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GOE 503 AIRFOIL (goe503-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 503 AIRFOIL (goe503-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.77 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe503-il-1000000-n5.txt
Download as CSV file: xf-goe503-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 503 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  -0.3324   0.08412   0.08176  -0.1090   0.9649   0.0076
 -14.250  -0.3365   0.07821   0.07580  -0.1143   0.9618   0.0076
 -14.000  -0.3426   0.07266   0.07018  -0.1188   0.9553   0.0077
 -13.750  -0.3538   0.06506   0.06250  -0.1269   0.9493   0.0076
 -13.500  -0.5180   0.03324   0.02999  -0.1618   0.9109   0.0070
 -13.250  -0.5380   0.02569   0.02203  -0.1632   0.8905   0.0070
 -13.000  -0.5292   0.02324   0.01934  -0.1626   0.8728   0.0071
 -12.750  -0.5226   0.02174   0.01762  -0.1604   0.8525   0.0072
 -12.500  -0.5120   0.02086   0.01656  -0.1581   0.8305   0.0073
 -12.250  -0.5027   0.02006   0.01555  -0.1553   0.8068   0.0075
 -12.000  -0.4915   0.01938   0.01469  -0.1528   0.7849   0.0076
 -11.750  -0.4788   0.01873   0.01388  -0.1504   0.7686   0.0077
 -11.500  -0.4633   0.01820   0.01321  -0.1484   0.7560   0.0079
 -11.000  -0.4303   0.01709   0.01185  -0.1448   0.7354   0.0080
 -10.750  -0.4148   0.01642   0.01105  -0.1428   0.7267   0.0083
 -10.500  -0.3968   0.01582   0.01034  -0.1412   0.7195   0.0085
 -10.250  -0.3780   0.01532   0.00975  -0.1396   0.7130   0.0088
 -10.000  -0.3576   0.01488   0.00922  -0.1383   0.7074   0.0090
  -9.750  -0.3364   0.01449   0.00876  -0.1371   0.7013   0.0093
  -9.500  -0.3156   0.01414   0.00831  -0.1358   0.6952   0.0096
  -9.250  -0.2934   0.01378   0.00788  -0.1348   0.6899   0.0099
  -9.000  -0.2710   0.01345   0.00748  -0.1337   0.6845   0.0102
  -8.750  -0.2487   0.01317   0.00711  -0.1326   0.6793   0.0105
  -8.500  -0.2262   0.01281   0.00669  -0.1316   0.6746   0.0109
  -8.250  -0.2034   0.01248   0.00630  -0.1306   0.6691   0.0115
  -8.000  -0.1809   0.01220   0.00595  -0.1295   0.6631   0.0121
  -7.750  -0.1574   0.01194   0.00563  -0.1286   0.6579   0.0128
  -7.500  -0.1334   0.01173   0.00536  -0.1278   0.6522   0.0134
  -7.250  -0.1106   0.01147   0.00504  -0.1267   0.6465   0.0146
  -7.000  -0.0870   0.01122   0.00474  -0.1258   0.6410   0.0160
  -6.750  -0.0634   0.01097   0.00445  -0.1249   0.6347   0.0183
  -6.500  -0.0412   0.01070   0.00417  -0.1238   0.6279   0.0238
  -6.250  -0.0175   0.01044   0.00394  -0.1229   0.6215   0.0345
  -6.000   0.0060   0.01030   0.00379  -0.1220   0.6146   0.0393
  -5.750   0.0303   0.01021   0.00366  -0.1212   0.6079   0.0422
  -5.500   0.0537   0.01008   0.00352  -0.1202   0.5998   0.0460
  -5.250   0.0775   0.01000   0.00339  -0.1193   0.5930   0.0481
  -5.000   0.1016   0.00994   0.00328  -0.1184   0.5857   0.0498
  -4.750   0.1249   0.00988   0.00316  -0.1174   0.5788   0.0514
  -4.500   0.1486   0.00977   0.00304  -0.1165   0.5716   0.0545
  -4.250   0.1712   0.00972   0.00294  -0.1154   0.5643   0.0567
  -4.000   0.1953   0.00965   0.00284  -0.1145   0.5582   0.0593
  -3.750   0.2184   0.00960   0.00275  -0.1135   0.5516   0.0619
  -3.500   0.2412   0.00952   0.00267  -0.1124   0.5459   0.0676
  -3.250   0.2643   0.00946   0.00259  -0.1113   0.5398   0.0722
  -3.000   0.2856   0.00940   0.00253  -0.1100   0.5341   0.0790
  -2.750   0.3077   0.00935   0.00247  -0.1087   0.5294   0.0854
  -2.500   0.3298   0.00929   0.00242  -0.1075   0.5240   0.0928
  -2.250   0.3515   0.00929   0.00238  -0.1061   0.5188   0.0970
  -2.000   0.3734   0.00925   0.00234  -0.1048   0.5143   0.1031
  -1.750   0.3964   0.00922   0.00231  -0.1038   0.5099   0.1081
  -1.500   0.4190   0.00922   0.00228  -0.1027   0.5052   0.1119
  -1.250   0.4401   0.00922   0.00227  -0.1013   0.5007   0.1193
  -1.000   0.4631   0.00920   0.00226  -0.1002   0.4972   0.1247
  -0.750   0.4859   0.00919   0.00225  -0.0992   0.4931   0.1313
  -0.500   0.5082   0.00920   0.00227  -0.0980   0.4889   0.1394
  -0.250   0.5297   0.00923   0.00230  -0.0968   0.4848   0.1497
   0.000   0.5526   0.00924   0.00234  -0.0958   0.4814   0.1608
   0.250   0.5757   0.00926   0.00238  -0.0948   0.4774   0.1729
   0.500   0.5979   0.00929   0.00243  -0.0937   0.4732   0.1821
   0.750   0.6198   0.00936   0.00248  -0.0925   0.4693   0.1879
   1.000   0.6421   0.00941   0.00254  -0.0914   0.4659   0.1952
   1.250   0.6653   0.00945   0.00259  -0.0906   0.4624   0.2035
   1.500   0.6879   0.00951   0.00264  -0.0896   0.4583   0.2088
   1.750   0.7092   0.00958   0.00272  -0.0883   0.4540   0.2155
   2.000   0.7310   0.00966   0.00279  -0.0872   0.4505   0.2208
   2.250   0.7538   0.00972   0.00286  -0.0863   0.4469   0.2257
   2.500   0.7759   0.00978   0.00294  -0.0852   0.4432   0.2330
   2.750   0.7970   0.00988   0.00303  -0.0840   0.4385   0.2390
   3.000   0.8181   0.00997   0.00313  -0.0827   0.4345   0.2473
   3.250   0.8404   0.01004   0.00323  -0.0818   0.4311   0.2566
   3.500   0.8616   0.01011   0.00334  -0.0806   0.4271   0.2713
   3.750   0.8801   0.01024   0.00349  -0.0789   0.4208   0.2926
   4.000   0.9009   0.01030   0.00362  -0.0777   0.4171   0.3219
   4.250   0.9209   0.01038   0.00376  -0.0764   0.4108   0.3518
   4.500   0.9375   0.01052   0.00395  -0.0744   0.4041   0.3943
   4.750   0.9548   0.01044   0.00412  -0.0726   0.4005   0.4949
   5.250   1.1229   0.01023   0.00496  -0.0987   0.3776   0.9881
   5.500   1.1466   0.01052   0.00523  -0.0983   0.3713   0.9969
   6.000   1.2030   0.01105   0.00570  -0.0996   0.3590   1.0000
   6.250   1.2190   0.01126   0.00590  -0.0976   0.3541   1.0000
   6.500   1.2353   0.01149   0.00612  -0.0956   0.3487   1.0000
   6.750   1.2496   0.01181   0.00640  -0.0934   0.3422   1.0000
   7.000   1.2668   0.01205   0.00665  -0.0918   0.3373   1.0000
   7.250   1.2832   0.01235   0.00694  -0.0900   0.3318   1.0000
   7.500   1.2988   0.01269   0.00726  -0.0882   0.3268   1.0000
   7.750   1.3146   0.01304   0.00760  -0.0864   0.3187   1.0000
   8.000   1.3285   0.01350   0.00803  -0.0844   0.3111   1.0000
   8.250   1.3432   0.01394   0.00845  -0.0826   0.3019   1.0000
   8.500   1.3568   0.01445   0.00893  -0.0806   0.2940   1.0000
   8.750   1.3690   0.01504   0.00948  -0.0786   0.2833   1.0000
   9.000   1.3816   0.01565   0.01006  -0.0766   0.2730   1.0000
   9.250   1.3917   0.01640   0.01076  -0.0744   0.2614   1.0000
   9.500   1.4015   0.01719   0.01151  -0.0722   0.2505   1.0000
   9.750   1.4130   0.01793   0.01223  -0.0704   0.2411   1.0000
  10.000   1.4211   0.01889   0.01315  -0.0682   0.2292   1.0000
  10.250   1.4262   0.02006   0.01426  -0.0658   0.2148   1.0000
  10.500   1.4274   0.02152   0.01563  -0.0631   0.1979   1.0000
  10.750   1.4299   0.02299   0.01704  -0.0607   0.1841   1.0000
  11.000   1.4341   0.02444   0.01845  -0.0586   0.1730   1.0000
  11.250   1.4339   0.02624   0.02020  -0.0563   0.1593   1.0000
  11.500   1.4314   0.02830   0.02219  -0.0540   0.1442   1.0000
  11.750   1.4302   0.03037   0.02422  -0.0520   0.1309   1.0000
  12.000   1.4091   0.03408   0.02776  -0.0488   0.1008   1.0000
  12.250   1.3841   0.03838   0.03194  -0.0457   0.0692   1.0000
  12.500   1.3683   0.04207   0.03559  -0.0435   0.0483   1.0000
  12.750   1.3452   0.04666   0.04008  -0.0413   0.0202   1.0000
  13.000   1.3442   0.04927   0.04272  -0.0403   0.0152   1.0000
  13.250   1.3468   0.05156   0.04506  -0.0396   0.0136   1.0000
  13.500   1.3503   0.05380   0.04734  -0.0390   0.0122   1.0000
  13.750   1.3542   0.05606   0.04966  -0.0385   0.0116   1.0000
  14.000   1.3566   0.05851   0.05216  -0.0381   0.0109   1.0000
  14.250   1.3592   0.06093   0.05464  -0.0376   0.0103   1.0000
  14.500   1.3604   0.06354   0.05731  -0.0373   0.0095   1.0000
  14.750   1.3629   0.06605   0.05987  -0.0370   0.0091   1.0000
  15.000   1.3653   0.06859   0.06247  -0.0367   0.0088   1.0000
  15.250   1.3659   0.07138   0.06531  -0.0365   0.0083   1.0000
  15.500   1.3663   0.07420   0.06819  -0.0364   0.0080   1.0000
  15.750   1.3653   0.07719   0.07124  -0.0362   0.0076   1.0000
  16.000   1.3644   0.08023   0.07433  -0.0362   0.0074   1.0000
  16.250   1.3660   0.08297   0.07715  -0.0362   0.0071   1.0000
  16.500   1.3651   0.08608   0.08032  -0.0363   0.0069   1.0000
  16.750   1.3654   0.08904   0.08333  -0.0364   0.0065   1.0000
  17.000   1.3632   0.09232   0.08669  -0.0366   0.0064   1.0000
  17.250   1.3620   0.09550   0.08993  -0.0368   0.0062   1.0000
  17.500   1.3601   0.09880   0.09328  -0.0372   0.0059   1.0000
  17.750   1.3560   0.10244   0.09698  -0.0376   0.0056   1.0000
  18.000   1.3536   0.10588   0.10049  -0.0380   0.0055   1.0000
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