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GOE 504 AIRFOIL (goe504-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 504 AIRFOIL (goe504-il)
Reynolds number: 500,000
Max Cl/Cd: 85.1 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe504-il-500000-n5.txt
Download as CSV file: xf-goe504-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 504 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.5164   0.09583   0.09308  -0.0809   0.9961   0.0126
 -16.000  -0.5587   0.08344   0.08048  -0.0889   0.9934   0.0126
 -15.750  -0.5719   0.07656   0.07350  -0.0942   0.9910   0.0127
 -15.500  -0.5980   0.06817   0.06492  -0.1005   0.9879   0.0126
 -15.250  -0.6008   0.06299   0.05967  -0.1055   0.9852   0.0129
 -15.000  -0.6091   0.05738   0.05395  -0.1104   0.9814   0.0130
 -14.750  -0.6138   0.05218   0.04864  -0.1153   0.9767   0.0131
 -14.500  -0.6129   0.04719   0.04352  -0.1208   0.9732   0.0132
 -14.250  -0.6085   0.04314   0.03937  -0.1252   0.9673   0.0134
 -14.000  -0.5995   0.03894   0.03503  -0.1309   0.9625   0.0136
 -13.750  -0.5844   0.03542   0.03137  -0.1366   0.9577   0.0138
 -13.500  -0.5646   0.03282   0.02864  -0.1414   0.9512   0.0143
 -13.250  -0.5419   0.03009   0.02573  -0.1470   0.9458   0.0147
 -13.000  -0.5262   0.02790   0.02335  -0.1500   0.9353   0.0151
 -12.750  -0.5086   0.02610   0.02134  -0.1522   0.9244   0.0157
 -12.500  -0.4912   0.02486   0.01999  -0.1533   0.9114   0.0159
 -12.250  -0.4743   0.02408   0.01912  -0.1534   0.8969   0.0162
 -12.000  -0.4609   0.02337   0.01829  -0.1524   0.8811   0.0165
 -11.750  -0.4499   0.02272   0.01750  -0.1507   0.8651   0.0168
 -11.500  -0.4391   0.02220   0.01686  -0.1486   0.8496   0.0172
 -11.250  -0.4315   0.02158   0.01608  -0.1459   0.8348   0.0175
 -10.750  -0.4142   0.02059   0.01479  -0.1402   0.8087   0.0186
 -10.500  -0.4012   0.02009   0.01412  -0.1380   0.7977   0.0191
 -10.250  -0.3866   0.01967   0.01359  -0.1360   0.7877   0.0196
 -10.000  -0.3716   0.01922   0.01306  -0.1342   0.7778   0.0199
  -9.750  -0.3548   0.01886   0.01262  -0.1325   0.7687   0.0203
  -9.500  -0.3372   0.01850   0.01218  -0.1310   0.7600   0.0208
  -9.250  -0.3193   0.01810   0.01169  -0.1295   0.7521   0.0213
  -9.000  -0.3005   0.01775   0.01124  -0.1281   0.7440   0.0220
  -8.750  -0.2815   0.01736   0.01074  -0.1267   0.7367   0.0226
  -8.500  -0.2613   0.01705   0.01031  -0.1254   0.7292   0.0232
  -8.250  -0.2407   0.01676   0.00991  -0.1242   0.7227   0.0237
  -8.000  -0.2234   0.01616   0.00927  -0.1226   0.7155   0.0243
  -7.500  -0.1831   0.01543   0.00845  -0.1201   0.7024   0.0255
  -7.250  -0.1620   0.01513   0.00807  -0.1190   0.6960   0.0263
  -7.000  -0.1407   0.01482   0.00769  -0.1179   0.6899   0.0269
  -6.750  -0.1193   0.01450   0.00731  -0.1168   0.6833   0.0274
  -6.500  -0.0971   0.01429   0.00701  -0.1158   0.6772   0.0281
  -6.250  -0.0741   0.01405   0.00671  -0.1149   0.6713   0.0285
  -6.000  -0.0541   0.01364   0.00624  -0.1135   0.6647   0.0292
  -5.750  -0.0333   0.01329   0.00583  -0.1123   0.6589   0.0298
  -5.500  -0.0109   0.01300   0.00550  -0.1113   0.6527   0.0305
  -5.250   0.0116   0.01277   0.00521  -0.1104   0.6466   0.0312
  -5.000   0.0348   0.01256   0.00495  -0.1095   0.6407   0.0320
  -4.750   0.0581   0.01237   0.00471  -0.1087   0.6342   0.0327
  -4.500   0.0814   0.01223   0.00449  -0.1078   0.6282   0.0333
  -4.250   0.1055   0.01207   0.00428  -0.1071   0.6220   0.0338
  -4.000   0.1291   0.01196   0.00410  -0.1062   0.6155   0.0344
  -3.750   0.1529   0.01182   0.00391  -0.1055   0.6096   0.0353
  -3.500   0.1766   0.01168   0.00372  -0.1047   0.6032   0.0370
  -3.000   0.2241   0.01149   0.00345  -0.1031   0.5908   0.0407
  -2.750   0.2472   0.01138   0.00332  -0.1022   0.5845   0.0470
  -2.500   0.2688   0.01113   0.00319  -0.1011   0.5786   0.0898
  -2.000   0.3098   0.01055   0.00299  -0.0985   0.5663   0.2119
  -1.750   0.3336   0.01050   0.00297  -0.0978   0.5603   0.2290
  -1.500   0.3569   0.01048   0.00296  -0.0969   0.5540   0.2452
  -1.250   0.3799   0.01049   0.00296  -0.0960   0.5484   0.2594
  -1.000   0.4037   0.01047   0.00296  -0.0953   0.5426   0.2729
  -0.750   0.4264   0.01047   0.00296  -0.0943   0.5367   0.2846
  -0.250   0.4725   0.01051   0.00297  -0.0925   0.5254   0.3021
   0.000   0.4944   0.01053   0.00299  -0.0914   0.5198   0.3135
   0.250   0.5163   0.01055   0.00301  -0.0903   0.5143   0.3262
   0.500   0.5373   0.01052   0.00304  -0.0890   0.5089   0.3457
   0.750   0.5563   0.01051   0.00307  -0.0873   0.5035   0.3683
   1.000   0.5767   0.01048   0.00311  -0.0859   0.4987   0.3933
   1.250   0.5970   0.01046   0.00316  -0.0845   0.4931   0.4182
   1.500   0.6158   0.01047   0.00322  -0.0828   0.4879   0.4493
   1.750   0.6349   0.01043   0.00331  -0.0812   0.4830   0.4937
   2.000   0.6533   0.01037   0.00341  -0.0795   0.4775   0.5514
   2.250   0.6684   0.01029   0.00354  -0.0770   0.4722   0.6260
   2.500   0.6821   0.01016   0.00369  -0.0742   0.4675   0.7180
   2.750   0.6969   0.00999   0.00387  -0.0715   0.4616   0.8263
   3.000   0.7827   0.01022   0.00427  -0.0843   0.4535   0.9370
   3.250   0.8466   0.01048   0.00450  -0.0924   0.4452   0.9626
   3.500   0.8847   0.01074   0.00470  -0.0950   0.4390   0.9793
   3.750   0.9187   0.01093   0.00487  -0.0967   0.4326   0.9904
   4.000   0.9496   0.01119   0.00509  -0.0978   0.4262   0.9996
   4.250   0.9653   0.01137   0.00523  -0.0956   0.4210   1.0000
   4.500   0.9803   0.01152   0.00537  -0.0933   0.4154   1.0000
   4.750   0.9933   0.01173   0.00554  -0.0907   0.4091   1.0000
   5.000   1.0093   0.01192   0.00572  -0.0887   0.4041   1.0000
   5.250   1.0256   0.01213   0.00591  -0.0867   0.3984   1.0000
   5.500   1.0405   0.01239   0.00614  -0.0846   0.3930   1.0000
   5.750   1.0577   0.01262   0.00637  -0.0829   0.3879   1.0000
   6.000   1.0746   0.01287   0.00662  -0.0811   0.3823   1.0000
   6.250   1.0895   0.01320   0.00692  -0.0791   0.3769   1.0000
   6.500   1.1073   0.01347   0.00719  -0.0777   0.3715   1.0000
   6.750   1.1232   0.01381   0.00752  -0.0759   0.3649   1.0000
   7.000   1.1385   0.01419   0.00789  -0.0742   0.3592   1.0000
   7.250   1.1550   0.01455   0.00825  -0.0726   0.3521   1.0000
   7.500   1.1678   0.01507   0.00872  -0.0706   0.3433   1.0000
   7.750   1.1834   0.01551   0.00916  -0.0690   0.3358   1.0000
   8.000   1.1966   0.01607   0.00969  -0.0672   0.3283   1.0000
   8.250   1.2110   0.01660   0.01022  -0.0656   0.3198   1.0000
   8.500   1.2227   0.01729   0.01087  -0.0637   0.3097   1.0000
   8.750   1.2340   0.01803   0.01158  -0.0618   0.3009   1.0000
   9.000   1.2468   0.01873   0.01227  -0.0602   0.2911   1.0000
   9.250   1.2569   0.01960   0.01311  -0.0584   0.2808   1.0000
   9.500   1.2662   0.02056   0.01403  -0.0566   0.2707   1.0000
   9.750   1.2771   0.02148   0.01494  -0.0551   0.2606   1.0000
  10.000   1.2857   0.02256   0.01600  -0.0534   0.2504   1.0000
  10.250   1.2914   0.02388   0.01726  -0.0515   0.2371   1.0000
  10.500   1.2965   0.02529   0.01863  -0.0497   0.2244   1.0000
  10.750   1.2985   0.02698   0.02025  -0.0478   0.2085   1.0000
  11.000   1.2982   0.02890   0.02210  -0.0458   0.1903   1.0000
  11.250   1.2902   0.03149   0.02456  -0.0435   0.1656   1.0000
  11.500   1.2640   0.03565   0.02846  -0.0402   0.1230   1.0000
  11.750   1.2343   0.04043   0.03302  -0.0372   0.0814   1.0000
  12.000   1.2148   0.04459   0.03707  -0.0352   0.0487   1.0000
  12.250   1.1974   0.04879   0.04123  -0.0337   0.0193   1.0000
  12.500   1.1998   0.05116   0.04364  -0.0331   0.0163   1.0000
  12.750   1.2028   0.05351   0.04606  -0.0326   0.0148   1.0000
  13.000   1.2057   0.05592   0.04854  -0.0321   0.0138   1.0000
  13.250   1.2097   0.05826   0.05095  -0.0318   0.0130   1.0000
  13.500   1.2128   0.06073   0.05349  -0.0315   0.0124   1.0000
  13.750   1.2157   0.06323   0.05607  -0.0313   0.0121   1.0000
  14.000   1.2159   0.06607   0.05900  -0.0310   0.0115   1.0000
  14.250   1.2157   0.06902   0.06203  -0.0309   0.0111   1.0000
  14.500   1.2132   0.07229   0.06538  -0.0308   0.0107   1.0000
  14.750   1.2142   0.07517   0.06834  -0.0308   0.0104   1.0000
  15.000   1.2141   0.07819   0.07145  -0.0309   0.0103   1.0000
  15.250   1.2126   0.08144   0.07479  -0.0310   0.0099   1.0000
  15.500   1.2112   0.08471   0.07814  -0.0312   0.0098   1.0000
  15.750   1.2090   0.08813   0.08164  -0.0314   0.0095   1.0000
  16.000   1.2063   0.09166   0.08525  -0.0318   0.0090   1.0000
  16.250   1.2031   0.09524   0.08892  -0.0322   0.0089   1.0000
  16.500   1.1983   0.09911   0.09286  -0.0327   0.0086   1.0000
  16.750   1.1928   0.10313   0.09697  -0.0333   0.0085   1.0000
  17.000   1.1856   0.10743   0.10136  -0.0340   0.0083   1.0000
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