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GOE 527 AIRFOIL (goe527-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 527 AIRFOIL (goe527-il)
Reynolds number: 200,000
Max Cl/Cd: 69.35 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe527-il-200000-n5.txt
Download as CSV file: xf-goe527-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 527 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.3891   0.03863   0.03371  -0.1350   0.8908   0.0385
 -11.000  -0.3897   0.03638   0.03123  -0.1347   0.8732   0.0388
 -10.750  -0.3834   0.03474   0.02939  -0.1340   0.8583   0.0392
 -10.500  -0.3763   0.03314   0.02757  -0.1329   0.8450   0.0397
 -10.250  -0.3690   0.03154   0.02572  -0.1315   0.8321   0.0403
 -10.000  -0.3620   0.02986   0.02375  -0.1297   0.8199   0.0408
  -9.750  -0.3516   0.02822   0.02179  -0.1282   0.8094   0.0414
  -9.500  -0.3398   0.02670   0.01995  -0.1265   0.7987   0.0419
  -9.250  -0.3248   0.02533   0.01825  -0.1251   0.7896   0.0425
  -9.000  -0.3072   0.02429   0.01700  -0.1238   0.7799   0.0431
  -8.750  -0.2864   0.02358   0.01621  -0.1229   0.7712   0.0436
  -8.500  -0.2656   0.02299   0.01553  -0.1219   0.7617   0.0442
  -8.250  -0.2438   0.02240   0.01481  -0.1210   0.7536   0.0451
  -8.000  -0.2227   0.02175   0.01402  -0.1199   0.7448   0.0460
  -7.750  -0.2005   0.02104   0.01311  -0.1190   0.7373   0.0470
  -7.500  -0.1786   0.02034   0.01222  -0.1180   0.7290   0.0480
  -7.250  -0.1558   0.01980   0.01161  -0.1172   0.7210   0.0488
  -7.000  -0.1326   0.01936   0.01111  -0.1163   0.7131   0.0497
  -6.750  -0.1093   0.01893   0.01060  -0.1155   0.7050   0.0508
  -6.500  -0.0853   0.01849   0.01003  -0.1147   0.6981   0.0522
  -6.250  -0.0616   0.01804   0.00947  -0.1139   0.6903   0.0539
  -6.000  -0.0375   0.01773   0.00912  -0.1131   0.6832   0.0554
  -5.750  -0.0131   0.01744   0.00878  -0.1124   0.6760   0.0574
  -5.500   0.0112   0.01710   0.00834  -0.1116   0.6683   0.0598
  -5.250   0.0359   0.01682   0.00800  -0.1110   0.6618   0.0620
  -5.000   0.0604   0.01657   0.00774  -0.1102   0.6545   0.0649
  -4.750   0.0853   0.01633   0.00742  -0.1095   0.6478   0.0684
  -4.500   0.1106   0.01618   0.00722  -0.1090   0.6417   0.0722
  -4.250   0.1355   0.01599   0.00699  -0.1083   0.6345   0.0767
  -4.000   0.1609   0.01585   0.00680  -0.1077   0.6281   0.0812
  -3.750   0.1863   0.01570   0.00658  -0.1071   0.6223   0.0860
  -3.500   0.2114   0.01556   0.00644  -0.1065   0.6161   0.0907
  -3.250   0.2371   0.01547   0.00624  -0.1059   0.6103   0.0958
  -3.000   0.2621   0.01530   0.00607  -0.1053   0.6050   0.1008
  -2.750   0.2875   0.01521   0.00594  -0.1048   0.5989   0.1065
  -2.500   0.3124   0.01505   0.00578  -0.1042   0.5935   0.1125
  -2.000   0.3629   0.01482   0.00552  -0.1030   0.5837   0.1261
  -1.750   0.3880   0.01472   0.00541  -0.1024   0.5783   0.1333
  -1.500   0.4133   0.01462   0.00530  -0.1019   0.5737   0.1412
  -1.250   0.4389   0.01455   0.00522  -0.1014   0.5695   0.1529
  -1.000   0.4635   0.01442   0.00521  -0.1007   0.5646   0.1744
  -0.750   0.4879   0.01426   0.00519  -0.1001   0.5598   0.2174
  -0.500   0.5122   0.01409   0.00518  -0.0995   0.5556   0.2789
  -0.250   0.5362   0.01392   0.00520  -0.0988   0.5518   0.3492
   0.000   0.5589   0.01374   0.00530  -0.0978   0.5472   0.4278
   0.250   0.5814   0.01358   0.00538  -0.0967   0.5428   0.5068
   0.500   0.6040   0.01344   0.00543  -0.0956   0.5387   0.5823
   0.750   0.6255   0.01321   0.00552  -0.0940   0.5352   0.6913
   1.000   0.6855   0.01303   0.00586  -0.0999   0.5298   0.9052
   1.250   0.7349   0.01318   0.00595  -0.1042   0.5238   0.9689
   1.500   0.7860   0.01335   0.00595  -0.1091   0.5174   0.9924
   1.750   0.8155   0.01348   0.00605  -0.1096   0.5101   1.0000
   2.000   0.8351   0.01361   0.00610  -0.1080   0.5038   1.0000
   2.250   0.8563   0.01377   0.00614  -0.1067   0.4991   1.0000
   2.500   0.8762   0.01391   0.00628  -0.1051   0.4940   1.0000
   2.750   0.8966   0.01406   0.00640  -0.1037   0.4892   1.0000
   3.000   0.9176   0.01422   0.00650  -0.1024   0.4850   1.0000
   3.250   0.9393   0.01441   0.00659  -0.1013   0.4812   1.0000
   3.500   0.9592   0.01457   0.00678  -0.0998   0.4766   1.0000
   3.750   0.9795   0.01474   0.00695  -0.0984   0.4719   1.0000
   4.000   1.0000   0.01492   0.00708  -0.0970   0.4674   1.0000
   4.250   1.0211   0.01512   0.00720  -0.0958   0.4633   1.0000
   4.500   1.0403   0.01530   0.00743  -0.0942   0.4580   1.0000
   4.750   1.0594   0.01549   0.00761  -0.0926   0.4525   1.0000
   5.000   1.0790   0.01569   0.00775  -0.0911   0.4476   1.0000
   5.250   1.0977   0.01590   0.00798  -0.0895   0.4422   1.0000
   5.500   1.1156   0.01611   0.00820  -0.0878   0.4364   1.0000
   5.750   1.1332   0.01634   0.00839  -0.0860   0.4308   1.0000
   6.000   1.1491   0.01657   0.00864  -0.0839   0.4251   1.0000
   6.250   1.1632   0.01681   0.00888  -0.0815   0.4185   1.0000
   6.500   1.1773   0.01708   0.00910  -0.0791   0.4122   1.0000
   6.750   1.1912   0.01737   0.00943  -0.0768   0.4049   1.0000
   7.000   1.2046   0.01769   0.00974  -0.0745   0.3978   1.0000
   7.250   1.2189   0.01805   0.01010  -0.0724   0.3910   1.0000
   7.500   1.2320   0.01844   0.01049  -0.0702   0.3836   1.0000
   7.750   1.2445   0.01888   0.01091  -0.0680   0.3761   1.0000
   8.000   1.2562   0.01937   0.01141  -0.0658   0.3674   1.0000
   8.250   1.2671   0.01993   0.01195  -0.0635   0.3590   1.0000
   8.500   1.2769   0.02056   0.01256  -0.0612   0.3499   1.0000
   8.750   1.2873   0.02123   0.01324  -0.0591   0.3415   1.0000
   9.000   1.2967   0.02198   0.01397  -0.0570   0.3335   1.0000
   9.250   1.3071   0.02275   0.01475  -0.0552   0.3262   1.0000
   9.500   1.3164   0.02361   0.01560  -0.0533   0.3188   1.0000
   9.750   1.3253   0.02452   0.01652  -0.0514   0.3122   1.0000
  10.000   1.3342   0.02550   0.01752  -0.0497   0.3049   1.0000
  10.250   1.3409   0.02663   0.01862  -0.0479   0.2981   1.0000
  10.500   1.3494   0.02772   0.01974  -0.0464   0.2908   1.0000
  10.750   1.3555   0.02898   0.02099  -0.0447   0.2846   1.0000
  11.000   1.3642   0.03015   0.02219  -0.0434   0.2793   1.0000
  11.250   1.3721   0.03141   0.02348  -0.0421   0.2737   1.0000
  11.500   1.3787   0.03276   0.02484  -0.0407   0.2688   1.0000
  11.750   1.3868   0.03407   0.02618  -0.0396   0.2645   1.0000
  12.000   1.3956   0.03538   0.02756  -0.0386   0.2601   1.0000
  12.250   1.4028   0.03682   0.02903  -0.0375   0.2558   1.0000
  12.500   1.4093   0.03833   0.03053  -0.0365   0.2519   1.0000
  12.750   1.4178   0.03974   0.03201  -0.0356   0.2483   1.0000
  13.000   1.4258   0.04124   0.03358  -0.0349   0.2445   1.0000
  13.250   1.4325   0.04285   0.03525  -0.0341   0.2405   1.0000
  13.500   1.4386   0.04452   0.03694  -0.0333   0.2369   1.0000
  13.750   1.4457   0.04613   0.03856  -0.0326   0.2335   1.0000
  14.000   1.4522   0.04791   0.04046  -0.0321   0.2297   1.0000
  14.250   1.4576   0.04978   0.04241  -0.0315   0.2257   1.0000
  14.500   1.4626   0.05169   0.04436  -0.0310   0.2220   1.0000
  14.750   1.4679   0.05354   0.04620  -0.0305   0.2184   1.0000
  15.000   1.4728   0.05560   0.04839  -0.0301   0.2149   1.0000
  15.250   1.4767   0.05778   0.05068  -0.0299   0.2110   1.0000
  15.500   1.4807   0.05993   0.05289  -0.0296   0.2073   1.0000
  15.750   1.4844   0.06209   0.05506  -0.0293   0.2037   1.0000
  16.000   1.4875   0.06442   0.05749  -0.0292   0.2000   1.0000
  16.250   1.4890   0.06702   0.06022  -0.0292   0.1960   1.0000
  16.500   1.4902   0.06964   0.06290  -0.0292   0.1918   1.0000
  16.750   1.4915   0.07218   0.06544  -0.0292   0.1878   1.0000
  17.000   1.4909   0.07516   0.06857  -0.0295   0.1834   1.0000
  17.250   1.4888   0.07831   0.07182  -0.0298   0.1786   1.0000
  17.500   1.4876   0.08132   0.07484  -0.0301   0.1743   1.0000
  17.750   1.4843   0.08476   0.07841  -0.0306   0.1693   1.0000
  18.000   1.4805   0.08826   0.08198  -0.0312   0.1646   1.0000
  18.250   1.4782   0.09150   0.08523  -0.0318   0.1605   1.0000
  18.500   1.4742   0.09516   0.08903  -0.0325   0.1561   1.0000
  18.750   1.4692   0.09893   0.09286  -0.0334   0.1515   1.0000
  19.000   1.4666   0.10233   0.09627  -0.0342   0.1479   1.0000
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