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GOE 502 AIRFOIL (goe502-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 502 AIRFOIL (goe502-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.71 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe502-il-1000000-n5.txt
Download as CSV file: xf-goe502-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 502 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.6427   0.09238   0.08957  -0.0947   0.9945   0.0282
 -16.750  -0.6543   0.08611   0.08321  -0.0996   0.9925   0.0284
 -16.500  -0.6604   0.08117   0.07819  -0.1032   0.9906   0.0285
 -16.250  -0.6661   0.07617   0.07310  -0.1072   0.9882   0.0286
 -16.000  -0.6704   0.07126   0.06811  -0.1114   0.9856   0.0287
 -15.750  -0.6687   0.06715   0.06394  -0.1153   0.9830   0.0288
 -15.500  -0.6716   0.06271   0.05942  -0.1192   0.9792   0.0289
 -15.250  -0.6768   0.05862   0.05528  -0.1223   0.9729   0.0291
 -14.750  -0.6793   0.04990   0.04643  -0.1316   0.9610   0.0293
 -14.500  -0.6748   0.04509   0.04153  -0.1386   0.9547   0.0294
 -14.250  -0.6681   0.04020   0.03654  -0.1463   0.9455   0.0296
 -14.000  -0.6488   0.03530   0.03152  -0.1564   0.9386   0.0298
 -13.750  -0.6316   0.03008   0.02615  -0.1671   0.9287   0.0299
 -13.500  -0.6314   0.02475   0.02062  -0.1752   0.9144   0.0301
 -13.250  -0.6207   0.02121   0.01686  -0.1805   0.9045   0.0302
 -13.000  -0.6081   0.02006   0.01562  -0.1804   0.8975   0.0304
 -12.750  -0.5908   0.01921   0.01468  -0.1803   0.8912   0.0306
 -12.500  -0.5723   0.01844   0.01384  -0.1800   0.8860   0.0308
 -12.250  -0.5532   0.01782   0.01316  -0.1795   0.8810   0.0311
 -12.000  -0.5328   0.01724   0.01251  -0.1790   0.8754   0.0314
 -11.750  -0.5114   0.01669   0.01187  -0.1786   0.8690   0.0316
 -11.500  -0.4901   0.01618   0.01131  -0.1781   0.8624   0.0319
 -11.250  -0.4683   0.01570   0.01074  -0.1775   0.8534   0.0321
 -11.000  -0.4457   0.01527   0.01024  -0.1770   0.8442   0.0323
 -10.750  -0.4230   0.01488   0.00976  -0.1763   0.8331   0.0325
 -10.500  -0.4001   0.01450   0.00929  -0.1757   0.8195   0.0327
 -10.250  -0.3789   0.01407   0.00875  -0.1748   0.8002   0.0330
 -10.000  -0.3578   0.01375   0.00831  -0.1738   0.7785   0.0333
  -9.750  -0.3352   0.01348   0.00793  -0.1729   0.7616   0.0336
  -9.500  -0.3113   0.01322   0.00759  -0.1723   0.7498   0.0339
  -9.250  -0.2873   0.01299   0.00728  -0.1717   0.7395   0.0343
  -9.000  -0.2617   0.01274   0.00698  -0.1713   0.7326   0.0346
  -8.750  -0.2363   0.01251   0.00670  -0.1709   0.7259   0.0350
  -8.500  -0.2109   0.01230   0.00641  -0.1705   0.7198   0.0354
  -8.250  -0.1845   0.01206   0.00613  -0.1702   0.7147   0.0358
  -8.000  -0.1582   0.01185   0.00587  -0.1699   0.7094   0.0362
  -7.750  -0.1319   0.01167   0.00564  -0.1696   0.7045   0.0366
  -7.500  -0.1059   0.01146   0.00538  -0.1692   0.7001   0.0370
  -7.250  -0.0789   0.01121   0.00511  -0.1690   0.6968   0.0376
  -7.000  -0.0518   0.01101   0.00490  -0.1688   0.6926   0.0381
  -6.750  -0.0249   0.01084   0.00470  -0.1686   0.6879   0.0386
  -6.500   0.0017   0.01070   0.00452  -0.1682   0.6832   0.0392
  -6.250   0.0286   0.01056   0.00434  -0.1679   0.6792   0.0397
  -6.000   0.0563   0.01040   0.00416  -0.1678   0.6758   0.0403
  -5.750   0.0838   0.01025   0.00399  -0.1676   0.6714   0.0408
  -5.500   0.1108   0.01013   0.00383  -0.1673   0.6663   0.0413
  -5.250   0.1372   0.00998   0.00364  -0.1669   0.6611   0.0420
  -5.000   0.1647   0.00984   0.00349  -0.1667   0.6571   0.0429
  -4.750   0.1923   0.00972   0.00336  -0.1665   0.6523   0.0437
  -4.500   0.2194   0.00962   0.00324  -0.1662   0.6463   0.0446
  -4.250   0.2458   0.00955   0.00312  -0.1658   0.6400   0.0453
  -4.000   0.2735   0.00946   0.00301  -0.1656   0.6342   0.0459
  -3.750   0.3002   0.00934   0.00287  -0.1652   0.6270   0.0470
  -3.500   0.3265   0.00927   0.00276  -0.1647   0.6195   0.0480
  -3.250   0.3533   0.00919   0.00266  -0.1644   0.6105   0.0491
  -3.000   0.3791   0.00917   0.00258  -0.1638   0.6008   0.0502
  -2.750   0.4055   0.00914   0.00251  -0.1633   0.5905   0.0512
  -2.500   0.4309   0.00909   0.00242  -0.1627   0.5798   0.0529
  -2.250   0.4563   0.00908   0.00236  -0.1620   0.5684   0.0545
  -2.000   0.4820   0.00908   0.00231  -0.1614   0.5584   0.0564
  -1.750   0.5072   0.00908   0.00227  -0.1607   0.5488   0.0595
  -1.500   0.5329   0.00898   0.00220  -0.1602   0.5407   0.0727
  -1.250   0.5577   0.00886   0.00216  -0.1595   0.5322   0.1115
  -1.000   0.5834   0.00884   0.00216  -0.1590   0.5255   0.1248
  -0.750   0.6093   0.00881   0.00216  -0.1584   0.5189   0.1388
  -0.500   0.6344   0.00883   0.00218  -0.1578   0.5124   0.1519
  -0.250   0.6602   0.00882   0.00220  -0.1572   0.5071   0.1665
   0.000   0.6861   0.00881   0.00223  -0.1567   0.5018   0.1815
   0.250   0.7115   0.00883   0.00227  -0.1561   0.4966   0.1952
   0.500   0.7361   0.00888   0.00232  -0.1553   0.4912   0.2075
   0.750   0.7623   0.00888   0.00237  -0.1548   0.4872   0.2201
   1.000   0.7879   0.00891   0.00242  -0.1542   0.4826   0.2329
   1.250   0.8129   0.00895   0.00248  -0.1535   0.4782   0.2436
   1.500   0.8366   0.00903   0.00255  -0.1525   0.4734   0.2511
   1.750   0.8609   0.00906   0.00261  -0.1517   0.4696   0.2619
   2.000   0.8853   0.00910   0.00267  -0.1508   0.4653   0.2698
   2.250   0.9090   0.00916   0.00274  -0.1498   0.4611   0.2778
   2.500   0.9315   0.00924   0.00283  -0.1487   0.4560   0.2887
   2.750   0.9547   0.00931   0.00292  -0.1476   0.4510   0.2995
   3.000   0.9784   0.00938   0.00300  -0.1467   0.4450   0.3109
   3.250   1.0004   0.00949   0.00312  -0.1454   0.4384   0.3217
   3.500   1.0228   0.00961   0.00324  -0.1442   0.4334   0.3308
   3.750   1.0465   0.00969   0.00336  -0.1433   0.4287   0.3410
   4.000   1.0689   0.00981   0.00349  -0.1422   0.4224   0.3522
   4.250   1.0900   0.00998   0.00365  -0.1408   0.4160   0.3636
   4.750   1.1347   0.01022   0.00394  -0.1385   0.4038   0.3931
   5.000   1.1552   0.01039   0.00413  -0.1371   0.3982   0.4086
   5.250   1.1780   0.01050   0.00428  -0.1360   0.3939   0.4243
   5.500   1.1994   0.01065   0.00446  -0.1348   0.3875   0.4415
   5.750   1.2186   0.01087   0.00468  -0.1331   0.3801   0.4584
   6.000   1.2397   0.01102   0.00487  -0.1319   0.3737   0.4753
   6.250   1.2586   0.01125   0.00511  -0.1302   0.3656   0.4927
   6.500   1.2785   0.01144   0.00534  -0.1288   0.3590   0.5146
   6.750   1.2966   0.01165   0.00561  -0.1270   0.3504   0.5521
   7.000   1.3121   0.01173   0.00598  -0.1249   0.3415   0.6970
   7.500   1.3615   0.01208   0.00673  -0.1245   0.3165   1.0000
   7.750   1.3782   0.01249   0.00709  -0.1227   0.3060   1.0000
   8.000   1.3940   0.01295   0.00750  -0.1208   0.2951   1.0000
   8.250   1.4098   0.01342   0.00792  -0.1189   0.2831   1.0000
   8.500   1.4239   0.01399   0.00842  -0.1168   0.2690   1.0000
   8.750   1.4351   0.01469   0.00904  -0.1144   0.2518   1.0000
   9.000   1.4427   0.01560   0.00982  -0.1115   0.2301   1.0000
   9.250   1.4514   0.01649   0.01061  -0.1089   0.2112   1.0000
   9.500   1.4565   0.01760   0.01159  -0.1059   0.1885   1.0000
   9.750   1.4656   0.01855   0.01247  -0.1036   0.1751   1.0000
  10.000   1.4769   0.01941   0.01330  -0.1016   0.1668   1.0000
  10.250   1.4874   0.02034   0.01420  -0.0996   0.1579   1.0000
  10.500   1.4989   0.02125   0.01509  -0.0978   0.1510   1.0000
  10.750   1.5114   0.02213   0.01596  -0.0962   0.1459   1.0000
  11.000   1.5226   0.02312   0.01695  -0.0945   0.1411   1.0000
  11.250   1.5363   0.02397   0.01782  -0.0932   0.1374   1.0000
  11.500   1.5483   0.02498   0.01883  -0.0917   0.1333   1.0000
  11.750   1.5587   0.02612   0.01996  -0.0902   0.1289   1.0000
  12.000   1.5711   0.02716   0.02103  -0.0889   0.1261   1.0000
  12.250   1.5829   0.02826   0.02215  -0.0877   0.1224   1.0000
  12.500   1.5921   0.02960   0.02349  -0.0863   0.1181   1.0000
  12.750   1.6013   0.03098   0.02488  -0.0850   0.1138   1.0000
  13.000   1.6117   0.03229   0.02622  -0.0839   0.1102   1.0000
  13.250   1.6185   0.03394   0.02787  -0.0826   0.1057   1.0000
  13.500   1.6269   0.03546   0.02941  -0.0815   0.1020   1.0000
  13.750   1.6335   0.03719   0.03115  -0.0803   0.0969   1.0000
  14.000   1.6379   0.03913   0.03310  -0.0791   0.0921   1.0000
  14.250   1.6414   0.04117   0.03513  -0.0779   0.0859   1.0000
  14.500   1.6416   0.04354   0.03750  -0.0766   0.0787   1.0000
  14.750   1.6408   0.04607   0.04002  -0.0754   0.0724   1.0000
  15.000   1.6394   0.04869   0.04264  -0.0743   0.0668   1.0000
  15.250   1.6392   0.05126   0.04523  -0.0733   0.0627   1.0000
  15.500   1.6384   0.05393   0.04793  -0.0724   0.0597   1.0000
  15.750   1.6398   0.05641   0.05044  -0.0716   0.0574   1.0000
  16.000   1.6390   0.05918   0.05326  -0.0709   0.0552   1.0000
  16.250   1.6389   0.06194   0.05605  -0.0703   0.0533   1.0000
  16.500   1.6406   0.06452   0.05868  -0.0698   0.0519   1.0000
  16.750   1.6396   0.06742   0.06163  -0.0693   0.0502   1.0000
  17.000   1.6374   0.07053   0.06479  -0.0689   0.0488   1.0000
  17.250   1.6385   0.07328   0.06759  -0.0687   0.0477   1.0000
  17.500   1.6394   0.07611   0.07048  -0.0685   0.0469   1.0000
  17.750   1.6401   0.07895   0.07338  -0.0684   0.0459   1.0000
  18.000   1.6395   0.08201   0.07649  -0.0683   0.0450   1.0000
  18.250   1.6376   0.08527   0.07980  -0.0684   0.0440   1.0000
  18.500   1.6364   0.08847   0.08305  -0.0685   0.0431   1.0000
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