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GOE 798 AIRFOIL (goe798-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 798 AIRFOIL (goe798-il)
Reynolds number: 200,000
Max Cl/Cd: 65.67 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe798-il-200000.txt
Download as CSV file: xf-goe798-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250   0.0470   0.09721   0.09286  -0.1258   0.8806   0.1042
 -10.000   0.0618   0.09524   0.09086  -0.1252   0.8733   0.1052
  -9.750  -0.1074   0.05966   0.05511  -0.1512   0.8621   0.0865
  -9.500  -0.1824   0.04969   0.04479  -0.1540   0.8498   0.0854
  -9.250  -0.2525   0.04040   0.03464  -0.1510   0.8414   0.0857
  -9.000  -0.2630   0.03690   0.03070  -0.1483   0.8339   0.0867
  -8.750  -0.2368   0.03667   0.03057  -0.1481   0.8284   0.0876
  -8.500  -0.2120   0.03613   0.03001  -0.1480   0.8240   0.0888
  -8.250  -0.1957   0.03475   0.02844  -0.1472   0.8197   0.0904
  -8.000  -0.1913   0.03266   0.02596  -0.1449   0.8131   0.0926
  -7.750  -0.1810   0.03057   0.02339  -0.1432   0.8082   0.0948
  -7.500  -0.1532   0.03005   0.02292  -0.1435   0.8047   0.0964
  -7.250  -0.1268   0.02941   0.02220  -0.1435   0.8015   0.0983
  -7.000  -0.1115   0.02856   0.02117  -0.1419   0.7956   0.1007
  -6.750  -0.0936   0.02737   0.01961  -0.1407   0.7907   0.1038
  -6.500  -0.0659   0.02685   0.01916  -0.1409   0.7871   0.1060
  -6.250  -0.0382   0.02630   0.01850  -0.1411   0.7841   0.1091
  -6.000  -0.0172   0.02575   0.01756  -0.1400   0.7804   0.1128
  -5.750   0.0044   0.02503   0.01698  -0.1394   0.7756   0.1155
  -5.500   0.0296   0.02472   0.01667  -0.1391   0.7714   0.1191
  -5.250   0.0556   0.02425   0.01588  -0.1388   0.7679   0.1238
  -5.000   0.0850   0.02349   0.01519  -0.1393   0.7651   0.1275
  -4.750   0.1124   0.02326   0.01489  -0.1394   0.7621   0.1319
  -4.500   0.1321   0.02311   0.01460  -0.1381   0.7575   0.1360
  -4.250   0.1564   0.02270   0.01431  -0.1377   0.7534   0.1397
  -4.000   0.1836   0.02247   0.01402  -0.1377   0.7498   0.1439
  -3.750   0.2133   0.02227   0.01364  -0.1380   0.7469   0.1480
  -3.500   0.2438   0.02171   0.01309  -0.1387   0.7444   0.1519
  -3.250   0.2671   0.02172   0.01314  -0.1380   0.7408   0.1554
  -3.000   0.2881   0.02174   0.01315  -0.1369   0.7360   0.1589
  -2.750   0.3143   0.02165   0.01296  -0.1366   0.7318   0.1621
  -2.500   0.3440   0.02113   0.01246  -0.1370   0.7282   0.1661
  -2.250   0.3772   0.02085   0.01215  -0.1379   0.7249   0.1707
  -2.000   0.4002   0.02087   0.01216  -0.1370   0.7200   0.1745
  -1.750   0.4222   0.02086   0.01212  -0.1360   0.7145   0.1772
  -1.500   0.4500   0.02047   0.01175  -0.1359   0.7102   0.1804
  -1.250   0.4822   0.02010   0.01137  -0.1366   0.7065   0.1838
  -1.000   0.5144   0.01991   0.01114  -0.1374   0.7028   0.1879
  -0.750   0.5311   0.01999   0.01128  -0.1354   0.6967   0.1917
  -0.500   0.5564   0.01985   0.01115  -0.1349   0.6919   0.1959
  -0.250   0.5854   0.01958   0.01093  -0.1351   0.6883   0.2019
   0.000   0.6184   0.01937   0.01069  -0.1359   0.6852   0.2102
   0.250   0.6429   0.01934   0.01076  -0.1355   0.6814   0.2211
   0.500   0.6601   0.01940   0.01099  -0.1336   0.6762   0.2380
   0.750   0.6837   0.01915   0.01099  -0.1330   0.6718   0.2853
   1.000   0.7083   0.01843   0.01090  -0.1326   0.6683   0.4454
   1.250   0.7292   0.01737   0.01097  -0.1305   0.6653   0.7865
   1.500   0.8059   0.01754   0.01133  -0.1395   0.6607   0.9708
   1.750   0.8770   0.01772   0.01145  -0.1487   0.6547   0.9990
   2.000   0.9025   0.01770   0.01134  -0.1483   0.6500   1.0000
   2.250   0.9318   0.01760   0.01110  -0.1485   0.6462   1.0000
   2.500   0.9515   0.01774   0.01118  -0.1471   0.6416   1.0000
   2.750   0.9608   0.01797   0.01143  -0.1436   0.6354   1.0000
   3.000   0.9835   0.01795   0.01133  -0.1426   0.6305   1.0000
   3.250   1.0151   0.01781   0.01106  -0.1432   0.6264   1.0000
   3.500   1.0278   0.01802   0.01128  -0.1404   0.6205   1.0000
   3.750   1.0411   0.01814   0.01139  -0.1376   0.6140   1.0000
   4.000   1.0693   0.01801   0.01116  -0.1376   0.6089   1.0000
   4.250   1.0915   0.01803   0.01112  -0.1365   0.6033   1.0000
   4.500   1.0991   0.01820   0.01132  -0.1326   0.5956   1.0000
   4.750   1.1265   0.01805   0.01107  -0.1324   0.5895   1.0000
   5.000   1.1392   0.01819   0.01120  -0.1296   0.5820   1.0000
   5.250   1.1532   0.01824   0.01123  -0.1269   0.5739   1.0000
   5.500   1.1801   0.01818   0.01105  -0.1267   0.5670   1.0000
   5.750   1.1792   0.01845   0.01138  -0.1213   0.5572   1.0000
   6.000   1.2071   0.01838   0.01116  -0.1212   0.5495   1.0000
   6.250   1.2004   0.01879   0.01164  -0.1149   0.5384   1.0000
   6.500   1.2198   0.01891   0.01166  -0.1134   0.5291   1.0000
   6.750   1.2264   0.01931   0.01204  -0.1098   0.5178   1.0000
   7.000   1.2383   0.01971   0.01239  -0.1072   0.5070   1.0000
   7.250   1.2565   0.02000   0.01256  -0.1057   0.4968   1.0000
   7.500   1.2634   0.02065   0.01320  -0.1026   0.4855   1.0000
   7.750   1.2829   0.02101   0.01342  -0.1014   0.4760   1.0000
   8.000   1.2906   0.02173   0.01414  -0.0986   0.4654   1.0000
   8.250   1.3082   0.02223   0.01453  -0.0973   0.4567   1.0000
   8.500   1.3189   0.02296   0.01526  -0.0951   0.4482   1.0000
   8.750   1.3445   0.02330   0.01543  -0.0950   0.4415   1.0000
   9.000   1.3529   0.02418   0.01639  -0.0926   0.4347   1.0000
   9.250   1.3696   0.02480   0.01697  -0.0914   0.4285   1.0000
   9.500   1.3957   0.02516   0.01721  -0.0915   0.4229   1.0000
   9.750   1.4036   0.02611   0.01825  -0.0892   0.4171   1.0000
  10.000   1.4186   0.02682   0.01896  -0.0879   0.4117   1.0000
  10.250   1.4458   0.02714   0.01915  -0.0881   0.4067   1.0000
  10.500   1.4572   0.02804   0.02012  -0.0864   0.4019   1.0000
  10.750   1.4684   0.02894   0.02108  -0.0848   0.3971   1.0000
  11.000   1.4852   0.02962   0.02175  -0.0838   0.3925   1.0000
  11.250   1.5170   0.02980   0.02180  -0.0846   0.3881   1.0000
  11.500   1.5227   0.03096   0.02310  -0.0824   0.3840   1.0000
  11.750   1.5319   0.03201   0.02422  -0.0807   0.3797   1.0000
  12.000   1.5470   0.03280   0.02503  -0.0796   0.3756   1.0000
  12.250   1.5724   0.03317   0.02535  -0.0798   0.3718   1.0000
  12.500   1.5915   0.03390   0.02610  -0.0792   0.3680   1.0000
  12.750   1.5925   0.03536   0.02770  -0.0768   0.3639   1.0000
  13.000   1.6014   0.03648   0.02888  -0.0752   0.3595   1.0000
  13.250   1.6191   0.03715   0.02954  -0.0746   0.3553   1.0000
  13.500   1.6478   0.03741   0.02973  -0.0750   0.3510   1.0000
  13.750   1.6398   0.03942   0.03193  -0.0720   0.3470   1.0000
  14.000   1.6433   0.04091   0.03352  -0.0702   0.3424   1.0000
  14.250   1.6578   0.04175   0.03436  -0.0693   0.3379   1.0000
  14.500   1.6851   0.04197   0.03449  -0.0696   0.3332   1.0000
  14.750   1.6689   0.04471   0.03746  -0.0663   0.3284   1.0000
  15.000   1.6701   0.04647   0.03930  -0.0646   0.3232   1.0000
  15.250   1.6891   0.04700   0.03978  -0.0642   0.3183   1.0000
  15.500   1.6887   0.04901   0.04189  -0.0626   0.3131   1.0000
  15.750   1.6781   0.05182   0.04484  -0.0604   0.3072   1.0000
  16.000   1.6893   0.05290   0.04589  -0.0596   0.3016   1.0000
  16.250   1.6878   0.05515   0.04822  -0.0582   0.2956   1.0000
  16.500   1.6757   0.05839   0.05160  -0.0565   0.2888   1.0000
  16.750   1.6924   0.05901   0.05212  -0.0561   0.2829   1.0000
  17.000   1.6705   0.06342   0.05675  -0.0542   0.2756   1.0000
  17.250   1.6695   0.06586   0.05922  -0.0534   0.2689   1.0000
  17.500   1.6690   0.06832   0.06170  -0.0525   0.2624   1.0000
  17.750   1.6569   0.07215   0.06565  -0.0516   0.2552   1.0000
  18.000   1.6736   0.07274   0.06610  -0.0513   0.2496   1.0000
  18.250   1.6501   0.07807   0.07167  -0.0505   0.2425   1.0000
  18.500   1.6534   0.08029   0.07387  -0.0502   0.2368   1.0000
  18.750   1.6515   0.08316   0.07678  -0.0498   0.2313   1.0000
  19.000   1.6425   0.08700   0.08073  -0.0495   0.2256   1.0000
  19.250   1.6536   0.08827   0.08192  -0.0494   0.2209   1.0000
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