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GOE 584 AIRFOIL (goe584-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 584 AIRFOIL (goe584-il)
Reynolds number: 1,000,000
Max Cl/Cd: 137.5 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe584-il-1000000.txt
Download as CSV file: xf-goe584-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 584 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  -1.0965   0.03224   0.02933  -0.1052   1.0000   0.0198
 -15.500  -1.1128   0.03018   0.02715  -0.1017   1.0000   0.0201
 -15.250  -1.1150   0.02851   0.02535  -0.0992   1.0000   0.0204
 -15.000  -1.1126   0.02712   0.02386  -0.0968   1.0000   0.0207
 -14.750  -1.1071   0.02593   0.02255  -0.0944   1.0000   0.0211
 -14.500  -1.0995   0.02493   0.02144  -0.0920   1.0000   0.0215
 -14.250  -1.0976   0.02365   0.02008  -0.0888   1.0000   0.0221
 -14.000  -1.0699   0.02254   0.01892  -0.0902   0.9983   0.0229
 -13.750  -1.0382   0.02165   0.01796  -0.0919   0.9957   0.0237
 -13.500  -1.0070   0.02080   0.01701  -0.0934   0.9927   0.0245
 -13.250  -0.9773   0.02000   0.01608  -0.0945   0.9886   0.0251
 -13.000  -0.9464   0.01912   0.01518  -0.0960   0.9847   0.0262
 -12.750  -0.9135   0.01866   0.01470  -0.0973   0.9810   0.0271
 -12.500  -0.8822   0.01823   0.01422  -0.0983   0.9745   0.0281
 -12.250  -0.8455   0.01777   0.01365  -0.1003   0.9706   0.0289
 -12.000  -0.8123   0.01716   0.01302  -0.1019   0.9624   0.0301
 -11.750  -0.7733   0.01699   0.01286  -0.1042   0.9549   0.0310
 -11.500  -0.7385   0.01680   0.01261  -0.1057   0.9413   0.0318
 -11.250  -0.7077   0.01655   0.01225  -0.1063   0.9239   0.0327
 -11.000  -0.6811   0.01635   0.01191  -0.1061   0.9050   0.0333
 -10.750  -0.6587   0.01589   0.01133  -0.1052   0.8875   0.0342
 -10.250  -0.6075   0.01593   0.01128  -0.1040   0.8601   0.0356
 -10.000  -0.5820   0.01588   0.01117  -0.1035   0.8494   0.0362
  -9.750  -0.5572   0.01575   0.01094  -0.1028   0.8392   0.0370
  -9.500  -0.5316   0.01563   0.01074  -0.1023   0.8303   0.0378
  -9.250  -0.5059   0.01563   0.01062  -0.1017   0.8214   0.0383
  -9.000  -0.4837   0.01483   0.00972  -0.1009   0.8135   0.0393
  -8.750  -0.4585   0.01463   0.00948  -0.1004   0.8057   0.0399
  -8.500  -0.4322   0.01456   0.00939  -0.1000   0.7986   0.0405
  -8.250  -0.4062   0.01446   0.00924  -0.0995   0.7909   0.0412
  -8.000  -0.3801   0.01435   0.00906  -0.0991   0.7841   0.0420
  -7.750  -0.3542   0.01411   0.00875  -0.0986   0.7771   0.0428
  -7.500  -0.3282   0.01396   0.00850  -0.0982   0.7701   0.0435
  -7.250  -0.3013   0.01390   0.00838  -0.0978   0.7632   0.0440
  -7.000  -0.2777   0.01304   0.00740  -0.0971   0.7561   0.0450
  -6.750  -0.2521   0.01267   0.00700  -0.0967   0.7497   0.0458
  -6.500  -0.2255   0.01248   0.00679  -0.0964   0.7427   0.0465
  -6.250  -0.1993   0.01227   0.00652  -0.0959   0.7357   0.0472
  -6.000  -0.1725   0.01207   0.00629  -0.0956   0.7288   0.0480
  -5.750  -0.1460   0.01185   0.00601  -0.0952   0.7217   0.0488
  -5.500  -0.1194   0.01161   0.00570  -0.0948   0.7153   0.0495
  -5.250  -0.0925   0.01138   0.00542  -0.0945   0.7082   0.0501
  -5.000  -0.0657   0.01129   0.00526  -0.0941   0.7012   0.0506
  -4.750  -0.0392   0.01090   0.00482  -0.0937   0.6945   0.0512
  -4.500  -0.0143   0.01033   0.00421  -0.0931   0.6877   0.0522
  -4.250   0.0121   0.01006   0.00391  -0.0927   0.6814   0.0530
  -4.000   0.0389   0.00986   0.00369  -0.0924   0.6747   0.0538
  -3.500   0.0927   0.00955   0.00333  -0.0917   0.6619   0.0555
  -3.250   0.1195   0.00940   0.00315  -0.0914   0.6555   0.0564
  -3.000   0.1464   0.00927   0.00297  -0.0910   0.6494   0.0571
  -2.750   0.1737   0.00914   0.00282  -0.0907   0.6432   0.0578
  -2.500   0.2006   0.00905   0.00269  -0.0904   0.6369   0.0583
  -2.250   0.2275   0.00891   0.00252  -0.0901   0.6311   0.0590
  -2.000   0.2538   0.00867   0.00225  -0.0896   0.6246   0.0607
  -1.750   0.2803   0.00858   0.00213  -0.0892   0.6178   0.0623
  -1.500   0.3078   0.00847   0.00202  -0.0890   0.6117   0.0635
  -1.250   0.3349   0.00841   0.00193  -0.0887   0.6055   0.0650
  -1.000   0.3620   0.00837   0.00187  -0.0884   0.5998   0.0664
  -0.750   0.3897   0.00831   0.00180  -0.0882   0.5943   0.0676
  -0.500   0.4165   0.00823   0.00170  -0.0879   0.5885   0.0706
  -0.250   0.4435   0.00818   0.00166  -0.0876   0.5831   0.0746
   0.000   0.4710   0.00812   0.00161  -0.0874   0.5776   0.0806
   0.250   0.4972   0.00798   0.00158  -0.0870   0.5719   0.1147
   0.500   0.5228   0.00778   0.00160  -0.0865   0.5667   0.1930
   0.750   0.5494   0.00764   0.00162  -0.0862   0.5610   0.2436
   1.000   0.5747   0.00747   0.00165  -0.0857   0.5553   0.3269
   1.250   0.5991   0.00721   0.00169  -0.0851   0.5498   0.4445
   1.500   0.6172   0.00654   0.00177  -0.0832   0.5446   0.7126
   1.750   0.6756   0.00612   0.00196  -0.0895   0.5374   0.9697
   2.000   0.7243   0.00622   0.00203  -0.0940   0.5312   0.9887
   2.250   0.7705   0.00632   0.00208  -0.0979   0.5241   0.9970
   2.500   0.8105   0.00641   0.00212  -0.1005   0.5174   1.0000
   2.750   0.8349   0.00647   0.00217  -0.0997   0.5109   1.0000
   3.000   0.8584   0.00658   0.00223  -0.0988   0.5041   1.0000
   3.250   0.8827   0.00665   0.00228  -0.0980   0.4964   1.0000
   3.750   0.9299   0.00687   0.00243  -0.0961   0.4770   1.0000
   4.000   0.9531   0.00701   0.00251  -0.0952   0.4657   1.0000
   4.250   0.9759   0.00717   0.00261  -0.0941   0.4544   1.0000
   4.500   0.9999   0.00728   0.00271  -0.0933   0.4448   1.0000
   4.750   1.0230   0.00744   0.00283  -0.0923   0.4344   1.0000
   5.000   1.0455   0.00763   0.00296  -0.0912   0.4223   1.0000
   5.250   1.0681   0.00781   0.00309  -0.0902   0.4086   1.0000
   5.500   1.0907   0.00800   0.00324  -0.0891   0.3958   1.0000
   5.750   1.1128   0.00821   0.00340  -0.0880   0.3826   1.0000
   6.000   1.1345   0.00845   0.00358  -0.0869   0.3694   1.0000
   6.250   1.1557   0.00870   0.00378  -0.0856   0.3556   1.0000
   6.500   1.1765   0.00898   0.00400  -0.0843   0.3415   1.0000
   6.750   1.1967   0.00927   0.00422  -0.0829   0.3271   1.0000
   7.000   1.2164   0.00959   0.00447  -0.0814   0.3114   1.0000
   7.500   1.2556   0.01021   0.00498  -0.0785   0.2833   1.0000
   7.750   1.2750   0.01052   0.00524  -0.0770   0.2702   1.0000
   8.000   1.2935   0.01085   0.00552  -0.0754   0.2571   1.0000
   8.250   1.3111   0.01121   0.00583  -0.0736   0.2435   1.0000
   8.500   1.3272   0.01161   0.00616  -0.0716   0.2283   1.0000
   8.750   1.3403   0.01203   0.00651  -0.0690   0.2141   1.0000
   9.000   1.3514   0.01248   0.00690  -0.0661   0.1990   1.0000
   9.250   1.3629   0.01296   0.00731  -0.0633   0.1851   1.0000
   9.500   1.3744   0.01348   0.00778  -0.0607   0.1716   1.0000
   9.750   1.3851   0.01408   0.00831  -0.0581   0.1578   1.0000
  10.000   1.3954   0.01474   0.00890  -0.0555   0.1445   1.0000
  10.250   1.4061   0.01542   0.00954  -0.0532   0.1339   1.0000
  10.500   1.4183   0.01607   0.01016  -0.0512   0.1253   1.0000
  10.750   1.4305   0.01677   0.01085  -0.0493   0.1182   1.0000
  11.000   1.4430   0.01750   0.01157  -0.0476   0.1123   1.0000
  11.250   1.4543   0.01833   0.01240  -0.0458   0.1048   1.0000
  11.500   1.4647   0.01927   0.01331  -0.0441   0.0979   1.0000
  11.750   1.4767   0.02017   0.01421  -0.0427   0.0914   1.0000
  12.000   1.4855   0.02132   0.01533  -0.0411   0.0830   1.0000
  12.250   1.4911   0.02275   0.01670  -0.0394   0.0704   1.0000
  12.500   1.4867   0.02499   0.01879  -0.0372   0.0496   1.0000
  12.750   1.4800   0.02751   0.02122  -0.0350   0.0345   1.0000
  13.000   1.4824   0.02942   0.02314  -0.0336   0.0298   1.0000
  13.250   1.4861   0.03128   0.02503  -0.0324   0.0275   1.0000
  13.500   1.4915   0.03303   0.02683  -0.0314   0.0259   1.0000
  13.750   1.4968   0.03483   0.02869  -0.0305   0.0247   1.0000
  14.000   1.4996   0.03690   0.03080  -0.0296   0.0235   1.0000
  14.250   1.5006   0.03919   0.03315  -0.0287   0.0224   1.0000
  14.500   1.5067   0.04107   0.03510  -0.0281   0.0219   1.0000
  14.750   1.5115   0.04311   0.03720  -0.0276   0.0211   1.0000
  15.000   1.5147   0.04534   0.03948  -0.0271   0.0204   1.0000
  15.250   1.5154   0.04788   0.04208  -0.0266   0.0198   1.0000
  15.500   1.5128   0.05084   0.04512  -0.0262   0.0191   1.0000
  15.750   1.5127   0.05359   0.04795  -0.0260   0.0187   1.0000
  16.000   1.5155   0.05606   0.05048  -0.0258   0.0183   1.0000
  16.250   1.5160   0.05883   0.05333  -0.0257   0.0180   1.0000
  16.500   1.5165   0.06163   0.05620  -0.0257   0.0175   1.0000
  16.750   1.5156   0.06463   0.05927  -0.0258   0.0171   1.0000
  17.000   1.5124   0.06796   0.06267  -0.0259   0.0167   1.0000
  17.250   1.5078   0.07152   0.06630  -0.0262   0.0165   1.0000
  17.500   1.4991   0.07567   0.07054  -0.0267   0.0161   1.0000
  17.750   1.4850   0.08060   0.07557  -0.0273   0.0157   1.0000
  18.000   1.4815   0.08417   0.07923  -0.0279   0.0156   1.0000
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