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GOE 593 AIRFOIL (goe593-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 593 AIRFOIL (goe593-il)
Reynolds number: 200,000
Max Cl/Cd: 74.61 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe593-il-200000.txt
Download as CSV file: xf-goe593-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.3495   0.10626   0.10268  -0.0395   1.0000   0.0601
  -9.750  -0.3759   0.10323   0.09976  -0.0426   1.0000   0.0612
  -9.500  -0.3975   0.10040   0.09703  -0.0435   1.0000   0.0614
  -9.250  -0.3927   0.09647   0.09312  -0.0403   1.0000   0.0622
  -9.000  -0.3878   0.09465   0.09133  -0.0371   1.0000   0.0630
  -8.750  -0.3875   0.09318   0.08989  -0.0343   1.0000   0.0641
  -8.500  -0.3935   0.09171   0.08848  -0.0319   1.0000   0.0656
  -8.250  -0.3314   0.07530   0.07233  -0.0470   0.9885   0.0733
  -8.000  -0.3012   0.07273   0.06973  -0.0459   0.9862   0.0751
  -7.750  -0.2872   0.06870   0.06569  -0.0489   0.9823   0.0777
  -7.500  -0.4098   0.07226   0.06906  -0.0536   0.9827   0.0741
  -7.250  -0.3891   0.06968   0.06648  -0.0547   0.9771   0.0759
  -7.000  -0.3647   0.06464   0.06132  -0.0618   0.9722   0.0806
  -6.750  -0.3584   0.05599   0.05228  -0.0703   0.9611   0.0862
  -6.500  -0.3676   0.03984   0.03496  -0.0732   0.9497   0.0626
  -6.250  -0.3393   0.03533   0.03014  -0.0751   0.9465   0.0587
  -6.000  -0.3256   0.03086   0.02512  -0.0738   0.9378   0.0569
  -5.750  -0.2956   0.02783   0.02157  -0.0749   0.9339   0.0582
  -5.500  -0.2603   0.02544   0.01867  -0.0765   0.9315   0.0597
  -5.250  -0.2395   0.02403   0.01691  -0.0751   0.9227   0.0607
  -5.000  -0.2046   0.02217   0.01478  -0.0766   0.9195   0.0629
  -4.750  -0.1649   0.02099   0.01354  -0.0790   0.9174   0.0656
  -4.500  -0.1388   0.02016   0.01259  -0.0785   0.9100   0.0676
  -4.250  -0.1024   0.01931   0.01159  -0.0799   0.9060   0.0710
  -4.000  -0.0623   0.01812   0.01036  -0.0822   0.9037   0.0748
  -3.750  -0.0190   0.01728   0.00954  -0.0850   0.9019   0.0798
  -3.500   0.0076   0.01681   0.00900  -0.0846   0.8941   0.0849
  -3.250   0.0440   0.01609   0.00835  -0.0861   0.8896   0.0941
  -3.000   0.0846   0.01532   0.00762  -0.0884   0.8866   0.1110
  -2.750   0.1102   0.01476   0.00720  -0.0878   0.8783   0.1388
  -2.500   0.1453   0.01413   0.00667  -0.0890   0.8725   0.1749
  -2.250   0.1796   0.01357   0.00625  -0.0901   0.8663   0.2098
  -2.000   0.2063   0.01309   0.00596  -0.0897   0.8568   0.2582
  -1.750   0.2311   0.01233   0.00567  -0.0890   0.8480   0.3695
  -1.500   0.2454   0.01111   0.00561  -0.0858   0.8392   0.6725
  -1.250   0.3401   0.01066   0.00568  -0.0975   0.8371   0.9347
  -1.000   0.3972   0.01075   0.00564  -0.1030   0.8280   0.9650
  -0.750   0.4630   0.01069   0.00539  -0.1103   0.8213   0.9839
  -0.500   0.5226   0.01059   0.00517  -0.1169   0.8104   0.9980
  -0.250   0.5511   0.01052   0.00499  -0.1170   0.7989   1.0000
   0.000   0.5745   0.01047   0.00482  -0.1161   0.7880   1.0000
   0.250   0.5948   0.01046   0.00472  -0.1145   0.7756   1.0000
   0.500   0.6148   0.01047   0.00465  -0.1128   0.7633   1.0000
   0.750   0.6364   0.01050   0.00459  -0.1114   0.7516   1.0000
   1.000   0.6594   0.01053   0.00451  -0.1103   0.7401   1.0000
   1.250   0.6805   0.01058   0.00448  -0.1087   0.7274   1.0000
   1.500   0.7004   0.01066   0.00450  -0.1070   0.7145   1.0000
   1.750   0.7213   0.01075   0.00453  -0.1054   0.7017   1.0000
   2.000   0.7424   0.01084   0.00454  -0.1039   0.6885   1.0000
   2.250   0.7634   0.01094   0.00457  -0.1023   0.6746   1.0000
   2.500   0.7841   0.01106   0.00461  -0.1007   0.6601   1.0000
   2.750   0.8042   0.01118   0.00466  -0.0989   0.6448   1.0000
   3.000   0.8238   0.01132   0.00473  -0.0971   0.6289   1.0000
   3.250   0.8428   0.01146   0.00482  -0.0951   0.6117   1.0000
   3.500   0.8612   0.01162   0.00493  -0.0931   0.5931   1.0000
   3.750   0.8791   0.01180   0.00503  -0.0909   0.5728   1.0000
   4.000   0.8968   0.01202   0.00513  -0.0887   0.5518   1.0000
   4.250   0.9135   0.01225   0.00529  -0.0864   0.5293   1.0000
   4.500   0.9302   0.01253   0.00546  -0.0840   0.5069   1.0000
   4.750   0.9469   0.01285   0.00566  -0.0817   0.4857   1.0000
   5.000   0.9637   0.01320   0.00590  -0.0795   0.4655   1.0000
   5.250   0.9809   0.01358   0.00618  -0.0774   0.4472   1.0000
   5.500   0.9986   0.01398   0.00649  -0.0754   0.4308   1.0000
   5.750   1.0171   0.01438   0.00682  -0.0737   0.4164   1.0000
   6.000   1.0364   0.01481   0.00717  -0.0721   0.4037   1.0000
   6.250   1.0561   0.01525   0.00754  -0.0706   0.3921   1.0000
   6.500   1.0745   0.01564   0.00790  -0.0689   0.3798   1.0000
   6.750   1.0926   0.01601   0.00827  -0.0671   0.3680   1.0000
   7.000   1.1121   0.01644   0.00867  -0.0656   0.3581   1.0000
   7.250   1.1311   0.01684   0.00905  -0.0641   0.3485   1.0000
   7.500   1.1495   0.01722   0.00947  -0.0624   0.3391   1.0000
   7.750   1.1689   0.01768   0.00985  -0.0610   0.3303   1.0000
   8.000   1.1844   0.01798   0.01026  -0.0588   0.3208   1.0000
   8.250   1.2015   0.01839   0.01067  -0.0570   0.3120   1.0000
   8.500   1.2168   0.01874   0.01108  -0.0548   0.3040   1.0000
   8.750   1.2338   0.01918   0.01153  -0.0530   0.2967   1.0000
   9.000   1.2472   0.01951   0.01196  -0.0505   0.2888   1.0000
   9.250   1.2617   0.01995   0.01242  -0.0483   0.2811   1.0000
   9.500   1.2741   0.02031   0.01288  -0.0457   0.2729   1.0000
   9.750   1.2869   0.02075   0.01337  -0.0433   0.2647   1.0000
  10.000   1.2974   0.02119   0.01387  -0.0406   0.2554   1.0000
  10.250   1.3071   0.02164   0.01444  -0.0379   0.2447   1.0000
  10.500   1.3155   0.02218   0.01505  -0.0351   0.2328   1.0000
  10.750   1.3217   0.02282   0.01574  -0.0321   0.2171   1.0000
  11.000   1.3250   0.02369   0.01660  -0.0290   0.1958   1.0000
  11.250   1.3252   0.02492   0.01774  -0.0259   0.1631   1.0000
  11.500   1.3196   0.02675   0.01934  -0.0225   0.1306   1.0000
  11.750   1.3137   0.02880   0.02124  -0.0194   0.1128   1.0000
  12.000   1.3111   0.03077   0.02315  -0.0168   0.1025   1.0000
  12.250   1.3111   0.03265   0.02507  -0.0147   0.0948   1.0000
  12.500   1.3062   0.03498   0.02737  -0.0126   0.0893   1.0000
  12.750   1.3091   0.03683   0.02933  -0.0111   0.0842   1.0000
  13.000   1.3069   0.03916   0.03168  -0.0096   0.0798   1.0000
  13.250   1.3041   0.04162   0.03419  -0.0081   0.0760   1.0000
  13.500   1.3057   0.04381   0.03649  -0.0071   0.0720   1.0000
  13.750   1.3033   0.04643   0.03913  -0.0062   0.0684   1.0000
  14.000   1.3010   0.04909   0.04181  -0.0052   0.0653   1.0000
  14.250   1.3017   0.05160   0.04447  -0.0046   0.0618   1.0000
  14.500   1.3005   0.05435   0.04727  -0.0042   0.0588   1.0000
  14.750   1.2992   0.05707   0.04995  -0.0033   0.0556   1.0000
  15.000   1.2984   0.05999   0.05305  -0.0033   0.0528   1.0000
  15.250   1.2984   0.06281   0.05595  -0.0032   0.0503   1.0000
  15.500   1.3008   0.06518   0.05821  -0.0023   0.0472   1.0000
  15.750   1.2990   0.06841   0.06165  -0.0026   0.0456   1.0000
  16.000   1.2982   0.07156   0.06495  -0.0029   0.0437   1.0000
  16.250   1.2982   0.07458   0.06804  -0.0032   0.0418   1.0000
  16.500   1.3011   0.07715   0.07058  -0.0032   0.0401   1.0000
  16.750   1.3004   0.08036   0.07392  -0.0033   0.0385   1.0000
  17.000   1.2967   0.08414   0.07789  -0.0042   0.0373   1.0000
  17.250   1.2937   0.08788   0.08177  -0.0052   0.0361   1.0000
  17.500   1.2924   0.09136   0.08536  -0.0061   0.0350   1.0000
  17.750   1.2928   0.09456   0.08863  -0.0069   0.0341   1.0000
  18.000   1.3013   0.09635   0.09035  -0.0061   0.0327   1.0000
  18.250   1.2914   0.10141   0.09565  -0.0082   0.0323   1.0000
  18.500   1.2813   0.10664   0.10111  -0.0103   0.0318   1.0000
  18.750   1.2708   0.11205   0.10674  -0.0128   0.0313   1.0000
  19.000   1.2590   0.11781   0.11270  -0.0156   0.0309   1.0000
  19.250   1.2460   0.12392   0.11901  -0.0188   0.0304   1.0000
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