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UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL (gu255118-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL (gu255118-il)
Reynolds number: 500,000
Max Cl/Cd: 63.3 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-gu255118-il-500000.txt
Download as CSV file: xf-gu255118-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500   0.1967   0.09109   0.08673  -0.1529   0.6466   0.0312
 -12.250   0.1927   0.08696   0.08261  -0.1548   0.6460   0.0313
 -12.000   0.1964   0.08330   0.07896  -0.1554   0.6452   0.0316
 -11.750   0.2091   0.08161   0.07727  -0.1552   0.6442   0.0320
 -11.500   0.2169   0.07931   0.07497  -0.1557   0.6434   0.0324
 -11.250   0.2231   0.07684   0.07250  -0.1563   0.6425   0.0328
 -11.000   0.2279   0.07421   0.06988  -0.1570   0.6417   0.0334
 -10.750   0.2306   0.07134   0.06702  -0.1578   0.6409   0.0343
 -10.500   0.2291   0.06782   0.06351  -0.1589   0.6403   0.0353
 -10.250   0.1825   0.05643   0.05218  -0.1662   0.6401   0.0371
 -10.000   0.1782   0.05268   0.04847  -0.1660   0.6394   0.0376
  -9.750   0.1870   0.05144   0.04722  -0.1654   0.6386   0.0380
  -9.500   0.1904   0.04922   0.04501  -0.1656   0.6379   0.0385
  -9.250   0.1812   0.04494   0.04075  -0.1677   0.6373   0.0388
  -9.000   0.0230   0.04502   0.04027  -0.1742   0.6380   0.0377
  -8.750   0.0283   0.04343   0.03866  -0.1726   0.6372   0.0380
  -8.500   0.0402   0.04262   0.03787  -0.1716   0.6363   0.0386
  -8.250   0.0423   0.04120   0.03638  -0.1695   0.6355   0.0390
  -8.000   0.0446   0.03972   0.03480  -0.1673   0.6345   0.0396
  -7.750   0.0471   0.03812   0.03310  -0.1648   0.6339   0.0408
  -7.500   0.0357   0.03791   0.03233  -0.1586   0.6334   0.0439
  -7.250   0.0324   0.03321   0.02754  -0.1561   0.6329   0.0450
  -7.000   0.0072   0.02492   0.01813  -0.1472   0.6324   0.0319
  -6.750   0.0240   0.02355   0.01659  -0.1456   0.6317   0.0320
  -6.500   0.0451   0.02268   0.01571  -0.1450   0.6311   0.0327
  -6.250   0.0658   0.02182   0.01477  -0.1441   0.6304   0.0331
  -6.000   0.0864   0.02075   0.01352  -0.1430   0.6297   0.0331
  -5.750   0.1089   0.01996   0.01263  -0.1423   0.6291   0.0333
  -5.500   0.1321   0.01929   0.01187  -0.1417   0.6284   0.0337
  -5.250   0.1557   0.01869   0.01120  -0.1412   0.6276   0.0342
  -5.000   0.1796   0.01815   0.01060  -0.1407   0.6268   0.0347
  -4.750   0.2036   0.01775   0.01014  -0.1402   0.6261   0.0356
  -4.500   0.2278   0.01742   0.00975  -0.1397   0.6255   0.0363
  -4.250   0.2521   0.01715   0.00942  -0.1393   0.6249   0.0369
  -4.000   0.2748   0.01662   0.00887  -0.1386   0.6243   0.0376
  -3.750   0.2962   0.01615   0.00840  -0.1377   0.6238   0.0384
  -3.500   0.3185   0.01587   0.00812  -0.1369   0.6232   0.0395
  -3.250   0.3413   0.01568   0.00792  -0.1362   0.6227   0.0406
  -3.000   0.3645   0.01554   0.00776  -0.1356   0.6222   0.0420
  -2.750   0.3885   0.01546   0.00766  -0.1351   0.6217   0.0435
  -2.500   0.4105   0.01527   0.00744  -0.1342   0.6212   0.0453
  -2.250   0.4337   0.01518   0.00735  -0.1336   0.6207   0.0474
  -2.000   0.4577   0.01518   0.00734  -0.1332   0.6202   0.0503
  -1.750   0.4811   0.01519   0.00735  -0.1326   0.6197   0.0553
  -1.500   0.5036   0.01526   0.00748  -0.1319   0.6191   0.0690
  -1.250   0.5167   0.01474   0.00755  -0.1296   0.6187   0.2291
  -1.000   0.5258   0.01410   0.00765  -0.1266   0.6184   0.4479
  -0.750   0.5389   0.01390   0.00783  -0.1239   0.6180   0.5669
  -0.500   0.5539   0.01385   0.00803  -0.1216   0.6175   0.6409
  -0.250   0.5678   0.01378   0.00822  -0.1190   0.6169   0.7121
   0.000   0.5831   0.01374   0.00845  -0.1166   0.6162   0.7868
   0.250   0.6485   0.01382   0.00883  -0.1250   0.6158   0.8910
   0.500   0.7466   0.01433   0.00934  -0.1401   0.6155   0.9470
   0.750   0.7901   0.01477   0.00975  -0.1437   0.6150   0.9627
   1.000   0.8280   0.01513   0.01009  -0.1464   0.6145   0.9711
   1.250   0.8678   0.01546   0.01039  -0.1495   0.6140   0.9765
   1.500   0.9033   0.01580   0.01073  -0.1518   0.6135   0.9828
   1.750   0.9441   0.01610   0.01101  -0.1553   0.6130   0.9865
   2.000   0.9824   0.01642   0.01132  -0.1583   0.6124   0.9912
   2.250   1.0214   0.01667   0.01156  -0.1614   0.6118   0.9950
   2.500   1.0618   0.01687   0.01176  -0.1649   0.6111   0.9984
   2.750   1.0875   0.01718   0.01208  -0.1653   0.6105   1.0000
   3.000   1.0983   0.01755   0.01245  -0.1627   0.6098   1.0000
   3.250   1.1108   0.01788   0.01280  -0.1603   0.6091   1.0000
   3.500   1.1260   0.01814   0.01306  -0.1584   0.6083   1.0000
   3.750   1.1415   0.01843   0.01335  -0.1566   0.6076   1.0000
   4.000   1.1593   0.01868   0.01360  -0.1552   0.6069   1.0000
   4.250   1.1781   0.01893   0.01385  -0.1539   0.6062   1.0000
   4.500   1.1968   0.01924   0.01416  -0.1527   0.6055   1.0000
   4.750   1.2162   0.01959   0.01451  -0.1517   0.6048   1.0000
   5.000   1.2347   0.02022   0.01514  -0.1506   0.6038   1.0000
   5.250   0.9508   0.02849   0.02378  -0.0991   0.5905   1.0000
   5.500   0.9836   0.02816   0.02343  -0.1000   0.5903   1.0000
   5.750   1.0140   0.02801   0.02327  -0.1006   0.5900   1.0000
   6.000   1.0451   0.02785   0.02310  -0.1014   0.5897   1.0000
   6.250   1.0779   0.02764   0.02290  -0.1024   0.5894   1.0000
   6.500   1.1131   0.02736   0.02261  -0.1038   0.5892   1.0000
   6.750   1.1477   0.02721   0.02245  -0.1052   0.5888   1.0000
   7.000   0.8153   0.04997   0.04543  -0.0685   0.5360   1.0000
   7.250   0.8408   0.04992   0.04539  -0.0686   0.5350   1.0000
   7.500   0.8682   0.04972   0.04518  -0.0688   0.5343   1.0000
   7.750   0.8949   0.04960   0.04507  -0.0690   0.5337   1.0000
   8.000   0.9227   0.04935   0.04482  -0.0693   0.5331   1.0000
   8.250   0.9504   0.04909   0.04458  -0.0696   0.5326   1.0000
   8.500   0.9784   0.04881   0.04431  -0.0699   0.5322   1.0000
   8.750   1.0077   0.04838   0.04390  -0.0703   0.5319   1.0000
   9.000   1.0359   0.04808   0.04362  -0.0706   0.5316   1.0000
   9.250   1.0655   0.04761   0.04318  -0.0711   0.5313   1.0000
   9.500   1.0952   0.04712   0.04271  -0.0716   0.5311   1.0000
   9.750   1.1252   0.04660   0.04221  -0.0721   0.5309   1.0000
  10.000   1.1565   0.04593   0.04158  -0.0727   0.5308   1.0000
  10.250   1.1876   0.04527   0.04095  -0.0733   0.5307   1.0000
  10.500   1.2197   0.04452   0.04024  -0.0741   0.5306   1.0000
  10.750   1.2532   0.04367   0.03943  -0.0749   0.5306   1.0000
  11.000   1.2868   0.04280   0.03860  -0.0758   0.5304   1.0000
  11.250   1.3247   0.04157   0.03741  -0.0771   0.5304   1.0000
  11.500   1.3687   0.03976   0.03565  -0.0789   0.5303   1.0000
  11.750   1.4199   0.03744   0.03336  -0.0814   0.5303   1.0000
  12.750   1.3461   0.05114   0.04724  -0.0684   0.4825   1.0000
  13.000   1.3865   0.04965   0.04575  -0.0698   0.4774   1.0000
  13.250   1.4083   0.04979   0.04588  -0.0698   0.4655   1.0000
  13.500   1.4354   0.04941   0.04546  -0.0701   0.4530   1.0000
  13.750   1.4569   0.04947   0.04545  -0.0700   0.4382   1.0000
  14.000   1.4667   0.05058   0.04649  -0.0690   0.4225   1.0000
  14.250   1.4669   0.05249   0.04825  -0.0672   0.4011   1.0000
  14.500   1.4629   0.05488   0.05057  -0.0653   0.3815   1.0000
  14.750   1.4501   0.05808   0.05363  -0.0628   0.3580   1.0000
  15.000   1.4424   0.06095   0.05640  -0.0608   0.3366   1.0000
  15.250   1.4259   0.06468   0.05998  -0.0583   0.3116   1.0000
  15.500   1.4196   0.06754   0.06275  -0.0567   0.2911   1.0000
  15.750   1.4079   0.07101   0.06610  -0.0548   0.2689   1.0000
  16.000   1.3953   0.07460   0.06954  -0.0529   0.2426   1.0000
  16.250   1.3853   0.07804   0.07287  -0.0514   0.2216   1.0000
  16.500   1.3757   0.08145   0.07614  -0.0499   0.1969   1.0000
  16.750   1.3650   0.08509   0.07965  -0.0486   0.1730   1.0000
  17.000   1.3574   0.08843   0.08286  -0.0475   0.1515   1.0000
  17.250   1.3472   0.09212   0.08641  -0.0464   0.1272   1.0000
  17.500   1.3329   0.09627   0.09034  -0.0452   0.0967   1.0000
  17.750   1.3211   0.10026   0.09415  -0.0443   0.0718   1.0000
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