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GOE 513 AIRFOIL (goe513-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 513 AIRFOIL (goe513-il)
Reynolds number: 1,000,000
Max Cl/Cd: 76.8 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe513-il-1000000-n5.txt
Download as CSV file: xf-goe513-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.6266   0.07762   0.07484  -0.1108   0.9831   0.0211
 -17.000  -0.6483   0.07081   0.06793  -0.1158   0.9825   0.0212
 -16.750  -0.6718   0.06389   0.06090  -0.1212   0.9819   0.0213
 -16.500  -0.7113   0.05579   0.05266  -0.1266   0.9798   0.0212
 -16.250  -0.7386   0.04876   0.04553  -0.1319   0.9773   0.0213
 -16.000  -0.7566   0.03871   0.03525  -0.1433   0.9754   0.0214
 -15.750  -0.7624   0.03428   0.03064  -0.1471   0.9735   0.0215
 -15.500  -0.7603   0.03154   0.02777  -0.1486   0.9717   0.0216
 -15.250  -0.7521   0.02955   0.02567  -0.1494   0.9702   0.0217
 -15.000  -0.7401   0.02786   0.02387  -0.1501   0.9689   0.0218
 -14.750  -0.7367   0.02669   0.02261  -0.1481   0.9655   0.0220
 -14.500  -0.7278   0.02554   0.02138  -0.1468   0.9625   0.0221
 -14.250  -0.7133   0.02451   0.02025  -0.1461   0.9598   0.0222
 -14.000  -0.6940   0.02345   0.01910  -0.1463   0.9577   0.0224
 -13.750  -0.6714   0.02241   0.01796  -0.1470   0.9562   0.0225
 -13.500  -0.6434   0.02157   0.01703  -0.1483   0.9550   0.0227
 -13.250  -0.6350   0.02092   0.01631  -0.1455   0.9509   0.0228
 -13.000  -0.6195   0.02024   0.01556  -0.1440   0.9467   0.0229
 -12.750  -0.5974   0.01959   0.01483  -0.1437   0.9439   0.0230
 -12.500  -0.5706   0.01897   0.01413  -0.1442   0.9415   0.0231
 -12.250  -0.5445   0.01839   0.01348  -0.1445   0.9394   0.0232
 -12.000  -0.5403   0.01801   0.01305  -0.1401   0.9344   0.0233
 -11.750  -0.5301   0.01732   0.01230  -0.1372   0.9295   0.0235
 -11.500  -0.5080   0.01672   0.01164  -0.1366   0.9254   0.0237
 -11.250  -0.4979   0.01628   0.01115  -0.1333   0.9198   0.0238
 -11.000  -0.4856   0.01590   0.01074  -0.1303   0.9136   0.0240
 -10.750  -0.4655   0.01542   0.01020  -0.1289   0.9087   0.0241
 -10.500  -0.4550   0.01511   0.00986  -0.1254   0.9010   0.0242
 -10.250  -0.4341   0.01479   0.00948  -0.1241   0.8924   0.0245
 -10.000  -0.4181   0.01447   0.00910  -0.1217   0.8796   0.0246
  -9.750  -0.3982   0.01413   0.00868  -0.1201   0.8646   0.0247
  -9.500  -0.3781   0.01385   0.00829  -0.1184   0.8456   0.0250
  -9.250  -0.3613   0.01365   0.00795  -0.1161   0.8191   0.0251
  -9.000  -0.3487   0.01353   0.00766  -0.1128   0.7905   0.0253
  -8.750  -0.3351   0.01337   0.00738  -0.1097   0.7702   0.0254
  -8.250  -0.3015   0.01303   0.00687  -0.1050   0.7452   0.0259
  -8.000  -0.2841   0.01287   0.00664  -0.1027   0.7353   0.0261
  -7.750  -0.2650   0.01267   0.00638  -0.1008   0.7262   0.0263
  -7.500  -0.2471   0.01253   0.00617  -0.0986   0.7165   0.0265
  -7.250  -0.2269   0.01236   0.00594  -0.0969   0.7076   0.0267
  -7.000  -0.2084   0.01221   0.00572  -0.0948   0.6984   0.0269
  -6.750  -0.1878   0.01204   0.00551  -0.0931   0.6901   0.0270
  -6.500  -0.1693   0.01186   0.00527  -0.0910   0.6798   0.0272
  -6.250  -0.1508   0.01166   0.00501  -0.0889   0.6663   0.0275
  -6.000  -0.1332   0.01151   0.00480  -0.0866   0.6504   0.0278
  -5.750  -0.1188   0.01145   0.00463  -0.0836   0.6237   0.0281
  -5.500  -0.1131   0.01158   0.00453  -0.0788   0.5687   0.0284
  -5.250  -0.0998   0.01161   0.00443  -0.0756   0.5402   0.0286
  -5.000  -0.0835   0.01157   0.00430  -0.0731   0.5250   0.0290
  -4.750  -0.0670   0.01151   0.00418  -0.0705   0.5152   0.0292
  -4.500  -0.0485   0.01142   0.00405  -0.0684   0.5076   0.0296
  -4.250  -0.0304   0.01135   0.00394  -0.0661   0.5005   0.0300
  -4.000  -0.0113   0.01127   0.00383  -0.0641   0.4947   0.0303
  -3.750   0.0092   0.01118   0.00371  -0.0624   0.4894   0.0307
  -3.500   0.0286   0.01112   0.00362  -0.0605   0.4823   0.0311
  -3.250   0.0480   0.01106   0.00351  -0.0586   0.4761   0.0316
  -3.000   0.0691   0.01096   0.00341  -0.0570   0.4703   0.0325
  -2.750   0.0888   0.01091   0.00333  -0.0551   0.4635   0.0332
  -2.500   0.1079   0.01089   0.00327  -0.0531   0.4558   0.0341
  -2.250   0.1287   0.01084   0.00321  -0.0515   0.4494   0.0350
  -2.000   0.1491   0.01082   0.00316  -0.0498   0.4438   0.0358
  -1.750   0.1692   0.01079   0.00312  -0.0481   0.4393   0.0374
  -1.500   0.1906   0.01075   0.00308  -0.0466   0.4358   0.0391
  -1.250   0.2116   0.01071   0.00304  -0.0450   0.4314   0.0417
  -1.000   0.2319   0.01068   0.00302  -0.0433   0.4264   0.0460
  -0.750   0.2510   0.01066   0.00299  -0.0414   0.4206   0.0553
  -0.500   0.2685   0.01036   0.00290  -0.0392   0.4169   0.1159
  -0.250   0.2847   0.01014   0.00291  -0.0368   0.4107   0.1831
   0.000   0.3040   0.01016   0.00295  -0.0350   0.4053   0.1977
   0.250   0.3236   0.01019   0.00299  -0.0332   0.4004   0.2072
   0.500   0.3446   0.01023   0.00303  -0.0317   0.3954   0.2150
   0.750   0.3648   0.01028   0.00307  -0.0301   0.3893   0.2208
   1.000   0.3846   0.01035   0.00312  -0.0284   0.3837   0.2258
   1.250   0.4058   0.01040   0.00317  -0.0269   0.3783   0.2315
   1.500   0.4257   0.01048   0.00322  -0.0253   0.3717   0.2359
   1.750   0.4451   0.01056   0.00330  -0.0235   0.3656   0.2423
   2.000   0.4652   0.01065   0.00336  -0.0219   0.3574   0.2457
   2.250   0.4846   0.01077   0.00345  -0.0202   0.3499   0.2496
   2.500   0.5052   0.01087   0.00352  -0.0188   0.3424   0.2537
   2.750   0.5242   0.01100   0.00362  -0.0170   0.3345   0.2574
   3.000   0.5440   0.01110   0.00372  -0.0155   0.3277   0.2622
   3.250   0.5633   0.01124   0.00383  -0.0138   0.3198   0.2660
   3.500   0.5829   0.01139   0.00394  -0.0122   0.3123   0.2693
   3.750   0.6025   0.01154   0.00406  -0.0107   0.3041   0.2727
   4.000   0.6218   0.01169   0.00420  -0.0091   0.2970   0.2791
   4.250   0.6413   0.01184   0.00434  -0.0076   0.2894   0.2836
   4.500   0.6597   0.01204   0.00450  -0.0059   0.2820   0.2885
   4.750   0.6793   0.01220   0.00465  -0.0045   0.2755   0.2940
   5.000   0.6979   0.01240   0.00483  -0.0028   0.2682   0.3004
   5.250   0.7177   0.01258   0.00500  -0.0015   0.2624   0.3063
   5.500   0.7368   0.01277   0.00519   0.0000   0.2554   0.3141
   5.750   0.7550   0.01300   0.00541   0.0016   0.2495   0.3225
   6.000   0.7749   0.01317   0.00560   0.0028   0.2455   0.3332
   6.250   0.7948   0.01334   0.00581   0.0041   0.2415   0.3486
   6.500   0.8141   0.01353   0.00605   0.0053   0.2371   0.3765
   7.000   1.0267   0.01345   0.00749  -0.0305   0.2241   0.9755
   7.250   1.0425   0.01381   0.00783  -0.0284   0.2210   0.9807
   7.500   1.0701   0.01418   0.00819  -0.0290   0.2174   0.9828
   7.750   1.1012   0.01449   0.00850  -0.0303   0.2158   0.9843
   8.000   1.1320   0.01479   0.00881  -0.0316   0.2142   0.9862
   8.250   1.1626   0.01514   0.00916  -0.0328   0.2122   0.9884
   8.500   1.1911   0.01551   0.00954  -0.0337   0.2102   0.9906
   8.750   1.2132   0.01587   0.00990  -0.0332   0.2084   0.9920
   9.000   1.2351   0.01628   0.01031  -0.0328   0.2062   0.9931
   9.250   1.2699   0.01669   0.01071  -0.0352   0.2035   0.9947
   9.500   1.2939   0.01710   0.01112  -0.0353   0.2010   0.9957
   9.750   1.3209   0.01742   0.01147  -0.0360   0.2002   0.9968
  10.000   1.3506   0.01777   0.01185  -0.0373   0.1992   0.9981
  10.250   1.3768   0.01815   0.01225  -0.0379   0.1972   0.9990
  10.500   1.4010   0.01857   0.01268  -0.0382   0.1945   0.9997
  10.750   1.4207   0.01902   0.01315  -0.0376   0.1929   1.0000
  11.000   1.4336   0.01951   0.01366  -0.0357   0.1915   1.0000
  11.250   1.4442   0.02012   0.01427  -0.0335   0.1877   1.0000
  11.500   1.4559   0.02071   0.01488  -0.0315   0.1861   1.0000
  11.750   1.4703   0.02118   0.01539  -0.0299   0.1848   1.0000
  12.000   1.4843   0.02169   0.01593  -0.0284   0.1834   1.0000
  12.250   1.4973   0.02227   0.01655  -0.0267   0.1810   1.0000
  12.500   1.5099   0.02290   0.01719  -0.0251   0.1791   1.0000
  12.750   1.5211   0.02362   0.01794  -0.0234   0.1770   1.0000
  13.000   1.5309   0.02445   0.01878  -0.0216   0.1740   1.0000
  13.250   1.5410   0.02531   0.01966  -0.0199   0.1709   1.0000
  13.500   1.5533   0.02604   0.02045  -0.0186   0.1704   1.0000
  13.750   1.5649   0.02685   0.02129  -0.0172   0.1684   1.0000
  14.000   1.5748   0.02778   0.02224  -0.0157   0.1647   1.0000
  14.250   1.5820   0.02893   0.02340  -0.0141   0.1610   1.0000
  14.500   1.5894   0.03010   0.02460  -0.0126   0.1583   1.0000
  14.750   1.5994   0.03112   0.02566  -0.0113   0.1557   1.0000
  15.000   1.6050   0.03249   0.02704  -0.0099   0.1505   1.0000
  15.250   1.6094   0.03397   0.02855  -0.0084   0.1469   1.0000
  15.500   1.6125   0.03561   0.03019  -0.0070   0.1406   1.0000
  15.750   1.6096   0.03779   0.03236  -0.0053   0.1335   1.0000
  16.000   1.6066   0.04006   0.03463  -0.0038   0.1256   1.0000
  16.250   1.5989   0.04281   0.03738  -0.0022   0.1174   1.0000
  16.500   1.5870   0.04606   0.04062  -0.0008   0.1087   1.0000
  16.750   1.5731   0.04970   0.04426   0.0004   0.1003   1.0000
  17.000   1.5570   0.05376   0.04834   0.0013   0.0915   1.0000
  17.250   1.5354   0.05860   0.05319   0.0019   0.0819   1.0000
  17.500   1.5061   0.06451   0.05911   0.0022   0.0706   1.0000
  17.750   1.4803   0.07013   0.06476   0.0022   0.0620   1.0000
  18.000   1.4539   0.07598   0.07065   0.0020   0.0545   1.0000
  18.500   1.4101   0.08699   0.08177   0.0010   0.0444   1.0000
  18.750   1.3706   0.09506   0.08988  -0.0002   0.0335   1.0000
  19.000   1.3555   0.10004   0.09494  -0.0011   0.0307   1.0000
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