0.05834   0.05237  -0.0640   0.2131   1.0000
  16.000   1.6127   0.06127   0.05527  -0.0629   0.2020   1.0000
  16.500   1.6053   0.06722   0.06119  -0.0608   0.1842   1.0000
  16.750   1.6013   0.07028   0.06424  -0.0599   0.1776   1.0000
  17.000   1.6005   0.07306   0.06705  -0.0593   0.1724   1.0000
  17.250   1.5965   0.07618   0.07017  -0.0585   0.1670   1.0000
  17.500   1.5946   0.07913   0.07315  -0.0580   0.1627   1.0000
  17.750   1.5955   0.08179   0.07584  -0.0576   0.1585   1.0000
  18.000   1.5916   0.08503   0.07912  -0.0571   0.1549   1.0000
  18.250   1.5894   0.08810   0.08222  -0.0568   0.1518   1.0000
  18.500   1.5928   0.09056   0.08474  -0.0567   0.1496   1.0000
  18.750   1.5955   0.09308   0.08732  -0.0566   0.1469   1.0000
  19.000   1.5944   0.09608   0.09037  -0.0565   0.1442   1.0000
  19.250   1.5920   0.09925   0.09359  -0.0565   0.1416   1.0000
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