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GOE 513 AIRFOIL (goe513-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 513 AIRFOIL (goe513-il)
Reynolds number: 1,000,000
Max Cl/Cd: 86.6 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe513-il-1000000.txt
Download as CSV file: xf-goe513-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 513 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.6601   0.04406   0.04101  -0.1335   0.9827   0.0247
 -14.500  -0.6613   0.04007   0.03689  -0.1376   0.9817   0.0249
 -14.250  -0.6713   0.03746   0.03415  -0.1369   0.9782   0.0250
 -14.000  -0.6639   0.03597   0.03262  -0.1368   0.9753   0.0252
 -13.750  -0.6574   0.03406   0.03060  -0.1369   0.9731   0.0253
 -13.500  -0.6510   0.03189   0.02828  -0.1369   0.9713   0.0254
 -13.250  -0.6327   0.03075   0.02708  -0.1373   0.9702   0.0256
 -13.000  -0.6124   0.02965   0.02591  -0.1377   0.9693   0.0258
 -12.750  -0.5950   0.02831   0.02447  -0.1378   0.9684   0.0260
 -12.500  -0.5980   0.02753   0.02360  -0.1332   0.9632   0.0262
 -12.250  -0.5876   0.02639   0.02235  -0.1312   0.9602   0.0264
 -12.000  -0.5703   0.02524   0.02109  -0.1304   0.9582   0.0266
 -11.750  -0.5474   0.02391   0.01962  -0.1307   0.9567   0.0269
 -11.500  -0.5202   0.02282   0.01840  -0.1316   0.9556   0.0272
 -11.250  -0.4909   0.02193   0.01741  -0.1327   0.9544   0.0275
 -11.000  -0.4906   0.02138   0.01677  -0.1275   0.9485   0.0276
 -10.750  -0.4721   0.02062   0.01591  -0.1261   0.9450   0.0278
 -10.500  -0.4464   0.02018   0.01537  -0.1260   0.9424   0.0280
 -10.250  -0.4180   0.01942   0.01451  -0.1264   0.9402   0.0281
 -10.000  -0.3897   0.01748   0.01246  -0.1276   0.9380   0.0286
  -9.750  -0.3867   0.01700   0.01195  -0.1225   0.9307   0.0288
  -9.500  -0.3628   0.01632   0.01124  -0.1219   0.9263   0.0291
  -9.250  -0.3341   0.01571   0.01059  -0.1223   0.9230   0.0293
  -9.000  -0.3226   0.01536   0.01021  -0.1189   0.9161   0.0296
  -8.750  -0.3036   0.01493   0.00974  -0.1170   0.9095   0.0299
  -8.500  -0.2769   0.01447   0.00923  -0.1168   0.9042   0.0302
  -8.250  -0.2644   0.01416   0.00889  -0.1135   0.8943   0.0305
  -8.000  -0.2406   0.01377   0.00844  -0.1126   0.8860   0.0310
  -7.750  -0.2185   0.01338   0.00798  -0.1113   0.8737   0.0313
  -7.500  -0.1970   0.01301   0.00753  -0.1099   0.8579   0.0316
  -7.250  -0.1746   0.01273   0.00714  -0.1086   0.8392   0.0319
  -7.000  -0.1548   0.01250   0.00680  -0.1067   0.8193   0.0321
  -6.750  -0.1366   0.01233   0.00652  -0.1046   0.7995   0.0323
  -6.500  -0.1202   0.01208   0.00615  -0.1020   0.7818   0.0326
  -6.250  -0.1060   0.01169   0.00566  -0.0991   0.7664   0.0331
  -6.000  -0.0888   0.01145   0.00536  -0.0968   0.7539   0.0335
  -5.750  -0.0699   0.01125   0.00512  -0.0947   0.7434   0.0339
  -5.250  -0.0315   0.01096   0.00472  -0.0908   0.7225   0.0349
  -5.000  -0.0126   0.01086   0.00455  -0.0887   0.7120   0.0355
  -4.750   0.0074   0.01073   0.00439  -0.0869   0.7014   0.0361
  -4.500   0.0259   0.01063   0.00423  -0.0847   0.6892   0.0366
  -4.250   0.0429   0.01057   0.00410  -0.0822   0.6744   0.0370
  -4.000   0.0580   0.01042   0.00386  -0.0793   0.6549   0.0377
  -3.750   0.0666   0.01038   0.00369  -0.0750   0.6208   0.0384
  -3.500   0.0620   0.01053   0.00362  -0.0679   0.5698   0.0389
  -3.250   0.0710   0.01059   0.00354  -0.0638   0.5437   0.0396
  -3.000   0.0853   0.01062   0.00347  -0.0607   0.5266   0.0404
  -2.750   0.1019   0.01062   0.00340  -0.0582   0.5148   0.0415
  -2.500   0.1214   0.01059   0.00333  -0.0563   0.5065   0.0424
  -2.250   0.1399   0.01050   0.00321  -0.0542   0.4990   0.0446
  -2.000   0.1583   0.01047   0.00316  -0.0521   0.4924   0.0471
  -1.750   0.1795   0.01037   0.00307  -0.0505   0.4881   0.0518
  -1.500   0.1991   0.01024   0.00299  -0.0487   0.4829   0.0657
  -1.250   0.2106   0.00972   0.00290  -0.0454   0.4777   0.1859
  -1.000   0.2296   0.00973   0.00294  -0.0434   0.4725   0.2049
  -0.750   0.2508   0.00972   0.00297  -0.0419   0.4684   0.2168
  -0.500   0.2710   0.00975   0.00300  -0.0402   0.4632   0.2253
  -0.250   0.2906   0.00981   0.00305  -0.0383   0.4583   0.2314
   0.000   0.3116   0.00988   0.00308  -0.0368   0.4538   0.2363
   0.250   0.3333   0.00987   0.00310  -0.0354   0.4497   0.2430
   0.500   0.3541   0.00991   0.00314  -0.0338   0.4449   0.2484
   0.750   0.3738   0.00999   0.00319  -0.0321   0.4399   0.2523
   1.000   0.3946   0.01007   0.00324  -0.0305   0.4351   0.2553
   1.250   0.4158   0.01006   0.00325  -0.0291   0.4308   0.2609
   1.500   0.4365   0.01011   0.00330  -0.0276   0.4255   0.2671
   1.750   0.4558   0.01021   0.00336  -0.0258   0.4191   0.2712
   2.000   0.4778   0.01026   0.00341  -0.0245   0.4146   0.2762
   2.250   0.4979   0.01029   0.00345  -0.0229   0.4087   0.2813
   2.500   0.5170   0.01038   0.00352  -0.0211   0.4026   0.2857
   2.750   0.5379   0.01045   0.00358  -0.0197   0.3973   0.2899
   3.000   0.5592   0.01052   0.00364  -0.0184   0.3911   0.2936
   3.250   0.5780   0.01062   0.00372  -0.0166   0.3844   0.3005
   3.500   0.5988   0.01069   0.00380  -0.0152   0.3786   0.3068
   3.750   0.6187   0.01080   0.00389  -0.0137   0.3714   0.3123
   4.000   0.6371   0.01092   0.00401  -0.0119   0.3644   0.3214
   4.500   0.6757   0.01117   0.00426  -0.0087   0.3480   0.3438
   4.750   0.8539   0.01045   0.00517  -0.0426   0.3253   0.9514
   5.000   0.8703   0.01079   0.00546  -0.0403   0.3163   0.9657
   5.250   0.9029   0.01117   0.00579  -0.0416   0.3067   0.9728
   5.500   0.9339   0.01162   0.00616  -0.0427   0.2963   0.9786
   5.750   0.9648   0.01200   0.00649  -0.0437   0.2870   0.9824
   6.000   1.0075   0.01236   0.00679  -0.0474   0.2773   0.9844
   6.250   1.0479   0.01274   0.00709  -0.0506   0.2681   0.9870
   6.500   1.0827   0.01308   0.00739  -0.0525   0.2605   0.9898
   6.750   1.1114   0.01348   0.00775  -0.0532   0.2547   0.9929
   7.000   1.1468   0.01377   0.00799  -0.0555   0.2482   0.9942
   7.250   1.1830   0.01395   0.00817  -0.0577   0.2449   0.9958
   7.500   1.2201   0.01419   0.00839  -0.0603   0.2407   0.9979
   7.750   1.2557   0.01450   0.00866  -0.0626   0.2362   0.9998
   8.000   1.2712   0.01484   0.00899  -0.0607   0.2325   1.0000
   8.250   1.2863   0.01507   0.00924  -0.0586   0.2308   1.0000
   8.500   1.3007   0.01533   0.00952  -0.0564   0.2289   1.0000
   8.750   1.3150   0.01562   0.00983  -0.0543   0.2269   1.0000
   9.000   1.3285   0.01596   0.01017  -0.0520   0.2249   1.0000
   9.250   1.3406   0.01635   0.01056  -0.0496   0.2226   1.0000
   9.500   1.3521   0.01679   0.01101  -0.0471   0.2201   1.0000
   9.750   1.3619   0.01732   0.01154  -0.0444   0.2174   1.0000
  10.000   1.3774   0.01763   0.01188  -0.0426   0.2163   1.0000
  10.250   1.3932   0.01795   0.01224  -0.0410   0.2148   1.0000
  10.500   1.4087   0.01829   0.01261  -0.0393   0.2127   1.0000
  10.750   1.4220   0.01873   0.01307  -0.0373   0.2109   1.0000
  11.000   1.4349   0.01922   0.01357  -0.0353   0.2091   1.0000
  11.250   1.4465   0.01977   0.01413  -0.0333   0.2068   1.0000
  11.500   1.4557   0.02046   0.01483  -0.0309   0.2040   1.0000
  11.750   1.4658   0.02114   0.01553  -0.0287   0.2017   1.0000
  12.000   1.4804   0.02161   0.01605  -0.0272   0.2010   1.0000
  12.250   1.4957   0.02207   0.01655  -0.0259   0.1995   1.0000
  12.500   1.5097   0.02261   0.01714  -0.0244   0.1978   1.0000
  12.750   1.5229   0.02321   0.01776  -0.0229   0.1959   1.0000
  13.000   1.5345   0.02392   0.01851  -0.0212   0.1944   1.0000
  13.250   1.5451   0.02472   0.01933  -0.0196   0.1925   1.0000
  13.500   1.5522   0.02575   0.02037  -0.0176   0.1893   1.0000
  13.750   1.5613   0.02669   0.02134  -0.0159   0.1870   1.0000
  14.000   1.5744   0.02741   0.02212  -0.0148   0.1862   1.0000
  14.250   1.5892   0.02805   0.02281  -0.0138   0.1842   1.0000
  14.500   1.6005   0.02892   0.02373  -0.0125   0.1825   1.0000
  14.750   1.6112   0.02986   0.02469  -0.0113   0.1796   1.0000
  15.000   1.6185   0.03107   0.02592  -0.0099   0.1771   1.0000
  15.250   1.6243   0.03241   0.02730  -0.0084   0.1748   1.0000
  15.500   1.6325   0.03361   0.02854  -0.0072   0.1727   1.0000
  15.750   1.6453   0.03449   0.02948  -0.0064   0.1699   1.0000
  16.000   1.6534   0.03575   0.03076  -0.0054   0.1655   1.0000
  16.250   1.6555   0.03753   0.03255  -0.0041   0.1615   1.0000
  16.500   1.6623   0.03896   0.03402  -0.0031   0.1583   1.0000
  16.750   1.6682   0.04048   0.03560  -0.0022   0.1547   1.0000
  17.000   1.6652   0.04284   0.03795  -0.0009   0.1485   1.0000
  17.250   1.6670   0.04482   0.03996   0.0000   0.1437   1.0000
  17.500   1.6579   0.04789   0.04303   0.0011   0.1357   1.0000
  17.750   1.6553   0.05045   0.04564   0.0018   0.1309   1.0000
  18.000   1.6364   0.05476   0.04992   0.0026   0.1201   1.0000
  18.250   1.6242   0.05854   0.05373   0.0031   0.1142   1.0000
  18.500   1.5992   0.06383   0.05902   0.0034   0.1037   1.0000
  18.750   1.5861   0.06787   0.06311   0.0035   0.0989   1.0000
  19.000   1.5581   0.07372   0.06898   0.0034   0.0902   1.0000
  19.250   1.5255   0.08026   0.07553   0.0030   0.0802   1.0000
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