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GOE 478 AIRFOIL (goe478-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 478 AIRFOIL (goe478-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.78 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe478-il-1000000-n5.txt
Download as CSV file: xf-goe478-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 478 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8171   0.06268   0.06001  -0.0817   1.0000   0.0233
 -14.500  -0.9279   0.03418   0.03087  -0.1127   0.9958   0.0232
 -14.250  -0.9290   0.03115   0.02768  -0.1148   0.9892   0.0232
 -13.750  -0.9157   0.02749   0.02374  -0.1144   0.9725   0.0233
 -13.500  -0.8983   0.02596   0.02208  -0.1149   0.9639   0.0234
 -13.000  -0.8397   0.02332   0.01918  -0.1194   0.9485   0.0235
 -12.750  -0.8015   0.02196   0.01768  -0.1233   0.9407   0.0236
 -12.500  -0.7658   0.02058   0.01614  -0.1267   0.9272   0.0238
 -12.250  -0.7377   0.01956   0.01497  -0.1280   0.9087   0.0240
 -12.000  -0.7169   0.01889   0.01416  -0.1274   0.8900   0.0241
 -11.750  -0.6985   0.01833   0.01348  -0.1261   0.8727   0.0243
 -11.500  -0.6802   0.01782   0.01285  -0.1247   0.8566   0.0244
 -11.250  -0.6613   0.01735   0.01227  -0.1233   0.8416   0.0245
 -11.000  -0.6420   0.01690   0.01171  -0.1219   0.8276   0.0246
 -10.750  -0.6216   0.01653   0.01124  -0.1206   0.8143   0.0247
 -10.500  -0.6012   0.01611   0.01073  -0.1194   0.8017   0.0249
 -10.250  -0.5799   0.01572   0.01025  -0.1183   0.7914   0.0250
 -10.000  -0.5587   0.01535   0.00978  -0.1171   0.7808   0.0252
  -9.750  -0.5364   0.01498   0.00933  -0.1161   0.7715   0.0253
  -9.250  -0.4907   0.01429   0.00848  -0.1143   0.7566   0.0257
  -9.000  -0.4670   0.01397   0.00810  -0.1135   0.7510   0.0260
  -8.500  -0.4189   0.01337   0.00736  -0.1120   0.7413   0.0264
  -8.250  -0.3941   0.01306   0.00700  -0.1114   0.7378   0.0266
  -8.000  -0.3693   0.01276   0.00665  -0.1107   0.7342   0.0267
  -7.750  -0.3444   0.01248   0.00632  -0.1101   0.7306   0.0269
  -7.500  -0.3193   0.01223   0.00601  -0.1095   0.7272   0.0270
  -7.250  -0.2940   0.01198   0.00571  -0.1089   0.7240   0.0271
  -7.000  -0.2691   0.01161   0.00532  -0.1083   0.7214   0.0275
  -6.750  -0.2436   0.01132   0.00501  -0.1077   0.7184   0.0277
  -6.500  -0.2178   0.01108   0.00475  -0.1072   0.7154   0.0280
  -6.250  -0.1919   0.01086   0.00450  -0.1067   0.7120   0.0283
  -6.000  -0.1659   0.01068   0.00428  -0.1062   0.7088   0.0287
  -5.500  -0.1130   0.01031   0.00388  -0.1053   0.7036   0.0293
  -5.250  -0.0863   0.01012   0.00368  -0.1049   0.7005   0.0297
  -5.000  -0.0596   0.00996   0.00350  -0.1046   0.6971   0.0301
  -4.750  -0.0329   0.00980   0.00332  -0.1041   0.6939   0.0305
  -4.500  -0.0063   0.00966   0.00316  -0.1037   0.6909   0.0308
  -4.250   0.0199   0.00952   0.00298  -0.1032   0.6870   0.0313
  -4.000   0.0468   0.00934   0.00282  -0.1029   0.6833   0.0320
  -3.750   0.0737   0.00920   0.00269  -0.1025   0.6789   0.0328
  -3.500   0.1005   0.00908   0.00256  -0.1021   0.6740   0.0336
  -3.250   0.1270   0.00899   0.00244  -0.1016   0.6696   0.0344
  -3.000   0.1541   0.00888   0.00233  -0.1013   0.6655   0.0351
  -2.750   0.1811   0.00875   0.00221  -0.1009   0.6603   0.0363
  -2.500   0.2075   0.00866   0.00211  -0.1004   0.6533   0.0376
  -2.250   0.2341   0.00858   0.00202  -0.0999   0.6456   0.0391
  -2.000   0.2598   0.00851   0.00193  -0.0993   0.6335   0.0410
  -1.750   0.2853   0.00846   0.00185  -0.0986   0.6165   0.0434
  -1.500   0.3084   0.00850   0.00179  -0.0975   0.5840   0.0463
  -1.000   0.3538   0.00868   0.00176  -0.0951   0.5301   0.0557
  -0.500   0.4029   0.00865   0.00177  -0.0935   0.5057   0.0895
  -0.250   0.4280   0.00869   0.00179  -0.0928   0.4965   0.0988
   0.000   0.4540   0.00868   0.00179  -0.0922   0.4902   0.1054
   0.250   0.4800   0.00869   0.00180  -0.0917   0.4838   0.1112
   0.500   0.5051   0.00871   0.00183  -0.0910   0.4771   0.1204
   0.750   0.5311   0.00869   0.00184  -0.0905   0.4718   0.1316
   1.000   0.5565   0.00865   0.00188  -0.0899   0.4663   0.1607
   1.250   0.5816   0.00865   0.00194  -0.0892   0.4609   0.1883
   1.500   0.6070   0.00867   0.00199  -0.0886   0.4552   0.2042
   1.750   0.6326   0.00869   0.00203  -0.0880   0.4478   0.2160
   2.000   0.6566   0.00876   0.00209  -0.0871   0.4382   0.2308
   2.250   0.6817   0.00878   0.00214  -0.0864   0.4295   0.2485
   2.500   0.7052   0.00878   0.00220  -0.0855   0.4218   0.2870
   2.750   0.7256   0.00840   0.00230  -0.0841   0.4169   0.4737
   3.000   0.7458   0.00816   0.00240  -0.0825   0.4101   0.6081
   3.250   0.7609   0.00789   0.00252  -0.0798   0.4027   0.7603
   3.500   0.8192   0.00771   0.00281  -0.0862   0.3921   0.9625
   3.750   0.8694   0.00792   0.00296  -0.0911   0.3838   0.9790
   4.000   0.9063   0.00807   0.00308  -0.0931   0.3759   0.9878
   4.250   0.9373   0.00827   0.00321  -0.0938   0.3658   0.9953
   4.500   0.9745   0.00849   0.00337  -0.0959   0.3524   0.9996
   4.750   0.9961   0.00869   0.00349  -0.0946   0.3377   1.0000
   5.000   1.0136   0.00891   0.00364  -0.0925   0.3222   1.0000
   5.250   1.0312   0.00913   0.00379  -0.0903   0.3078   1.0000
   5.500   1.0471   0.00942   0.00398  -0.0879   0.2891   1.0000
   5.750   1.0604   0.00982   0.00423  -0.0850   0.2636   1.0000
   6.000   1.0716   0.01028   0.00453  -0.0818   0.2365   1.0000
   6.250   1.0836   0.01062   0.00478  -0.0786   0.2196   1.0000
   6.500   1.0962   0.01095   0.00503  -0.0756   0.2044   1.0000
   6.750   1.1107   0.01126   0.00528  -0.0730   0.1921   1.0000
   7.000   1.1266   0.01156   0.00553  -0.0708   0.1822   1.0000
   7.250   1.1422   0.01189   0.00581  -0.0685   0.1719   1.0000
   7.500   1.1584   0.01222   0.00610  -0.0664   0.1624   1.0000
   7.750   1.1753   0.01256   0.00639  -0.0644   0.1540   1.0000
   8.000   1.1907   0.01295   0.00673  -0.0623   0.1444   1.0000
   8.250   1.2076   0.01331   0.00706  -0.0605   0.1364   1.0000
   8.500   1.2239   0.01372   0.00743  -0.0586   0.1290   1.0000
   8.750   1.2404   0.01413   0.00781  -0.0568   0.1221   1.0000
   9.000   1.2568   0.01455   0.00821  -0.0550   0.1160   1.0000
   9.250   1.2730   0.01500   0.00864  -0.0533   0.1099   1.0000
   9.500   1.2888   0.01549   0.00910  -0.0516   0.1039   1.0000
   9.750   1.3038   0.01604   0.00962  -0.0498   0.0973   1.0000
  10.000   1.3196   0.01656   0.01014  -0.0482   0.0923   1.0000
  10.250   1.3330   0.01724   0.01077  -0.0464   0.0848   1.0000
  10.500   1.3475   0.01787   0.01139  -0.0448   0.0787   1.0000
  10.750   1.3612   0.01858   0.01208  -0.0432   0.0736   1.0000
  11.000   1.3750   0.01930   0.01279  -0.0417   0.0692   1.0000
  11.250   1.3884   0.02008   0.01357  -0.0401   0.0655   1.0000
  11.500   1.4027   0.02082   0.01431  -0.0388   0.0632   1.0000
  11.750   1.4156   0.02166   0.01517  -0.0374   0.0609   1.0000
  12.000   1.4287   0.02251   0.01603  -0.0360   0.0591   1.0000
  12.250   1.4425   0.02334   0.01689  -0.0348   0.0577   1.0000
  12.500   1.4553   0.02427   0.01785  -0.0336   0.0564   1.0000
  12.750   1.4672   0.02527   0.01888  -0.0324   0.0552   1.0000
  13.000   1.4779   0.02637   0.02000  -0.0311   0.0537   1.0000
  13.250   1.4887   0.02751   0.02117  -0.0299   0.0526   1.0000
  13.500   1.5008   0.02857   0.02227  -0.0289   0.0521   1.0000
  13.750   1.5122   0.02969   0.02344  -0.0279   0.0514   1.0000
  14.000   1.5226   0.03092   0.02472  -0.0269   0.0505   1.0000
  14.250   1.5326   0.03220   0.02603  -0.0259   0.0497   1.0000
  14.500   1.5401   0.03370   0.02757  -0.0249   0.0485   1.0000
  14.750   1.5469   0.03529   0.02919  -0.0238   0.0472   1.0000
  15.000   1.5537   0.03692   0.03086  -0.0229   0.0463   1.0000
  15.250   1.5627   0.03840   0.03239  -0.0222   0.0458   1.0000
  15.500   1.5711   0.03994   0.03399  -0.0214   0.0450   1.0000
  15.750   1.5777   0.04169   0.03579  -0.0207   0.0444   1.0000
  16.000   1.5840   0.04348   0.03764  -0.0201   0.0436   1.0000
  16.250   1.5886   0.04549   0.03970  -0.0194   0.0428   1.0000
  16.500   1.5924   0.04764   0.04189  -0.0189   0.0421   1.0000
  16.750   1.5960   0.04985   0.04417  -0.0185   0.0417   1.0000
  17.000   1.5977   0.05230   0.04667  -0.0181   0.0410   1.0000
  17.250   1.6002   0.05473   0.04917  -0.0179   0.0405   1.0000
  17.500   1.6035   0.05713   0.05164  -0.0177   0.0400   1.0000
  17.750   1.6059   0.05968   0.05427  -0.0177   0.0396   1.0000
  18.000   1.6075   0.06236   0.05701  -0.0177   0.0391   1.0000
  18.250   1.6084   0.06513   0.05985  -0.0178   0.0384   1.0000
  18.500   1.6082   0.06806   0.06285  -0.0180   0.0379   1.0000
  18.750   1.6065   0.07121   0.06606  -0.0183   0.0372   1.0000
  19.000   1.6039   0.07450   0.06942  -0.0187   0.0368   1.0000
  19.250   1.6003   0.07792   0.07290  -0.0191   0.0360   1.0000
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