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GOE 797 AIRFOIL (goe797-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 797 AIRFOIL (goe797-il)
Reynolds number: 100,000
Max Cl/Cd: 50.33 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe797-il-100000-n5.txt
Download as CSV file: xf-goe797-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.3105   0.14241   0.13677  -0.0530   1.0000   0.0619
 -12.750  -0.3050   0.14025   0.13464  -0.0517   1.0000   0.0615
 -12.500  -0.3043   0.13803   0.13247  -0.0507   1.0000   0.0611
 -12.250  -0.3072   0.13574   0.13022  -0.0497   1.0000   0.0608
 -12.000  -0.3143   0.13327   0.12781  -0.0489   1.0000   0.0608
 -11.750  -0.3127   0.12863   0.12316  -0.0522   0.9973   0.0612
 -11.500  -0.3058   0.12337   0.11788  -0.0567   0.9939   0.0614
 -11.250  -0.2969   0.11852   0.11301  -0.0605   0.9899   0.0613
 -11.000  -0.2889   0.11350   0.10797  -0.0645   0.9857   0.0612
 -10.750  -0.2822   0.10799   0.10245  -0.0692   0.9823   0.0613
 -10.500  -0.2886   0.10057   0.09500  -0.0749   0.9760   0.0619
 -10.250  -0.2735   0.09704   0.09147  -0.0784   0.9721   0.0628
 -10.000  -0.2589   0.09390   0.08832  -0.0814   0.9668   0.0636
  -9.750  -0.2515   0.08901   0.08343  -0.0858   0.9612   0.0641
  -9.500  -0.2516   0.08315   0.07756  -0.0907   0.9540   0.0645
  -9.250  -0.2578   0.07605   0.07045  -0.0969   0.9460   0.0650
  -9.000  -0.3687   0.05209   0.04603  -0.1144   0.9198   0.0654
  -8.750  -0.3798   0.04627   0.03977  -0.1161   0.9091   0.0668
  -8.500  -0.3784   0.04147   0.03444  -0.1170   0.9008   0.0686
  -8.250  -0.3747   0.03767   0.03005  -0.1163   0.8911   0.0704
  -8.000  -0.3577   0.03482   0.02671  -0.1165   0.8848   0.0719
  -7.750  -0.3326   0.03375   0.02559  -0.1168   0.8795   0.0732
  -7.500  -0.3116   0.03300   0.02478  -0.1162   0.8714   0.0747
  -7.250  -0.2846   0.03193   0.02354  -0.1167   0.8666   0.0770
  -7.000  -0.2634   0.03072   0.02206  -0.1162   0.8594   0.0796
  -6.750  -0.2404   0.02928   0.02023  -0.1160   0.8529   0.0823
  -6.500  -0.2121   0.02821   0.01906  -0.1165   0.8488   0.0847
  -6.250  -0.1887   0.02780   0.01864  -0.1160   0.8419   0.0871
  -6.000  -0.1628   0.02722   0.01795  -0.1159   0.8359   0.0903
  -5.750  -0.1335   0.02631   0.01681  -0.1163   0.8318   0.0944
  -5.500  -0.1092   0.02560   0.01591  -0.1159   0.8255   0.0979
  -5.250  -0.0834   0.02523   0.01557  -0.1157   0.8197   0.1014
  -5.000  -0.0540   0.02472   0.01497  -0.1161   0.8157   0.1061
  -4.750  -0.0263   0.02417   0.01420  -0.1161   0.8109   0.1116
  -4.500  -0.0020   0.02381   0.01385  -0.1156   0.8045   0.1160
  -4.250   0.0267   0.02343   0.01342  -0.1158   0.8001   0.1217
  -4.000   0.0580   0.02296   0.01272  -0.1163   0.7969   0.1288
  -3.750   0.0807   0.02276   0.01261  -0.1157   0.7905   0.1340
  -3.500   0.1080   0.02247   0.01225  -0.1156   0.7856   0.1411
  -3.250   0.1379   0.02207   0.01179  -0.1160   0.7818   0.1482
  -3.000   0.1659   0.02181   0.01151  -0.1161   0.7777   0.1558
  -2.750   0.1900   0.02167   0.01135  -0.1155   0.7719   0.1630
  -2.500   0.2179   0.02142   0.01111  -0.1156   0.7675   0.1711
  -2.250   0.2483   0.02110   0.01077  -0.1160   0.7641   0.1800
  -2.000   0.2739   0.02099   0.01068  -0.1157   0.7592   0.1889
  -1.750   0.2985   0.02089   0.01063  -0.1152   0.7538   0.1977
  -1.500   0.3270   0.02072   0.01044  -0.1153   0.7497   0.2086
  -1.250   0.3577   0.02042   0.01019  -0.1158   0.7463   0.2201
  -1.000   0.3807   0.02043   0.01026  -0.1150   0.7399   0.2329
  -0.750   0.4073   0.02027   0.01015  -0.1147   0.7338   0.2503
  -0.500   0.4390   0.01988   0.00982  -0.1152   0.7289   0.2760
  -0.250   0.4613   0.01980   0.00988  -0.1142   0.7205   0.3098
   0.250   0.5139   0.01875   0.00963  -0.1134   0.7069   0.5284
   0.500   0.5305   0.01827   0.00987  -0.1104   0.6996   0.7351
   0.750   0.5754   0.01799   0.00982  -0.1125   0.6948   0.9263
   1.000   0.6259   0.01805   0.00979  -0.1172   0.6891   1.0000
   1.250   0.6460   0.01827   0.00993  -0.1158   0.6823   1.0000
   1.500   0.6728   0.01833   0.00985  -0.1156   0.6771   1.0000
   1.750   0.6967   0.01849   0.00992  -0.1148   0.6714   1.0000
   2.000   0.7171   0.01873   0.01013  -0.1135   0.6643   1.0000
   2.250   0.7450   0.01877   0.01005  -0.1134   0.6587   1.0000
   2.500   0.7665   0.01899   0.01024  -0.1123   0.6517   1.0000
   2.750   0.7895   0.01916   0.01036  -0.1114   0.6444   1.0000
   3.000   0.8192   0.01915   0.01024  -0.1116   0.6389   1.0000
   3.250   0.8359   0.01950   0.01063  -0.1097   0.6300   1.0000
   3.500   0.8633   0.01956   0.01061  -0.1095   0.6236   1.0000
   3.750   0.8830   0.01983   0.01089  -0.1081   0.6152   1.0000
   4.000   0.9079   0.01994   0.01095  -0.1075   0.6075   1.0000
   4.250   0.9285   0.02017   0.01118  -0.1062   0.5985   1.0000
   4.500   0.9528   0.02027   0.01124  -0.1055   0.5899   1.0000
   4.750   0.9718   0.02054   0.01153  -0.1040   0.5797   1.0000
   5.000   0.9981   0.02058   0.01151  -0.1035   0.5712   1.0000
   5.250   1.0144   0.02095   0.01191  -0.1016   0.5599   1.0000
   5.500   1.0363   0.02115   0.01209  -0.1005   0.5499   1.0000
   5.750   1.0578   0.02135   0.01226  -0.0994   0.5394   1.0000
   6.000   1.0752   0.02169   0.01261  -0.0976   0.5276   1.0000
   6.250   1.0954   0.02195   0.01284  -0.0963   0.5164   1.0000
   6.500   1.1163   0.02218   0.01302  -0.0951   0.5052   1.0000
   6.750   1.1310   0.02259   0.01343  -0.0929   0.4928   1.0000
   7.000   1.1475   0.02298   0.01378  -0.0910   0.4812   1.0000
   7.250   1.1661   0.02333   0.01406  -0.0895   0.4698   1.0000
   7.500   1.1814   0.02382   0.01450  -0.0875   0.4578   1.0000
   7.750   1.1963   0.02436   0.01502  -0.0856   0.4461   1.0000
   8.000   1.2132   0.02487   0.01547  -0.0840   0.4354   1.0000
   8.250   1.2289   0.02546   0.01603  -0.0823   0.4251   1.0000
   8.500   1.2441   0.02610   0.01666  -0.0806   0.4154   1.0000
   8.750   1.2612   0.02668   0.01718  -0.0792   0.4064   1.0000
   9.000   1.2749   0.02744   0.01798  -0.0774   0.3974   1.0000
   9.250   1.2929   0.02804   0.01854  -0.0762   0.3900   1.0000
   9.500   1.3073   0.02883   0.01938  -0.0747   0.3826   1.0000
   9.750   1.3233   0.02955   0.02012  -0.0734   0.3755   1.0000
  10.000   1.3393   0.03029   0.02087  -0.0721   0.3686   1.0000
  10.250   1.3517   0.03120   0.02185  -0.0704   0.3611   1.0000
  10.500   1.3694   0.03188   0.02247  -0.0693   0.3544   1.0000
  10.750   1.3786   0.03297   0.02372  -0.0675   0.3470   1.0000
  11.000   1.3929   0.03382   0.02457  -0.0661   0.3401   1.0000
  11.250   1.4035   0.03490   0.02573  -0.0645   0.3330   1.0000
  11.500   1.4127   0.03605   0.02695  -0.0628   0.3253   1.0000
  11.750   1.4239   0.03711   0.02804  -0.0613   0.3181   1.0000
  12.000   1.4292   0.03855   0.02961  -0.0595   0.3100   1.0000
  12.250   1.4398   0.03966   0.03071  -0.0581   0.3027   1.0000
  12.500   1.4414   0.04145   0.03268  -0.0562   0.2941   1.0000
  12.750   1.4484   0.04283   0.03406  -0.0547   0.2862   1.0000
  13.000   1.4479   0.04491   0.03632  -0.0529   0.2768   1.0000
  13.250   1.4512   0.04668   0.03814  -0.0515   0.2683   1.0000
  13.500   1.4507   0.04889   0.04048  -0.0500   0.2587   1.0000
  13.750   1.4510   0.05114   0.04281  -0.0487   0.2493   1.0000
  14.000   1.4511   0.05341   0.04511  -0.0475   0.2402   1.0000
  14.250   1.4495   0.05604   0.04788  -0.0465   0.2306   1.0000
  14.500   1.4491   0.05856   0.05042  -0.0456   0.2221   1.0000
  14.750   1.4476   0.06129   0.05321  -0.0447   0.2135   1.0000
  15.000   1.4467   0.06402   0.05598  -0.0440   0.2060   1.0000
  15.250   1.4454   0.06681   0.05880  -0.0433   0.1990   1.0000
  15.500   1.4448   0.06961   0.06164  -0.0428   0.1927   1.0000
  15.750   1.4437   0.07252   0.06461  -0.0423   0.1867   1.0000
  16.000   1.4448   0.07511   0.06717  -0.0419   0.1816   1.0000
  16.250   1.4429   0.07828   0.07047  -0.0416   0.1761   1.0000
  16.500   1.4437   0.08099   0.07319  -0.0413   0.1712   1.0000
  16.750   1.4447   0.08375   0.07599  -0.0411   0.1664   1.0000
  17.000   1.4413   0.08724   0.07961  -0.0412   0.1614   1.0000
  17.250   1.4433   0.08983   0.08218  -0.0411   0.1565   1.0000
  17.500   1.4404   0.09329   0.08577  -0.0414   0.1519   1.0000
  17.750   1.4346   0.09728   0.08989  -0.0420   0.1470   1.0000
  18.000   1.4355   0.10010   0.09270  -0.0423   0.1422   1.0000
  18.250   1.4282   0.10447   0.09722  -0.0432   0.1377   1.0000
  18.500   1.4193   0.10917   0.10208  -0.0445   0.1330   1.0000
  18.750   1.4170   0.11270   0.10563  -0.0455   0.1284   1.0000
  19.000   1.4096   0.11725   0.11030  -0.0470   0.1241   1.0000
  19.250   1.3977   0.12274   0.11599  -0.0491   0.1195   1.0000
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