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GOE 476 AIRFOIL (goe476-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 476 AIRFOIL (goe476-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.85 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe476-il-1000000.txt
Download as CSV file: xf-goe476-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 476 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.3254   0.16207   0.16016  -0.0377   1.0000   0.0289
 -15.500  -0.3186   0.15982   0.15793  -0.0382   1.0000   0.0296
 -15.000  -0.9880   0.03469   0.03173  -0.1131   0.9991   0.0373
 -14.750  -0.9708   0.03260   0.02954  -0.1160   0.9964   0.0376
 -14.500  -0.9539   0.03059   0.02740  -0.1182   0.9930   0.0379
 -14.250  -0.9413   0.02893   0.02561  -0.1185   0.9879   0.0382
 -14.000  -0.9181   0.02746   0.02403  -0.1199   0.9844   0.0385
 -13.750  -0.8937   0.02593   0.02236  -0.1215   0.9819   0.0389
 -13.500  -0.8709   0.02481   0.02113  -0.1220   0.9783   0.0392
 -13.250  -0.8480   0.02394   0.02015  -0.1222   0.9733   0.0396
 -13.000  -0.8203   0.02310   0.01920  -0.1231   0.9701   0.0399
 -12.750  -0.7944   0.02154   0.01748  -0.1245   0.9674   0.0403
 -12.500  -0.7749   0.02037   0.01623  -0.1240   0.9594   0.0408
 -12.250  -0.7411   0.01960   0.01541  -0.1259   0.9553   0.0412
 -12.000  -0.7072   0.01900   0.01478  -0.1277   0.9500   0.0416
 -11.750  -0.6766   0.01844   0.01416  -0.1287   0.9408   0.0420
 -11.500  -0.6453   0.01788   0.01352  -0.1298   0.9312   0.0425
 -11.250  -0.6151   0.01735   0.01289  -0.1306   0.9192   0.0430
 -11.000  -0.5907   0.01686   0.01227  -0.1301   0.9037   0.0434
 -10.750  -0.5676   0.01644   0.01173  -0.1294   0.8878   0.0439
 -10.500  -0.5444   0.01618   0.01135  -0.1284   0.8724   0.0443
 -10.250  -0.5225   0.01587   0.01091  -0.1273   0.8578   0.0446
 -10.000  -0.5023   0.01541   0.01031  -0.1259   0.8437   0.0450
  -9.750  -0.4844   0.01469   0.00947  -0.1242   0.8303   0.0456
  -9.500  -0.4628   0.01432   0.00904  -0.1230   0.8191   0.0461
  -9.250  -0.4404   0.01407   0.00872  -0.1219   0.8080   0.0466
  -9.000  -0.4173   0.01381   0.00841  -0.1209   0.7973   0.0470
  -8.750  -0.3943   0.01357   0.00808  -0.1198   0.7868   0.0475
  -8.500  -0.3711   0.01332   0.00776  -0.1188   0.7755   0.0481
  -8.250  -0.3475   0.01309   0.00745  -0.1178   0.7650   0.0487
  -8.000  -0.3239   0.01291   0.00717  -0.1168   0.7536   0.0493
  -7.750  -0.2996   0.01273   0.00691  -0.1159   0.7417   0.0497
  -7.500  -0.2758   0.01258   0.00666  -0.1149   0.7289   0.0501
  -7.250  -0.2552   0.01201   0.00600  -0.1135   0.7165   0.0510
  -7.000  -0.2312   0.01176   0.00571  -0.1126   0.7058   0.0517
  -6.500  -0.1820   0.01141   0.00527  -0.1110   0.6877   0.0530
  -6.250  -0.1573   0.01127   0.00506  -0.1102   0.6793   0.0538
  -6.000  -0.1318   0.01110   0.00485  -0.1095   0.6727   0.0545
  -5.750  -0.1059   0.01099   0.00468  -0.1089   0.6662   0.0552
  -5.500  -0.0805   0.01091   0.00453  -0.1082   0.6598   0.0558
  -5.250  -0.0566   0.01051   0.00412  -0.1073   0.6546   0.0570
  -5.000  -0.0310   0.01033   0.00392  -0.1067   0.6492   0.0580
  -4.750  -0.0055   0.01022   0.00377  -0.1061   0.6439   0.0589
  -4.500   0.0202   0.01012   0.00363  -0.1054   0.6389   0.0600
  -4.250   0.0469   0.00998   0.00349  -0.1050   0.6353   0.0609
  -4.000   0.0734   0.00989   0.00337  -0.1045   0.6310   0.0618
  -3.750   0.0986   0.00969   0.00314  -0.1038   0.6268   0.0633
  -3.500   0.1239   0.00958   0.00301  -0.1031   0.6222   0.0648
  -3.250   0.1504   0.00948   0.00290  -0.1026   0.6186   0.0662
  -3.000   0.1772   0.00937   0.00280  -0.1022   0.6149   0.0677
  -2.750   0.2038   0.00931   0.00271  -0.1017   0.6108   0.0689
  -2.500   0.2290   0.00916   0.00255  -0.1010   0.6068   0.0714
  -2.250   0.2548   0.00912   0.00249  -0.1004   0.6022   0.0738
  -2.000   0.2817   0.00903   0.00241  -0.1000   0.5994   0.0761
  -1.750   0.3080   0.00890   0.00231  -0.0995   0.5960   0.0796
  -1.500   0.3342   0.00882   0.00225  -0.0990   0.5922   0.0836
  -1.250   0.3599   0.00875   0.00218  -0.0983   0.5882   0.0890
  -1.000   0.3853   0.00872   0.00215  -0.0977   0.5837   0.0972
  -0.750   0.4117   0.00862   0.00214  -0.0972   0.5806   0.1104
  -0.500   0.4381   0.00855   0.00213  -0.0967   0.5761   0.1233
  -0.250   0.4638   0.00854   0.00212  -0.0961   0.5704   0.1322
   0.000   0.4890   0.00857   0.00215  -0.0954   0.5649   0.1401
   0.250   0.5160   0.00854   0.00214  -0.0950   0.5609   0.1453
   0.500   0.5420   0.00851   0.00214  -0.0945   0.5562   0.1527
   0.750   0.5676   0.00853   0.00215  -0.0939   0.5512   0.1576
   1.000   0.5927   0.00855   0.00215  -0.0931   0.5455   0.1621
   1.250   0.6187   0.00851   0.00215  -0.0926   0.5400   0.1686
   1.500   0.6439   0.00852   0.00216  -0.0919   0.5342   0.1739
   1.750   0.6682   0.00856   0.00218  -0.0910   0.5285   0.1797
   2.000   0.6940   0.00852   0.00220  -0.0905   0.5235   0.1884
   2.750   0.7659   0.00847   0.00232  -0.0877   0.5051   0.2601
   3.000   0.7821   0.00808   0.00243  -0.0854   0.4977   0.4622
   3.250   0.8791   0.00741   0.00301  -0.1006   0.4879   0.9801
   3.500   0.9351   0.00767   0.00319  -0.1066   0.4797   0.9881
   3.750   0.9782   0.00786   0.00335  -0.1099   0.4724   0.9931
   4.000   1.0285   0.00801   0.00343  -0.1148   0.4631   0.9969
   4.250   1.0717   0.00816   0.00352  -0.1182   0.4526   0.9995
   4.750   1.1173   0.00843   0.00371  -0.1161   0.4361   1.0000
   5.000   1.1368   0.00858   0.00383  -0.1144   0.4292   1.0000
   5.250   1.1557   0.00873   0.00395  -0.1125   0.4228   1.0000
   5.500   1.1757   0.00885   0.00406  -0.1109   0.4157   1.0000
   6.000   1.2120   0.00917   0.00433  -0.1069   0.4005   1.0000
   6.250   1.2289   0.00935   0.00448  -0.1047   0.3929   1.0000
   6.500   1.2463   0.00951   0.00463  -0.1025   0.3858   1.0000
   6.750   1.2625   0.00968   0.00478  -0.1002   0.3769   1.0000
   7.000   1.2760   0.00987   0.00494  -0.0973   0.3675   1.0000
   7.250   1.2840   0.01010   0.00512  -0.0932   0.3555   1.0000
   7.500   1.2927   0.01037   0.00533  -0.0894   0.3390   1.0000
   7.750   1.2979   0.01079   0.00562  -0.0851   0.3121   1.0000
   8.000   1.2945   0.01153   0.00614  -0.0793   0.2744   1.0000
   8.250   1.2957   0.01224   0.00670  -0.0746   0.2475   1.0000
   8.500   1.3038   0.01281   0.00719  -0.0712   0.2328   1.0000
   8.750   1.3143   0.01332   0.00766  -0.0684   0.2226   1.0000
   9.000   1.3265   0.01382   0.00813  -0.0659   0.2148   1.0000
   9.250   1.3394   0.01432   0.00861  -0.0636   0.2080   1.0000
   9.500   1.3541   0.01476   0.00906  -0.0617   0.2028   1.0000
   9.750   1.3668   0.01533   0.00962  -0.0595   0.1971   1.0000
  10.000   1.3807   0.01587   0.01016  -0.0576   0.1922   1.0000
  10.250   1.3960   0.01638   0.01068  -0.0560   0.1873   1.0000
  10.500   1.4081   0.01706   0.01135  -0.0540   0.1814   1.0000
  10.750   1.4215   0.01772   0.01201  -0.0523   0.1762   1.0000
  11.000   1.4356   0.01837   0.01267  -0.0508   0.1708   1.0000
  11.250   1.4459   0.01925   0.01353  -0.0489   0.1642   1.0000
  11.500   1.4594   0.02000   0.01430  -0.0474   0.1592   1.0000
  11.750   1.4700   0.02094   0.01523  -0.0458   0.1526   1.0000
  12.000   1.4803   0.02194   0.01623  -0.0442   0.1459   1.0000
  12.250   1.4883   0.02313   0.01739  -0.0425   0.1383   1.0000
  12.500   1.4963   0.02437   0.01862  -0.0409   0.1307   1.0000
  12.750   1.5015   0.02585   0.02008  -0.0392   0.1230   1.0000
  13.000   1.5059   0.02743   0.02163  -0.0376   0.1143   1.0000
  13.250   1.5083   0.02923   0.02341  -0.0359   0.1046   1.0000
  13.500   1.5093   0.03121   0.02536  -0.0343   0.0948   1.0000
  13.750   1.5059   0.03360   0.02769  -0.0326   0.0828   1.0000
  14.000   1.5030   0.03606   0.03010  -0.0312   0.0733   1.0000
  14.250   1.5043   0.03821   0.03226  -0.0300   0.0684   1.0000
  14.500   1.5053   0.04044   0.03449  -0.0289   0.0647   1.0000
  14.750   1.5091   0.04248   0.03657  -0.0281   0.0629   1.0000
  15.000   1.5116   0.04466   0.03878  -0.0273   0.0611   1.0000
  15.250   1.5133   0.04695   0.04110  -0.0265   0.0593   1.0000
  15.500   1.5145   0.04935   0.04354  -0.0258   0.0580   1.0000
  15.750   1.5204   0.05128   0.04553  -0.0253   0.0570   1.0000
  16.000   1.5239   0.05350   0.04781  -0.0248   0.0562   1.0000
  16.250   1.5273   0.05576   0.05012  -0.0243   0.0554   1.0000
  16.500   1.5282   0.05828   0.05269  -0.0239   0.0543   1.0000
  16.750   1.5278   0.06100   0.05545  -0.0235   0.0533   1.0000
  17.000   1.5265   0.06385   0.05834  -0.0232   0.0522   1.0000
  17.250   1.5258   0.06671   0.06127  -0.0230   0.0515   1.0000
  17.500   1.5306   0.06894   0.06356  -0.0229   0.0511   1.0000
  17.750   1.5327   0.07151   0.06620  -0.0228   0.0506   1.0000
  18.000   1.5357   0.07396   0.06872  -0.0228   0.0500   1.0000
  18.250   1.5361   0.07680   0.07162  -0.0228   0.0494   1.0000
  18.500   1.5380   0.07945   0.07433  -0.0229   0.0488   1.0000
  18.750   1.5369   0.08252   0.07745  -0.0231   0.0481   1.0000
  19.000   1.5353   0.08562   0.08061  -0.0233   0.0476   1.0000
  19.250   1.5318   0.08904   0.08408  -0.0237   0.0469   1.0000
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