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GOE 646 AIRFOIL (goe646-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 646 AIRFOIL (goe646-il)
Reynolds number: 100,000
Max Cl/Cd: 46.39 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe646-il-100000-n5.txt
Download as CSV file: xf-goe646-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 646 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.6379   0.07507   0.06869  -0.0803   1.0000   0.0755
 -13.250  -0.6998   0.06627   0.05968  -0.0834   1.0000   0.0757
 -13.000  -0.7426   0.06071   0.05395  -0.0843   1.0000   0.0761
 -12.750  -0.7583   0.05762   0.05083  -0.0844   0.9992   0.0768
 -12.500  -0.7421   0.05546   0.04869  -0.0872   0.9950   0.0783
 -12.250  -0.7380   0.05182   0.04494  -0.0916   0.9893   0.0801
 -12.000  -0.7366   0.04779   0.04068  -0.0967   0.9822   0.0819
 -11.750  -0.7393   0.04403   0.03662  -0.1008   0.9726   0.0837
 -11.500  -0.7254   0.04201   0.03455  -0.1033   0.9654   0.0855
 -11.250  -0.7144   0.04047   0.03298  -0.1039   0.9567   0.0874
 -11.000  -0.7013   0.03874   0.03112  -0.1049   0.9493   0.0900
 -10.750  -0.6885   0.03690   0.02902  -0.1056   0.9417   0.0928
 -10.500  -0.6633   0.03571   0.02788  -0.1071   0.9371   0.0957
 -10.250  -0.6521   0.03461   0.02672  -0.1060   0.9283   0.0984
 -10.000  -0.6273   0.03319   0.02510  -0.1074   0.9235   0.1026
  -9.750  -0.6097   0.03234   0.02428  -0.1069   0.9166   0.1056
  -9.500  -0.5889   0.03137   0.02323  -0.1070   0.9100   0.1097
  -9.250  -0.5597   0.03031   0.02208  -0.1084   0.9059   0.1144
  -9.000  -0.5384   0.02955   0.02129  -0.1082   0.8997   0.1188
  -8.750  -0.5186   0.02876   0.02036  -0.1076   0.8924   0.1241
  -8.500  -0.4883   0.02797   0.01960  -0.1088   0.8883   0.1296
  -8.250  -0.4535   0.02709   0.01860  -0.1107   0.8854   0.1370
  -8.000  -0.4422   0.02668   0.01821  -0.1082   0.8752   0.1418
  -7.750  -0.4120   0.02595   0.01738  -0.1091   0.8702   0.1498
  -7.500  -0.3765   0.02527   0.01669  -0.1109   0.8668   0.1582
  -7.250  -0.3584   0.02483   0.01621  -0.1095   0.8585   0.1652
  -7.000  -0.3320   0.02433   0.01568  -0.1095   0.8518   0.1740
  -6.750  -0.2965   0.02376   0.01510  -0.1111   0.8477   0.1838
  -6.500  -0.2666   0.02329   0.01455  -0.1116   0.8421   0.1943
  -6.250  -0.2477   0.02304   0.01431  -0.1100   0.8325   0.2026
  -6.000  -0.2132   0.02261   0.01384  -0.1112   0.8278   0.2135
  -5.750  -0.1831   0.02227   0.01338  -0.1116   0.8219   0.2247
  -5.500  -0.1633   0.02212   0.01328  -0.1101   0.8124   0.2327
  -5.250  -0.1279   0.02175   0.01280  -0.1114   0.8074   0.2442
  -5.000  -0.1049   0.02162   0.01267  -0.1104   0.7987   0.2528
  -4.750  -0.0771   0.02137   0.01233  -0.1102   0.7910   0.2627
  -4.500  -0.0398   0.02109   0.01200  -0.1118   0.7862   0.2732
  -4.250  -0.0228   0.02103   0.01188  -0.1097   0.7755   0.2813
  -4.000   0.0099   0.02085   0.01167  -0.1104   0.7695   0.2915
  -3.750   0.0369   0.02072   0.01148  -0.1101   0.7620   0.3016
  -3.500   0.0620   0.02066   0.01139  -0.1094   0.7534   0.3113
  -3.250   0.0978   0.02040   0.01105  -0.1106   0.7480   0.3214
  -3.000   0.1169   0.02039   0.01104  -0.1089   0.7380   0.3287
  -2.750   0.1487   0.02018   0.01069  -0.1095   0.7315   0.3378
  -2.500   0.1765   0.02006   0.01059  -0.1093   0.7246   0.3447
  -2.250   0.2010   0.02000   0.01049  -0.1085   0.7167   0.3527
  -2.000   0.2342   0.01981   0.01021  -0.1093   0.7112   0.3608
  -1.750   0.2579   0.01977   0.01019  -0.1084   0.7035   0.3680
  -1.500   0.2853   0.01970   0.01004  -0.1082   0.6964   0.3767
  -1.250   0.3189   0.01952   0.00983  -0.1091   0.6913   0.3846
  -1.000   0.3406   0.01957   0.00989  -0.1079   0.6840   0.3926
  -0.750   0.3678   0.01954   0.00981  -0.1077   0.6778   0.4010
  -0.500   0.4004   0.01941   0.00968  -0.1083   0.6728   0.4099
  -0.250   0.4234   0.01947   0.00970  -0.1074   0.6658   0.4189
   0.000   0.4489   0.01942   0.00971  -0.1068   0.6587   0.4272
   0.250   0.4834   0.01928   0.00947  -0.1077   0.6524   0.4381
   0.500   0.5008   0.01934   0.00960  -0.1057   0.6426   0.4465
   0.750   0.5311   0.01924   0.00946  -0.1059   0.6349   0.4578
   1.000   0.5543   0.01929   0.00954  -0.1049   0.6272   0.4683
   1.250   0.5786   0.01935   0.00963  -0.1041   0.6204   0.4807
   1.500   0.6090   0.01933   0.00964  -0.1044   0.6150   0.4941
   1.750   0.6316   0.01944   0.00981  -0.1033   0.6086   0.5087
   2.000   0.6532   0.01956   0.01000  -0.1021   0.6018   0.5256
   2.250   0.6818   0.01960   0.01007  -0.1020   0.5960   0.5456
   2.500   0.7063   0.01972   0.01025  -0.1013   0.5900   0.5677
   2.750   0.7256   0.01990   0.01054  -0.0996   0.5830   0.5915
   3.000   0.7523   0.01997   0.01066  -0.0992   0.5770   0.6188
   3.250   0.7775   0.02007   0.01081  -0.0985   0.5709   0.6475
   3.500   0.7940   0.02027   0.01111  -0.0964   0.5634   0.6749
   3.750   0.8194   0.02030   0.01121  -0.0957   0.5569   0.7047
   4.000   0.8428   0.02037   0.01138  -0.0946   0.5506   0.7379
   4.250   0.8586   0.02047   0.01169  -0.0923   0.5427   0.7790
   4.750   0.9280   0.02062   0.01210  -0.0950   0.5267   1.0000
   5.000   0.9477   0.02086   0.01228  -0.0935   0.5187   1.0000
   5.250   0.9692   0.02109   0.01243  -0.0924   0.5112   1.0000
   5.500   0.9793   0.02141   0.01276  -0.0893   0.5018   1.0000
   5.750   1.0011   0.02158   0.01282  -0.0881   0.4933   1.0000
   6.000   1.0074   0.02199   0.01327  -0.0844   0.4828   1.0000
   6.250   1.0251   0.02223   0.01342  -0.0826   0.4734   1.0000
   6.500   1.0337   0.02266   0.01388  -0.0795   0.4625   1.0000
   6.750   1.0480   0.02303   0.01420  -0.0773   0.4526   1.0000
   7.000   1.0603   0.02346   0.01461  -0.0749   0.4422   1.0000
   7.250   1.0721   0.02396   0.01511  -0.0725   0.4319   1.0000
   7.500   1.0868   0.02437   0.01546  -0.0706   0.4221   1.0000
   7.750   1.0968   0.02501   0.01612  -0.0681   0.4115   1.0000
   8.000   1.1125   0.02547   0.01650  -0.0664   0.4027   1.0000
   8.250   1.1225   0.02619   0.01725  -0.0641   0.3925   1.0000
   8.500   1.1373   0.02675   0.01773  -0.0624   0.3840   1.0000
   8.750   1.1480   0.02752   0.01850  -0.0604   0.3746   1.0000
   9.000   1.1630   0.02813   0.01904  -0.0588   0.3667   1.0000
   9.250   1.1733   0.02901   0.01994  -0.0569   0.3579   1.0000
   9.500   1.1890   0.02965   0.02049  -0.0555   0.3507   1.0000
   9.750   1.1997   0.03060   0.02149  -0.0538   0.3433   1.0000
  10.000   1.2129   0.03142   0.02229  -0.0523   0.3361   1.0000
  10.250   1.2270   0.03225   0.02307  -0.0510   0.3293   1.0000
  10.500   1.2355   0.03335   0.02423  -0.0492   0.3217   1.0000
  10.750   1.2510   0.03409   0.02486  -0.0480   0.3146   1.0000
  11.000   1.2560   0.03544   0.02631  -0.0461   0.3070   1.0000
  11.250   1.2652   0.03655   0.02740  -0.0446   0.2995   1.0000
  11.500   1.2751   0.03768   0.02852  -0.0432   0.2927   1.0000
  11.750   1.2800   0.03916   0.03009  -0.0416   0.2858   1.0000
  12.000   1.2917   0.04020   0.03110  -0.0405   0.2797   1.0000
  12.250   1.2975   0.04171   0.03268  -0.0391   0.2735   1.0000
  12.500   1.3012   0.04338   0.03444  -0.0377   0.2671   1.0000
  12.750   1.3117   0.04455   0.03557  -0.0367   0.2614   1.0000
  13.000   1.3131   0.04653   0.03767  -0.0354   0.2553   1.0000
  13.250   1.3152   0.04848   0.03971  -0.0343   0.2491   1.0000
  13.500   1.3243   0.04981   0.04100  -0.0334   0.2435   1.0000
  13.750   1.3213   0.05240   0.04376  -0.0325   0.2373   1.0000
  14.000   1.3224   0.05463   0.04606  -0.0317   0.2314   1.0000
  14.250   1.3292   0.05632   0.04772  -0.0311   0.2264   1.0000
  14.500   1.3256   0.05926   0.05085  -0.0306   0.2206   1.0000
  14.750   1.3259   0.06177   0.05343  -0.0301   0.2152   1.0000
  15.000   1.3297   0.06391   0.05557  -0.0297   0.2102   1.0000
  15.250   1.3239   0.06734   0.05918  -0.0297   0.2044   1.0000
  15.500   1.3232   0.07015   0.06205  -0.0296   0.1990   1.0000
  15.750   1.3227   0.07299   0.06494  -0.0295   0.1939   1.0000
  16.000   1.3146   0.07695   0.06905  -0.0299   0.1881   1.0000
  16.250   1.3149   0.07973   0.07183  -0.0300   0.1826   1.0000
  16.500   1.3065   0.08390   0.07613  -0.0307   0.1769   1.0000
  16.750   1.2989   0.08797   0.08029  -0.0314   0.1710   1.0000
  17.000   1.2971   0.09121   0.08354  -0.0319   0.1655   1.0000
  17.250   1.2824   0.09656   0.08905  -0.0333   0.1592   1.0000
  17.500   1.2841   0.09935   0.09179  -0.0338   0.1536   1.0000
  17.750   1.2661   0.10544   0.09807  -0.0358   0.1473   1.0000
  18.000   1.2628   0.10915   0.10179  -0.0368   0.1417   1.0000
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