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GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 217 (MVA MK.12) AIRFOIL (goe217-il)
Reynolds number: 500,000
Max Cl/Cd: 99.62 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe217-il-500000-n5.txt
Download as CSV file: xf-goe217-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 217 (MVA MK.12) AIRFOIL                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.4616   0.08357   0.08026  -0.0705   1.0000   0.0254
 -13.250  -0.5086   0.06516   0.06143  -0.0878   0.9679   0.0254
 -13.000  -0.5125   0.05829   0.05430  -0.0966   0.9307   0.0254
 -12.750  -0.5190   0.05348   0.04921  -0.1013   0.8980   0.0255
 -12.500  -0.5252   0.04964   0.04512  -0.1046   0.8741   0.0255
 -12.250  -0.5280   0.04626   0.04153  -0.1075   0.8531   0.0255
 -12.000  -0.5281   0.04323   0.03830  -0.1102   0.8331   0.0256
 -11.750  -0.5277   0.04057   0.03544  -0.1127   0.8133   0.0256
 -11.500  -0.5163   0.03832   0.03305  -0.1148   0.7946   0.0258
 -11.250  -0.5005   0.03645   0.03105  -0.1169   0.7758   0.0259
 -11.000  -0.4816   0.03476   0.02923  -0.1192   0.7575   0.0260
 -10.750  -0.4604   0.03318   0.02751  -0.1217   0.7401   0.0262
 -10.500  -0.4369   0.03167   0.02588  -0.1243   0.7245   0.0263
 -10.250  -0.4120   0.03023   0.02432  -0.1267   0.7113   0.0264
 -10.000  -0.3858   0.02893   0.02289  -0.1290   0.6981   0.0265
  -9.750  -0.3585   0.02775   0.02160  -0.1311   0.6865   0.0266
  -9.500  -0.3307   0.02668   0.02043  -0.1329   0.6735   0.0268
  -9.250  -0.3021   0.02568   0.01933  -0.1346   0.6615   0.0269
  -8.750  -0.2441   0.02393   0.01738  -0.1376   0.6364   0.0272
  -8.500  -0.2147   0.02317   0.01650  -0.1389   0.6248   0.0274
  -8.250  -0.1847   0.02243   0.01569  -0.1402   0.6140   0.0276
  -7.750  -0.1243   0.02113   0.01423  -0.1425   0.5929   0.0280
  -7.500  -0.0938   0.02056   0.01357  -0.1436   0.5823   0.0281
  -7.250  -0.0627   0.02001   0.01294  -0.1448   0.5729   0.0283
  -7.000  -0.0315   0.01950   0.01235  -0.1459   0.5626   0.0285
  -6.750   0.0003   0.01901   0.01179  -0.1471   0.5539   0.0287
  -6.500   0.0324   0.01852   0.01125  -0.1484   0.5455   0.0289
  -6.250   0.0648   0.01808   0.01073  -0.1498   0.5377   0.0291
  -6.000   0.0977   0.01764   0.01023  -0.1512   0.5313   0.0292
  -5.750   0.1309   0.01720   0.00975  -0.1526   0.5246   0.0294
  -5.500   0.1648   0.01665   0.00916  -0.1545   0.5180   0.0298
  -5.250   0.1988   0.01619   0.00866  -0.1562   0.5124   0.0302
  -5.000   0.2331   0.01575   0.00820  -0.1579   0.5071   0.0306
  -4.750   0.2670   0.01536   0.00776  -0.1595   0.5012   0.0309
  -4.500   0.3004   0.01503   0.00736  -0.1609   0.4954   0.0312
  -4.250   0.3338   0.01472   0.00700  -0.1622   0.4905   0.0316
  -4.000   0.3671   0.01442   0.00666  -0.1634   0.4861   0.0319
  -3.750   0.4001   0.01416   0.00636  -0.1645   0.4816   0.0323
  -3.500   0.4325   0.01395   0.00610  -0.1654   0.4771   0.0327
  -3.250   0.4645   0.01380   0.00587  -0.1662   0.4729   0.0331
  -3.000   0.4967   0.01361   0.00565  -0.1671   0.4694   0.0335
  -2.750   0.5293   0.01339   0.00541  -0.1680   0.4661   0.0341
  -2.500   0.5611   0.01325   0.00524  -0.1687   0.4626   0.0347
  -2.250   0.5925   0.01315   0.00511  -0.1692   0.4590   0.0355
  -2.000   0.6235   0.01309   0.00500  -0.1697   0.4554   0.0364
  -1.750   0.6541   0.01307   0.00492  -0.1701   0.4517   0.0375
  -1.500   0.6850   0.01302   0.00485  -0.1705   0.4485   0.0391
  -1.250   0.7159   0.01297   0.00479  -0.1709   0.4458   0.0410
  -1.000   0.7467   0.01293   0.00475  -0.1713   0.4431   0.0437
  -0.750   0.7819   0.01234   0.00450  -0.1732   0.4402   0.1843
  -0.500   0.8131   0.01221   0.00448  -0.1739   0.4373   0.2265
  -0.250   0.8438   0.01215   0.00449  -0.1744   0.4346   0.2588
   0.000   0.8743   0.01209   0.00453  -0.1748   0.4319   0.3001
   0.250   0.9042   0.01212   0.00462  -0.1751   0.4288   0.3333
   0.500   0.9342   0.01212   0.00470  -0.1753   0.4253   0.3575
   0.750   0.9638   0.01218   0.00478  -0.1755   0.4202   0.3739
   1.000   0.9928   0.01228   0.00488  -0.1755   0.4153   0.3873
   1.250   1.0216   0.01241   0.00499  -0.1755   0.4115   0.4018
   1.500   1.0503   0.01255   0.00515  -0.1754   0.4081   0.4146
   1.750   1.0796   0.01264   0.00526  -0.1755   0.4052   0.4230
   2.000   1.1085   0.01274   0.00538  -0.1755   0.4015   0.4287
   2.250   1.1371   0.01286   0.00550  -0.1754   0.3969   0.4336
   2.500   1.1652   0.01302   0.00562  -0.1753   0.3926   0.4382
   2.750   1.1932   0.01319   0.00575  -0.1751   0.3887   0.4421
   3.000   1.2220   0.01328   0.00588  -0.1751   0.3857   0.4458
   3.250   1.2503   0.01340   0.00603  -0.1751   0.3818   0.4500
   3.500   1.2782   0.01355   0.00619  -0.1749   0.3778   0.4553
   3.750   1.3057   0.01373   0.00635  -0.1747   0.3739   0.4613
   4.000   1.3328   0.01393   0.00652  -0.1745   0.3701   0.4664
   4.250   1.3608   0.01405   0.00670  -0.1744   0.3662   0.4712
   4.500   1.3882   0.01421   0.00689  -0.1742   0.3611   0.4755
   4.750   1.4147   0.01441   0.00708  -0.1739   0.3556   0.4796
   5.000   1.4412   0.01462   0.00727  -0.1735   0.3507   0.4831
   5.250   1.4681   0.01479   0.00745  -0.1733   0.3450   0.4858
   5.500   1.4938   0.01502   0.00766  -0.1729   0.3378   0.4884
   5.750   1.5192   0.01525   0.00790  -0.1724   0.3300   0.4915
   6.000   1.5428   0.01558   0.00820  -0.1717   0.3175   0.4948
   6.250   1.5651   0.01600   0.00854  -0.1707   0.3001   0.4980
   6.500   1.5843   0.01659   0.00901  -0.1694   0.2766   0.5008
   6.750   1.6011   0.01732   0.00959  -0.1677   0.2549   0.5036
   7.000   1.6176   0.01802   0.01020  -0.1659   0.2385   0.5062
   7.250   1.6342   0.01865   0.01077  -0.1641   0.2267   0.5089
   7.500   1.6494   0.01928   0.01137  -0.1621   0.2175   0.5118
   7.750   1.6619   0.01990   0.01198  -0.1596   0.2096   0.5147
   8.000   1.6725   0.02057   0.01266  -0.1569   0.2033   0.5173
   8.250   1.6862   0.02124   0.01335  -0.1548   0.1975   0.5201
   8.500   1.6975   0.02209   0.01420  -0.1525   0.1918   0.5228
   8.750   1.7109   0.02287   0.01500  -0.1506   0.1873   0.5258
   9.000   1.7236   0.02371   0.01586  -0.1487   0.1829   0.5290
   9.250   1.7345   0.02471   0.01688  -0.1468   0.1790   0.5319
   9.500   1.7444   0.02584   0.01804  -0.1450   0.1755   0.5347
   9.750   1.7570   0.02684   0.01910  -0.1435   0.1727   0.5376
  10.000   1.7682   0.02799   0.02031  -0.1420   0.1699   0.5406
  10.250   1.7778   0.02931   0.02168  -0.1405   0.1671   0.5436
  10.500   1.7853   0.03086   0.02328  -0.1390   0.1645   0.5466
  10.750   1.7915   0.03261   0.02507  -0.1376   0.1621   0.5498
  11.000   1.8010   0.03413   0.02666  -0.1365   0.1603   0.5532
  11.500   1.8151   0.03776   0.03043  -0.1344   0.1561   0.5595
  11.750   1.8193   0.03994   0.03269  -0.1334   0.1540   0.5625
  12.000   1.8209   0.04245   0.03526  -0.1324   0.1518   0.5655
  12.250   1.8199   0.04527   0.03814  -0.1315   0.1496   0.5685
  12.500   1.8234   0.04765   0.04061  -0.1308   0.1479   0.5718
  12.750   1.8259   0.05019   0.04322  -0.1301   0.1462   0.5750
  13.000   1.8268   0.05296   0.04607  -0.1295   0.1445   0.5779
  13.250   1.8265   0.05590   0.04910  -0.1289   0.1428   0.5808
  13.500   1.8247   0.05904   0.05233  -0.1284   0.1412   0.5839
  13.750   1.8214   0.06241   0.05577  -0.1279   0.1396   0.5873
  14.000   1.8162   0.06608   0.05951  -0.1276   0.1379   0.5906
  14.250   1.8144   0.06934   0.06285  -0.1273   0.1365   0.5941
  14.500   1.8154   0.07226   0.06585  -0.1270   0.1350   0.5976
  14.750   1.8142   0.07551   0.06918  -0.1268   0.1334   0.6006
  15.000   1.8138   0.07865   0.07240  -0.1267   0.1318   0.6034
  15.250   1.8108   0.08215   0.07598  -0.1266   0.1301   0.6064
  15.500   1.8077   0.08564   0.07954  -0.1265   0.1283   0.6095
  15.750   1.8019   0.08956   0.08351  -0.1267   0.1265   0.6126
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