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GOE 620 AIRFOIL (goe620-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 620 AIRFOIL (goe620-il)
Reynolds number: 500,000
Max Cl/Cd: 97.7 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe620-il-500000.txt
Download as CSV file: xf-goe620-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 620 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.4995   0.05094   0.04740  -0.1421   0.9696   0.0415
 -13.500  -0.5175   0.04284   0.03901  -0.1535   0.9618   0.0415
 -13.250  -0.5214   0.03635   0.03218  -0.1647   0.9541   0.0418
 -13.000  -0.5034   0.03341   0.02914  -0.1692   0.9473   0.0423
 -12.750  -0.4818   0.03134   0.02696  -0.1726   0.9396   0.0427
 -12.500  -0.4627   0.02992   0.02544  -0.1741   0.9296   0.0431
 -12.250  -0.4421   0.02855   0.02395  -0.1754   0.9202   0.0435
 -12.000  -0.4342   0.02752   0.02278  -0.1738   0.9066   0.0439
 -11.750  -0.4241   0.02641   0.02151  -0.1725   0.8945   0.0443
 -11.500  -0.4100   0.02536   0.02028  -0.1716   0.8844   0.0448
 -11.250  -0.4016   0.02445   0.01921  -0.1693   0.8733   0.0451
 -11.000  -0.3866   0.02354   0.01810  -0.1680   0.8650   0.0456
 -10.750  -0.3745   0.02279   0.01719  -0.1660   0.8557   0.0460
 -10.500  -0.3570   0.02211   0.01630  -0.1648   0.8484   0.0464
 -10.250  -0.3426   0.02138   0.01543  -0.1630   0.8408   0.0469
 -10.000  -0.3234   0.02024   0.01426  -0.1621   0.8343   0.0476
  -9.750  -0.3012   0.01962   0.01358  -0.1615   0.8286   0.0482
  -9.500  -0.2823   0.01911   0.01304  -0.1601   0.8222   0.0489
  -9.250  -0.2615   0.01859   0.01245  -0.1591   0.8162   0.0495
  -9.000  -0.2382   0.01810   0.01183  -0.1585   0.8107   0.0502
  -8.750  -0.2183   0.01762   0.01129  -0.1571   0.8051   0.0509
  -8.500  -0.1966   0.01716   0.01076  -0.1561   0.7998   0.0515
  -8.250  -0.1729   0.01681   0.01028  -0.1554   0.7951   0.0521
  -8.000  -0.1510   0.01611   0.00951  -0.1546   0.7907   0.0530
  -7.750  -0.1303   0.01556   0.00899  -0.1534   0.7860   0.0539
  -7.500  -0.1075   0.01519   0.00861  -0.1525   0.7815   0.0549
  -7.250  -0.0834   0.01485   0.00822  -0.1519   0.7773   0.0560
  -7.000  -0.0579   0.01456   0.00784  -0.1514   0.7732   0.0571
  -6.750  -0.0354   0.01426   0.00751  -0.1504   0.7691   0.0580
  -6.500  -0.0128   0.01387   0.00708  -0.1494   0.7648   0.0590
  -6.250   0.0096   0.01342   0.00663  -0.1484   0.7607   0.0603
  -6.000   0.0348   0.01314   0.00630  -0.1479   0.7569   0.0618
  -5.750   0.0597   0.01292   0.00605  -0.1473   0.7530   0.0634
  -5.500   0.0836   0.01271   0.00582  -0.1465   0.7488   0.0650
  -5.250   0.1065   0.01235   0.00546  -0.1455   0.7447   0.0671
  -5.000   0.1315   0.01211   0.00520  -0.1449   0.7407   0.0694
  -4.750   0.1588   0.01196   0.00498  -0.1447   0.7366   0.0719
  -4.500   0.1823   0.01172   0.00476  -0.1438   0.7328   0.0752
  -4.250   0.2067   0.01153   0.00459  -0.1430   0.7286   0.0798
  -4.000   0.2315   0.01131   0.00439  -0.1423   0.7242   0.0874
  -3.750   0.2573   0.01107   0.00420  -0.1418   0.7201   0.1032
  -3.500   0.2828   0.01083   0.00406  -0.1414   0.7161   0.1320
  -3.250   0.3059   0.01063   0.00398  -0.1404   0.7116   0.1592
  -3.000   0.3311   0.01051   0.00391  -0.1397   0.7069   0.1811
  -2.750   0.3575   0.01043   0.00384  -0.1393   0.7025   0.1984
  -2.500   0.3854   0.01040   0.00380  -0.1393   0.6981   0.2140
  -2.250   0.4086   0.01030   0.00377  -0.1382   0.6933   0.2275
  -2.000   0.4334   0.01022   0.00372  -0.1374   0.6881   0.2408
  -1.750   0.4598   0.01018   0.00366  -0.1370   0.6833   0.2547
  -1.500   0.4861   0.01015   0.00365  -0.1366   0.6785   0.2692
  -1.250   0.5091   0.01007   0.00363  -0.1355   0.6729   0.2833
  -1.000   0.5336   0.01001   0.00359  -0.1347   0.6672   0.2976
  -0.750   0.5607   0.01002   0.00355  -0.1344   0.6617   0.3128
  -0.500   0.5819   0.00994   0.00355  -0.1329   0.6551   0.3290
  -0.250   0.6048   0.00987   0.00351  -0.1318   0.6478   0.3462
   0.000   0.6278   0.00984   0.00350  -0.1306   0.6406   0.3648
   0.250   0.6489   0.00978   0.00349  -0.1291   0.6321   0.3840
   0.500   0.6707   0.00976   0.00347  -0.1278   0.6240   0.4043
   0.750   0.6903   0.00972   0.00347  -0.1260   0.6142   0.4248
   1.000   0.7099   0.00970   0.00348  -0.1242   0.6047   0.4486
   1.250   0.7288   0.00967   0.00352  -0.1223   0.5954   0.4783
   1.500   0.7480   0.00967   0.00357  -0.1204   0.5875   0.5129
   1.750   0.7648   0.00964   0.00364  -0.1181   0.5791   0.5496
   2.000   0.7815   0.00966   0.00370  -0.1157   0.5714   0.5872
   2.250   0.7974   0.00963   0.00379  -0.1132   0.5629   0.6304
   2.500   0.8106   0.00961   0.00391  -0.1101   0.5545   0.6938
   2.750   0.9403   0.00963   0.00446  -0.1321   0.5396   1.0000
   3.000   0.9545   0.00977   0.00455  -0.1293   0.5318   1.0000
   3.250   0.9685   0.00994   0.00465  -0.1264   0.5235   1.0000
   3.500   0.9838   0.01012   0.00477  -0.1239   0.5160   1.0000
   3.750   0.9995   0.01029   0.00490  -0.1215   0.5079   1.0000
   4.000   1.0151   0.01052   0.00505  -0.1191   0.5005   1.0000
   4.250   1.0332   0.01069   0.00521  -0.1172   0.4934   1.0000
   4.500   1.0491   0.01093   0.00538  -0.1149   0.4857   1.0000
   4.750   1.0672   0.01114   0.00557  -0.1131   0.4789   1.0000
   5.000   1.0844   0.01137   0.00578  -0.1111   0.4713   1.0000
   5.250   1.1008   0.01166   0.00601  -0.1091   0.4643   1.0000
   5.500   1.1194   0.01189   0.00623  -0.1075   0.4569   1.0000
   5.750   1.1351   0.01221   0.00650  -0.1054   0.4492   1.0000
   6.000   1.1535   0.01248   0.00676  -0.1038   0.4420   1.0000
   6.250   1.1696   0.01282   0.00707  -0.1019   0.4338   1.0000
   6.500   1.1860   0.01318   0.00740  -0.1001   0.4257   1.0000
   6.750   1.2021   0.01356   0.00775  -0.0982   0.4169   1.0000
   7.000   1.2178   0.01398   0.00814  -0.0964   0.4090   1.0000
   7.250   1.2343   0.01439   0.00854  -0.0948   0.4002   1.0000
   7.500   1.2489   0.01490   0.00901  -0.0929   0.3919   1.0000
   7.750   1.2649   0.01537   0.00947  -0.0913   0.3828   1.0000
   8.000   1.2787   0.01595   0.01002  -0.0894   0.3736   1.0000
   8.250   1.2926   0.01656   0.01060  -0.0876   0.3635   1.0000
   8.500   1.3067   0.01719   0.01120  -0.0859   0.3543   1.0000
   8.750   1.3196   0.01789   0.01187  -0.0841   0.3452   1.0000
   9.000   1.3337   0.01857   0.01254  -0.0825   0.3364   1.0000
   9.250   1.3452   0.01941   0.01334  -0.0807   0.3274   1.0000
   9.500   1.3590   0.02015   0.01408  -0.0793   0.3188   1.0000
   9.750   1.3698   0.02108   0.01497  -0.0775   0.3104   1.0000
  10.000   1.3833   0.02189   0.01578  -0.0761   0.3026   1.0000
  10.250   1.3943   0.02286   0.01673  -0.0745   0.2951   1.0000
  10.500   1.4068   0.02377   0.01764  -0.0731   0.2885   1.0000
  10.750   1.4190   0.02472   0.01859  -0.0717   0.2817   1.0000
  11.000   1.4281   0.02589   0.01972  -0.0701   0.2755   1.0000
  11.250   1.4428   0.02673   0.02061  -0.0691   0.2703   1.0000
  11.500   1.4544   0.02778   0.02167  -0.0679   0.2651   1.0000
  11.750   1.4629   0.02906   0.02293  -0.0664   0.2596   1.0000
  12.000   1.4764   0.03002   0.02394  -0.0654   0.2539   1.0000
  12.250   1.4874   0.03117   0.02510  -0.0643   0.2489   1.0000
  12.500   1.4941   0.03266   0.02658  -0.0628   0.2433   1.0000
  12.750   1.5080   0.03364   0.02762  -0.0620   0.2387   1.0000
  13.000   1.5166   0.03505   0.02903  -0.0608   0.2326   1.0000
  13.250   1.5231   0.03662   0.03061  -0.0596   0.2265   1.0000
  13.500   1.5326   0.03801   0.03204  -0.0586   0.2194   1.0000
  13.750   1.5356   0.03995   0.03394  -0.0573   0.2115   1.0000
  14.000   1.5431   0.04157   0.03559  -0.0563   0.2024   1.0000
  14.250   1.5466   0.04354   0.03755  -0.0552   0.1926   1.0000
  14.500   1.5468   0.04586   0.03985  -0.0540   0.1810   1.0000
  14.750   1.5454   0.04838   0.04233  -0.0528   0.1674   1.0000
  15.000   1.5426   0.05110   0.04500  -0.0517   0.1556   1.0000
  15.250   1.5400   0.05383   0.04770  -0.0507   0.1477   1.0000
  15.500   1.5359   0.05678   0.05065  -0.0498   0.1419   1.0000
  15.750   1.5373   0.05922   0.05312  -0.0491   0.1389   1.0000
  16.000   1.5370   0.06187   0.05581  -0.0484   0.1359   1.0000
  16.250   1.5355   0.06470   0.05867  -0.0478   0.1337   1.0000
  16.500   1.5324   0.06770   0.06169  -0.0473   0.1310   1.0000
  16.750   1.5349   0.07014   0.06420  -0.0469   0.1294   1.0000
  17.000   1.5385   0.07246   0.06660  -0.0466   0.1279   1.0000
  17.250   1.5398   0.07509   0.06929  -0.0463   0.1260   1.0000
  17.500   1.5399   0.07784   0.07210  -0.0461   0.1242   1.0000
  17.750   1.5394   0.08067   0.07497  -0.0459   0.1228   1.0000
  18.000   1.5371   0.08372   0.07805  -0.0457   0.1209   1.0000
  18.250   1.5362   0.08657   0.08092  -0.0456   0.1189   1.0000
  18.500   1.5395   0.08899   0.08341  -0.0456   0.1177   1.0000
  18.750   1.5421   0.09157   0.08609  -0.0457   0.1165   1.0000
  19.000   1.5453   0.09403   0.08863  -0.0458   0.1152   1.0000
  19.250   1.5461   0.09682   0.09150  -0.0460   0.1136   1.0000
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