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GOE 223 (MVA H.34) AIRFOIL (goe223-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 223 (MVA H.34) AIRFOIL (goe223-il)
Reynolds number: 500,000
Max Cl/Cd: 95.51 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe223-il-500000.txt
Download as CSV file: xf-goe223-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 223 (MVA H.34) 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.0764   0.10112   0.09859  -0.0878   0.8687   0.0354
 -12.250  -0.4200   0.05671   0.05350  -0.1172   0.8947   0.0277
 -12.000  -0.4213   0.05332   0.05003  -0.1194   0.8868   0.0279
 -11.750  -0.4256   0.04971   0.04629  -0.1223   0.8789   0.0280
 -11.500  -0.4286   0.04622   0.04266  -0.1255   0.8711   0.0282
 -11.250  -0.3966   0.04796   0.04453  -0.1248   0.8651   0.0310
 -11.000  -0.4085   0.04302   0.03935  -0.1294   0.8572   0.0303
 -10.750  -0.4158   0.03744   0.03337  -0.1369   0.8489   0.0294
 -10.500  -0.4099   0.03342   0.02890  -0.1400   0.8429   0.0289
 -10.250  -0.3935   0.03101   0.02626  -0.1416   0.8368   0.0291
 -10.000  -0.3739   0.02909   0.02411  -0.1427   0.8313   0.0295
  -9.750  -0.3524   0.02742   0.02221  -0.1436   0.8269   0.0299
  -9.500  -0.3290   0.02607   0.02067  -0.1445   0.8223   0.0306
  -9.250  -0.3042   0.02501   0.01942  -0.1452   0.8175   0.0314
  -9.000  -0.2782   0.02430   0.01847  -0.1459   0.8131   0.0319
  -8.750  -0.2530   0.02304   0.01698  -0.1464   0.8089   0.0324
  -8.500  -0.2290   0.02115   0.01509  -0.1463   0.8042   0.0329
  -8.250  -0.2037   0.02003   0.01398  -0.1464   0.7993   0.0335
  -8.000  -0.1775   0.01927   0.01319  -0.1466   0.7947   0.0343
  -7.750  -0.1508   0.01858   0.01247  -0.1468   0.7899   0.0351
  -7.500  -0.1240   0.01788   0.01173  -0.1470   0.7847   0.0357
  -7.250  -0.0969   0.01723   0.01102  -0.1472   0.7798   0.0362
  -7.000  -0.0695   0.01665   0.01037  -0.1475   0.7750   0.0368
  -6.750  -0.0417   0.01612   0.00981  -0.1478   0.7694   0.0374
  -6.500  -0.0133   0.01574   0.00935  -0.1482   0.7637   0.0380
  -6.250   0.0140   0.01503   0.00858  -0.1486   0.7583   0.0385
  -6.000   0.0417   0.01426   0.00782  -0.1493   0.7516   0.0392
  -5.750   0.0703   0.01368   0.00718  -0.1499   0.7449   0.0399
  -5.500   0.0994   0.01318   0.00665  -0.1506   0.7376   0.0407
  -5.250   0.1285   0.01276   0.00617  -0.1512   0.7297   0.0417
  -5.000   0.1578   0.01240   0.00575  -0.1518   0.7215   0.0429
  -4.750   0.1870   0.01208   0.00534  -0.1523   0.7121   0.0439
  -4.500   0.2161   0.01181   0.00499  -0.1528   0.7009   0.0447
  -4.250   0.2450   0.01153   0.00462  -0.1532   0.6878   0.0458
  -4.000   0.2736   0.01130   0.00429  -0.1535   0.6721   0.0479
  -3.750   0.3018   0.01116   0.00403  -0.1537   0.6533   0.0504
  -3.500   0.3296   0.01105   0.00381  -0.1538   0.6330   0.0568
  -3.250   0.3575   0.01060   0.00349  -0.1544   0.6138   0.1281
  -3.000   0.3856   0.00976   0.00321  -0.1556   0.5976   0.3261
  -2.750   0.4135   0.00987   0.00327  -0.1556   0.5843   0.3512
  -2.500   0.4412   0.01003   0.00335  -0.1556   0.5725   0.3676
  -2.250   0.4687   0.01023   0.00342  -0.1556   0.5618   0.3786
  -2.000   0.4965   0.01037   0.00353  -0.1556   0.5526   0.3886
  -1.750   0.5243   0.01056   0.00360  -0.1557   0.5453   0.3969
  -1.500   0.5526   0.01067   0.00371  -0.1558   0.5390   0.4046
  -1.250   0.5805   0.01084   0.00378  -0.1559   0.5334   0.4100
  -1.000   0.6087   0.01094   0.00383  -0.1560   0.5286   0.4147
  -0.750   0.6370   0.01102   0.00393  -0.1562   0.5236   0.4205
  -0.500   0.6649   0.01119   0.00404  -0.1562   0.5186   0.4274
  -0.250   0.6925   0.01134   0.00412  -0.1563   0.5144   0.4329
   0.000   0.7208   0.01142   0.00423  -0.1565   0.5110   0.4384
   0.250   0.7492   0.01151   0.00432  -0.1566   0.5074   0.4435
   0.500   0.7772   0.01162   0.00438  -0.1568   0.5035   0.4469
   0.750   0.8048   0.01169   0.00443  -0.1569   0.4997   0.4503
   1.000   0.8323   0.01181   0.00453  -0.1570   0.4960   0.4537
   1.250   0.8605   0.01186   0.00461  -0.1571   0.4929   0.4573
   1.500   0.8884   0.01192   0.00468  -0.1573   0.4892   0.4608
   1.750   0.9159   0.01203   0.00475  -0.1573   0.4852   0.4640
   2.000   0.9430   0.01213   0.00484  -0.1574   0.4817   0.4675
   2.250   0.9703   0.01224   0.00496  -0.1574   0.4785   0.4714
   2.500   0.9979   0.01229   0.00506  -0.1575   0.4753   0.4756
   2.750   1.0251   0.01238   0.00515  -0.1576   0.4714   0.4798
   3.000   1.0514   0.01249   0.00525  -0.1574   0.4667   0.4836
   3.250   1.0774   0.01263   0.00539  -0.1573   0.4626   0.4878
   3.500   1.1044   0.01267   0.00550  -0.1573   0.4585   0.4924
   3.750   1.1308   0.01277   0.00562  -0.1572   0.4540   0.4974
   4.000   1.1564   0.01289   0.00575  -0.1570   0.4498   0.5025
   4.250   1.1815   0.01304   0.00592  -0.1567   0.4457   0.5079
   4.500   1.2078   0.01312   0.00606  -0.1566   0.4413   0.5138
   4.750   1.2328   0.01324   0.00621  -0.1563   0.4358   0.5195
   5.000   1.2558   0.01342   0.00640  -0.1557   0.4299   0.5257
   5.250   1.2811   0.01352   0.00657  -0.1554   0.4239   0.5330
   5.500   1.3035   0.01369   0.00677  -0.1547   0.4170   0.5402
   5.750   1.3247   0.01387   0.00699  -0.1536   0.4097   0.5489
   6.000   1.3438   0.01411   0.00725  -0.1523   0.3998   0.5576
   6.250   1.3650   0.01437   0.00754  -0.1515   0.3891   0.5678
   6.500   1.3840   0.01473   0.00792  -0.1503   0.3759   0.5783
   6.750   1.4003   0.01524   0.00839  -0.1487   0.3573   0.5901
   7.000   1.4088   0.01616   0.00916  -0.1461   0.3246   0.6025
   7.250   1.4084   0.01764   0.01041  -0.1424   0.2794   0.6145
   7.500   1.4121   0.01899   0.01164  -0.1394   0.2522   0.6282
   7.750   1.4210   0.02009   0.01270  -0.1373   0.2372   0.6441
   8.000   1.4321   0.02108   0.01369  -0.1355   0.2271   0.6611
   8.250   1.4448   0.02200   0.01464  -0.1340   0.2192   0.6792
   8.500   1.4578   0.02293   0.01562  -0.1326   0.2130   0.6983
   8.750   1.4720   0.02378   0.01655  -0.1314   0.2068   0.7201
   9.000   1.4833   0.02481   0.01767  -0.1299   0.2008   0.7494
   9.250   1.4930   0.02527   0.01852  -0.1277   0.1961   1.0000
   9.500   1.5050   0.02641   0.01965  -0.1265   0.1881   1.0000
   9.750   1.5158   0.02764   0.02087  -0.1252   0.1792   1.0000
  10.000   1.5202   0.02940   0.02252  -0.1234   0.1555   1.0000
  10.250   1.5121   0.03217   0.02510  -0.1207   0.1288   1.0000
  10.500   1.5136   0.03427   0.02719  -0.1189   0.1220   1.0000
  10.750   1.5194   0.03609   0.02904  -0.1176   0.1185   1.0000
  11.000   1.5245   0.03802   0.03101  -0.1163   0.1160   1.0000
  11.250   1.5278   0.04015   0.03318  -0.1150   0.1136   1.0000
  11.500   1.5294   0.04253   0.03559  -0.1137   0.1108   1.0000
  11.750   1.5298   0.04509   0.03820  -0.1125   0.1075   1.0000
  12.000   1.5379   0.04693   0.04013  -0.1117   0.1056   1.0000
  12.250   1.5417   0.04923   0.04250  -0.1108   0.1029   1.0000
  12.500   1.5412   0.05205   0.04536  -0.1098   0.0998   1.0000
  12.750   1.5377   0.05527   0.04862  -0.1089   0.0964   1.0000
  13.000   1.5493   0.05687   0.05029  -0.1085   0.0917   1.0000
  13.250   1.5506   0.05962   0.05304  -0.1078   0.0853   1.0000
  13.500   1.5447   0.06321   0.05648  -0.1071   0.0559   1.0000
  13.750   1.5163   0.06959   0.06275  -0.1060   0.0311   1.0000
  14.000   1.5038   0.07418   0.06737  -0.1054   0.0229   1.0000
  14.250   1.5001   0.07776   0.07100  -0.1051   0.0205   1.0000
  14.500   1.4986   0.08111   0.07443  -0.1048   0.0193   1.0000
  14.750   1.4959   0.08463   0.07804  -0.1046   0.0183   1.0000
  15.000   1.4922   0.08830   0.08179  -0.1045   0.0175   1.0000
  15.250   1.4909   0.09166   0.08524  -0.1044   0.0171   1.0000
  15.500   1.4889   0.09517   0.08884  -0.1044   0.0167   1.0000
  15.750   1.4868   0.09869   0.09244  -0.1045   0.0163   1.0000
  16.000   1.4831   0.10249   0.09634  -0.1047   0.0159   1.0000
  16.250   1.4795   0.10629   0.10022  -0.1049   0.0156   1.0000
  16.500   1.4741   0.11036   0.10439  -0.1053   0.0153   1.0000
  16.750   1.4678   0.11461   0.10873  -0.1059   0.0150   1.0000
  17.000   1.4602   0.11913   0.11333  -0.1066   0.0147   1.0000
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