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GOE 601 AIRFOIL (goe601-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 601 AIRFOIL (goe601-il)
Reynolds number: 1,000,000
Max Cl/Cd: 91.16 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe601-il-1000000.txt
Download as CSV file: xf-goe601-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 601 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.9503   0.09903   0.09590  -0.0674   1.0000   0.0199
 -19.500  -0.9608   0.09404   0.09083  -0.0699   1.0000   0.0201
 -19.250  -0.9697   0.08923   0.08597  -0.0723   1.0000   0.0203
 -19.000  -0.9794   0.08445   0.08112  -0.0747   1.0000   0.0205
 -18.750  -0.9882   0.07988   0.07648  -0.0769   1.0000   0.0206
 -18.500  -0.9966   0.07542   0.07195  -0.0790   1.0000   0.0208
 -18.250  -1.0035   0.07127   0.06772  -0.0809   1.0000   0.0210
 -18.000  -1.0099   0.06728   0.06366  -0.0826   1.0000   0.0212
 -17.750  -1.0192   0.06315   0.05945  -0.0842   1.0000   0.0213
 -17.500  -1.0231   0.05969   0.05592  -0.0856   1.0000   0.0216
 -17.250  -1.0304   0.05615   0.05229  -0.0867   1.0000   0.0217
 -17.000  -1.0351   0.05297   0.04903  -0.0876   1.0000   0.0219
 -16.750  -1.0385   0.05007   0.04605  -0.0882   1.0000   0.0222
 -16.500  -1.0392   0.04753   0.04343  -0.0887   1.0000   0.0225
 -16.250  -1.0464   0.04460   0.04042  -0.0888   1.0000   0.0225
 -16.000  -1.0445   0.04255   0.03829  -0.0888   1.0000   0.0227
 -15.750  -1.0473   0.04029   0.03596  -0.0884   1.0000   0.0228
 -15.500  -1.0630   0.03713   0.03273  -0.0874   1.0000   0.0232
 -15.250  -1.0713   0.03478   0.03031  -0.0862   1.0000   0.0233
 -15.000  -1.0778   0.03276   0.02824  -0.0848   1.0000   0.0236
 -14.750  -1.0838   0.03093   0.02636  -0.0830   1.0000   0.0238
 -14.500  -1.0794   0.02941   0.02479  -0.0824   0.9997   0.0241
 -14.250  -1.0607   0.02781   0.02313  -0.0843   0.9983   0.0244
 -14.000  -1.0383   0.02665   0.02193  -0.0861   0.9968   0.0250
 -13.750  -1.0162   0.02546   0.02068  -0.0878   0.9950   0.0255
 -13.500  -0.9932   0.02429   0.01943  -0.0896   0.9934   0.0259
 -13.250  -0.9725   0.02340   0.01847  -0.0902   0.9909   0.0263
 -13.000  -0.9483   0.02266   0.01767  -0.0911   0.9885   0.0266
 -12.750  -0.9312   0.02119   0.01612  -0.0919   0.9858   0.0272
 -12.500  -0.9089   0.02002   0.01492  -0.0931   0.9838   0.0278
 -12.250  -0.8811   0.01919   0.01406  -0.0947   0.9825   0.0284
 -12.000  -0.8617   0.01853   0.01337  -0.0942   0.9782   0.0289
 -11.750  -0.8360   0.01793   0.01273  -0.0948   0.9753   0.0295
 -11.500  -0.8067   0.01733   0.01209  -0.0960   0.9732   0.0302
 -11.250  -0.7752   0.01672   0.01143  -0.0976   0.9715   0.0307
 -11.000  -0.7403   0.01621   0.01087  -0.0997   0.9701   0.0311
 -10.750  -0.7247   0.01529   0.00991  -0.0985   0.9633   0.0320
 -10.500  -0.6993   0.01462   0.00921  -0.0988   0.9583   0.0328
 -10.250  -0.6722   0.01413   0.00868  -0.0993   0.9532   0.0335
 -10.000  -0.6528   0.01374   0.00825  -0.0979   0.9441   0.0342
  -9.750  -0.6304   0.01335   0.00781  -0.0972   0.9356   0.0348
  -9.500  -0.6079   0.01301   0.00741  -0.0964   0.9254   0.0354
  -9.250  -0.5880   0.01274   0.00708  -0.0950   0.9115   0.0359
  -9.000  -0.5703   0.01227   0.00652  -0.0933   0.8946   0.0371
  -8.750  -0.5502   0.01192   0.00610  -0.0919   0.8781   0.0380
  -8.500  -0.5297   0.01165   0.00575  -0.0906   0.8638   0.0390
  -8.250  -0.5084   0.01143   0.00545  -0.0894   0.8525   0.0402
  -7.750  -0.4654   0.01098   0.00487  -0.0871   0.8357   0.0430
  -7.500  -0.4440   0.01074   0.00459  -0.0859   0.8288   0.0452
  -7.250  -0.4214   0.01052   0.00434  -0.0850   0.8232   0.0482
  -7.000  -0.4006   0.01019   0.00405  -0.0837   0.8178   0.0571
  -6.750  -0.3799   0.00985   0.00385  -0.0825   0.8125   0.0818
  -6.500  -0.3550   0.00974   0.00374  -0.0820   0.8077   0.0935
  -6.250  -0.3304   0.00959   0.00363  -0.0814   0.8036   0.1005
  -6.000  -0.3043   0.00953   0.00354  -0.0810   0.7993   0.1038
  -5.750  -0.2795   0.00940   0.00338  -0.0805   0.7950   0.1082
  -5.500  -0.2540   0.00929   0.00325  -0.0800   0.7907   0.1122
  -5.250  -0.2288   0.00916   0.00313  -0.0795   0.7873   0.1154
  -5.000  -0.2029   0.00908   0.00302  -0.0791   0.7834   0.1178
  -4.750  -0.1781   0.00894   0.00287  -0.0785   0.7786   0.1230
  -4.500  -0.1527   0.00883   0.00274  -0.0780   0.7734   0.1285
  -4.250  -0.1278   0.00869   0.00261  -0.0774   0.7692   0.1336
  -4.000  -0.1037   0.00849   0.00247  -0.0767   0.7646   0.1460
  -3.750  -0.0832   0.00805   0.00227  -0.0754   0.7600   0.2061
  -3.500  -0.0600   0.00779   0.00216  -0.0746   0.7552   0.2530
  -3.250  -0.0358   0.00759   0.00208  -0.0739   0.7510   0.2821
  -3.000  -0.0109   0.00743   0.00199  -0.0733   0.7465   0.3063
  -2.750   0.0141   0.00729   0.00191  -0.0727   0.7421   0.3298
  -2.500   0.0387   0.00714   0.00184  -0.0721   0.7375   0.3585
  -2.250   0.0625   0.00693   0.00178  -0.0712   0.7324   0.3960
  -2.000   0.0873   0.00681   0.00175  -0.0706   0.7273   0.4298
  -1.750   0.1133   0.00677   0.00173  -0.0701   0.7226   0.4498
  -1.500   0.1397   0.00673   0.00172  -0.0698   0.7177   0.4648
  -1.250   0.1656   0.00668   0.00170  -0.0693   0.7118   0.4791
  -1.000   0.1914   0.00666   0.00167  -0.0688   0.7058   0.4903
  -0.750   0.2182   0.00665   0.00167  -0.0685   0.7005   0.5003
  -0.500   0.2439   0.00660   0.00165  -0.0680   0.6940   0.5092
  -0.250   0.2695   0.00662   0.00163  -0.0675   0.6867   0.5170
   0.000   0.2955   0.00658   0.00162  -0.0670   0.6794   0.5246
   0.250   0.3206   0.00659   0.00161  -0.0664   0.6717   0.5326
   0.500   0.3463   0.00657   0.00161  -0.0659   0.6639   0.5408
   0.750   0.3708   0.00658   0.00161  -0.0651   0.6552   0.5501
   1.000   0.3959   0.00656   0.00162  -0.0645   0.6464   0.5609
   1.250   0.4197   0.00659   0.00164  -0.0636   0.6368   0.5727
   1.500   0.4442   0.00657   0.00166  -0.0628   0.6270   0.5856
   1.750   0.4671   0.00657   0.00169  -0.0618   0.6160   0.6026
   2.000   0.4886   0.00659   0.00173  -0.0604   0.6027   0.6265
   2.250   0.5096   0.00659   0.00178  -0.0589   0.5882   0.6536
   2.750   0.5489   0.00664   0.00192  -0.0554   0.5556   0.7124
   3.000   0.5656   0.00669   0.00201  -0.0529   0.5358   0.7471
   3.250   0.5800   0.00677   0.00212  -0.0500   0.5095   0.7854
   3.500   0.5881   0.00693   0.00227  -0.0458   0.4732   0.8271
   3.750   0.5926   0.00722   0.00250  -0.0409   0.4215   0.8747
   4.000   0.6122   0.00772   0.00286  -0.0395   0.3666   0.9219
   4.250   0.6588   0.00823   0.00324  -0.0440   0.3335   0.9475
   4.500   0.7095   0.00865   0.00356  -0.0494   0.3132   0.9603
   4.750   0.7492   0.00899   0.00383  -0.0522   0.3000   0.9705
   5.000   0.7826   0.00925   0.00406  -0.0536   0.2910   0.9792
   5.250   0.8166   0.00952   0.00429  -0.0551   0.2826   0.9848
   5.500   0.8515   0.00975   0.00449  -0.0569   0.2749   0.9895
   5.750   0.8837   0.01003   0.00472  -0.0581   0.2662   0.9942
   6.000   0.9200   0.01025   0.00491  -0.0602   0.2574   0.9975
   6.250   0.9558   0.01051   0.00513  -0.0622   0.2484   0.9996
   6.500   0.9699   0.01064   0.00525  -0.0596   0.2421   1.0000
   6.750   0.9770   0.01083   0.00540  -0.0556   0.2355   1.0000
   7.000   0.9894   0.01098   0.00556  -0.0526   0.2291   1.0000
   7.250   0.9995   0.01124   0.00576  -0.0492   0.2188   1.0000
   7.500   1.0120   0.01150   0.00598  -0.0464   0.2070   1.0000
   7.750   1.0234   0.01185   0.00626  -0.0435   0.1923   1.0000
   8.000   1.0317   0.01237   0.00664  -0.0401   0.1688   1.0000
   8.250   1.0307   0.01332   0.00732  -0.0353   0.1254   1.0000
   8.500   1.0140   0.01513   0.00867  -0.0285   0.0515   1.0000
   8.750   1.0237   0.01587   0.00933  -0.0258   0.0390   1.0000
   9.000   1.0385   0.01640   0.00985  -0.0240   0.0358   1.0000
   9.250   1.0533   0.01695   0.01040  -0.0222   0.0342   1.0000
   9.500   1.0674   0.01757   0.01103  -0.0204   0.0324   1.0000
   9.750   1.0833   0.01810   0.01159  -0.0189   0.0318   1.0000
  10.000   1.0991   0.01866   0.01218  -0.0175   0.0311   1.0000
  10.250   1.1142   0.01928   0.01282  -0.0160   0.0304   1.0000
  10.500   1.1287   0.01996   0.01352  -0.0145   0.0296   1.0000
  10.750   1.1416   0.02075   0.01434  -0.0129   0.0289   1.0000
  11.000   1.1535   0.02162   0.01525  -0.0113   0.0283   1.0000
  11.250   1.1634   0.02266   0.01634  -0.0095   0.0277   1.0000
  11.500   1.1772   0.02346   0.01718  -0.0083   0.0274   1.0000
  11.750   1.1906   0.02431   0.01807  -0.0070   0.0271   1.0000
  12.000   1.2037   0.02519   0.01899  -0.0058   0.0266   1.0000
  12.250   1.2151   0.02621   0.02006  -0.0046   0.0263   1.0000
  12.500   1.2263   0.02727   0.02116  -0.0033   0.0259   1.0000
  12.750   1.2365   0.02842   0.02235  -0.0021   0.0255   1.0000
  13.000   1.2457   0.02966   0.02364  -0.0009   0.0250   1.0000
  13.250   1.2539   0.03103   0.02505   0.0004   0.0247   1.0000
  13.500   1.2597   0.03262   0.02669   0.0016   0.0243   1.0000
  13.750   1.2622   0.03452   0.02865   0.0030   0.0240   1.0000
  14.000   1.2569   0.03714   0.03136   0.0045   0.0235   1.0000
  14.250   1.2621   0.03896   0.03324   0.0054   0.0234   1.0000
  14.500   1.2728   0.04033   0.03467   0.0060   0.0232   1.0000
  14.750   1.2809   0.04197   0.03636   0.0066   0.0229   1.0000
  15.000   1.2858   0.04395   0.03841   0.0072   0.0227   1.0000
  15.250   1.2891   0.04615   0.04068   0.0077   0.0225   1.0000
  15.500   1.2941   0.04825   0.04284   0.0081   0.0221   1.0000
  15.750   1.2964   0.05066   0.04532   0.0084   0.0219   1.0000
  16.000   1.2989   0.05311   0.04783   0.0086   0.0216   1.0000
  16.250   1.3021   0.05557   0.05035   0.0086   0.0213   1.0000
  16.500   1.3015   0.05851   0.05335   0.0086   0.0210   1.0000
  16.750   1.2995   0.06166   0.05657   0.0084   0.0210   1.0000
  17.000   1.2987   0.06473   0.05970   0.0081   0.0207   1.0000
  17.250   1.2959   0.06811   0.06314   0.0077   0.0204   1.0000
  17.500   1.2892   0.07201   0.06711   0.0071   0.0202   1.0000
  17.750   1.2760   0.07664   0.07182   0.0065   0.0198   1.0000
  18.000   1.2747   0.08001   0.07527   0.0058   0.0197   1.0000
  18.250   1.2740   0.08338   0.07872   0.0050   0.0196   1.0000
  18.500   1.2740   0.08678   0.08221   0.0040   0.0195   1.0000
  18.750   1.2724   0.09038   0.08589   0.0029   0.0193   1.0000
  19.000   1.2704   0.09409   0.08967   0.0017   0.0190   1.0000
  19.250   1.2673   0.09789   0.09355   0.0005   0.0188   1.0000
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