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GOE 797 AIRFOIL (goe797-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 797 AIRFOIL (goe797-il)
Reynolds number: 200,000
Max Cl/Cd: 73.32 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe797-il-200000-n5.txt
Download as CSV file: xf-goe797-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 797 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.6100   0.04556   0.04073  -0.1203   0.9710   0.0450
 -11.750  -0.6307   0.04031   0.03508  -0.1230   0.9588   0.0453
 -11.500  -0.6332   0.03715   0.03158  -0.1230   0.9489   0.0458
 -11.250  -0.6256   0.03451   0.02859  -0.1232   0.9420   0.0464
 -11.000  -0.6150   0.03239   0.02615  -0.1228   0.9340   0.0470
 -10.750  -0.5987   0.03063   0.02412  -0.1226   0.9277   0.0476
 -10.500  -0.5796   0.02957   0.02301  -0.1221   0.9200   0.0482
 -10.250  -0.5557   0.02863   0.02200  -0.1223   0.9150   0.0489
 -10.000  -0.5366   0.02782   0.02112  -0.1214   0.9064   0.0497
  -9.750  -0.5137   0.02687   0.02003  -0.1213   0.9002   0.0507
  -9.500  -0.4931   0.02592   0.01893  -0.1206   0.8922   0.0517
  -9.250  -0.4707   0.02491   0.01772  -0.1202   0.8848   0.0527
  -9.000  -0.4481   0.02396   0.01656  -0.1198   0.8773   0.0537
  -8.750  -0.4251   0.02308   0.01555  -0.1193   0.8693   0.0546
  -8.500  -0.4004   0.02238   0.01479  -0.1191   0.8628   0.0556
  -8.250  -0.3764   0.02182   0.01419  -0.1187   0.8541   0.0568
  -8.000  -0.3504   0.02124   0.01350  -0.1185   0.8475   0.0583
  -7.750  -0.3259   0.02069   0.01284  -0.1181   0.8384   0.0600
  -7.500  -0.2997   0.02010   0.01207  -0.1179   0.8315   0.0616
  -7.250  -0.2747   0.01950   0.01143  -0.1176   0.8237   0.0632
  -7.000  -0.2484   0.01904   0.01092  -0.1175   0.8166   0.0648
  -6.750  -0.2219   0.01863   0.01043  -0.1173   0.8097   0.0668
  -6.500  -0.1953   0.01824   0.00995  -0.1172   0.8023   0.0692
  -6.250  -0.1678   0.01785   0.00940  -0.1171   0.7964   0.0716
  -6.000  -0.1417   0.01745   0.00902  -0.1170   0.7893   0.0743
  -5.750  -0.1143   0.01717   0.00868  -0.1169   0.7835   0.0772
  -5.500  -0.0865   0.01688   0.00830  -0.1169   0.7783   0.0806
  -5.250  -0.0594   0.01659   0.00794  -0.1169   0.7720   0.0842
  -5.000  -0.0318   0.01634   0.00769  -0.1169   0.7665   0.0882
  -4.750  -0.0037   0.01615   0.00742  -0.1169   0.7618   0.0928
  -4.500   0.0239   0.01596   0.00717  -0.1169   0.7564   0.0975
  -4.250   0.0516   0.01577   0.00700  -0.1169   0.7514   0.1026
  -4.000   0.0801   0.01564   0.00679  -0.1170   0.7470   0.1084
  -3.750   0.1081   0.01550   0.00659  -0.1171   0.7424   0.1139
  -3.500   0.1357   0.01537   0.00649  -0.1171   0.7374   0.1196
  -3.250   0.1641   0.01528   0.00633  -0.1172   0.7332   0.1259
  -3.000   0.1926   0.01516   0.00616  -0.1173   0.7293   0.1315
  -2.750   0.2205   0.01506   0.00606  -0.1174   0.7250   0.1376
  -2.500   0.2484   0.01499   0.00595  -0.1174   0.7198   0.1437
  -2.250   0.2762   0.01485   0.00582  -0.1174   0.7148   0.1495
  -2.000   0.3048   0.01477   0.00567  -0.1175   0.7099   0.1563
  -1.750   0.3317   0.01467   0.00560  -0.1174   0.7037   0.1628
  -1.500   0.3593   0.01455   0.00550  -0.1174   0.6981   0.1703
  -1.250   0.3877   0.01448   0.00538  -0.1174   0.6933   0.1780
  -1.000   0.4148   0.01437   0.00534  -0.1174   0.6875   0.1869
  -0.750   0.4420   0.01429   0.00528  -0.1173   0.6812   0.1965
  -0.500   0.4701   0.01420   0.00518  -0.1173   0.6756   0.2090
  -0.250   0.4969   0.01410   0.00517  -0.1172   0.6692   0.2271
   0.000   0.5239   0.01398   0.00517  -0.1171   0.6635   0.2552
   0.250   0.5516   0.01385   0.00515  -0.1171   0.6590   0.2965
   0.500   0.5785   0.01367   0.00516  -0.1171   0.6543   0.3547
   0.750   0.6034   0.01334   0.00525  -0.1167   0.6486   0.4665
   1.000   0.6262   0.01286   0.00535  -0.1157   0.6434   0.6367
   1.250   0.6472   0.01252   0.00546  -0.1136   0.6390   0.8004
   1.500   0.6774   0.01247   0.00562  -0.1135   0.6331   0.9110
   1.750   0.7178   0.01252   0.00566  -0.1160   0.6272   0.9689
   2.000   0.7607   0.01260   0.00564  -0.1193   0.6219   1.0000
   2.250   0.7841   0.01270   0.00574  -0.1185   0.6153   1.0000
   2.500   0.8086   0.01280   0.00578  -0.1178   0.6087   1.0000
   2.750   0.8333   0.01290   0.00583  -0.1172   0.6021   1.0000
   3.000   0.8573   0.01302   0.00592  -0.1165   0.5942   1.0000
   3.250   0.8822   0.01313   0.00596  -0.1159   0.5870   1.0000
   3.500   0.9060   0.01327   0.00609  -0.1152   0.5785   1.0000
   3.750   0.9306   0.01340   0.00615  -0.1146   0.5706   1.0000
   4.000   0.9541   0.01355   0.00631  -0.1138   0.5611   1.0000
   4.250   0.9778   0.01371   0.00641  -0.1130   0.5517   1.0000
   4.500   1.0009   0.01388   0.00656  -0.1121   0.5408   1.0000
   4.750   1.0235   0.01408   0.00672  -0.1112   0.5293   1.0000
   5.000   1.0454   0.01429   0.00688  -0.1101   0.5169   1.0000
   5.250   1.0661   0.01454   0.00706  -0.1088   0.5026   1.0000
   5.500   1.0854   0.01483   0.00726  -0.1073   0.4865   1.0000
   5.750   1.1035   0.01516   0.00751  -0.1056   0.4696   1.0000
   6.000   1.1202   0.01554   0.00780  -0.1036   0.4528   1.0000
   6.250   1.1356   0.01597   0.00813  -0.1014   0.4370   1.0000
   6.500   1.1497   0.01640   0.00848  -0.0990   0.4234   1.0000
   6.750   1.1647   0.01683   0.00888  -0.0969   0.4120   1.0000
   7.000   1.1798   0.01732   0.00931  -0.0948   0.4022   1.0000
   7.250   1.1945   0.01784   0.00978  -0.0927   0.3917   1.0000
   7.500   1.2100   0.01837   0.01027  -0.0908   0.3821   1.0000
   7.750   1.2251   0.01894   0.01080  -0.0889   0.3738   1.0000
   8.000   1.2425   0.01945   0.01132  -0.0875   0.3673   1.0000
   8.250   1.2588   0.02002   0.01188  -0.0859   0.3601   1.0000
   8.500   1.2743   0.02064   0.01248  -0.0843   0.3534   1.0000
   8.750   1.2913   0.02120   0.01307  -0.0829   0.3468   1.0000
   9.000   1.3069   0.02185   0.01371  -0.0814   0.3408   1.0000
   9.250   1.3235   0.02248   0.01435  -0.0801   0.3357   1.0000
   9.500   1.3406   0.02308   0.01501  -0.0788   0.3303   1.0000
   9.750   1.3558   0.02378   0.01573  -0.0774   0.3246   1.0000
  10.000   1.3705   0.02453   0.01648  -0.0759   0.3192   1.0000
  10.250   1.3861   0.02523   0.01726  -0.0747   0.3131   1.0000
  10.500   1.3998   0.02606   0.01811  -0.0732   0.3072   1.0000
  10.750   1.4136   0.02689   0.01898  -0.0718   0.3017   1.0000
  11.000   1.4273   0.02774   0.01992  -0.0705   0.2949   1.0000
  11.250   1.4381   0.02878   0.02096  -0.0689   0.2882   1.0000
  11.500   1.4508   0.02974   0.02201  -0.0676   0.2809   1.0000
  11.750   1.4604   0.03090   0.02321  -0.0660   0.2730   1.0000
  12.000   1.4708   0.03206   0.02444  -0.0646   0.2643   1.0000
  12.250   1.4775   0.03349   0.02589  -0.0630   0.2550   1.0000
  12.500   1.4865   0.03484   0.02731  -0.0617   0.2441   1.0000
  12.750   1.4924   0.03644   0.02894  -0.0603   0.2326   1.0000
  13.000   1.4964   0.03826   0.03076  -0.0588   0.2203   1.0000
  13.250   1.4986   0.04030   0.03280  -0.0574   0.2080   1.0000
  13.500   1.4991   0.04258   0.03504  -0.0560   0.1965   1.0000
  13.750   1.5001   0.04485   0.03732  -0.0547   0.1868   1.0000
  14.000   1.5004   0.04725   0.03972  -0.0535   0.1788   1.0000
  14.250   1.5005   0.04974   0.04220  -0.0523   0.1716   1.0000
  14.500   1.5015   0.05217   0.04466  -0.0513   0.1652   1.0000
  14.750   1.5022   0.05469   0.04721  -0.0504   0.1591   1.0000
  15.000   1.5016   0.05737   0.04990  -0.0496   0.1540   1.0000
  15.250   1.5058   0.05963   0.05225  -0.0489   0.1488   1.0000
  15.500   1.5061   0.06234   0.05500  -0.0483   0.1441   1.0000
  15.750   1.5064   0.06506   0.05777  -0.0477   0.1400   1.0000
  16.000   1.5105   0.06745   0.06026  -0.0474   0.1353   1.0000
  16.250   1.5107   0.07029   0.06317  -0.0470   0.1308   1.0000
  16.500   1.5084   0.07347   0.06636  -0.0467   0.1269   1.0000
  16.750   1.5123   0.07600   0.06903  -0.0466   0.1229   1.0000
  17.000   1.5131   0.07893   0.07205  -0.0466   0.1186   1.0000
  17.250   1.5104   0.08231   0.07548  -0.0466   0.1145   1.0000
  17.500   1.5085   0.08565   0.07888  -0.0467   0.1106   1.0000
  17.750   1.5089   0.08875   0.08210  -0.0470   0.1062   1.0000
  18.000   1.5057   0.09236   0.08578  -0.0474   0.1019   1.0000
  18.250   1.4994   0.09643   0.08989  -0.0479   0.0982   1.0000
  18.500   1.4994   0.09967   0.09326  -0.0484   0.0945   1.0000
  18.750   1.4965   0.10334   0.09702  -0.0491   0.0906   1.0000
  19.000   1.4906   0.10748   0.10122  -0.0500   0.0869   1.0000
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