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GOE 683 AIRFOIL (goe683-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 683 AIRFOIL (goe683-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.24 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe683-il-1000000.txt
Download as CSV file: xf-goe683-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 683 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1053   0.07278   0.06900  -0.0721   1.0000   0.0375
 -19.500  -1.1189   0.06792   0.06404  -0.0743   1.0000   0.0378
 -19.250  -1.1294   0.06347   0.05950  -0.0764   1.0000   0.0381
 -19.000  -1.1406   0.05904   0.05498  -0.0783   1.0000   0.0384
 -18.750  -1.1492   0.05501   0.05084  -0.0800   1.0000   0.0386
 -18.500  -1.1573   0.05115   0.04688  -0.0815   1.0000   0.0388
 -18.250  -1.1588   0.04809   0.04372  -0.0825   1.0000   0.0391
 -18.000  -1.1683   0.04433   0.03987  -0.0836   1.0000   0.0395
 -17.750  -1.1774   0.04081   0.03628  -0.0843   1.0000   0.0399
 -17.500  -1.1822   0.03793   0.03333  -0.0845   1.0000   0.0402
 -17.250  -1.1828   0.03561   0.03095  -0.0843   1.0000   0.0407
 -17.000  -1.1816   0.03360   0.02888  -0.0838   1.0000   0.0410
 -16.750  -1.1768   0.03201   0.02725  -0.0830   1.0000   0.0415
 -16.500  -1.1727   0.03049   0.02567  -0.0820   1.0000   0.0419
 -16.250  -1.1674   0.02917   0.02429  -0.0807   1.0000   0.0424
 -16.000  -1.1618   0.02796   0.02303  -0.0791   1.0000   0.0428
 -15.750  -1.1540   0.02696   0.02198  -0.0775   1.0000   0.0432
 -15.500  -1.1465   0.02602   0.02097  -0.0757   1.0000   0.0437
 -15.250  -1.1378   0.02520   0.02009  -0.0738   1.0000   0.0440
 -15.000  -1.1395   0.02393   0.01879  -0.0707   1.0000   0.0447
 -14.750  -1.1341   0.02308   0.01792  -0.0681   1.0000   0.0452
 -14.500  -1.1267   0.02238   0.01720  -0.0655   1.0000   0.0458
 -14.250  -1.1183   0.02178   0.01657  -0.0629   1.0000   0.0464
 -14.000  -1.1098   0.02124   0.01601  -0.0602   1.0000   0.0469
 -13.750  -1.0813   0.02073   0.01547  -0.0611   0.9990   0.0478
 -13.500  -1.0448   0.02010   0.01480  -0.0637   0.9961   0.0486
 -13.250  -1.0198   0.01953   0.01420  -0.0636   0.9818   0.0491
 -13.000  -0.9947   0.01850   0.01314  -0.0644   0.9583   0.0503
 -12.750  -0.9446   0.01782   0.01245  -0.0697   0.9402   0.0516
 -12.500  -0.8845   0.01726   0.01182  -0.0769   0.9182   0.0529
 -12.250  -0.8223   0.01684   0.01128  -0.0844   0.8949   0.0543
 -12.000  -0.7700   0.01627   0.01057  -0.0903   0.8709   0.0556
 -11.750  -0.7372   0.01583   0.01004  -0.0921   0.8485   0.0569
 -11.500  -0.7104   0.01554   0.00967  -0.0924   0.8307   0.0580
 -11.250  -0.6864   0.01530   0.00933  -0.0920   0.8148   0.0591
 -11.000  -0.6652   0.01505   0.00903  -0.0910   0.8027   0.0599
 -10.750  -0.6439   0.01484   0.00873  -0.0900   0.7897   0.0606
 -10.500  -0.6265   0.01450   0.00832  -0.0883   0.7775   0.0618
 -10.250  -0.6098   0.01415   0.00793  -0.0864   0.7655   0.0631
 -10.000  -0.5909   0.01394   0.00765  -0.0848   0.7530   0.0643
  -9.750  -0.5719   0.01370   0.00738  -0.0832   0.7416   0.0652
  -9.500  -0.5526   0.01352   0.00713  -0.0816   0.7302   0.0662
  -9.250  -0.5329   0.01334   0.00688  -0.0801   0.7181   0.0672
  -9.000  -0.5126   0.01319   0.00666  -0.0786   0.7072   0.0680
  -8.750  -0.4972   0.01285   0.00627  -0.0763   0.6959   0.0695
  -8.500  -0.4787   0.01261   0.00600  -0.0745   0.6861   0.0711
  -8.250  -0.4595   0.01242   0.00577  -0.0728   0.6765   0.0725
  -8.000  -0.4396   0.01226   0.00555  -0.0712   0.6679   0.0736
  -7.750  -0.4190   0.01211   0.00536  -0.0697   0.6592   0.0747
  -7.500  -0.3994   0.01195   0.00513  -0.0680   0.6510   0.0762
  -7.250  -0.3800   0.01168   0.00486  -0.0664   0.6439   0.0785
  -7.000  -0.3598   0.01151   0.00466  -0.0648   0.6365   0.0803
  -6.750  -0.3390   0.01136   0.00447  -0.0633   0.6300   0.0821
  -6.500  -0.3174   0.01121   0.00429  -0.0620   0.6238   0.0841
  -6.250  -0.2974   0.01100   0.00408  -0.0603   0.6170   0.0876
  -6.000  -0.2771   0.01083   0.00389  -0.0588   0.6105   0.0918
  -5.750  -0.2565   0.01057   0.00370  -0.0573   0.6046   0.1018
  -5.500  -0.2377   0.01025   0.00353  -0.0555   0.5985   0.1348
  -5.250  -0.2167   0.01014   0.00343  -0.0541   0.5919   0.1489
  -5.000  -0.1940   0.00998   0.00333  -0.0530   0.5868   0.1592
  -4.750  -0.1712   0.00989   0.00323  -0.0518   0.5807   0.1669
  -4.500  -0.1496   0.00981   0.00315  -0.0504   0.5737   0.1747
  -4.250  -0.1258   0.00974   0.00307  -0.0495   0.5676   0.1792
  -4.000  -0.1031   0.00963   0.00298  -0.0483   0.5613   0.1873
  -3.750  -0.0809   0.00958   0.00291  -0.0471   0.5544   0.1941
  -3.500  -0.0576   0.00948   0.00284  -0.0460   0.5485   0.2022
  -3.250  -0.0345   0.00941   0.00278  -0.0450   0.5414   0.2103
  -3.000  -0.0128   0.00935   0.00271  -0.0436   0.5338   0.2206
  -2.750   0.0109   0.00928   0.00266  -0.0426   0.5271   0.2306
  -2.500   0.0332   0.00920   0.00261  -0.0414   0.5197   0.2442
  -2.250   0.0554   0.00914   0.00257  -0.0402   0.5125   0.2575
  -2.000   0.0785   0.00906   0.00253  -0.0391   0.5053   0.2734
  -1.750   0.1003   0.00901   0.00250  -0.0378   0.4978   0.2903
  -1.500   0.1229   0.00895   0.00247  -0.0366   0.4909   0.3075
  -1.250   0.1451   0.00887   0.00244  -0.0354   0.4841   0.3277
  -1.000   0.1657   0.00881   0.00243  -0.0338   0.4768   0.3518
  -0.750   0.1877   0.00867   0.00241  -0.0326   0.4713   0.3867
  -0.500   0.2078   0.00854   0.00240  -0.0310   0.4650   0.4301
  -0.250   0.2258   0.00843   0.00241  -0.0289   0.4586   0.4753
   0.000   0.2446   0.00828   0.00241  -0.0270   0.4541   0.5191
   0.250   0.2605   0.00812   0.00242  -0.0244   0.4493   0.5664
   0.500   0.2700   0.00795   0.00242  -0.0204   0.4444   0.6243
   0.750   0.2762   0.00782   0.00244  -0.0157   0.4390   0.6785
   1.000   0.2813   0.00756   0.00244  -0.0107   0.4361   0.7418
   1.250   0.3859   0.00771   0.00303  -0.0271   0.4285   0.8729
   1.500   0.4255   0.00806   0.00334  -0.0294   0.4215   0.8908
   1.750   0.4610   0.00832   0.00360  -0.0308   0.4180   0.8997
   2.000   0.4774   0.00842   0.00369  -0.0282   0.4137   0.9105
   2.250   0.5080   0.00871   0.00394  -0.0286   0.4084   0.9147
   2.500   0.5155   0.00886   0.00407  -0.0241   0.4042   0.9250
   2.750   0.5534   0.00914   0.00433  -0.0261   0.3997   0.9266
   3.000   0.5930   0.00943   0.00460  -0.0285   0.3959   0.9288
   3.250   0.6297   0.00974   0.00487  -0.0302   0.3918   0.9320
   3.500   0.6365   0.00990   0.00502  -0.0257   0.3883   0.9400
   3.750   0.6840   0.01030   0.00537  -0.0297   0.3834   0.9412
   4.000   0.7277   0.01053   0.00561  -0.0330   0.3799   0.9426
   4.250   0.7676   0.01077   0.00583  -0.0355   0.3758   0.9442
   4.500   0.8031   0.01101   0.00603  -0.0371   0.3713   0.9465
   4.750   0.8107   0.01131   0.00631  -0.0328   0.3673   0.9541
   5.000   0.8528   0.01146   0.00646  -0.0359   0.3639   0.9549
   5.250   0.8924   0.01158   0.00657  -0.0384   0.3595   0.9558
   5.500   0.9275   0.01173   0.00670  -0.0400   0.3545   0.9569
   5.750   0.9628   0.01194   0.00687  -0.0417   0.3498   0.9586
   6.000   0.9985   0.01209   0.00703  -0.0435   0.3465   0.9610
   6.250   1.0120   0.01242   0.00737  -0.0405   0.3436   0.9678
   6.500   1.0500   0.01246   0.00741  -0.0428   0.3391   0.9686
   6.750   1.0843   0.01257   0.00749  -0.0444   0.3343   0.9696
   7.000   1.1180   0.01268   0.00759  -0.0459   0.3300   0.9710
   7.250   1.1507   0.01276   0.00768  -0.0471   0.3263   0.9728
   7.500   1.1784   0.01291   0.00783  -0.0473   0.3221   0.9753
   7.750   1.1846   0.01336   0.00827  -0.0430   0.3180   0.9806
   8.000   1.2137   0.01335   0.00825  -0.0437   0.3124   0.9813
   8.250   1.2440   0.01335   0.00826  -0.0445   0.3081   0.9822
   8.500   1.2710   0.01342   0.00833  -0.0447   0.3035   0.9835
   8.750   1.2913   0.01357   0.00845  -0.0436   0.2985   0.9852
   9.000   1.3129   0.01365   0.00857  -0.0427   0.2949   0.9869
   9.250   1.3314   0.01380   0.00873  -0.0412   0.2901   0.9890
   9.500   1.3511   0.01414   0.00905  -0.0400   0.2852   0.9928
   9.750   1.3786   0.01420   0.00911  -0.0405   0.2802   0.9941
  10.000   1.4039   0.01429   0.00922  -0.0406   0.2748   0.9954
  10.250   1.4258   0.01453   0.00943  -0.0402   0.2679   0.9975
  10.750   1.4662   0.01502   0.00994  -0.0386   0.2563   1.0000
  11.000   1.4679   0.01551   0.01043  -0.0344   0.2512   1.0000
  11.250   1.4730   0.01597   0.01090  -0.0309   0.2458   1.0000
  11.500   1.4755   0.01656   0.01150  -0.0272   0.2392   1.0000
  11.750   1.4756   0.01732   0.01225  -0.0233   0.2321   1.0000
  12.000   1.4782   0.01807   0.01300  -0.0200   0.2249   1.0000
  12.250   1.4767   0.01907   0.01399  -0.0164   0.2166   1.0000
  12.500   1.4738   0.02024   0.01513  -0.0128   0.2064   1.0000
  12.750   1.4670   0.02172   0.01657  -0.0091   0.1926   1.0000
  13.000   1.4652   0.02305   0.01789  -0.0062   0.1834   1.0000
  13.250   1.4462   0.02550   0.02024  -0.0020   0.1633   1.0000
  13.500   1.4287   0.02808   0.02275   0.0016   0.1473   1.0000
  13.750   1.4147   0.03062   0.02526   0.0046   0.1371   1.0000
  14.000   1.4094   0.03270   0.02736   0.0067   0.1324   1.0000
  14.250   1.4067   0.03467   0.02936   0.0084   0.1296   1.0000
  14.500   1.4003   0.03703   0.03174   0.0102   0.1257   1.0000
  14.750   1.4007   0.03891   0.03368   0.0115   0.1238   1.0000
  15.000   1.3974   0.04117   0.03598   0.0129   0.1213   1.0000
  15.250   1.3955   0.04337   0.03823   0.0140   0.1201   1.0000
  15.500   1.3883   0.04611   0.04101   0.0152   0.1174   1.0000
  15.750   1.3846   0.04861   0.04356   0.0162   0.1161   1.0000
  16.000   1.3800   0.05126   0.04625   0.0170   0.1139   1.0000
  16.250   1.3798   0.05355   0.04861   0.0177   0.1131   1.0000
  16.500   1.3799   0.05581   0.05093   0.0183   0.1115   1.0000
  16.750   1.3780   0.05834   0.05352   0.0188   0.1104   1.0000
  17.000   1.3737   0.06118   0.05641   0.0193   0.1088   1.0000
  17.250   1.3691   0.06408   0.05936   0.0197   0.1073   1.0000
  17.500   1.3602   0.06750   0.06282   0.0200   0.1054   1.0000
  17.750   1.3511   0.07101   0.06639   0.0201   0.1037   1.0000
  18.000   1.3528   0.07331   0.06875   0.0203   0.1029   1.0000
  18.250   1.3540   0.07575   0.07125   0.0204   0.1016   1.0000
  18.500   1.3543   0.07823   0.07379   0.0205   0.1000   1.0000
  18.750   1.3498   0.08133   0.07694   0.0204   0.0983   1.0000
  19.000   1.3463   0.08432   0.07996   0.0203   0.0965   1.0000
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