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GOE 436 AIRFOIL (goe436-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 436 AIRFOIL (goe436-il)
Reynolds number: 500,000
Max Cl/Cd: 92.5 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe436-il-500000-n5.txt
Download as CSV file: xf-goe436-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 436 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.9437   0.03448   0.03145  -0.0762   1.0000   0.0216
 -12.500  -0.9355   0.03339   0.03032  -0.0742   1.0000   0.0221
 -12.250  -0.9232   0.03194   0.02878  -0.0732   0.9994   0.0227
 -12.000  -0.9014   0.02957   0.02617  -0.0749   0.9967   0.0236
 -11.750  -0.8799   0.02698   0.02325  -0.0765   0.9938   0.0246
 -11.500  -0.8592   0.02476   0.02069  -0.0772   0.9902   0.0256
 -11.250  -0.8283   0.02458   0.02054  -0.0782   0.9878   0.0263
 -11.000  -0.7962   0.02432   0.02027  -0.0794   0.9857   0.0270
 -10.750  -0.7641   0.02389   0.01977  -0.0808   0.9838   0.0277
 -10.500  -0.7388   0.02301   0.01875  -0.0810   0.9793   0.0285
 -10.250  -0.7109   0.02187   0.01738  -0.0819   0.9760   0.0296
 -10.000  -0.6815   0.02064   0.01590  -0.0831   0.9736   0.0304
  -9.750  -0.6528   0.02025   0.01550  -0.0836   0.9699   0.0311
  -9.500  -0.6233   0.02006   0.01530  -0.0841   0.9659   0.0317
  -9.250  -0.5909   0.01988   0.01510  -0.0852   0.9630   0.0324
  -9.000  -0.5580   0.01944   0.01458  -0.0865   0.9603   0.0332
  -8.750  -0.5317   0.01884   0.01384  -0.0865   0.9537   0.0341
  -8.500  -0.5025   0.01807   0.01290  -0.0871   0.9488   0.0350
  -8.250  -0.4717   0.01727   0.01191  -0.0880   0.9454   0.0356
  -8.000  -0.4471   0.01652   0.01105  -0.0876   0.9382   0.0363
  -7.750  -0.4175   0.01602   0.01049  -0.0882   0.9326   0.0370
  -7.500  -0.3889   0.01560   0.01001  -0.0884   0.9251   0.0375
  -7.250  -0.3595   0.01516   0.00948  -0.0887   0.9156   0.0380
  -7.000  -0.3318   0.01474   0.00897  -0.0887   0.9041   0.0387
  -6.750  -0.3038   0.01435   0.00847  -0.0887   0.8926   0.0395
  -6.500  -0.2763   0.01394   0.00795  -0.0885   0.8813   0.0403
  -6.250  -0.2497   0.01352   0.00740  -0.0882   0.8695   0.0410
  -6.000  -0.2235   0.01313   0.00688  -0.0877   0.8578   0.0416
  -5.750  -0.1972   0.01279   0.00642  -0.0873   0.8470   0.0422
  -5.500  -0.1714   0.01240   0.00592  -0.0868   0.8368   0.0427
  -5.250  -0.1462   0.01198   0.00544  -0.0862   0.8261   0.0436
  -5.000  -0.1203   0.01173   0.00513  -0.0857   0.8157   0.0444
  -4.500  -0.0683   0.01139   0.00467  -0.0846   0.7923   0.0463
  -4.250  -0.0423   0.01119   0.00442  -0.0841   0.7816   0.0473
  -4.000  -0.0164   0.01099   0.00414  -0.0836   0.7708   0.0482
  -3.750   0.0094   0.01079   0.00388  -0.0830   0.7578   0.0492
  -3.500   0.0351   0.01063   0.00364  -0.0824   0.7425   0.0500
  -3.250   0.0607   0.01051   0.00343  -0.0817   0.7249   0.0506
  -3.000   0.0851   0.01024   0.00309  -0.0809   0.7050   0.0522
  -2.750   0.1099   0.01014   0.00291  -0.0802   0.6830   0.0536
  -2.500   0.1346   0.01012   0.00279  -0.0793   0.6613   0.0552
  -2.250   0.1595   0.01009   0.00266  -0.0786   0.6407   0.0567
  -2.000   0.1846   0.01006   0.00253  -0.0779   0.6229   0.0582
  -1.750   0.2100   0.01003   0.00243  -0.0773   0.6069   0.0595
  -1.500   0.2356   0.01002   0.00233  -0.0767   0.5916   0.0605
  -1.250   0.2608   0.00993   0.00220  -0.0760   0.5753   0.0632
  -1.000   0.2860   0.00991   0.00213  -0.0754   0.5557   0.0659
  -0.750   0.3109   0.00995   0.00208  -0.0747   0.5321   0.0686
  -0.500   0.3355   0.01002   0.00203  -0.0739   0.5030   0.0709
  -0.250   0.3599   0.01012   0.00200  -0.0732   0.4759   0.0731
   0.500   0.4349   0.01027   0.00200  -0.0712   0.4271   0.0926
   0.750   0.4603   0.01029   0.00203  -0.0707   0.4166   0.1081
   1.000   0.4852   0.01028   0.00208  -0.0701   0.4069   0.1439
   1.250   0.5098   0.01011   0.00213  -0.0695   0.3987   0.2284
   1.500   0.5288   0.00942   0.00222  -0.0681   0.3918   0.5188
   1.750   0.5408   0.00850   0.00240  -0.0645   0.3867   0.8679
   2.000   0.6321   0.00867   0.00261  -0.0782   0.3763   0.9904
   2.250   0.6730   0.00882   0.00270  -0.0810   0.3702   1.0000
   2.500   0.6963   0.00893   0.00277  -0.0800   0.3644   1.0000
   2.750   0.7188   0.00910   0.00286  -0.0789   0.3574   1.0000
   3.000   0.7423   0.00921   0.00295  -0.0779   0.3496   1.0000
   3.250   0.7651   0.00937   0.00304  -0.0769   0.3425   1.0000
   3.500   0.7888   0.00949   0.00315  -0.0759   0.3380   1.0000
   3.750   0.8125   0.00962   0.00326  -0.0750   0.3328   1.0000
   4.000   0.8352   0.00980   0.00338  -0.0740   0.3251   1.0000
   4.250   0.8589   0.00993   0.00350  -0.0731   0.3175   1.0000
   4.500   0.8816   0.01012   0.00363  -0.0721   0.3103   1.0000
   4.750   0.9053   0.01026   0.00376  -0.0712   0.3023   1.0000
   5.000   0.9279   0.01046   0.00391  -0.0701   0.2946   1.0000
   5.250   0.9517   0.01060   0.00406  -0.0693   0.2884   1.0000
   5.500   0.9749   0.01078   0.00422  -0.0684   0.2822   1.0000
   5.750   0.9981   0.01096   0.00439  -0.0675   0.2765   1.0000
   6.000   1.0215   0.01113   0.00457  -0.0666   0.2696   1.0000
   6.250   1.0442   0.01134   0.00476  -0.0656   0.2624   1.0000
   6.500   1.0672   0.01154   0.00496  -0.0647   0.2539   1.0000
   6.750   1.0896   0.01178   0.00518  -0.0637   0.2441   1.0000
   7.000   1.1112   0.01206   0.00541  -0.0626   0.2305   1.0000
   7.250   1.1319   0.01239   0.00568  -0.0614   0.2135   1.0000
   7.500   1.1498   0.01291   0.00605  -0.0597   0.1860   1.0000
   7.750   1.1668   0.01350   0.00650  -0.0580   0.1608   1.0000
   8.000   1.1842   0.01404   0.00696  -0.0563   0.1416   1.0000
   8.250   1.2017   0.01456   0.00741  -0.0546   0.1266   1.0000
   8.500   1.2173   0.01518   0.00793  -0.0527   0.1090   1.0000
   8.750   1.2285   0.01599   0.00858  -0.0500   0.0768   1.0000
   9.000   1.2391   0.01672   0.00920  -0.0472   0.0631   1.0000
   9.250   1.2536   0.01722   0.00971  -0.0451   0.0592   1.0000
   9.500   1.2678   0.01774   0.01025  -0.0429   0.0564   1.0000
   9.750   1.2822   0.01828   0.01081  -0.0408   0.0540   1.0000
  10.000   1.2972   0.01878   0.01137  -0.0389   0.0525   1.0000
  10.250   1.3129   0.01925   0.01191  -0.0372   0.0509   1.0000
  10.500   1.3273   0.01980   0.01251  -0.0354   0.0490   1.0000
  10.750   1.3405   0.02043   0.01318  -0.0335   0.0472   1.0000
  11.000   1.3524   0.02115   0.01394  -0.0315   0.0456   1.0000
  11.250   1.3625   0.02199   0.01484  -0.0294   0.0435   1.0000
  11.500   1.3776   0.02256   0.01548  -0.0279   0.0419   1.0000
  11.750   1.3904   0.02329   0.01626  -0.0263   0.0398   1.0000
  12.000   1.4012   0.02416   0.01717  -0.0246   0.0375   1.0000
  12.250   1.4114   0.02511   0.01816  -0.0229   0.0351   1.0000
  12.500   1.4218   0.02608   0.01918  -0.0214   0.0312   1.0000
  12.750   1.4287   0.02734   0.02044  -0.0198   0.0252   1.0000
  13.000   1.4318   0.02895   0.02202  -0.0181   0.0202   1.0000
  13.250   1.4338   0.03074   0.02384  -0.0165   0.0176   1.0000
  13.500   1.4365   0.03257   0.02573  -0.0152   0.0163   1.0000
  13.750   1.4387   0.03454   0.02779  -0.0140   0.0153   1.0000
  14.000   1.4395   0.03674   0.03008  -0.0131   0.0144   1.0000
  14.250   1.4385   0.03926   0.03268  -0.0124   0.0137   1.0000
  14.500   1.4363   0.04205   0.03557  -0.0120   0.0132   1.0000
  14.750   1.4359   0.04477   0.03840  -0.0118   0.0127   1.0000
  15.000   1.4338   0.04782   0.04156  -0.0119   0.0124   1.0000
  15.250   1.4300   0.05120   0.04506  -0.0122   0.0121   1.0000
  15.500   1.4251   0.05482   0.04879  -0.0127   0.0118   1.0000
  15.750   1.4193   0.05868   0.05275  -0.0134   0.0115   1.0000
  16.000   1.4107   0.06307   0.05726  -0.0144   0.0112   1.0000
  16.250   1.4026   0.06748   0.06178  -0.0156   0.0110   1.0000
  16.500   1.3926   0.07229   0.06670  -0.0170   0.0108   1.0000
  16.750   1.3814   0.07739   0.07191  -0.0186   0.0106   1.0000
  17.000   1.3704   0.08248   0.07711  -0.0202   0.0105   1.0000
  17.250   1.3587   0.08777   0.08251  -0.0220   0.0103   1.0000
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