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GOE 526 AIRFOIL (goe526-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 526 AIRFOIL (goe526-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.58 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe526-il-1000000-n5.txt
Download as CSV file: xf-goe526-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 526 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -1.1203   0.03353   0.03033  -0.1057   1.0000   0.0224
 -15.750  -1.1362   0.03126   0.02793  -0.1029   1.0000   0.0224
 -15.500  -1.1521   0.02987   0.02645  -0.0979   1.0000   0.0225
 -15.250  -1.1471   0.02866   0.02516  -0.0957   0.9992   0.0228
 -15.000  -1.1264   0.02723   0.02362  -0.0966   0.9966   0.0230
 -14.750  -1.1071   0.02597   0.02224  -0.0968   0.9926   0.0232
 -14.500  -1.0866   0.02492   0.02109  -0.0968   0.9889   0.0235
 -14.250  -1.0627   0.02400   0.02008  -0.0973   0.9856   0.0238
 -14.000  -1.0374   0.02306   0.01902  -0.0979   0.9831   0.0240
 -13.750  -1.0144   0.02223   0.01809  -0.0979   0.9790   0.0242
 -13.500  -0.9906   0.02129   0.01705  -0.0981   0.9750   0.0243
 -13.250  -0.9640   0.02024   0.01593  -0.0990   0.9721   0.0248
 -13.000  -0.9339   0.01946   0.01509  -0.1003   0.9696   0.0251
 -12.750  -0.9076   0.01879   0.01435  -0.1006   0.9638   0.0253
 -12.500  -0.8775   0.01815   0.01365  -0.1016   0.9590   0.0256
 -12.250  -0.8478   0.01757   0.01300  -0.1024   0.9539   0.0260
 -12.000  -0.8212   0.01701   0.01236  -0.1026   0.9461   0.0262
 -11.750  -0.7938   0.01648   0.01174  -0.1028   0.9384   0.0265
 -11.500  -0.7689   0.01601   0.01119  -0.1025   0.9277   0.0268
 -11.250  -0.7441   0.01561   0.01070  -0.1020   0.9166   0.0271
 -11.000  -0.7202   0.01520   0.01019  -0.1013   0.9045   0.0274
 -10.750  -0.6969   0.01482   0.00971  -0.1005   0.8916   0.0276
 -10.500  -0.6739   0.01445   0.00923  -0.0996   0.8783   0.0278
 -10.250  -0.6504   0.01414   0.00882  -0.0987   0.8654   0.0280
 -10.000  -0.6284   0.01372   0.00829  -0.0976   0.8528   0.0283
  -9.750  -0.6057   0.01334   0.00783  -0.0966   0.8411   0.0287
  -9.500  -0.5820   0.01301   0.00743  -0.0958   0.8315   0.0290
  -9.000  -0.5335   0.01245   0.00674  -0.0943   0.8135   0.0297
  -8.750  -0.5089   0.01221   0.00643  -0.0935   0.8048   0.0302
  -8.500  -0.4837   0.01197   0.00614  -0.0929   0.7977   0.0306
  -8.250  -0.4586   0.01173   0.00584  -0.0923   0.7907   0.0310
  -8.000  -0.4334   0.01150   0.00554  -0.0916   0.7844   0.0314
  -7.750  -0.4076   0.01128   0.00527  -0.0911   0.7781   0.0318
  -7.500  -0.3819   0.01108   0.00501  -0.0905   0.7716   0.0321
  -7.250  -0.3565   0.01083   0.00471  -0.0899   0.7661   0.0326
  -7.000  -0.3305   0.01059   0.00445  -0.0894   0.7610   0.0332
  -6.750  -0.3046   0.01039   0.00422  -0.0889   0.7550   0.0339
  -6.500  -0.2788   0.01022   0.00401  -0.0883   0.7483   0.0345
  -6.250  -0.2525   0.01005   0.00380  -0.0879   0.7408   0.0352
  -6.000  -0.2264   0.00991   0.00361  -0.0873   0.7336   0.0359
  -5.750  -0.1998   0.00977   0.00343  -0.0869   0.7278   0.0367
  -5.500  -0.1735   0.00959   0.00324  -0.0864   0.7214   0.0378
  -5.000  -0.1207   0.00931   0.00291  -0.0855   0.7086   0.0401
  -4.750  -0.0941   0.00920   0.00277  -0.0851   0.7016   0.0414
  -4.500  -0.0677   0.00909   0.00262  -0.0846   0.6948   0.0427
  -4.250  -0.0410   0.00895   0.00249  -0.0842   0.6881   0.0446
  -4.000  -0.0142   0.00885   0.00237  -0.0838   0.6825   0.0464
  -3.750   0.0126   0.00877   0.00226  -0.0834   0.6775   0.0482
  -3.500   0.0395   0.00864   0.00215  -0.0830   0.6720   0.0510
  -3.250   0.0663   0.00856   0.00205  -0.0826   0.6658   0.0536
  -3.000   0.0930   0.00847   0.00196  -0.0822   0.6605   0.0565
  -2.750   0.1201   0.00837   0.00187  -0.0819   0.6551   0.0599
  -2.500   0.1468   0.00830   0.00179  -0.0815   0.6483   0.0633
  -2.250   0.1734   0.00823   0.00172  -0.0810   0.6416   0.0678
  -2.000   0.2002   0.00816   0.00166  -0.0806   0.6341   0.0728
  -1.750   0.2265   0.00811   0.00161  -0.0801   0.6268   0.0793
  -1.500   0.2533   0.00803   0.00156  -0.0798   0.6193   0.0874
  -1.250   0.2792   0.00801   0.00153  -0.0792   0.6086   0.0955
  -1.000   0.3053   0.00799   0.00150  -0.0787   0.5953   0.1042
  -0.750   0.3304   0.00801   0.00149  -0.0780   0.5769   0.1144
  -0.500   0.3553   0.00805   0.00149  -0.0772   0.5565   0.1232
  -0.250   0.3802   0.00812   0.00150  -0.0765   0.5346   0.1299
   0.000   0.4047   0.00821   0.00152  -0.0757   0.5124   0.1373
   0.250   0.4291   0.00832   0.00156  -0.0749   0.4905   0.1439
   0.500   0.4536   0.00842   0.00160  -0.0741   0.4698   0.1504
   0.750   0.4778   0.00854   0.00165  -0.0733   0.4495   0.1577
   1.250   0.5269   0.00873   0.00177  -0.0718   0.4188   0.1765
   1.500   0.5518   0.00876   0.00183  -0.0711   0.4091   0.1938
   1.750   0.5770   0.00878   0.00189  -0.0704   0.4014   0.2168
   2.000   0.6013   0.00877   0.00195  -0.0697   0.3926   0.2560
   2.250   0.6249   0.00870   0.00203  -0.0688   0.3849   0.3225
   2.750   0.6595   0.00791   0.00221  -0.0646   0.3715   0.6912
   3.000   0.6835   0.00747   0.00243  -0.0635   0.3655   0.9375
   3.250   0.7349   0.00769   0.00262  -0.0686   0.3561   0.9622
   3.500   0.7727   0.00785   0.00275  -0.0707   0.3497   0.9709
   3.750   0.8090   0.00802   0.00288  -0.0725   0.3420   0.9769
   4.000   0.8427   0.00822   0.00303  -0.0738   0.3328   0.9836
   4.250   0.8810   0.00847   0.00320  -0.0762   0.3189   0.9883
   4.500   0.9130   0.00866   0.00335  -0.0771   0.3082   0.9916
   4.750   0.9443   0.00889   0.00350  -0.0780   0.2945   0.9941
   5.000   0.9796   0.00912   0.00367  -0.0798   0.2811   0.9967
   5.250   1.0123   0.00941   0.00385  -0.0810   0.2619   0.9987
   5.500   1.0411   0.00980   0.00410  -0.0815   0.2361   1.0000
   5.750   1.0512   0.01030   0.00440  -0.0782   0.2001   1.0000
   6.000   1.0629   0.01073   0.00470  -0.0750   0.1779   1.0000
   6.250   1.0778   0.01102   0.00494  -0.0725   0.1678   1.0000
   6.500   1.0941   0.01127   0.00516  -0.0703   0.1607   1.0000
   6.750   1.1104   0.01152   0.00538  -0.0680   0.1553   1.0000
   7.000   1.1267   0.01176   0.00561  -0.0657   0.1503   1.0000
   7.250   1.1442   0.01196   0.00581  -0.0637   0.1470   1.0000
   7.500   1.1587   0.01217   0.00602  -0.0611   0.1431   1.0000
   7.750   1.1721   0.01242   0.00625  -0.0583   0.1385   1.0000
   8.000   1.1871   0.01267   0.00649  -0.0559   0.1347   1.0000
   8.250   1.2034   0.01291   0.00674  -0.0537   0.1296   1.0000
   8.500   1.2187   0.01322   0.00703  -0.0515   0.1239   1.0000
   8.750   1.2351   0.01353   0.00732  -0.0495   0.1185   1.0000
   9.000   1.2497   0.01393   0.00768  -0.0473   0.1096   1.0000
   9.250   1.2628   0.01443   0.00811  -0.0450   0.0973   1.0000
   9.500   1.2768   0.01493   0.00856  -0.0429   0.0889   1.0000
   9.750   1.2911   0.01543   0.00903  -0.0408   0.0825   1.0000
  10.000   1.3048   0.01598   0.00956  -0.0388   0.0773   1.0000
  10.250   1.3205   0.01645   0.01005  -0.0372   0.0740   1.0000
  10.500   1.3355   0.01698   0.01058  -0.0355   0.0709   1.0000
  10.750   1.3494   0.01759   0.01119  -0.0337   0.0676   1.0000
  11.000   1.3648   0.01813   0.01175  -0.0322   0.0653   1.0000
  11.250   1.3797   0.01873   0.01237  -0.0307   0.0629   1.0000
  11.500   1.3928   0.01945   0.01310  -0.0291   0.0600   1.0000
  11.750   1.4065   0.02016   0.01382  -0.0276   0.0578   1.0000
  12.000   1.4209   0.02085   0.01454  -0.0262   0.0559   1.0000
  12.250   1.4333   0.02169   0.01540  -0.0248   0.0533   1.0000
  12.500   1.4449   0.02261   0.01633  -0.0233   0.0509   1.0000
  12.750   1.4582   0.02345   0.01719  -0.0221   0.0491   1.0000
  13.000   1.4699   0.02441   0.01818  -0.0209   0.0471   1.0000
  13.250   1.4801   0.02551   0.01930  -0.0195   0.0451   1.0000
  13.500   1.4914   0.02656   0.02038  -0.0184   0.0437   1.0000
  13.750   1.5026   0.02764   0.02150  -0.0173   0.0423   1.0000
  14.000   1.5125   0.02885   0.02274  -0.0162   0.0410   1.0000
  14.250   1.5204   0.03023   0.02415  -0.0151   0.0393   1.0000
  14.500   1.5294   0.03155   0.02551  -0.0141   0.0382   1.0000
  14.750   1.5383   0.03292   0.02694  -0.0132   0.0373   1.0000
  15.000   1.5460   0.03444   0.02849  -0.0123   0.0358   1.0000
  15.250   1.5520   0.03611   0.03020  -0.0114   0.0346   1.0000
  15.500   1.5586   0.03778   0.03192  -0.0106   0.0340   1.0000
  15.750   1.5640   0.03961   0.03381  -0.0099   0.0329   1.0000
  16.000   1.5699   0.04144   0.03570  -0.0093   0.0321   1.0000
  16.250   1.5744   0.04342   0.03773  -0.0087   0.0312   1.0000
  16.500   1.5779   0.04557   0.03993  -0.0082   0.0303   1.0000
  16.750   1.5799   0.04793   0.04234  -0.0078   0.0295   1.0000
  17.000   1.5814   0.05040   0.04488  -0.0076   0.0287   1.0000
  17.250   1.5838   0.05282   0.04737  -0.0074   0.0281   1.0000
  17.500   1.5847   0.05545   0.05006  -0.0073   0.0270   1.0000
  17.750   1.5844   0.05827   0.05295  -0.0073   0.0263   1.0000
  18.000   1.5831   0.06129   0.05604  -0.0075   0.0257   1.0000
  18.250   1.5791   0.06468   0.05949  -0.0078   0.0249   1.0000
  18.500   1.5775   0.06783   0.06273  -0.0081   0.0243   1.0000
  18.750   1.5745   0.07122   0.06620  -0.0086   0.0238   1.0000
  19.000   1.5697   0.07487   0.06993  -0.0093   0.0228   1.0000
  19.250   1.5636   0.07877   0.07389  -0.0101   0.0221   1.0000
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