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GOE 477 AIRFOIL (goe477-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 477 AIRFOIL (goe477-il)
Reynolds number: 100,000
Max Cl/Cd: 54.69 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe477-il-100000-n5.txt
Download as CSV file: xf-goe477-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 477 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.2866   0.12959   0.12471  -0.0437   1.0000   0.0478
 -11.000  -0.2898   0.12768   0.12288  -0.0438   1.0000   0.0480
 -10.750  -0.2976   0.12624   0.12154  -0.0427   1.0000   0.0481
 -10.500  -0.2987   0.12389   0.11925  -0.0440   0.9963   0.0483
 -10.250  -0.2885   0.11995   0.11531  -0.0478   0.9895   0.0484
  -9.750  -0.2632   0.10789   0.10318  -0.0521   0.9802   0.0332
  -9.500  -0.2506   0.10378   0.09906  -0.0548   0.9758   0.0323
  -9.250  -0.2404   0.09976   0.09505  -0.0579   0.9703   0.0318
  -9.000  -0.2292   0.09565   0.09093  -0.0618   0.9661   0.0315
  -8.750  -0.2204   0.09160   0.08688  -0.0657   0.9602   0.0320
  -8.500  -0.2085   0.08719   0.08247  -0.0706   0.9560   0.0322
  -8.250  -0.2016   0.08319   0.07847  -0.0744   0.9490   0.0325
  -8.000  -0.1931   0.07873   0.07402  -0.0792   0.9436   0.0325
  -7.750  -0.1891   0.07486   0.07016  -0.0826   0.9357   0.0325
  -7.500  -0.1798   0.07019   0.06546  -0.0880   0.9300   0.0324
  -7.250  -0.1741   0.06543   0.06066  -0.0929   0.9228   0.0327
  -7.000  -0.1609   0.05898   0.05410  -0.1005   0.9177   0.0335
  -6.750  -0.1575   0.05312   0.04809  -0.1044   0.9097   0.0341
  -6.500  -0.1467   0.04501   0.03962  -0.1098   0.9046   0.0349
  -6.250  -0.1357   0.04194   0.03636  -0.1103   0.8994   0.0358
  -6.000  -0.1200   0.04017   0.03443  -0.1103   0.8945   0.0373
  -5.750  -0.0985   0.03811   0.03213  -0.1112   0.8910   0.0403
  -5.500  -0.0774   0.03354   0.02693  -0.1127   0.8881   0.0438
  -5.250  -0.0661   0.02992   0.02248  -0.1111   0.8824   0.0478
  -5.000  -0.0449   0.02856   0.02089  -0.1106   0.8784   0.0513
  -4.750  -0.0190   0.02753   0.01959  -0.1107   0.8755   0.0564
  -4.500   0.0087   0.02584   0.01733  -0.1109   0.8733   0.0628
  -4.250   0.0317   0.02540   0.01683  -0.1104   0.8698   0.0682
  -4.000   0.0519   0.02472   0.01571  -0.1090   0.8650   0.0738
  -3.750   0.0774   0.02408   0.01508  -0.1090   0.8617   0.0791
  -3.500   0.1061   0.02346   0.01422  -0.1091   0.8593   0.0848
  -3.250   0.1363   0.02275   0.01336  -0.1096   0.8573   0.0897
  -3.000   0.1548   0.02246   0.01301  -0.1081   0.8521   0.0924
  -2.750   0.1786   0.02210   0.01256  -0.1074   0.8480   0.0955
  -2.500   0.2066   0.02177   0.01209  -0.1073   0.8451   0.1000
  -2.250   0.2378   0.02125   0.01153  -0.1079   0.8424   0.1051
  -2.000   0.2579   0.02106   0.01134  -0.1064   0.8359   0.1084
  -1.750   0.2850   0.02070   0.01094  -0.1060   0.8305   0.1129
  -1.500   0.3183   0.02020   0.01038  -0.1066   0.8268   0.1196
  -1.250   0.3380   0.02010   0.01031  -0.1050   0.8192   0.1275
  -1.000   0.3668   0.01976   0.01000  -0.1049   0.8138   0.1434
  -0.750   0.4010   0.01928   0.00960  -0.1057   0.8102   0.1789
  -0.500   0.4199   0.01917   0.00964  -0.1040   0.8009   0.2266
  -0.250   0.4524   0.01842   0.00931  -0.1046   0.7958   0.3555
   0.000   0.5095   0.01668   0.00905  -0.1098   0.7876   1.0000
   0.250   0.5403   0.01642   0.00859  -0.1096   0.7801   1.0000
   0.500   0.5598   0.01646   0.00852  -0.1077   0.7691   1.0000
   0.750   0.5850   0.01637   0.00831  -0.1068   0.7606   1.0000
   1.000   0.6089   0.01633   0.00818  -0.1057   0.7518   1.0000
   1.250   0.6296   0.01639   0.00820  -0.1041   0.7421   1.0000
   1.500   0.6575   0.01622   0.00794  -0.1037   0.7344   1.0000
   1.750   0.6758   0.01632   0.00802  -0.1018   0.7222   1.0000
   2.000   0.6957   0.01638   0.00806  -0.1001   0.7097   1.0000
   2.250   0.7167   0.01639   0.00805  -0.0986   0.6961   1.0000
   2.500   0.7387   0.01635   0.00798  -0.0972   0.6808   1.0000
   2.750   0.7622   0.01625   0.00785  -0.0960   0.6638   1.0000
   3.000   0.7883   0.01607   0.00760  -0.0951   0.6445   1.0000
   3.250   0.8134   0.01599   0.00742  -0.0941   0.6205   1.0000
   3.500   0.8399   0.01589   0.00720  -0.0934   0.5911   1.0000
   3.750   0.8645   0.01595   0.00704  -0.0923   0.5530   1.0000
   4.000   0.8860   0.01620   0.00704  -0.0908   0.5095   1.0000
   4.250   0.9047   0.01665   0.00718  -0.0890   0.4717   1.0000
   4.500   0.9229   0.01717   0.00747  -0.0872   0.4434   1.0000
   4.750   0.9415   0.01770   0.00785  -0.0856   0.4210   1.0000
   5.000   0.9610   0.01821   0.00826  -0.0843   0.4028   1.0000
   5.250   0.9809   0.01872   0.00869  -0.0830   0.3868   1.0000
   5.500   1.0011   0.01922   0.00915  -0.0818   0.3729   1.0000
   6.000   1.0422   0.02021   0.01011  -0.0795   0.3488   1.0000
   6.250   1.0630   0.02071   0.01061  -0.0785   0.3387   1.0000
   6.500   1.0835   0.02125   0.01114  -0.0774   0.3296   1.0000
   6.750   1.1048   0.02174   0.01169  -0.0764   0.3210   1.0000
   7.000   1.1259   0.02229   0.01225  -0.0755   0.3141   1.0000
   7.250   1.1481   0.02281   0.01287  -0.0747   0.3078   1.0000
   7.500   1.1703   0.02336   0.01351  -0.0740   0.3022   1.0000
   7.750   1.1900   0.02393   0.01411  -0.0729   0.2951   1.0000
   8.000   1.2029   0.02445   0.01469  -0.0706   0.2838   1.0000
   8.250   1.2131   0.02499   0.01531  -0.0681   0.2707   1.0000
   8.500   1.2257   0.02559   0.01598  -0.0660   0.2597   1.0000
   8.750   1.2360   0.02625   0.01669  -0.0636   0.2472   1.0000
   9.000   1.2452   0.02698   0.01749  -0.0613   0.2327   1.0000
   9.250   1.2530   0.02782   0.01838  -0.0589   0.2137   1.0000
   9.500   1.2601   0.02881   0.01941  -0.0567   0.1897   1.0000
   9.750   1.2558   0.03082   0.02089  -0.0537   0.0910   1.0000
  10.000   1.2456   0.03398   0.02357  -0.0503   0.0509   1.0000
  10.250   1.2482   0.03601   0.02569  -0.0482   0.0423   1.0000
  10.500   1.2486   0.03822   0.02799  -0.0460   0.0380   1.0000
  10.750   1.2518   0.04016   0.03016  -0.0442   0.0352   1.0000
  11.000   1.2524   0.04234   0.03254  -0.0424   0.0328   1.0000
  11.250   1.2498   0.04487   0.03526  -0.0407   0.0308   1.0000
  11.500   1.2447   0.04771   0.03829  -0.0392   0.0295   1.0000
  11.750   1.2365   0.05098   0.04173  -0.0379   0.0287   1.0000
  12.000   1.2239   0.05489   0.04583  -0.0370   0.0278   1.0000
  12.250   1.2106   0.05913   0.05027  -0.0365   0.0271   1.0000
  12.500   1.2014   0.06319   0.05448  -0.0364   0.0266   1.0000
  12.750   1.1954   0.06710   0.05857  -0.0367   0.0259   1.0000
  13.000   1.1894   0.07119   0.06283  -0.0371   0.0252   1.0000
  13.250   1.1842   0.07530   0.06709  -0.0377   0.0245   1.0000
  13.500   1.1808   0.07918   0.07110  -0.0383   0.0238   1.0000
  13.750   1.1806   0.08251   0.07453  -0.0385   0.0231   1.0000
  14.000   1.1841   0.08519   0.07727  -0.0382   0.0223   1.0000
  14.250   1.1900   0.08747   0.07959  -0.0378   0.0215   1.0000
  14.500   1.1985   0.08927   0.08137  -0.0369   0.0205   1.0000
  14.750   1.2146   0.08993   0.08198  -0.0349   0.0194   1.0000
  15.000   1.2215   0.09255   0.08478  -0.0348   0.0188   1.0000
  15.250   1.2286   0.09520   0.08766  -0.0346   0.0183   1.0000
  15.500   1.2338   0.09825   0.09089  -0.0346   0.0179   1.0000
  15.750   1.2366   0.10173   0.09458  -0.0351   0.0176   1.0000
  16.000   1.2362   0.10575   0.09879  -0.0361   0.0173   1.0000
  16.250   1.2336   0.11013   0.10336  -0.0375   0.0170   1.0000
  16.500   1.2295   0.11481   0.10823  -0.0394   0.0167   1.0000
  16.750   1.2249   0.11959   0.11318  -0.0415   0.0164   1.0000
  17.000   1.2195   0.12466   0.11841  -0.0440   0.0162   1.0000
  17.250   1.2129   0.13006   0.12398  -0.0468   0.0160   1.0000
  17.500   1.2070   0.13532   0.12937  -0.0498   0.0157   1.0000
  17.750   1.1999   0.14097   0.13516  -0.0531   0.0155   1.0000
  18.000   1.1875   0.14812   0.14252  -0.0576   0.0156   1.0000
  18.250   1.1740   0.15587   0.15047  -0.0627   0.0156   1.0000
  18.500   1.1588   0.16444   0.15924  -0.0684   0.0157   1.0000
  18.750   1.1184   0.18183   0.17696  -0.0804   0.0169   1.0000
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