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GOE 702 AIRFOIL (goe702-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 702 AIRFOIL (goe702-il)
Reynolds number: 500,000
Max Cl/Cd: 88.18 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe702-il-500000.txt
Download as CSV file: xf-goe702-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 702 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7882   0.05056   0.04708  -0.0864   0.9254   0.0445
 -14.250  -0.8089   0.04166   0.03773  -0.0981   0.8831   0.0447
 -14.000  -0.8371   0.03637   0.03213  -0.1021   0.8566   0.0448
 -13.750  -0.8514   0.03406   0.02962  -0.1011   0.8377   0.0450
 -13.500  -0.8613   0.03232   0.02770  -0.0985   0.8222   0.0452
 -13.000  -0.8639   0.02987   0.02490  -0.0930   0.7972   0.0460
 -12.750  -0.8568   0.02875   0.02356  -0.0911   0.7878   0.0465
 -12.500  -0.8462   0.02766   0.02230  -0.0895   0.7787   0.0468
 -12.250  -0.8340   0.02658   0.02101  -0.0878   0.7709   0.0472
 -12.000  -0.8199   0.02522   0.01959  -0.0865   0.7640   0.0478
 -11.750  -0.8016   0.02439   0.01873  -0.0855   0.7572   0.0483
 -11.500  -0.7823   0.02372   0.01797  -0.0844   0.7507   0.0489
 -11.250  -0.7621   0.02305   0.01724  -0.0834   0.7442   0.0495
 -11.000  -0.7416   0.02237   0.01646  -0.0824   0.7372   0.0502
 -10.750  -0.7207   0.02176   0.01570  -0.0814   0.7309   0.0510
 -10.500  -0.6988   0.02118   0.01498  -0.0805   0.7254   0.0517
 -10.250  -0.6758   0.02067   0.01434  -0.0797   0.7199   0.0524
 -10.000  -0.6556   0.01964   0.01327  -0.0787   0.7145   0.0533
  -9.750  -0.6326   0.01912   0.01269  -0.0779   0.7090   0.0542
  -9.500  -0.6085   0.01863   0.01218  -0.0772   0.7041   0.0550
  -9.250  -0.5841   0.01815   0.01164  -0.0765   0.6987   0.0561
  -9.000  -0.5594   0.01770   0.01108  -0.0759   0.6938   0.0571
  -8.750  -0.5343   0.01735   0.01058  -0.0752   0.6894   0.0580
  -8.500  -0.5108   0.01666   0.00989  -0.0745   0.6856   0.0593
  -8.250  -0.4854   0.01625   0.00949  -0.0739   0.6814   0.0606
  -8.000  -0.4594   0.01591   0.00911  -0.0734   0.6770   0.0621
  -7.750  -0.4332   0.01559   0.00870  -0.0729   0.6726   0.0636
  -7.500  -0.4077   0.01520   0.00821  -0.0723   0.6682   0.0651
  -7.250  -0.3819   0.01478   0.00783  -0.0718   0.6646   0.0668
  -7.000  -0.3551   0.01449   0.00752  -0.0714   0.6603   0.0686
  -6.750  -0.3280   0.01423   0.00720  -0.0709   0.6558   0.0706
  -6.500  -0.3018   0.01387   0.00681  -0.0704   0.6513   0.0729
  -6.250  -0.2748   0.01369   0.00659  -0.0700   0.6467   0.0752
  -6.000  -0.2470   0.01348   0.00636  -0.0697   0.6426   0.0779
  -5.750  -0.2201   0.01316   0.00605  -0.0693   0.6379   0.0807
  -5.500  -0.1924   0.01298   0.00586  -0.0690   0.6331   0.0837
  -5.250  -0.1645   0.01290   0.00567  -0.0686   0.6280   0.0869
  -5.000  -0.1373   0.01261   0.00544  -0.0683   0.6230   0.0907
  -4.750  -0.1090   0.01248   0.00530  -0.0680   0.6175   0.0947
  -4.500  -0.0816   0.01225   0.00505  -0.0676   0.6122   0.0989
  -4.250  -0.0537   0.01216   0.00492  -0.0674   0.6068   0.1032
  -4.000  -0.0256   0.01198   0.00473  -0.0671   0.6005   0.1077
  -3.750   0.0020   0.01179   0.00456  -0.0668   0.5937   0.1123
  -3.500   0.0301   0.01173   0.00442  -0.0665   0.5870   0.1166
  -3.250   0.0577   0.01147   0.00421  -0.0662   0.5792   0.1214
  -3.000   0.0854   0.01137   0.00406  -0.0659   0.5714   0.1260
  -2.750   0.1139   0.01129   0.00395  -0.0657   0.5627   0.1297
  -2.500   0.1408   0.01108   0.00373  -0.0653   0.5528   0.1352
  -2.250   0.1687   0.01097   0.00362  -0.0650   0.5414   0.1400
  -2.000   0.1963   0.01092   0.00349  -0.0647   0.5291   0.1443
  -1.750   0.2231   0.01079   0.00335  -0.0643   0.5152   0.1506
  -1.500   0.2505   0.01076   0.00327  -0.0640   0.5010   0.1566
  -1.250   0.2773   0.01069   0.00319  -0.0636   0.4877   0.1646
  -0.500   0.3571   0.01060   0.00314  -0.0624   0.4559   0.2180
  -0.250   0.3837   0.01061   0.00320  -0.0620   0.4475   0.2492
   0.000   0.4104   0.01067   0.00328  -0.0616   0.4405   0.2734
   0.250   0.4378   0.01071   0.00335  -0.0614   0.4345   0.2913
   0.500   0.4647   0.01081   0.00342  -0.0610   0.4286   0.3061
   0.750   0.4914   0.01093   0.00351  -0.0607   0.4232   0.3205
   1.000   0.5188   0.01095   0.00358  -0.0604   0.4186   0.3338
   1.250   0.5459   0.01103   0.00366  -0.0601   0.4136   0.3460
   1.500   0.5722   0.01113   0.00375  -0.0597   0.4088   0.3590
   1.750   0.5986   0.01125   0.00386  -0.0593   0.4045   0.3720
   2.000   0.6259   0.01128   0.00395  -0.0591   0.4010   0.3869
   2.750   0.7042   0.01148   0.00428  -0.0578   0.3898   0.4505
   3.000   0.7292   0.01151   0.00443  -0.0573   0.3862   0.4913
   3.250   0.8021   0.01056   0.00476  -0.0663   0.3817   0.9792
   3.500   0.8694   0.01076   0.00489  -0.0744   0.3772   1.0000
   3.750   0.8930   0.01095   0.00502  -0.0735   0.3741   1.0000
   4.000   0.9160   0.01120   0.00520  -0.0725   0.3708   1.0000
   4.250   0.9397   0.01140   0.00538  -0.0717   0.3680   1.0000
   4.500   0.9637   0.01153   0.00552  -0.0709   0.3656   1.0000
   4.750   0.9874   0.01168   0.00566  -0.0701   0.3627   1.0000
   5.000   1.0109   0.01185   0.00581  -0.0692   0.3598   1.0000
   5.250   1.0341   0.01204   0.00597  -0.0683   0.3569   1.0000
   5.500   1.0568   0.01230   0.00617  -0.0674   0.3540   1.0000
   5.750   1.0797   0.01260   0.00644  -0.0665   0.3511   1.0000
   6.000   1.1030   0.01275   0.00662  -0.0656   0.3491   1.0000
   6.250   1.1261   0.01292   0.00681  -0.0647   0.3466   1.0000
   6.500   1.1490   0.01311   0.00700  -0.0638   0.3440   1.0000
   6.750   1.1716   0.01330   0.00719  -0.0629   0.3413   1.0000
   7.000   1.1939   0.01354   0.00741  -0.0620   0.3388   1.0000
   7.250   1.2159   0.01385   0.00767  -0.0610   0.3361   1.0000
   7.500   1.2384   0.01417   0.00799  -0.0601   0.3336   1.0000
   7.750   1.2600   0.01436   0.00822  -0.0591   0.3316   1.0000
   8.000   1.2815   0.01456   0.00847  -0.0581   0.3292   1.0000
   8.250   1.3026   0.01479   0.00872  -0.0570   0.3267   1.0000
   8.500   1.3235   0.01504   0.00897  -0.0559   0.3245   1.0000
   8.750   1.3438   0.01530   0.00924  -0.0548   0.3221   1.0000
   9.000   1.3641   0.01564   0.00955  -0.0537   0.3195   1.0000
   9.250   1.3853   0.01604   0.00993  -0.0527   0.3168   1.0000
   9.500   1.4035   0.01629   0.01025  -0.0513   0.3151   1.0000
   9.750   1.4192   0.01656   0.01058  -0.0494   0.3128   1.0000
  10.000   1.4322   0.01683   0.01089  -0.0471   0.3099   1.0000
  10.250   1.4452   0.01714   0.01122  -0.0450   0.3069   1.0000
  10.500   1.4593   0.01755   0.01161  -0.0433   0.3038   1.0000
  10.750   1.4774   0.01805   0.01208  -0.0422   0.3005   1.0000
  11.000   1.4894   0.01852   0.01265  -0.0404   0.2982   1.0000
  11.250   1.5028   0.01903   0.01323  -0.0390   0.2952   1.0000
  11.500   1.5175   0.01958   0.01382  -0.0378   0.2925   1.0000
  11.750   1.5321   0.02017   0.01444  -0.0367   0.2899   1.0000
  12.000   1.5466   0.02082   0.01507  -0.0356   0.2869   1.0000
  12.250   1.5614   0.02150   0.01577  -0.0345   0.2838   1.0000
  12.500   1.5739   0.02227   0.01664  -0.0335   0.2812   1.0000
  12.750   1.5869   0.02307   0.01751  -0.0326   0.2781   1.0000
  13.000   1.5988   0.02395   0.01843  -0.0317   0.2747   1.0000
  13.250   1.6100   0.02492   0.01939  -0.0308   0.2713   1.0000
  13.500   1.6220   0.02588   0.02038  -0.0299   0.2680   1.0000
  13.750   1.6331   0.02695   0.02156  -0.0293   0.2650   1.0000
  14.000   1.6436   0.02809   0.02277  -0.0286   0.2617   1.0000
  14.250   1.6530   0.02931   0.02403  -0.0279   0.2582   1.0000
  14.500   1.6611   0.03062   0.02533  -0.0271   0.2546   1.0000
  14.750   1.6699   0.03197   0.02677  -0.0265   0.2515   1.0000
  15.000   1.6781   0.03340   0.02829  -0.0260   0.2478   1.0000
  15.250   1.6842   0.03500   0.02994  -0.0254   0.2439   1.0000
  15.500   1.6873   0.03687   0.03180  -0.0248   0.2397   1.0000
  15.750   1.6928   0.03868   0.03372  -0.0244   0.2352   1.0000
  16.000   1.6952   0.04082   0.03592  -0.0241   0.2298   1.0000
  16.250   1.6925   0.04341   0.03850  -0.0237   0.2245   1.0000
  16.500   1.6962   0.04553   0.04073  -0.0235   0.2197   1.0000
  16.750   1.6921   0.04846   0.04369  -0.0233   0.2131   1.0000
  17.000   1.6884   0.05139   0.04667  -0.0232   0.2077   1.0000
  17.250   1.6825   0.05463   0.04998  -0.0232   0.2009   1.0000
  17.500   1.6705   0.05860   0.05397  -0.0233   0.1935   1.0000
  17.750   1.6572   0.06283   0.05824  -0.0236   0.1857   1.0000
  18.000   1.6419   0.06735   0.06280  -0.0240   0.1779   1.0000
  18.250   1.6178   0.07307   0.06851  -0.0247   0.1691   1.0000
  18.500   1.5952   0.07870   0.07418  -0.0255   0.1597   1.0000
  18.750   1.5704   0.08473   0.08024  -0.0266   0.1507   1.0000
  19.000   1.5410   0.09146   0.08698  -0.0279   0.1412   1.0000
  19.250   1.5110   0.09840   0.09391  -0.0295   0.1315   1.0000
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