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GOE 798 AIRFOIL (goe798-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 798 AIRFOIL (goe798-il)
Reynolds number: 500,000
Max Cl/Cd: 98.93 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe798-il-500000.txt
Download as CSV file: xf-goe798-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 798 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6851   0.05254   0.04857  -0.1457   0.9813   0.0493
 -15.500  -0.7056   0.04442   0.04015  -0.1552   0.9759   0.0495
 -15.250  -0.7146   0.03940   0.03489  -0.1607   0.9683   0.0497
 -15.000  -0.7200   0.03589   0.03124  -0.1626   0.9608   0.0501
 -14.750  -0.7191   0.03368   0.02895  -0.1627   0.9524   0.0505
 -14.500  -0.7161   0.03196   0.02716  -0.1622   0.9444   0.0508
 -14.250  -0.7128   0.03050   0.02563  -0.1610   0.9358   0.0511
 -14.000  -0.7079   0.02924   0.02428  -0.1596   0.9276   0.0515
 -13.750  -0.7026   0.02810   0.02305  -0.1577   0.9187   0.0519
 -13.500  -0.6965   0.02708   0.02192  -0.1555   0.9101   0.0524
 -13.250  -0.6914   0.02622   0.02094  -0.1528   0.9006   0.0528
 -13.000  -0.6804   0.02533   0.01992  -0.1510   0.8920   0.0533
 -12.750  -0.6673   0.02448   0.01893  -0.1494   0.8826   0.0539
 -12.500  -0.6519   0.02371   0.01800  -0.1480   0.8740   0.0544
 -12.250  -0.6350   0.02303   0.01716  -0.1468   0.8640   0.0548
 -12.000  -0.6193   0.02195   0.01603  -0.1455   0.8549   0.0556
 -11.750  -0.6001   0.02130   0.01535  -0.1445   0.8446   0.0564
 -11.500  -0.5794   0.02076   0.01474  -0.1437   0.8350   0.0571
 -11.250  -0.5584   0.02023   0.01411  -0.1428   0.8249   0.0580
 -11.000  -0.5368   0.01970   0.01347  -0.1421   0.8157   0.0588
 -10.750  -0.5146   0.01920   0.01283  -0.1413   0.8066   0.0596
 -10.500  -0.4917   0.01873   0.01221  -0.1407   0.7988   0.0603
 -10.250  -0.4704   0.01806   0.01153  -0.1399   0.7910   0.0614
 -10.000  -0.4469   0.01766   0.01106  -0.1394   0.7842   0.0624
  -9.750  -0.4225   0.01730   0.01066  -0.1389   0.7779   0.0634
  -9.500  -0.3978   0.01696   0.01024  -0.1385   0.7715   0.0647
  -9.250  -0.3724   0.01667   0.00980  -0.1382   0.7657   0.0659
  -9.000  -0.3482   0.01625   0.00938  -0.1377   0.7604   0.0674
  -8.750  -0.3224   0.01599   0.00912  -0.1375   0.7555   0.0688
  -8.500  -0.2962   0.01576   0.00883  -0.1372   0.7507   0.0705
  -8.250  -0.2695   0.01554   0.00849  -0.1370   0.7463   0.0722
  -8.000  -0.2431   0.01532   0.00828  -0.1369   0.7421   0.0740
  -7.750  -0.2158   0.01520   0.00816  -0.1368   0.7383   0.0760
  -7.500  -0.1883   0.01507   0.00796  -0.1367   0.7341   0.0785
  -7.250  -0.1611   0.01494   0.00783  -0.1367   0.7301   0.0808
  -7.000  -0.1327   0.01495   0.00779  -0.1367   0.7263   0.0833
  -6.750  -0.1040   0.01495   0.00767  -0.1369   0.7227   0.0863
  -6.500  -0.0769   0.01481   0.00760  -0.1368   0.7196   0.0887
  -6.250  -0.0487   0.01481   0.00758  -0.1368   0.7163   0.0917
  -6.000  -0.0206   0.01476   0.00745  -0.1369   0.7129   0.0949
  -5.750   0.0071   0.01467   0.00738  -0.1369   0.7095   0.0975
  -5.500   0.0358   0.01470   0.00735  -0.1370   0.7062   0.1006
  -5.250   0.0648   0.01481   0.00734  -0.1373   0.7029   0.1032
  -5.000   0.0915   0.01445   0.00706  -0.1372   0.7004   0.1060
  -4.750   0.1193   0.01438   0.00701  -0.1372   0.6974   0.1086
  -4.500   0.1474   0.01434   0.00692  -0.1373   0.6940   0.1112
  -4.250   0.1754   0.01423   0.00675  -0.1373   0.6905   0.1134
  -4.000   0.2028   0.01393   0.00646  -0.1373   0.6868   0.1159
  -3.750   0.2315   0.01388   0.00638  -0.1375   0.6830   0.1181
  -3.500   0.2587   0.01376   0.00627  -0.1374   0.6799   0.1203
  -3.250   0.2864   0.01367   0.00617  -0.1374   0.6764   0.1223
  -3.000   0.3144   0.01358   0.00605  -0.1374   0.6731   0.1238
  -2.750   0.3413   0.01325   0.00573  -0.1373   0.6698   0.1261
  -2.500   0.3695   0.01313   0.00559  -0.1374   0.6663   0.1281
  -2.250   0.3978   0.01308   0.00553  -0.1376   0.6627   0.1302
  -2.000   0.4247   0.01297   0.00544  -0.1374   0.6594   0.1324
  -1.750   0.4522   0.01291   0.00537  -0.1373   0.6558   0.1346
  -1.500   0.4792   0.01272   0.00519  -0.1372   0.6520   0.1372
  -1.250   0.5065   0.01257   0.00504  -0.1371   0.6484   0.1394
  -1.000   0.5352   0.01253   0.00496  -0.1373   0.6448   0.1412
  -0.750   0.5622   0.01245   0.00492  -0.1372   0.6418   0.1430
  -0.500   0.5889   0.01237   0.00486  -0.1370   0.6384   0.1452
  -0.250   0.6160   0.01231   0.00480  -0.1369   0.6347   0.1473
   0.000   0.6431   0.01222   0.00471  -0.1367   0.6312   0.1500
   0.250   0.6708   0.01215   0.00465  -0.1368   0.6278   0.1540
   0.500   0.6995   0.01215   0.00465  -0.1370   0.6243   0.1590
   0.750   0.7251   0.01207   0.00465  -0.1366   0.6211   0.1665
   1.000   0.7510   0.01198   0.00465  -0.1363   0.6173   0.1832
   1.250   0.7767   0.01181   0.00466  -0.1360   0.6135   0.2317
   1.500   0.8024   0.01160   0.00468  -0.1358   0.6097   0.3062
   1.750   0.8286   0.01135   0.00473  -0.1358   0.6057   0.4211
   2.000   0.8484   0.01085   0.00485  -0.1344   0.6020   0.6077
   2.250   0.8655   0.01036   0.00500  -0.1321   0.5977   0.8001
   2.500   0.9020   0.01034   0.00527  -0.1333   0.5929   0.9498
   2.750   0.9448   0.01053   0.00537  -0.1365   0.5877   0.9795
   3.000   0.9968   0.01071   0.00555  -0.1418   0.5821   0.9930
   3.250   1.0489   0.01086   0.00567  -0.1473   0.5757   1.0000
   3.500   1.0662   0.01095   0.00569  -0.1452   0.5702   1.0000
   3.750   1.0824   0.01104   0.00576  -0.1429   0.5646   1.0000
   4.000   1.0971   0.01112   0.00584  -0.1404   0.5580   1.0000
   4.250   1.1106   0.01124   0.00589  -0.1375   0.5515   1.0000
   4.500   1.1228   0.01135   0.00600  -0.1344   0.5445   1.0000
   4.750   1.1289   0.01147   0.00609  -0.1300   0.5366   1.0000
   5.000   1.1384   0.01165   0.00623  -0.1265   0.5286   1.0000
   5.250   1.1496   0.01186   0.00642  -0.1233   0.5185   1.0000
   5.500   1.1617   0.01215   0.00666  -0.1204   0.5074   1.0000
   5.750   1.1721   0.01254   0.00697  -0.1174   0.4944   1.0000
   6.000   1.1828   0.01300   0.00736  -0.1145   0.4794   1.0000
   6.250   1.1930   0.01355   0.00783  -0.1116   0.4634   1.0000
   6.500   1.2026   0.01419   0.00839  -0.1088   0.4471   1.0000
   6.750   1.2116   0.01492   0.00903  -0.1059   0.4315   1.0000
   7.000   1.2210   0.01570   0.00972  -0.1033   0.4177   1.0000
   7.500   1.2444   0.01721   0.01113  -0.0991   0.3967   1.0000
   7.750   1.2550   0.01807   0.01191  -0.0969   0.3884   1.0000
   8.000   1.2709   0.01872   0.01256  -0.0955   0.3819   1.0000
   8.250   1.2849   0.01947   0.01328  -0.0940   0.3757   1.0000
   8.500   1.2963   0.02038   0.01413  -0.0921   0.3699   1.0000
   8.750   1.3139   0.02099   0.01476  -0.0911   0.3656   1.0000
   9.000   1.3301   0.02168   0.01546  -0.0900   0.3612   1.0000
   9.250   1.3443   0.02250   0.01626  -0.0887   0.3572   1.0000
   9.500   1.3575   0.02338   0.01710  -0.0872   0.3530   1.0000
   9.750   1.3745   0.02408   0.01782  -0.0863   0.3497   1.0000
  10.000   1.3912   0.02481   0.01859  -0.0854   0.3464   1.0000
  10.250   1.4069   0.02560   0.01940  -0.0844   0.3428   1.0000
  10.500   1.4212   0.02649   0.02027  -0.0833   0.3392   1.0000
  10.750   1.4351   0.02740   0.02116  -0.0822   0.3357   1.0000
  11.000   1.4518   0.02815   0.02191  -0.0813   0.3329   1.0000
  11.250   1.4680   0.02898   0.02280  -0.0806   0.3303   1.0000
  11.500   1.4834   0.02987   0.02374  -0.0798   0.3273   1.0000
  11.750   1.4984   0.03077   0.02466  -0.0789   0.3243   1.0000
  12.000   1.5123   0.03175   0.02564  -0.0780   0.3212   1.0000
  12.250   1.5266   0.03267   0.02654  -0.0770   0.3179   1.0000
  12.500   1.5426   0.03350   0.02740  -0.0763   0.3152   1.0000
  12.750   1.5570   0.03452   0.02850  -0.0756   0.3128   1.0000
  13.000   1.5705   0.03563   0.02966  -0.0749   0.3098   1.0000
  13.250   1.5836   0.03674   0.03081  -0.0741   0.3066   1.0000
  13.500   1.5956   0.03792   0.03200  -0.0732   0.3032   1.0000
  13.750   1.6087   0.03893   0.03298  -0.0723   0.2994   1.0000
  14.000   1.6209   0.04018   0.03431  -0.0716   0.2967   1.0000
  14.250   1.6324   0.04153   0.03574  -0.0709   0.2935   1.0000
  14.500   1.6426   0.04297   0.03724  -0.0702   0.2897   1.0000
  14.750   1.6520   0.04444   0.03871  -0.0693   0.2856   1.0000
  15.000   1.6608   0.04593   0.04020  -0.0684   0.2813   1.0000
  15.250   1.6702   0.04754   0.04193  -0.0678   0.2774   1.0000
  15.500   1.6781   0.04926   0.04370  -0.0671   0.2724   1.0000
  15.750   1.6822   0.05128   0.04571  -0.0661   0.2671   1.0000
  16.000   1.6898   0.05308   0.04759  -0.0654   0.2615   1.0000
  16.250   1.6933   0.05530   0.04985  -0.0647   0.2546   1.0000
  16.500   1.6948   0.05770   0.05226  -0.0638   0.2470   1.0000
  16.750   1.6935   0.06042   0.05500  -0.0629   0.2371   1.0000
  17.000   1.6912   0.06327   0.05786  -0.0620   0.2263   1.0000
  17.250   1.6854   0.06648   0.06104  -0.0610   0.2151   1.0000
  17.500   1.6753   0.07019   0.06471  -0.0599   0.2047   1.0000
  17.750   1.6700   0.07342   0.06793  -0.0591   0.1960   1.0000
  18.000   1.6633   0.07678   0.07128  -0.0583   0.1892   1.0000
  18.250   1.6589   0.07995   0.07447  -0.0577   0.1836   1.0000
  18.500   1.6522   0.08338   0.07788  -0.0571   0.1785   1.0000
  18.750   1.6529   0.08606   0.08062  -0.0568   0.1750   1.0000
  19.000   1.6521   0.08891   0.08350  -0.0565   0.1713   1.0000
  19.250   1.6475   0.09216   0.08676  -0.0562   0.1676   1.0000
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