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GOE 532 AIRFOIL (goe532-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 532 AIRFOIL (goe532-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.69 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe532-il-1000000-n5.txt
Download as CSV file: xf-goe532-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 532 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.7488   0.02559   0.02226  -0.1040   0.9739   0.0203
 -11.750  -0.7188   0.02338   0.01985  -0.1075   0.9647   0.0205
 -11.500  -0.6833   0.02215   0.01852  -0.1105   0.9549   0.0207
 -11.250  -0.6475   0.02125   0.01752  -0.1130   0.9414   0.0209
 -11.000  -0.6152   0.02067   0.01684  -0.1144   0.9220   0.0210
 -10.750  -0.5892   0.02012   0.01617  -0.1145   0.8993   0.0212
 -10.500  -0.5657   0.01965   0.01556  -0.1140   0.8788   0.0213
 -10.250  -0.5431   0.01907   0.01484  -0.1134   0.8609   0.0215
 -10.000  -0.5206   0.01841   0.01404  -0.1128   0.8463   0.0217
  -9.750  -0.4976   0.01779   0.01327  -0.1122   0.8333   0.0219
  -9.500  -0.4745   0.01713   0.01246  -0.1115   0.8201   0.0221
  -9.250  -0.4506   0.01653   0.01172  -0.1110   0.8068   0.0223
  -9.000  -0.4267   0.01592   0.01097  -0.1104   0.7935   0.0225
  -8.750  -0.4024   0.01537   0.01028  -0.1098   0.7789   0.0227
  -8.500  -0.3777   0.01488   0.00965  -0.1092   0.7634   0.0229
  -8.250  -0.3525   0.01449   0.00912  -0.1087   0.7461   0.0232
  -8.000  -0.3274   0.01412   0.00861  -0.1081   0.7254   0.0234
  -7.750  -0.3023   0.01377   0.00811  -0.1074   0.6995   0.0235
  -7.500  -0.2774   0.01348   0.00765  -0.1068   0.6718   0.0236
  -7.250  -0.2526   0.01305   0.00706  -0.1062   0.6481   0.0238
  -7.000  -0.2275   0.01260   0.00650  -0.1056   0.6288   0.0240
  -6.750  -0.2015   0.01230   0.00610  -0.1052   0.6128   0.0242
  -6.500  -0.1751   0.01203   0.00575  -0.1047   0.6000   0.0244
  -6.250  -0.1482   0.01180   0.00545  -0.1044   0.5882   0.0247
  -6.000  -0.1213   0.01156   0.00516  -0.1040   0.5780   0.0249
  -5.750  -0.0943   0.01135   0.00488  -0.1037   0.5674   0.0251
  -5.500  -0.0672   0.01115   0.00462  -0.1033   0.5557   0.0254
  -5.250  -0.0404   0.01098   0.00436  -0.1029   0.5407   0.0256
  -5.000  -0.0134   0.01083   0.00413  -0.1025   0.5263   0.0260
  -4.750   0.0137   0.01069   0.00391  -0.1022   0.5134   0.0264
  -4.500   0.0412   0.01052   0.00369  -0.1019   0.5047   0.0267
  -4.250   0.0686   0.01038   0.00348  -0.1016   0.4958   0.0269
  -4.000   0.0962   0.01023   0.00328  -0.1013   0.4888   0.0272
  -3.750   0.1239   0.01010   0.00311  -0.1010   0.4813   0.0274
  -3.500   0.1513   0.00993   0.00289  -0.1007   0.4747   0.0277
  -3.250   0.1789   0.00976   0.00269  -0.1004   0.4685   0.0281
  -3.000   0.2066   0.00965   0.00255  -0.1002   0.4620   0.0286
  -2.750   0.2344   0.00956   0.00243  -0.0999   0.4560   0.0290
  -2.500   0.2621   0.00948   0.00232  -0.0996   0.4481   0.0295
  -2.250   0.2897   0.00944   0.00223  -0.0994   0.4399   0.0300
  -2.000   0.3177   0.00937   0.00214  -0.0991   0.4340   0.0306
  -1.750   0.3455   0.00933   0.00207  -0.0989   0.4282   0.0312
  -1.500   0.3733   0.00930   0.00201  -0.0986   0.4230   0.0318
  -1.250   0.4014   0.00922   0.00193  -0.0984   0.4193   0.0329
  -1.000   0.4293   0.00918   0.00188  -0.0982   0.4146   0.0339
  -0.750   0.4572   0.00916   0.00184  -0.0980   0.4098   0.0350
  -0.500   0.4850   0.00916   0.00182  -0.0977   0.4051   0.0363
  -0.250   0.5130   0.00912   0.00179  -0.0975   0.3999   0.0388
   0.000   0.5407   0.00912   0.00179  -0.0973   0.3941   0.0427
   0.250   0.5683   0.00911   0.00179  -0.0970   0.3885   0.0528
   0.500   0.5959   0.00903   0.00179  -0.0968   0.3821   0.0848
   0.750   0.6222   0.00876   0.00180  -0.0966   0.3735   0.2090
   1.000   0.6492   0.00862   0.00185  -0.0963   0.3652   0.2866
   1.250   0.6758   0.00861   0.00191  -0.0960   0.3533   0.3405
   1.500   0.7021   0.00861   0.00200  -0.0956   0.3379   0.4000
   1.750   0.7274   0.00864   0.00213  -0.0951   0.3139   0.4825
   2.000   0.7465   0.00932   0.00253  -0.0937   0.2312   0.5405
   2.500   0.7944   0.00972   0.00300  -0.0921   0.1851   0.6620
   2.750   0.8199   0.00979   0.00315  -0.0916   0.1788   0.7114
   3.000   0.8450   0.00986   0.00330  -0.0909   0.1736   0.7558
   3.250   0.8683   0.00980   0.00343  -0.0898   0.1693   0.8311
   3.500   0.9086   0.00973   0.00358  -0.0924   0.1666   1.0000
   3.750   0.9350   0.00989   0.00371  -0.0920   0.1644   1.0000
   4.000   0.9614   0.01005   0.00385  -0.0916   0.1624   1.0000
   4.250   0.9875   0.01023   0.00399  -0.0912   0.1603   1.0000
   4.500   1.0135   0.01042   0.00415  -0.0907   0.1578   1.0000
   4.750   1.0393   0.01061   0.00432  -0.0903   0.1548   1.0000
   5.000   1.0655   0.01077   0.00447  -0.0899   0.1535   1.0000
   5.250   1.0916   0.01092   0.00462  -0.0895   0.1523   1.0000
   5.500   1.1175   0.01109   0.00478  -0.0891   0.1509   1.0000
   5.750   1.1431   0.01127   0.00496  -0.0886   0.1490   1.0000
   6.000   1.1683   0.01147   0.00514  -0.0881   0.1462   1.0000
   6.250   1.1930   0.01171   0.00535  -0.0876   0.1424   1.0000
   6.500   1.2177   0.01193   0.00556  -0.0870   0.1394   1.0000
   6.750   1.2428   0.01211   0.00575  -0.0865   0.1371   1.0000
   7.000   1.2672   0.01234   0.00596  -0.0859   0.1321   1.0000
   7.250   1.2900   0.01267   0.00622  -0.0851   0.1211   1.0000
   7.500   1.3044   0.01355   0.00684  -0.0830   0.0852   1.0000
   7.750   1.3252   0.01396   0.00723  -0.0819   0.0810   1.0000
   8.000   1.3464   0.01432   0.00759  -0.0808   0.0779   1.0000
   8.250   1.3682   0.01462   0.00791  -0.0798   0.0765   1.0000
   8.500   1.3892   0.01495   0.00825  -0.0787   0.0751   1.0000
   8.750   1.4093   0.01531   0.00862  -0.0775   0.0736   1.0000
   9.000   1.4283   0.01570   0.00903  -0.0761   0.0722   1.0000
   9.250   1.4449   0.01610   0.00944  -0.0743   0.0707   1.0000
   9.500   1.4599   0.01652   0.00988  -0.0722   0.0692   1.0000
   9.750   1.4769   0.01686   0.01025  -0.0704   0.0686   1.0000
  10.000   1.4932   0.01724   0.01066  -0.0687   0.0680   1.0000
  10.250   1.5088   0.01766   0.01111  -0.0668   0.0672   1.0000
  10.500   1.5238   0.01812   0.01160  -0.0650   0.0664   1.0000
  10.750   1.5382   0.01863   0.01215  -0.0632   0.0656   1.0000
  11.000   1.5516   0.01920   0.01275  -0.0613   0.0647   1.0000
  11.250   1.5643   0.01984   0.01342  -0.0594   0.0638   1.0000
  11.500   1.5762   0.02054   0.01416  -0.0576   0.0630   1.0000
  11.750   1.5869   0.02135   0.01501  -0.0558   0.0620   1.0000
  12.000   1.5966   0.02227   0.01597  -0.0539   0.0611   1.0000
  12.250   1.6080   0.02314   0.01689  -0.0524   0.0607   1.0000
  12.500   1.6197   0.02403   0.01784  -0.0510   0.0603   1.0000
  12.750   1.6307   0.02502   0.01888  -0.0497   0.0598   1.0000
  13.000   1.6417   0.02604   0.01996  -0.0486   0.0588   1.0000
  13.250   1.6507   0.02727   0.02124  -0.0473   0.0583   1.0000
  13.500   1.6595   0.02856   0.02259  -0.0463   0.0574   1.0000
  13.750   1.6674   0.03000   0.02405  -0.0453   0.0561   1.0000
  14.000   1.6736   0.03163   0.02573  -0.0443   0.0550   1.0000
  14.250   1.6777   0.03354   0.02768  -0.0435   0.0538   1.0000
  14.500   1.6838   0.03533   0.02954  -0.0429   0.0533   1.0000
  14.750   1.6901   0.03717   0.03145  -0.0424   0.0528   1.0000
  15.000   1.6952   0.03919   0.03354  -0.0420   0.0523   1.0000
  15.250   1.6997   0.04132   0.03575  -0.0417   0.0514   1.0000
  15.500   1.7030   0.04365   0.03814  -0.0415   0.0507   1.0000
  15.750   1.7050   0.04615   0.04071  -0.0414   0.0499   1.0000
  16.000   1.7063   0.04879   0.04341  -0.0414   0.0490   1.0000
  16.250   1.7059   0.05168   0.04635  -0.0415   0.0480   1.0000
  16.500   1.7045   0.05473   0.04946  -0.0417   0.0472   1.0000
  16.750   1.7045   0.05767   0.05248  -0.0419   0.0466   1.0000
  17.000   1.7046   0.06064   0.05553  -0.0423   0.0460   1.0000
  17.250   1.7034   0.06384   0.05881  -0.0428   0.0454   1.0000
  17.500   1.7017   0.06714   0.06218  -0.0433   0.0445   1.0000
  17.750   1.6993   0.07057   0.06568  -0.0440   0.0437   1.0000
  18.000   1.6961   0.07417   0.06934  -0.0448   0.0427   1.0000
  18.250   1.6915   0.07805   0.07329  -0.0457   0.0420   1.0000
  18.500   1.6860   0.08209   0.07740  -0.0468   0.0411   1.0000
  18.750   1.6839   0.08568   0.08108  -0.0478   0.0404   1.0000
  19.000   1.6801   0.08962   0.08510  -0.0490   0.0395   1.0000
  19.250   1.6751   0.09377   0.08933  -0.0504   0.0385   1.0000
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