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GOE 593 AIRFOIL (goe593-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 593 AIRFOIL (goe593-il)
Reynolds number: 500,000
Max Cl/Cd: 88.93 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe593-il-500000-n5.txt
Download as CSV file: xf-goe593-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 593 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.8704   0.04166   0.03876  -0.0850   1.0000   0.0117
 -13.000  -0.8889   0.03647   0.03327  -0.0869   0.9961   0.0118
 -12.750  -0.8762   0.03307   0.02962  -0.0896   0.9917   0.0120
 -12.500  -0.8588   0.03060   0.02693  -0.0913   0.9877   0.0124
 -12.250  -0.8380   0.02848   0.02458  -0.0929   0.9847   0.0128
 -12.000  -0.8209   0.02675   0.02264  -0.0929   0.9794   0.0131
 -11.750  -0.7980   0.02505   0.02070  -0.0938   0.9763   0.0135
 -11.500  -0.7777   0.02376   0.01926  -0.0937   0.9715   0.0140
 -11.250  -0.7532   0.02284   0.01825  -0.0940   0.9673   0.0144
 -11.000  -0.7248   0.02208   0.01740  -0.0949   0.9648   0.0150
 -10.750  -0.7021   0.02129   0.01651  -0.0945   0.9599   0.0155
 -10.500  -0.6776   0.02048   0.01557  -0.0945   0.9553   0.0162
 -10.250  -0.6503   0.01958   0.01447  -0.0950   0.9524   0.0169
 -10.000  -0.6241   0.01895   0.01380  -0.0951   0.9484   0.0176
  -9.750  -0.5980   0.01849   0.01327  -0.0951   0.9433   0.0181
  -9.500  -0.5674   0.01795   0.01265  -0.0960   0.9402   0.0189
  -9.250  -0.5349   0.01730   0.01187  -0.0973   0.9378   0.0198
  -9.000  -0.5056   0.01674   0.01117  -0.0978   0.9334   0.0207
  -8.750  -0.4751   0.01619   0.01057  -0.0987   0.9290   0.0215
  -8.500  -0.4413   0.01580   0.01013  -0.1002   0.9253   0.0224
  -8.250  -0.4065   0.01534   0.00958  -0.1019   0.9221   0.0234
  -8.000  -0.3777   0.01488   0.00902  -0.1022   0.9162   0.0243
  -7.750  -0.3453   0.01451   0.00852  -0.1033   0.9108   0.0252
  -7.500  -0.3131   0.01390   0.00786  -0.1045   0.9059   0.0263
  -7.250  -0.2867   0.01356   0.00746  -0.1043   0.8987   0.0272
  -7.000  -0.2567   0.01322   0.00706  -0.1048   0.8925   0.0282
  -6.750  -0.2293   0.01291   0.00667  -0.1047   0.8855   0.0292
  -6.500  -0.2022   0.01261   0.00627  -0.1046   0.8780   0.0301
  -6.250  -0.1751   0.01227   0.00585  -0.1044   0.8713   0.0309
  -6.000  -0.1508   0.01185   0.00541  -0.1037   0.8631   0.0321
  -5.750  -0.1241   0.01158   0.00508  -0.1035   0.8558   0.0331
  -5.500  -0.0992   0.01131   0.00477  -0.1028   0.8473   0.0340
  -5.250  -0.0729   0.01108   0.00447  -0.1024   0.8396   0.0352
  -5.000  -0.0478   0.01087   0.00421  -0.1018   0.8306   0.0362
  -4.750  -0.0220   0.01068   0.00393  -0.1012   0.8219   0.0370
  -4.500   0.0027   0.01040   0.00361  -0.1005   0.8124   0.0384
  -4.250   0.0278   0.01020   0.00337  -0.0998   0.8026   0.0399
  -4.000   0.0533   0.01004   0.00315  -0.0992   0.7928   0.0417
  -3.750   0.0783   0.00990   0.00296  -0.0985   0.7813   0.0437
  -3.500   0.1032   0.00977   0.00277  -0.0978   0.7690   0.0462
  -3.250   0.1274   0.00964   0.00258  -0.0969   0.7541   0.0504
  -3.000   0.1515   0.00954   0.00242  -0.0959   0.7386   0.0564
  -2.750   0.1755   0.00942   0.00230  -0.0950   0.7247   0.0686
  -2.500   0.1999   0.00932   0.00221  -0.0942   0.7134   0.0885
  -2.250   0.2248   0.00925   0.00214  -0.0935   0.7025   0.1041
  -2.000   0.2498   0.00919   0.00207  -0.0928   0.6923   0.1168
  -1.750   0.2745   0.00915   0.00201  -0.0921   0.6820   0.1278
  -1.500   0.2995   0.00911   0.00195  -0.0914   0.6710   0.1387
  -1.250   0.3243   0.00908   0.00190  -0.0907   0.6601   0.1513
  -1.000   0.3483   0.00901   0.00187  -0.0898   0.6484   0.1729
  -0.750   0.3714   0.00881   0.00186  -0.0889   0.6381   0.2404
  -0.500   0.3943   0.00861   0.00184  -0.0879   0.6279   0.3136
  -0.250   0.4152   0.00832   0.00184  -0.0866   0.6173   0.4199
   0.000   0.4367   0.00809   0.00186  -0.0853   0.6065   0.5197
   0.250   0.4573   0.00789   0.00189  -0.0837   0.5958   0.6072
   0.500   0.4755   0.00764   0.00193  -0.0816   0.5857   0.7127
   0.750   0.4948   0.00742   0.00202  -0.0794   0.5744   0.8177
   1.000   0.5394   0.00743   0.00219  -0.0828   0.5582   0.9182
   1.250   0.5955   0.00766   0.00232  -0.0890   0.5383   0.9543
   1.500   0.6358   0.00785   0.00241  -0.0917   0.5189   0.9704
   1.750   0.6702   0.00806   0.00251  -0.0932   0.4983   0.9821
   2.000   0.7112   0.00832   0.00264  -0.0961   0.4752   0.9932
   2.250   0.7538   0.00858   0.00276  -0.0996   0.4506   1.0000
   2.500   0.7711   0.00880   0.00287  -0.0974   0.4302   1.0000
   3.000   0.8073   0.00922   0.00310  -0.0934   0.3968   1.0000
   3.250   0.8263   0.00941   0.00322  -0.0917   0.3830   1.0000
   3.500   0.8456   0.00960   0.00335  -0.0899   0.3704   1.0000
   3.750   0.8649   0.00980   0.00349  -0.0882   0.3589   1.0000
   4.000   0.8841   0.01000   0.00364  -0.0864   0.3485   1.0000
   4.250   0.9039   0.01019   0.00380  -0.0848   0.3384   1.0000
   4.500   0.9234   0.01040   0.00396  -0.0832   0.3290   1.0000
   4.750   0.9428   0.01061   0.00413  -0.0815   0.3199   1.0000
   5.000   0.9622   0.01082   0.00431  -0.0798   0.3096   1.0000
   5.250   0.9810   0.01106   0.00451  -0.0780   0.3009   1.0000
   5.500   1.0003   0.01128   0.00470  -0.0764   0.2914   1.0000
   5.750   1.0191   0.01152   0.00491  -0.0746   0.2827   1.0000
   6.000   1.0377   0.01174   0.00512  -0.0728   0.2749   1.0000
   6.250   1.0552   0.01197   0.00533  -0.0709   0.2680   1.0000
   6.500   1.0734   0.01218   0.00554  -0.0690   0.2619   1.0000
   6.750   1.0901   0.01244   0.00579  -0.0669   0.2551   1.0000
   7.000   1.1088   0.01266   0.00602  -0.0652   0.2479   1.0000
   7.250   1.1258   0.01296   0.00629  -0.0632   0.2408   1.0000
   7.500   1.1446   0.01320   0.00655  -0.0616   0.2336   1.0000
   8.000   1.1797   0.01382   0.00715  -0.0581   0.2167   1.0000
   8.500   1.2153   0.01447   0.00781  -0.0547   0.2027   1.0000
   8.750   1.2318   0.01486   0.00819  -0.0529   0.1938   1.0000
   9.000   1.2484   0.01527   0.00858  -0.0512   0.1828   1.0000
   9.250   1.2643   0.01572   0.00901  -0.0494   0.1703   1.0000
   9.500   1.2772   0.01632   0.00954  -0.0472   0.1523   1.0000
   9.750   1.2848   0.01725   0.01030  -0.0444   0.1227   1.0000
  10.000   1.2903   0.01833   0.01123  -0.0413   0.0962   1.0000
  10.250   1.2978   0.01933   0.01214  -0.0387   0.0796   1.0000
  10.500   1.3078   0.02022   0.01299  -0.0365   0.0703   1.0000
  10.750   1.3187   0.02107   0.01384  -0.0345   0.0639   1.0000
  11.000   1.3300   0.02192   0.01471  -0.0327   0.0593   1.0000
  11.250   1.3409   0.02282   0.01563  -0.0309   0.0560   1.0000
  11.500   1.3537   0.02362   0.01650  -0.0294   0.0534   1.0000
  11.750   1.3654   0.02451   0.01744  -0.0279   0.0510   1.0000
  12.000   1.3757   0.02552   0.01848  -0.0263   0.0486   1.0000
  12.250   1.3842   0.02670   0.01969  -0.0246   0.0458   1.0000
  12.500   1.3959   0.02767   0.02075  -0.0234   0.0443   1.0000
  12.750   1.4061   0.02878   0.02192  -0.0221   0.0421   1.0000
  13.000   1.4144   0.03006   0.02324  -0.0208   0.0397   1.0000
  13.250   1.4216   0.03149   0.02472  -0.0195   0.0376   1.0000
  13.500   1.4304   0.03282   0.02612  -0.0184   0.0354   1.0000
  13.750   1.4369   0.03438   0.02774  -0.0173   0.0328   1.0000
  14.000   1.4424   0.03609   0.02950  -0.0163   0.0303   1.0000
  14.250   1.4470   0.03793   0.03138  -0.0154   0.0272   1.0000
  14.500   1.4501   0.03997   0.03348  -0.0145   0.0247   1.0000
  15.000   1.4513   0.04480   0.03841  -0.0132   0.0192   1.0000
  15.250   1.4494   0.04759   0.04125  -0.0128   0.0175   1.0000
  15.500   1.4482   0.05040   0.04415  -0.0125   0.0164   1.0000
  15.750   1.4454   0.05350   0.04734  -0.0124   0.0153   1.0000
  16.000   1.4404   0.05695   0.05087  -0.0125   0.0144   1.0000
  16.250   1.4354   0.06050   0.05453  -0.0127   0.0137   1.0000
  16.500   1.4304   0.06416   0.05829  -0.0131   0.0131   1.0000
  16.750   1.4250   0.06796   0.06221  -0.0137   0.0127   1.0000
  17.000   1.4174   0.07217   0.06653  -0.0146   0.0123   1.0000
  17.250   1.4086   0.07662   0.07108  -0.0155   0.0120   1.0000
  17.500   1.3987   0.08133   0.07590  -0.0167   0.0117   1.0000
  17.750   1.3871   0.08640   0.08109  -0.0182   0.0113   1.0000
  18.000   1.3748   0.09165   0.08644  -0.0197   0.0110   1.0000
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