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GOE 508 AIRFOIL (goe508-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 508 AIRFOIL (goe508-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.88 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe508-il-1000000-n5.txt
Download as CSV file: xf-goe508-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 508 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7336   0.05365   0.05065  -0.1201   0.9460   0.0242
 -15.750  -0.7515   0.03595   0.03244  -0.1472   0.9278   0.0243
 -15.500  -0.7378   0.03076   0.02690  -0.1570   0.8890   0.0244
 -15.250  -0.7463   0.02825   0.02412  -0.1573   0.8559   0.0245
 -15.000  -0.7551   0.02644   0.02212  -0.1557   0.8361   0.0245
 -14.750  -0.7591   0.02512   0.02066  -0.1534   0.8223   0.0245
 -14.500  -0.7601   0.02410   0.01948  -0.1507   0.8100   0.0246
 -14.250  -0.7600   0.02314   0.01842  -0.1478   0.7997   0.0247
 -14.000  -0.7557   0.02244   0.01760  -0.1448   0.7905   0.0248
 -13.750  -0.7499   0.02178   0.01684  -0.1418   0.7828   0.0249
 -13.500  -0.7438   0.02122   0.01619  -0.1387   0.7760   0.0250
 -13.250  -0.7344   0.02058   0.01546  -0.1362   0.7705   0.0250
 -13.000  -0.7188   0.02008   0.01487  -0.1345   0.7655   0.0251
 -12.750  -0.7063   0.01939   0.01410  -0.1324   0.7599   0.0253
 -12.250  -0.6755   0.01817   0.01273  -0.1290   0.7501   0.0256
 -12.000  -0.6572   0.01765   0.01216  -0.1276   0.7451   0.0258
 -11.750  -0.6378   0.01719   0.01164  -0.1263   0.7405   0.0260
 -11.250  -0.5964   0.01635   0.01068  -0.1241   0.7319   0.0263
 -11.000  -0.5746   0.01596   0.01024  -0.1231   0.7268   0.0265
 -10.750  -0.5526   0.01560   0.00981  -0.1221   0.7218   0.0267
 -10.500  -0.5302   0.01526   0.00941  -0.1211   0.7172   0.0269
 -10.250  -0.5070   0.01491   0.00901  -0.1203   0.7134   0.0271
 -10.000  -0.4836   0.01457   0.00862  -0.1195   0.7090   0.0273
  -9.750  -0.4601   0.01425   0.00825  -0.1187   0.7043   0.0275
  -9.250  -0.4121   0.01366   0.00754  -0.1173   0.6951   0.0280
  -9.000  -0.3877   0.01338   0.00721  -0.1166   0.6897   0.0282
  -8.750  -0.3632   0.01312   0.00690  -0.1159   0.6846   0.0284
  -8.500  -0.3385   0.01288   0.00659  -0.1152   0.6802   0.0286
  -8.250  -0.3131   0.01262   0.00630  -0.1147   0.6758   0.0288
  -8.000  -0.2888   0.01231   0.00595  -0.1140   0.6708   0.0292
  -7.750  -0.2639   0.01207   0.00567  -0.1133   0.6656   0.0296
  -7.500  -0.2385   0.01185   0.00542  -0.1128   0.6610   0.0299
  -7.250  -0.2126   0.01164   0.00519  -0.1123   0.6555   0.0303
  -7.000  -0.1870   0.01147   0.00498  -0.1117   0.6494   0.0308
  -6.750  -0.1613   0.01131   0.00478  -0.1112   0.6440   0.0313
  -6.500  -0.1351   0.01113   0.00457  -0.1108   0.6386   0.0317
  -6.250  -0.1091   0.01098   0.00437  -0.1103   0.6329   0.0321
  -6.000  -0.0833   0.01084   0.00419  -0.1097   0.6275   0.0325
  -5.750  -0.0570   0.01066   0.00399  -0.1093   0.6223   0.0330
  -5.500  -0.0311   0.01050   0.00381  -0.1088   0.6164   0.0337
  -5.250  -0.0054   0.01038   0.00366  -0.1083   0.6106   0.0344
  -5.000   0.0213   0.01025   0.00352  -0.1079   0.6050   0.0352
  -4.750   0.0475   0.01015   0.00338  -0.1074   0.5986   0.0359
  -4.500   0.0735   0.01007   0.00326  -0.1069   0.5927   0.0367
  -4.250   0.1000   0.00995   0.00313  -0.1065   0.5875   0.0376
  -4.000   0.1263   0.00985   0.00301  -0.1061   0.5821   0.0387
  -3.750   0.1523   0.00978   0.00292  -0.1056   0.5768   0.0401
  -3.500   0.1790   0.00971   0.00283  -0.1052   0.5719   0.0414
  -3.250   0.2051   0.00963   0.00274  -0.1047   0.5652   0.0429
  -3.000   0.2304   0.00959   0.00267  -0.1041   0.5574   0.0446
  -2.750   0.2569   0.00953   0.00259  -0.1037   0.5513   0.0463
  -2.500   0.2831   0.00947   0.00252  -0.1033   0.5462   0.0481
  -2.250   0.3089   0.00942   0.00246  -0.1027   0.5419   0.0505
  -2.000   0.3355   0.00938   0.00241  -0.1024   0.5385   0.0527
  -1.750   0.3618   0.00930   0.00235  -0.1020   0.5344   0.0565
  -1.500   0.3875   0.00925   0.00230  -0.1014   0.5289   0.0621
  -1.000   0.4384   0.00914   0.00227  -0.1003   0.5189   0.0878
  -0.750   0.4647   0.00911   0.00226  -0.0999   0.5153   0.0960
  -0.500   0.4908   0.00911   0.00226  -0.0995   0.5113   0.1022
  -0.250   0.5161   0.00911   0.00226  -0.0989   0.5072   0.1085
   0.000   0.5421   0.00910   0.00227  -0.0985   0.5034   0.1145
   0.250   0.5682   0.00908   0.00227  -0.0980   0.4996   0.1216
   0.500   0.5939   0.00908   0.00228  -0.0975   0.4954   0.1298
   0.750   0.6187   0.00908   0.00231  -0.0969   0.4909   0.1413
   1.000   0.6432   0.00907   0.00234  -0.0962   0.4868   0.1599
   1.250   0.6683   0.00901   0.00236  -0.0956   0.4823   0.1870
   1.500   0.6926   0.00899   0.00240  -0.0949   0.4771   0.2168
   1.750   0.7150   0.00897   0.00246  -0.0938   0.4710   0.2566
   2.000   0.7381   0.00886   0.00252  -0.0929   0.4657   0.3202
   2.250   0.7594   0.00872   0.00259  -0.0917   0.4599   0.4055
   2.500   0.7783   0.00857   0.00268  -0.0899   0.4541   0.5073
   2.750   0.7981   0.00841   0.00276  -0.0884   0.4495   0.6010
   3.000   0.8155   0.00826   0.00285  -0.0862   0.4437   0.6940
   3.250   0.8276   0.00813   0.00295  -0.0829   0.4377   0.7826
   3.500   0.8446   0.00797   0.00311  -0.0804   0.4322   0.8937
   4.000   1.0055   0.00873   0.00378  -0.1036   0.4013   0.9933
   4.250   1.0568   0.00912   0.00404  -0.1090   0.3805   1.0000
   4.500   1.0648   0.00944   0.00425  -0.1051   0.3605   1.0000
   4.750   1.0643   0.00983   0.00451  -0.0996   0.3373   1.0000
   5.000   1.0621   0.01024   0.00479  -0.0938   0.3131   1.0000
   5.250   1.0647   0.01071   0.00513  -0.0890   0.2918   1.0000
   5.500   1.0709   0.01119   0.00551  -0.0852   0.2730   1.0000
   5.750   1.0808   0.01164   0.00588  -0.0821   0.2587   1.0000
   6.000   1.0955   0.01199   0.00619  -0.0799   0.2510   1.0000
   6.250   1.1096   0.01239   0.00655  -0.0777   0.2435   1.0000
   6.500   1.1249   0.01278   0.00691  -0.0758   0.2371   1.0000
   6.750   1.1409   0.01317   0.00728  -0.0741   0.2318   1.0000
   7.000   1.1545   0.01370   0.00776  -0.0721   0.2244   1.0000
   7.250   1.1722   0.01408   0.00814  -0.0707   0.2218   1.0000
   7.500   1.1899   0.01448   0.00854  -0.0694   0.2187   1.0000
   7.750   1.2070   0.01493   0.00899  -0.0681   0.2157   1.0000
   8.000   1.2230   0.01546   0.00951  -0.0667   0.2121   1.0000
   8.250   1.2383   0.01604   0.01007  -0.0653   0.2082   1.0000
   8.500   1.2552   0.01657   0.01061  -0.0641   0.2058   1.0000
   8.750   1.2733   0.01706   0.01112  -0.0632   0.2036   1.0000
   9.000   1.2907   0.01760   0.01168  -0.0622   0.2020   1.0000
   9.250   1.3071   0.01821   0.01229  -0.0611   0.1992   1.0000
   9.500   1.3231   0.01887   0.01296  -0.0600   0.1970   1.0000
   9.750   1.3384   0.01958   0.01367  -0.0590   0.1946   1.0000
  10.000   1.3527   0.02037   0.01448  -0.0578   0.1920   1.0000
  10.250   1.3687   0.02107   0.01520  -0.0569   0.1902   1.0000
  10.500   1.3850   0.02177   0.01593  -0.0560   0.1887   1.0000
  10.750   1.4010   0.02249   0.01668  -0.0552   0.1868   1.0000
  11.000   1.4147   0.02337   0.01757  -0.0542   0.1831   1.0000
  11.250   1.4264   0.02441   0.01859  -0.0530   0.1786   1.0000
  11.500   1.4388   0.02542   0.01962  -0.0520   0.1749   1.0000
  11.750   1.4518   0.02640   0.02060  -0.0511   0.1698   1.0000
  12.000   1.4594   0.02778   0.02196  -0.0498   0.1627   1.0000
  12.250   1.4705   0.02895   0.02313  -0.0488   0.1568   1.0000
  12.500   1.4746   0.03066   0.02478  -0.0474   0.1460   1.0000
  12.750   1.4798   0.03233   0.02643  -0.0462   0.1386   1.0000
  13.000   1.4821   0.03425   0.02832  -0.0448   0.1288   1.0000
  13.250   1.4854   0.03616   0.03021  -0.0436   0.1211   1.0000
  13.500   1.4901   0.03800   0.03205  -0.0426   0.1161   1.0000
  13.750   1.4944   0.03989   0.03393  -0.0416   0.1098   1.0000
  14.000   1.4998   0.04174   0.03580  -0.0407   0.1060   1.0000
  14.250   1.5042   0.04369   0.03775  -0.0399   0.1011   1.0000
  14.500   1.5055   0.04596   0.04000  -0.0390   0.0938   1.0000
  14.750   1.4998   0.04891   0.04290  -0.0379   0.0797   1.0000
  15.000   1.4888   0.05246   0.04637  -0.0367   0.0650   1.0000
  15.250   1.4889   0.05500   0.04891  -0.0361   0.0602   1.0000
  15.500   1.4927   0.05721   0.05115  -0.0356   0.0581   1.0000
  15.750   1.4959   0.05950   0.05347  -0.0352   0.0561   1.0000
  16.000   1.4973   0.06202   0.05602  -0.0348   0.0538   1.0000
  16.250   1.5017   0.06424   0.05829  -0.0345   0.0528   1.0000
  16.500   1.5060   0.06651   0.06061  -0.0343   0.0515   1.0000
  16.750   1.5105   0.06874   0.06288  -0.0341   0.0507   1.0000
  17.000   1.5119   0.07133   0.06552  -0.0339   0.0492   1.0000
  17.250   1.5151   0.07375   0.06798  -0.0338   0.0484   1.0000
  17.500   1.5154   0.07655   0.07083  -0.0338   0.0473   1.0000
  17.750   1.5186   0.07899   0.07331  -0.0337   0.0459   1.0000
  18.000   1.5203   0.08167   0.07605  -0.0338   0.0450   1.0000
  18.250   1.5222   0.08428   0.07871  -0.0339   0.0435   1.0000
  18.500   1.5215   0.08726   0.08175  -0.0340   0.0424   1.0000
  18.750   1.5203   0.09032   0.08484  -0.0342   0.0410   1.0000
  19.000   1.5201   0.09331   0.08789  -0.0345   0.0395   1.0000
  19.250   1.5170   0.09664   0.09124  -0.0349   0.0364   1.0000
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