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GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 493 AIRFOIL (goe493-il)
Reynolds number: 200,000
Max Cl/Cd: 75.69 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe493-il-200000.txt
Download as CSV file: xf-goe493-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 493 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.5903   0.08290   0.07897  -0.0776   1.0000   0.0365
 -13.500  -0.6285   0.07395   0.06994  -0.0822   1.0000   0.0357
 -13.250  -0.6700   0.06592   0.06178  -0.0862   1.0000   0.0349
 -13.000  -0.7051   0.06034   0.05607  -0.0879   1.0000   0.0346
 -12.750  -0.7402   0.05594   0.05156  -0.0878   1.0000   0.0344
 -12.500  -0.7731   0.05269   0.04819  -0.0862   1.0000   0.0342
 -12.250  -0.8067   0.05004   0.04542  -0.0834   1.0000   0.0339
 -12.000  -0.8416   0.04799   0.04325  -0.0792   1.0000   0.0336
 -11.750  -0.8766   0.04668   0.04183  -0.0733   1.0000   0.0335
 -11.500  -0.8950   0.04516   0.04017  -0.0691   0.9993   0.0337
 -11.250  -0.8825   0.04230   0.03700  -0.0712   0.9943   0.0346
 -11.000  -0.8708   0.03963   0.03397  -0.0722   0.9888   0.0356
 -10.750  -0.8526   0.03724   0.03110  -0.0737   0.9840   0.0367
 -10.500  -0.8362   0.03463   0.02824  -0.0739   0.9791   0.0375
 -10.250  -0.8130   0.03290   0.02650  -0.0747   0.9748   0.0390
 -10.000  -0.7841   0.03138   0.02483  -0.0764   0.9715   0.0406
  -9.750  -0.7631   0.03011   0.02336  -0.0763   0.9664   0.0424
  -9.500  -0.7402   0.02860   0.02166  -0.0766   0.9614   0.0447
  -9.250  -0.7095   0.02744   0.02052  -0.0782   0.9582   0.0475
  -9.000  -0.6816   0.02643   0.01935  -0.0790   0.9545   0.0507
  -8.750  -0.6638   0.02525   0.01816  -0.0780   0.9480   0.0540
  -8.500  -0.6324   0.02446   0.01728  -0.0794   0.9444   0.0596
  -8.250  -0.5983   0.02348   0.01632  -0.0814   0.9420   0.0671
  -8.000  -0.5841   0.02278   0.01560  -0.0794   0.9343   0.0739
  -7.750  -0.5540   0.02214   0.01494  -0.0804   0.9302   0.0854
  -7.500  -0.5178   0.02154   0.01431  -0.0825   0.9276   0.0994
  -7.250  -0.4956   0.02115   0.01388  -0.0818   0.9217   0.1110
  -7.000  -0.4689   0.02082   0.01346  -0.0819   0.9162   0.1228
  -6.750  -0.4330   0.02041   0.01299  -0.0839   0.9133   0.1359
  -6.500  -0.3948   0.01989   0.01248  -0.0862   0.9114   0.1494
  -6.250  -0.3795   0.01959   0.01221  -0.0841   0.9033   0.1581
  -6.000  -0.3465   0.01913   0.01172  -0.0853   0.8995   0.1704
  -5.750  -0.3083   0.01863   0.01121  -0.0875   0.8972   0.1844
  -5.500  -0.2683   0.01807   0.01068  -0.0901   0.8956   0.2007
  -5.250  -0.2533   0.01792   0.01050  -0.0877   0.8872   0.2133
  -5.000  -0.2197   0.01734   0.01004  -0.0891   0.8838   0.2328
  -4.750  -0.1821   0.01677   0.00956  -0.0911   0.8814   0.2599
  -4.500  -0.1447   0.01616   0.00909  -0.0931   0.8795   0.2949
  -4.250  -0.1299   0.01600   0.00904  -0.0907   0.8710   0.3254
  -4.000  -0.0983   0.01557   0.00877  -0.0914   0.8670   0.3659
  -3.750  -0.0618   0.01520   0.00847  -0.0930   0.8645   0.4078
  -3.500  -0.0242   0.01488   0.00822  -0.0947   0.8625   0.4435
  -3.250  -0.0114   0.01495   0.00833  -0.0918   0.8527   0.4658
  -3.000   0.0238   0.01470   0.00809  -0.0930   0.8494   0.4931
  -2.750   0.0613   0.01443   0.00783  -0.0946   0.8470   0.5185
  -2.500   0.0772   0.01452   0.00793  -0.0922   0.8380   0.5364
  -2.250   0.1105   0.01431   0.00771  -0.0930   0.8340   0.5573
  -2.000   0.1472   0.01403   0.00746  -0.0944   0.8312   0.5775
  -1.750   0.1646   0.01408   0.00754  -0.0923   0.8223   0.5942
  -1.500   0.1969   0.01387   0.00736  -0.0929   0.8180   0.6139
  -1.250   0.2325   0.01363   0.00713  -0.0941   0.8149   0.6348
  -1.000   0.2496   0.01368   0.00724  -0.0918   0.8057   0.6519
  -0.750   0.2823   0.01346   0.00705  -0.0925   0.8013   0.6715
  -0.500   0.3092   0.01339   0.00701  -0.0921   0.7954   0.6901
  -0.250   0.3336   0.01332   0.00700  -0.0912   0.7883   0.7088
   0.000   0.3671   0.01311   0.00683  -0.0920   0.7841   0.7290
   0.250   0.3871   0.01311   0.00691  -0.0902   0.7756   0.7497
   0.500   0.4177   0.01290   0.00673  -0.0903   0.7696   0.7732
   0.750   0.4414   0.01279   0.00668  -0.0891   0.7612   0.7958
   1.000   0.4706   0.01255   0.00648  -0.0889   0.7539   0.8211
   1.250   0.4946   0.01245   0.00646  -0.0877   0.7454   0.8479
   1.500   0.5258   0.01231   0.00638  -0.0880   0.7386   0.8777
   1.750   0.5634   0.01229   0.00641  -0.0897   0.7319   0.9085
   2.000   0.6104   0.01231   0.00645  -0.0935   0.7244   0.9350
   2.250   0.6632   0.01233   0.00643  -0.0986   0.7185   0.9551
   2.500   0.7124   0.01242   0.00655  -0.1032   0.7100   0.9729
   2.750   0.7650   0.01241   0.00649  -0.1083   0.7034   0.9865
   3.000   0.8096   0.01249   0.00659  -0.1123   0.6939   1.0000
   3.250   0.8274   0.01252   0.00655  -0.1107   0.6869   1.0000
   3.500   0.8404   0.01265   0.00668  -0.1080   0.6781   1.0000
   3.750   0.8644   0.01274   0.00671  -0.1073   0.6711   1.0000
   4.000   0.8814   0.01289   0.00689  -0.1053   0.6620   1.0000
   4.250   0.9053   0.01301   0.00698  -0.1045   0.6542   1.0000
   4.500   0.9249   0.01316   0.00713  -0.1029   0.6449   1.0000
   4.750   0.9465   0.01332   0.00728  -0.1016   0.6361   1.0000
   5.000   0.9705   0.01340   0.00732  -0.1007   0.6257   1.0000
   5.250   0.9870   0.01351   0.00745  -0.0984   0.6127   1.0000
   5.500   1.0048   0.01361   0.00753  -0.0962   0.5988   1.0000
   5.750   1.0230   0.01373   0.00765  -0.0942   0.5851   1.0000
   6.000   1.0401   0.01385   0.00774  -0.0919   0.5700   1.0000
   6.250   1.0552   0.01398   0.00785  -0.0893   0.5534   1.0000
   6.500   1.0702   0.01414   0.00799  -0.0867   0.5369   1.0000
   6.750   1.0846   0.01434   0.00818  -0.0840   0.5201   1.0000
   7.000   1.0976   0.01456   0.00838  -0.0811   0.5025   1.0000
   7.250   1.1085   0.01482   0.00859  -0.0778   0.4834   1.0000
   7.500   1.1164   0.01511   0.00884  -0.0740   0.4645   1.0000
   7.750   1.1233   0.01544   0.00917  -0.0700   0.4440   1.0000
   8.000   1.1300   0.01586   0.00953  -0.0662   0.4222   1.0000
   8.250   1.1362   0.01637   0.00998  -0.0624   0.3984   1.0000
   8.500   1.1397   0.01703   0.01052  -0.0584   0.3722   1.0000
   8.750   1.1408   0.01787   0.01122  -0.0542   0.3423   1.0000
   9.000   1.1394   0.01891   0.01210  -0.0499   0.3072   1.0000
   9.250   1.1306   0.02039   0.01332  -0.0448   0.2507   1.0000
   9.500   1.1088   0.02283   0.01517  -0.0389   0.1660   1.0000
   9.750   1.0923   0.02539   0.01733  -0.0341   0.1119   1.0000
  10.000   1.0855   0.02753   0.01927  -0.0306   0.0882   1.0000
  10.250   1.0832   0.02946   0.02114  -0.0279   0.0791   1.0000
  10.500   1.0855   0.03116   0.02288  -0.0257   0.0733   1.0000
  10.750   1.0825   0.03331   0.02501  -0.0233   0.0693   1.0000
  11.000   1.0892   0.03482   0.02661  -0.0217   0.0661   1.0000
  11.250   1.0945   0.03649   0.02833  -0.0202   0.0633   1.0000
  11.500   1.0982   0.03834   0.03021  -0.0186   0.0608   1.0000
  11.750   1.0995   0.04043   0.03225  -0.0169   0.0586   1.0000
  12.000   1.1095   0.04187   0.03380  -0.0158   0.0569   1.0000
  12.250   1.1188   0.04339   0.03539  -0.0147   0.0549   1.0000
  12.500   1.1281   0.04493   0.03697  -0.0137   0.0530   1.0000
  12.750   1.1379   0.04647   0.03848  -0.0126   0.0511   1.0000
  13.000   1.1557   0.04760   0.03954  -0.0113   0.0492   1.0000
  13.250   1.1666   0.04908   0.04117  -0.0105   0.0478   1.0000
  13.500   1.1794   0.05050   0.04269  -0.0097   0.0463   1.0000
  13.750   1.1932   0.05190   0.04416  -0.0088   0.0448   1.0000
  14.000   1.2076   0.05331   0.04560  -0.0081   0.0435   1.0000
  14.250   1.2423   0.05428   0.04648  -0.0077   0.0413   1.0000
  14.500   1.2456   0.05634   0.04876  -0.0067   0.0405   1.0000
  14.750   1.2527   0.05842   0.05104  -0.0059   0.0396   1.0000
  15.000   1.2610   0.06061   0.05341  -0.0051   0.0387   1.0000
  15.250   1.2681   0.06289   0.05585  -0.0044   0.0378   1.0000
  15.500   1.2752   0.06518   0.05827  -0.0039   0.0369   1.0000
  15.750   1.2803   0.06757   0.06077  -0.0034   0.0361   1.0000
  16.000   1.1328   0.07472   0.06896   0.0002   0.0376   1.0000
  16.250   1.1250   0.07834   0.07276  -0.0001   0.0370   1.0000
  16.500   1.1155   0.08193   0.07653  -0.0006   0.0365   1.0000
  16.750   1.0976   0.08562   0.08045  -0.0015   0.0362   1.0000
  17.000   1.0800   0.08959   0.08462  -0.0028   0.0359   1.0000
  17.250   1.0618   0.09395   0.08920  -0.0046   0.0356   1.0000
  17.500   1.0369   0.09940   0.09490  -0.0073   0.0356   1.0000
  17.750   1.1961   0.10354   0.09846  -0.0076   0.0336   1.0000
  18.000   1.1749   0.11010   0.10525  -0.0102   0.0336   1.0000
  18.250   1.1526   0.11717   0.11253  -0.0135   0.0337   1.0000
  18.500   1.1298   0.12477   0.12032  -0.0174   0.0339   1.0000
  18.750   1.1061   0.13301   0.12874  -0.0219   0.0341   1.0000
  19.000   1.0856   0.14124   0.13710  -0.0263   0.0344   1.0000
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