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UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL (gu255118-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL (gu255118-il)
Reynolds number: 1,000,000
Max Cl/Cd: 137.44 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-gu255118-il-1000000-n5.txt
Download as CSV file: xf-gu255118-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: UNIVERSITY OF GLASGOW GU25-5(11)8 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.2881   0.04433   0.04003  -0.1821   0.6109   0.0143
 -14.250  -0.3364   0.03648   0.03196  -0.1864   0.6103   0.0142
 -14.000  -0.3425   0.03396   0.02936  -0.1871   0.6093   0.0143
 -13.750  -0.3603   0.03097   0.02623  -0.1867   0.6085   0.0144
 -13.500  -0.3746   0.02868   0.02381  -0.1851   0.6074   0.0144
 -13.250  -0.3808   0.02713   0.02216  -0.1829   0.6063   0.0145
 -13.000  -0.3838   0.02588   0.02079  -0.1804   0.6052   0.0146
 -12.750  -0.3840   0.02484   0.01965  -0.1777   0.6040   0.0147
 -12.500  -0.3874   0.02365   0.01834  -0.1743   0.6029   0.0148
 -12.250  -0.3842   0.02284   0.01742  -0.1713   0.6018   0.0149
 -12.000  -0.3806   0.02206   0.01654  -0.1681   0.6008   0.0150
 -11.750  -0.3767   0.02134   0.01573  -0.1647   0.5996   0.0151
 -11.500  -0.3709   0.02084   0.01512  -0.1614   0.5986   0.0152
 -11.250  -0.3621   0.02024   0.01442  -0.1587   0.5974   0.0153
 -11.000  -0.3487   0.01973   0.01382  -0.1567   0.5963   0.0154
 -10.750  -0.3348   0.01915   0.01315  -0.1548   0.5958   0.0155
 -10.500  -0.3188   0.01865   0.01257  -0.1532   0.5952   0.0156
 -10.250  -0.3068   0.01780   0.01163  -0.1510   0.5946   0.0158
 -10.000  -0.2896   0.01733   0.01111  -0.1495   0.5939   0.0161
  -9.750  -0.2711   0.01691   0.01063  -0.1482   0.5932   0.0162
  -9.500  -0.2513   0.01656   0.01024  -0.1471   0.5925   0.0164
  -9.250  -0.2310   0.01622   0.00985  -0.1460   0.5917   0.0165
  -9.000  -0.2098   0.01594   0.00953  -0.1451   0.5910   0.0167
  -8.750  -0.1887   0.01563   0.00918  -0.1442   0.5902   0.0169
  -8.500  -0.1670   0.01535   0.00886  -0.1433   0.5895   0.0172
  -8.250  -0.1452   0.01507   0.00854  -0.1425   0.5889   0.0174
  -8.000  -0.1235   0.01477   0.00818  -0.1416   0.5881   0.0177
  -7.750  -0.1019   0.01445   0.00781  -0.1407   0.5874   0.0179
  -7.500  -0.0797   0.01417   0.00748  -0.1399   0.5867   0.0182
  -7.250  -0.0579   0.01387   0.00712  -0.1390   0.5860   0.0184
  -7.000  -0.0355   0.01362   0.00683  -0.1382   0.5852   0.0186
  -6.750  -0.0132   0.01336   0.00652  -0.1374   0.5845   0.0189
  -6.500   0.0095   0.01314   0.00626  -0.1366   0.5837   0.0191
  -6.250   0.0325   0.01295   0.00602  -0.1359   0.5829   0.0192
  -6.000   0.0540   0.01265   0.00568  -0.1349   0.5822   0.0195
  -5.750   0.0759   0.01238   0.00539  -0.1340   0.5814   0.0200
  -5.500   0.0993   0.01219   0.00518  -0.1334   0.5811   0.0204
  -5.250   0.1231   0.01201   0.00499  -0.1328   0.5808   0.0207
  -5.000   0.1472   0.01185   0.00482  -0.1323   0.5805   0.0211
  -4.750   0.1715   0.01171   0.00468  -0.1319   0.5801   0.0216
  -4.500   0.1956   0.01157   0.00451  -0.1313   0.5798   0.0221
  -4.250   0.2196   0.01142   0.00435  -0.1308   0.5794   0.0225
  -4.000   0.2439   0.01129   0.00421  -0.1303   0.5790   0.0230
  -3.750   0.2682   0.01117   0.00407  -0.1298   0.5786   0.0233
  -3.500   0.2927   0.01106   0.00395  -0.1294   0.5782   0.0236
  -3.250   0.3161   0.01089   0.00377  -0.1288   0.5777   0.0243
  -3.000   0.3400   0.01076   0.00363  -0.1282   0.5773   0.0251
  -2.750   0.3644   0.01066   0.00353  -0.1278   0.5769   0.0257
  -2.500   0.3890   0.01058   0.00345  -0.1273   0.5765   0.0266
  -2.250   0.4136   0.01051   0.00338  -0.1270   0.5761   0.0276
  -2.000   0.4383   0.01044   0.00331  -0.1266   0.5757   0.0283
  -1.750   0.4630   0.01039   0.00325  -0.1262   0.5752   0.0289
  -1.500   0.4871   0.01030   0.00317  -0.1257   0.5748   0.0308
  -1.250   0.5117   0.01025   0.00313  -0.1253   0.5744   0.0323
  -1.000   0.5362   0.01021   0.00309  -0.1249   0.5740   0.0341
  -0.750   0.5605   0.01016   0.00306  -0.1244   0.5736   0.0390
  -0.500   0.5831   0.01003   0.00303  -0.1237   0.5732   0.0697
  -0.250   0.6054   0.00988   0.00302  -0.1229   0.5728   0.1121
   0.000   0.6261   0.00968   0.00302  -0.1218   0.5724   0.1832
   0.500   0.6647   0.00920   0.00304  -0.1192   0.5716   0.3638
   0.750   0.6808   0.00892   0.00308  -0.1171   0.5713   0.4795
   1.000   0.6971   0.00871   0.00314  -0.1151   0.5709   0.5686
   1.250   0.7126   0.00853   0.00320  -0.1128   0.5705   0.6509
   1.500   0.7240   0.00832   0.00329  -0.1095   0.5700   0.7458
   1.750   0.7410   0.00807   0.00343  -0.1074   0.5696   0.8645
   2.000   0.8881   0.00837   0.00384  -0.1344   0.5694   0.9419
   2.250   0.9290   0.00851   0.00396  -0.1377   0.5689   0.9500
   2.750   0.9921   0.00879   0.00421  -0.1402   0.5680   0.9654
   3.000   1.0196   0.00891   0.00432  -0.1406   0.5676   0.9719
   3.250   1.0541   0.00905   0.00445  -0.1425   0.5671   0.9751
   3.500   1.0861   0.00919   0.00458  -0.1439   0.5667   0.9790
   4.000   1.1488   0.00944   0.00484  -0.1466   0.5662   0.9849
   4.250   1.1824   0.00955   0.00497  -0.1484   0.5660   0.9869
   4.500   1.2146   0.00967   0.00510  -0.1499   0.5658   0.9891
   4.750   1.2454   0.00979   0.00524  -0.1512   0.5655   0.9913
   5.000   1.2752   0.00992   0.00539  -0.1522   0.5653   0.9934
   5.250   1.3087   0.01003   0.00552  -0.1541   0.5649   0.9951
   5.500   1.3415   0.01013   0.00565  -0.1558   0.5645   0.9968
   5.750   1.3746   0.01023   0.00579  -0.1577   0.5639   0.9984
   6.000   1.4086   0.01034   0.00592  -0.1597   0.5632   0.9998
   6.250   1.4247   0.01041   0.00603  -0.1578   0.5623   1.0000
   6.500   1.4353   0.01048   0.00613  -0.1547   0.5614   1.0000
   6.750   1.4480   0.01056   0.00624  -0.1521   0.5606   1.0000
   7.000   1.4615   0.01065   0.00637  -0.1497   0.5597   1.0000
   7.250   1.4761   0.01075   0.00650  -0.1475   0.5588   1.0000
   7.500   1.4900   0.01085   0.00662  -0.1452   0.5575   1.0000
   7.750   1.5009   0.01093   0.00672  -0.1423   0.5553   1.0000
   8.000   1.5173   0.01104   0.00681  -0.1407   0.5524   1.0000
   8.250   1.5308   0.01123   0.00705  -0.1385   0.5511   1.0000
   8.500   1.5378   0.01147   0.00736  -0.1351   0.5489   1.0000
   8.750   1.5439   0.01175   0.00769  -0.1317   0.5449   1.0000
   9.000   1.5554   0.01203   0.00802  -0.1294   0.5419   1.0000
   9.250   1.5655   0.01240   0.00837  -0.1269   0.5378   1.0000
   9.500   1.5761   0.01286   0.00892  -0.1247   0.5337   1.0000
   9.750   1.5832   0.01348   0.00957  -0.1221   0.5265   1.0000
  10.000   1.5893   0.01425   0.01038  -0.1195   0.5170   1.0000
  10.250   1.5861   0.01554   0.01166  -0.1157   0.5007   1.0000
  10.500   1.5669   0.01782   0.01387  -0.1102   0.4803   1.0000
  10.750   1.5194   0.02202   0.01797  -0.1017   0.4543   1.0000
  11.000   1.4795   0.02620   0.02209  -0.0948   0.4318   1.0000
  11.250   1.4606   0.02927   0.02514  -0.0905   0.4184   1.0000
  11.500   1.4260   0.03356   0.02936  -0.0849   0.3973   1.0000
  11.750   1.3926   0.03799   0.03371  -0.0797   0.3737   1.0000
  12.000   1.3763   0.04125   0.03691  -0.0763   0.3568   1.0000
  12.250   1.3526   0.04518   0.04073  -0.0724   0.3331   1.0000
  12.500   1.3328   0.04885   0.04426  -0.0690   0.3064   1.0000
  12.750   1.3258   0.05160   0.04694  -0.0668   0.2893   1.0000
  13.000   1.3105   0.05504   0.05021  -0.0640   0.2592   1.0000
  13.250   1.3033   0.05787   0.05293  -0.0620   0.2363   1.0000
  13.500   1.2979   0.06056   0.05548  -0.0601   0.2119   1.0000
  13.750   1.2920   0.06337   0.05816  -0.0584   0.1888   1.0000
  14.000   1.2932   0.06557   0.06027  -0.0571   0.1717   1.0000
  14.250   1.2905   0.06810   0.06266  -0.0557   0.1483   1.0000
  14.500   1.2887   0.07063   0.06508  -0.0544   0.1275   1.0000
  14.750   1.2875   0.07317   0.06751  -0.0532   0.1092   1.0000
  15.250   1.2785   0.07891   0.07295  -0.0505   0.0625   1.0000
  15.500   1.2810   0.08118   0.07517  -0.0497   0.0519   1.0000
  15.750   1.2803   0.08377   0.07767  -0.0488   0.0365   1.0000
  16.000   1.2718   0.08725   0.08101  -0.0475   0.0151   1.0000
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