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GOE 620 AIRFOIL (goe620-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 620 AIRFOIL (goe620-il)
Reynolds number: 500,000
Max Cl/Cd: 82.52 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe620-il-500000-n5.txt
Download as CSV file: xf-goe620-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.5662   0.07983   0.07631  -0.1085   0.9835   0.0325
 -16.000  -0.5824   0.07250   0.06886  -0.1149   0.9810   0.0327
 -15.750  -0.5966   0.06665   0.06291  -0.1193   0.9751   0.0328
 -15.500  -0.6058   0.06111   0.05727  -0.1243   0.9705   0.0330
 -15.250  -0.6095   0.05617   0.05224  -0.1293   0.9661   0.0331
 -15.000  -0.6143   0.05139   0.04735  -0.1340   0.9592   0.0333
 -14.750  -0.6109   0.04670   0.04254  -0.1400   0.9542   0.0335
 -14.500  -0.6038   0.04270   0.03844  -0.1453   0.9468   0.0337
 -14.250  -0.5897   0.03854   0.03415  -0.1523   0.9403   0.0339
 -14.000  -0.5676   0.03485   0.03032  -0.1599   0.9335   0.0342
 -13.750  -0.5436   0.03157   0.02688  -0.1671   0.9238   0.0346
 -13.500  -0.5224   0.02875   0.02389  -0.1729   0.9112   0.0349
 -13.250  -0.5060   0.02646   0.02142  -0.1770   0.8966   0.0352
 -13.000  -0.4978   0.02478   0.01956  -0.1781   0.8813   0.0355
 -12.750  -0.4920   0.02367   0.01828  -0.1771   0.8671   0.0358
 -12.500  -0.4890   0.02280   0.01727  -0.1746   0.8537   0.0361
 -12.250  -0.4850   0.02211   0.01644  -0.1717   0.8424   0.0363
 -12.000  -0.4777   0.02152   0.01570  -0.1692   0.8318   0.0366
 -11.750  -0.4675   0.02087   0.01496  -0.1670   0.8224   0.0369
 -11.500  -0.4550   0.02027   0.01427  -0.1651   0.8139   0.0371
 -11.250  -0.4406   0.01972   0.01366  -0.1634   0.8069   0.0375
 -11.000  -0.4244   0.01923   0.01310  -0.1618   0.8000   0.0378
 -10.750  -0.4067   0.01878   0.01257  -0.1605   0.7938   0.0381
 -10.500  -0.3884   0.01835   0.01208  -0.1592   0.7878   0.0385
 -10.250  -0.3694   0.01793   0.01159  -0.1579   0.7819   0.0389
 -10.000  -0.3494   0.01753   0.01110  -0.1568   0.7768   0.0393
  -9.750  -0.3289   0.01714   0.01065  -0.1557   0.7721   0.0399
  -9.500  -0.3082   0.01675   0.01019  -0.1546   0.7669   0.0403
  -9.250  -0.2868   0.01641   0.00975  -0.1536   0.7615   0.0408
  -9.000  -0.2645   0.01611   0.00935  -0.1527   0.7565   0.0413
  -8.750  -0.2436   0.01569   0.00891  -0.1516   0.7516   0.0419
  -8.500  -0.2219   0.01533   0.00851  -0.1506   0.7468   0.0424
  -8.250  -0.1992   0.01503   0.00816  -0.1497   0.7424   0.0430
  -7.750  -0.1524   0.01446   0.00750  -0.1482   0.7349   0.0442
  -7.500  -0.1288   0.01418   0.00719  -0.1474   0.7309   0.0449
  -7.250  -0.1049   0.01393   0.00689  -0.1466   0.7269   0.0456
  -7.000  -0.0805   0.01371   0.00660  -0.1459   0.7231   0.0463
  -6.750  -0.0562   0.01347   0.00629  -0.1453   0.7196   0.0470
  -6.500  -0.0326   0.01317   0.00599  -0.1445   0.7161   0.0479
  -6.250  -0.0083   0.01292   0.00574  -0.1438   0.7123   0.0489
  -6.000   0.0164   0.01272   0.00551  -0.1431   0.7084   0.0499
  -5.750   0.0414   0.01254   0.00528  -0.1425   0.7047   0.0510
  -5.500   0.0668   0.01239   0.00506  -0.1419   0.7011   0.0520
  -5.250   0.0917   0.01219   0.00485  -0.1413   0.6977   0.0530
  -5.000   0.1163   0.01196   0.00462  -0.1406   0.6937   0.0543
  -4.750   0.1412   0.01178   0.00443  -0.1400   0.6895   0.0558
  -4.500   0.1666   0.01165   0.00425  -0.1394   0.6856   0.0575
  -4.250   0.1922   0.01153   0.00408  -0.1388   0.6819   0.0593
  -4.000   0.2170   0.01134   0.00392  -0.1382   0.6778   0.0617
  -3.750   0.2421   0.01120   0.00378  -0.1375   0.6734   0.0647
  -3.500   0.2670   0.01106   0.00364  -0.1368   0.6690   0.0693
  -3.250   0.2916   0.01090   0.00351  -0.1361   0.6646   0.0804
  -3.000   0.3161   0.01072   0.00341  -0.1354   0.6601   0.0994
  -2.750   0.3407   0.01058   0.00332  -0.1347   0.6550   0.1141
  -2.500   0.3650   0.01046   0.00323  -0.1339   0.6500   0.1292
  -2.250   0.3893   0.01036   0.00316  -0.1331   0.6450   0.1466
  -2.000   0.4137   0.01025   0.00313  -0.1323   0.6393   0.1663
  -1.750   0.4377   0.01018   0.00309  -0.1315   0.6332   0.1827
  -1.500   0.4614   0.01014   0.00305  -0.1305   0.6275   0.1976
  -1.250   0.4856   0.01008   0.00304  -0.1297   0.6210   0.2110
  -1.000   0.5088   0.01006   0.00302  -0.1286   0.6137   0.2224
  -0.750   0.5316   0.01004   0.00301  -0.1275   0.6063   0.2350
  -0.500   0.5526   0.01004   0.00300  -0.1260   0.5958   0.2459
  -0.250   0.5734   0.01006   0.00300  -0.1245   0.5851   0.2585
   0.000   0.5913   0.01010   0.00301  -0.1224   0.5725   0.2720
   0.250   0.6085   0.01014   0.00303  -0.1201   0.5608   0.2843
   0.500   0.6255   0.01020   0.00306  -0.1178   0.5489   0.2989
   0.750   0.6419   0.01027   0.00312  -0.1154   0.5386   0.3151
   1.000   0.6601   0.01034   0.00320  -0.1134   0.5280   0.3314
   1.250   0.6774   0.01045   0.00331  -0.1113   0.5183   0.3505
   1.500   0.6960   0.01055   0.00343  -0.1094   0.5091   0.3700
   1.750   0.7147   0.01066   0.00355  -0.1076   0.5019   0.3892
   2.000   0.7342   0.01075   0.00368  -0.1059   0.4941   0.4103
   2.250   0.7509   0.01092   0.00384  -0.1038   0.4852   0.4272
   2.500   0.7705   0.01103   0.00398  -0.1022   0.4770   0.4465
   2.750   0.7874   0.01119   0.00416  -0.1001   0.4693   0.4682
   3.000   0.8068   0.01129   0.00433  -0.0985   0.4626   0.4955
   3.250   0.8241   0.01142   0.00452  -0.0965   0.4545   0.5297
   3.500   0.8408   0.01157   0.00473  -0.0944   0.4474   0.5638
   3.750   0.8587   0.01169   0.00493  -0.0926   0.4400   0.5987
   4.250   0.8874   0.01184   0.00541  -0.0875   0.4256   0.7209
   4.750   1.0150   0.01230   0.00622  -0.1038   0.4004   1.0000
   5.000   1.0322   0.01263   0.00650  -0.1021   0.3925   1.0000
   5.250   1.0496   0.01297   0.00679  -0.1004   0.3838   1.0000
   5.500   1.0663   0.01334   0.00713  -0.0986   0.3756   1.0000
   5.750   1.0828   0.01375   0.00748  -0.0969   0.3660   1.0000
   6.000   1.0995   0.01417   0.00786  -0.0952   0.3576   1.0000
   6.250   1.1156   0.01463   0.00828  -0.0935   0.3485   1.0000
   6.500   1.1313   0.01513   0.00873  -0.0919   0.3383   1.0000
   6.750   1.1448   0.01574   0.00928  -0.0899   0.3271   1.0000
   7.000   1.1600   0.01631   0.00981  -0.0883   0.3165   1.0000
   7.250   1.1743   0.01695   0.01040  -0.0866   0.3068   1.0000
   7.500   1.1888   0.01760   0.01100  -0.0850   0.2977   1.0000
   7.750   1.2039   0.01824   0.01162  -0.0835   0.2899   1.0000
   8.000   1.2181   0.01895   0.01229  -0.0819   0.2816   1.0000
   8.250   1.2327   0.01966   0.01298  -0.0805   0.2746   1.0000
   8.500   1.2472   0.02039   0.01369  -0.0791   0.2672   1.0000
   8.750   1.2600   0.02124   0.01452  -0.0776   0.2604   1.0000
   9.000   1.2756   0.02194   0.01522  -0.0764   0.2550   1.0000
   9.250   1.2888   0.02281   0.01608  -0.0751   0.2487   1.0000
   9.500   1.3023   0.02368   0.01694  -0.0738   0.2439   1.0000
   9.750   1.3176   0.02446   0.01773  -0.0727   0.2397   1.0000
  10.000   1.3318   0.02531   0.01859  -0.0716   0.2354   1.0000
  10.250   1.3433   0.02636   0.01964  -0.0702   0.2300   1.0000
  10.500   1.3568   0.02731   0.02059  -0.0691   0.2256   1.0000
  10.750   1.3714   0.02819   0.02150  -0.0681   0.2217   1.0000
  11.000   1.3830   0.02929   0.02261  -0.0670   0.2166   1.0000
  11.250   1.3935   0.03049   0.02380  -0.0657   0.2123   1.0000
  11.500   1.4075   0.03145   0.02481  -0.0648   0.2087   1.0000
  11.750   1.4199   0.03255   0.02593  -0.0639   0.2035   1.0000
  12.000   1.4295   0.03388   0.02726  -0.0627   0.1984   1.0000
  12.250   1.4400   0.03516   0.02856  -0.0617   0.1922   1.0000
  12.500   1.4469   0.03673   0.03011  -0.0605   0.1825   1.0000
  12.750   1.4517   0.03852   0.03186  -0.0592   0.1690   1.0000
  13.000   1.4474   0.04112   0.03434  -0.0575   0.1474   1.0000
  13.250   1.4464   0.04349   0.03666  -0.0560   0.1369   1.0000
  13.500   1.4487   0.04562   0.03878  -0.0549   0.1312   1.0000
  13.750   1.4533   0.04761   0.04080  -0.0539   0.1279   1.0000
  14.000   1.4562   0.04977   0.04298  -0.0530   0.1242   1.0000
  14.250   1.4594   0.05197   0.04521  -0.0522   0.1219   1.0000
  14.500   1.4628   0.05417   0.04744  -0.0514   0.1195   1.0000
  14.750   1.4675   0.05628   0.04960  -0.0507   0.1175   1.0000
  15.000   1.4733   0.05830   0.05169  -0.0502   0.1162   1.0000
  15.250   1.4778   0.06048   0.05393  -0.0496   0.1148   1.0000
  15.500   1.4813   0.06279   0.05629  -0.0491   0.1131   1.0000
  15.750   1.4850   0.06510   0.05866  -0.0487   0.1121   1.0000
  16.000   1.4868   0.06764   0.06125  -0.0483   0.1108   1.0000
  16.250   1.4886   0.07019   0.06386  -0.0479   0.1096   1.0000
  16.500   1.4877   0.07312   0.06684  -0.0476   0.1080   1.0000
  16.750   1.4870   0.07601   0.06978  -0.0474   0.1065   1.0000
  17.000   1.4929   0.07819   0.07204  -0.0473   0.1055   1.0000
  17.250   1.4981   0.08041   0.07434  -0.0471   0.1044   1.0000
  17.500   1.5013   0.08291   0.07691  -0.0471   0.1034   1.0000
  17.750   1.5050   0.08534   0.07942  -0.0471   0.1021   1.0000
  18.000   1.5060   0.08814   0.08229  -0.0471   0.1005   1.0000
  18.250   1.5076   0.09086   0.08506  -0.0472   0.0994   1.0000
  18.500   1.5065   0.09393   0.08820  -0.0474   0.0980   1.0000
  18.750   1.5056   0.09699   0.09130  -0.0476   0.0967   1.0000
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