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GOE 528 AIRFOIL (goe528-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 528 AIRFOIL (goe528-il)
Reynolds number: 1,000,000
Max Cl/Cd: 137.7 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe528-il-1000000.txt
Download as CSV file: xf-goe528-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 528 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.2231   0.11465   0.11299  -0.0498   0.9969   0.0176
 -11.250  -0.2068   0.11198   0.11032  -0.0518   0.9905   0.0179
 -11.000  -0.1945   0.10885   0.10719  -0.0541   0.9794   0.0180
 -10.750  -0.1776   0.10522   0.10355  -0.0580   0.9660   0.0182
 -10.500  -0.1531   0.10138   0.09968  -0.0637   0.9544   0.0191
 -10.250  -0.1381   0.09225   0.09049  -0.0763   0.9421   0.0207
 -10.000  -0.1076   0.08637   0.08455  -0.0854   0.9321   0.0210
  -9.750  -0.0661   0.08321   0.08131  -0.0931   0.9213   0.0213
  -9.500  -0.0291   0.07979   0.07777  -0.1010   0.9035   0.0221
  -9.250  -0.0100   0.07649   0.07434  -0.1057   0.8811   0.0227
  -9.000  -0.0229   0.06963   0.06738  -0.1112   0.8571   0.0244
  -8.750  -0.0011   0.05416   0.05183  -0.1008   0.8048   0.0248
  -8.250   0.0109   0.05014   0.04776  -0.1008   0.7861   0.0251
  -8.000  -0.0272   0.05934   0.05692  -0.1120   0.8028   0.0251
  -7.750  -0.0245   0.05678   0.05432  -0.1134   0.7923   0.0253
  -7.500  -0.0167   0.05455   0.05206  -0.1147   0.7823   0.0256
  -7.250  -0.0098   0.05155   0.04901  -0.1170   0.7732   0.0261
  -7.000  -0.0028   0.04769   0.04507  -0.1200   0.7636   0.0270
  -6.500  -0.0418   0.01929   0.01508  -0.1270   0.7486   0.0266
  -6.250  -0.0230   0.01724   0.01266  -0.1260   0.7412   0.0270
  -6.000  -0.0009   0.01594   0.01110  -0.1251   0.7333   0.0276
  -5.750   0.0230   0.01514   0.01007  -0.1244   0.7258   0.0281
  -5.500   0.0482   0.01461   0.00936  -0.1238   0.7172   0.0285
  -5.250   0.0721   0.01370   0.00822  -0.1231   0.7090   0.0288
  -5.000   0.0956   0.01243   0.00680  -0.1224   0.7001   0.0293
  -4.750   0.1210   0.01190   0.00619  -0.1219   0.6913   0.0297
  -4.500   0.1468   0.01154   0.00576  -0.1214   0.6811   0.0302
  -4.250   0.1731   0.01130   0.00546  -0.1210   0.6712   0.0308
  -4.000   0.1989   0.01100   0.00508  -0.1204   0.6605   0.0314
  -3.750   0.2249   0.01066   0.00465  -0.1199   0.6490   0.0317
  -3.500   0.2509   0.01037   0.00428  -0.1194   0.6373   0.0322
  -3.250   0.2767   0.01012   0.00395  -0.1188   0.6253   0.0326
  -3.000   0.3024   0.00992   0.00366  -0.1182   0.6128   0.0330
  -2.750   0.3287   0.00976   0.00344  -0.1177   0.6006   0.0333
  -2.500   0.3542   0.00948   0.00309  -0.1171   0.5895   0.0338
  -2.250   0.3792   0.00920   0.00275  -0.1165   0.5787   0.0349
  -2.000   0.4055   0.00908   0.00259  -0.1160   0.5687   0.0357
  -1.750   0.4317   0.00899   0.00245  -0.1156   0.5600   0.0364
  -1.500   0.4580   0.00891   0.00233  -0.1151   0.5514   0.0373
  -1.250   0.4845   0.00885   0.00222  -0.1147   0.5441   0.0381
  -1.000   0.5112   0.00880   0.00213  -0.1143   0.5370   0.0389
  -0.750   0.5372   0.00871   0.00200  -0.1138   0.5302   0.0406
  -0.500   0.5642   0.00864   0.00193  -0.1135   0.5241   0.0428
  -0.250   0.5907   0.00864   0.00189  -0.1131   0.5180   0.0452
   0.000   0.6172   0.00859   0.00185  -0.1128   0.5124   0.0509
   0.250   0.6437   0.00847   0.00184  -0.1124   0.5069   0.0854
   0.500   0.6688   0.00828   0.00186  -0.1119   0.5013   0.1749
   0.750   0.6939   0.00808   0.00192  -0.1114   0.4962   0.2840
   1.000   0.7193   0.00788   0.00199  -0.1110   0.4911   0.3937
   1.250   0.7428   0.00763   0.00208  -0.1102   0.4858   0.5375
   1.500   0.8124   0.00684   0.00229  -0.1195   0.4790   1.0000
   1.750   0.8375   0.00692   0.00233  -0.1188   0.4735   1.0000
   2.000   0.8618   0.00704   0.00239  -0.1180   0.4677   1.0000
   2.250   0.8869   0.00712   0.00244  -0.1174   0.4625   1.0000
   2.500   0.9120   0.00721   0.00249  -0.1167   0.4564   1.0000
   2.750   0.9359   0.00735   0.00257  -0.1159   0.4501   1.0000
   3.000   0.9613   0.00743   0.00263  -0.1153   0.4449   1.0000
   3.250   0.9861   0.00754   0.00271  -0.1147   0.4392   1.0000
   3.500   1.0100   0.00769   0.00280  -0.1138   0.4333   1.0000
   3.750   1.0356   0.00776   0.00288  -0.1133   0.4285   1.0000
   4.000   1.0602   0.00788   0.00297  -0.1127   0.4226   1.0000
   4.250   1.0842   0.00804   0.00309  -0.1119   0.4166   1.0000
   4.500   1.1093   0.00814   0.00318  -0.1113   0.4104   1.0000
   4.750   1.1330   0.00830   0.00330  -0.1106   0.4037   1.0000
   5.000   1.1576   0.00843   0.00342  -0.1099   0.3974   1.0000
   5.250   1.1812   0.00859   0.00355  -0.1091   0.3895   1.0000
   5.500   1.2049   0.00875   0.00369  -0.1084   0.3817   1.0000
   5.750   1.2281   0.00894   0.00384  -0.1075   0.3736   1.0000
   6.000   1.2515   0.00911   0.00400  -0.1068   0.3667   1.0000
   6.250   1.2746   0.00929   0.00416  -0.1059   0.3593   1.0000
   6.500   1.2971   0.00949   0.00434  -0.1050   0.3518   1.0000
   6.750   1.3194   0.00970   0.00453  -0.1040   0.3434   1.0000
   7.000   1.3414   0.00992   0.00473  -0.1030   0.3359   1.0000
   7.250   1.3630   0.01014   0.00493  -0.1020   0.3281   1.0000
   7.500   1.3842   0.01037   0.00515  -0.1008   0.3203   1.0000
   7.750   1.4035   0.01067   0.00540  -0.0994   0.3101   1.0000
   8.000   1.4232   0.01090   0.00563  -0.0980   0.3018   1.0000
   8.250   1.4396   0.01122   0.00591  -0.0960   0.2927   1.0000
   8.500   1.4578   0.01148   0.00617  -0.0943   0.2842   1.0000
   8.750   1.4744   0.01180   0.00647  -0.0924   0.2762   1.0000
   9.000   1.4916   0.01211   0.00677  -0.0906   0.2679   1.0000
   9.250   1.5081   0.01246   0.00711  -0.0888   0.2597   1.0000
   9.500   1.5220   0.01293   0.00752  -0.0866   0.2486   1.0000
   9.750   1.5376   0.01333   0.00791  -0.0848   0.2384   1.0000
  10.000   1.5519   0.01381   0.00836  -0.0828   0.2282   1.0000
  10.250   1.5647   0.01436   0.00887  -0.0806   0.2188   1.0000
  10.500   1.5785   0.01489   0.00939  -0.0787   0.2092   1.0000
  10.750   1.5916   0.01547   0.00995  -0.0767   0.2006   1.0000
  11.000   1.6020   0.01621   0.01065  -0.0745   0.1903   1.0000
  11.250   1.6134   0.01693   0.01136  -0.0726   0.1802   1.0000
  11.500   1.6231   0.01778   0.01218  -0.0705   0.1691   1.0000
  11.750   1.6311   0.01878   0.01314  -0.0684   0.1574   1.0000
  12.000   1.6347   0.02010   0.01438  -0.0660   0.1406   1.0000
  12.250   1.6275   0.02220   0.01631  -0.0627   0.1118   1.0000
  12.500   1.6150   0.02487   0.01882  -0.0594   0.0868   1.0000
  12.750   1.6169   0.02665   0.02060  -0.0576   0.0799   1.0000
  13.000   1.6225   0.02822   0.02221  -0.0562   0.0754   1.0000
  13.250   1.6257   0.03002   0.02404  -0.0548   0.0714   1.0000
  13.500   1.6303   0.03178   0.02584  -0.0536   0.0677   1.0000
  13.750   1.6373   0.03337   0.02749  -0.0527   0.0654   1.0000
  14.000   1.6399   0.03539   0.02955  -0.0516   0.0619   1.0000
  14.250   1.6410   0.03762   0.03182  -0.0506   0.0586   1.0000
  14.500   1.6467   0.03948   0.03374  -0.0499   0.0561   1.0000
  14.750   1.6476   0.04185   0.03614  -0.0492   0.0528   1.0000
  15.000   1.6472   0.04441   0.03873  -0.0485   0.0495   1.0000
  15.250   1.6480   0.04693   0.04130  -0.0480   0.0461   1.0000
  15.500   1.6439   0.05003   0.04442  -0.0475   0.0424   1.0000
  15.750   1.6420   0.05294   0.04738  -0.0471   0.0389   1.0000
  16.000   1.6355   0.05644   0.05091  -0.0468   0.0352   1.0000
  16.250   1.6286   0.06007   0.05458  -0.0467   0.0315   1.0000
  16.500   1.6202   0.06394   0.05850  -0.0466   0.0280   1.0000
  16.750   1.6100   0.06808   0.06268  -0.0467   0.0251   1.0000
  17.000   1.6008   0.07219   0.06685  -0.0469   0.0228   1.0000
  17.250   1.5915   0.07639   0.07111  -0.0473   0.0212   1.0000
  17.500   1.5824   0.08062   0.07541  -0.0477   0.0197   1.0000
  17.750   1.5733   0.08493   0.07979  -0.0483   0.0189   1.0000
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