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GOE 683 AIRFOIL (goe683-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 683 AIRFOIL (goe683-il)
Reynolds number: 200,000
Max Cl/Cd: 59.26 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe683-il-200000-n5.txt
Download as CSV file: xf-goe683-il-200000-n5.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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8015   0.08320   0.07779  -0.0730   1.0000   0.0525
 -17.250  -0.8337   0.07519   0.06955  -0.0778   1.0000   0.0529
 -17.000  -0.8573   0.06889   0.06303  -0.0813   1.0000   0.0533
 -16.750  -0.8756   0.06364   0.05759  -0.0839   1.0000   0.0537
 -16.500  -0.8927   0.05888   0.05260  -0.0860   1.0000   0.0542
 -16.250  -0.9078   0.05470   0.04819  -0.0875   1.0000   0.0547
 -16.000  -0.9062   0.05245   0.04591  -0.0876   1.0000   0.0551
 -15.750  -0.9043   0.05035   0.04379  -0.0876   1.0000   0.0556
 -15.500  -0.9035   0.04825   0.04164  -0.0875   1.0000   0.0561
 -15.250  -0.9033   0.04615   0.03948  -0.0871   1.0000   0.0565
 -15.000  -0.9032   0.04420   0.03746  -0.0864   1.0000   0.0570
 -14.750  -0.9029   0.04238   0.03555  -0.0855   1.0000   0.0576
 -14.500  -0.9023   0.04068   0.03376  -0.0843   1.0000   0.0582
 -14.250  -0.9016   0.03911   0.03209  -0.0827   1.0000   0.0588
 -14.000  -0.9012   0.03765   0.03051  -0.0809   1.0000   0.0596
 -13.750  -0.9002   0.03633   0.02907  -0.0787   1.0000   0.0603
 -13.500  -0.9002   0.03514   0.02772  -0.0762   1.0000   0.0610
 -13.250  -0.8937   0.03413   0.02673  -0.0741   1.0000   0.0616
 -13.000  -0.8886   0.03322   0.02584  -0.0717   1.0000   0.0623
 -12.750  -0.8850   0.03240   0.02501  -0.0689   1.0000   0.0630
 -12.500  -0.8617   0.03111   0.02371  -0.0696   0.9870   0.0640
 -12.250  -0.8383   0.03001   0.02254  -0.0703   0.9691   0.0652
 -12.000  -0.8107   0.02895   0.02136  -0.0717   0.9500   0.0664
 -11.750  -0.7768   0.02795   0.02017  -0.0743   0.9340   0.0679
 -11.500  -0.7368   0.02674   0.01897  -0.0780   0.9210   0.0694
 -11.250  -0.6933   0.02566   0.01784  -0.0824   0.9073   0.0711
 -11.000  -0.6489   0.02466   0.01673  -0.0869   0.8921   0.0730
 -10.750  -0.6068   0.02381   0.01571  -0.0907   0.8755   0.0750
 -10.500  -0.5722   0.02295   0.01476  -0.0932   0.8583   0.0768
 -10.250  -0.5465   0.02222   0.01397  -0.0937   0.8411   0.0784
 -10.000  -0.5258   0.02166   0.01331  -0.0931   0.8249   0.0800
  -9.750  -0.5072   0.02118   0.01273  -0.0919   0.8098   0.0817
  -9.500  -0.4889   0.02075   0.01217  -0.0905   0.7962   0.0834
  -9.250  -0.4746   0.02030   0.01164  -0.0883   0.7827   0.0850
  -9.000  -0.4620   0.01981   0.01112  -0.0859   0.7705   0.0870
  -8.750  -0.4471   0.01941   0.01065  -0.0837   0.7594   0.0891
  -8.500  -0.4322   0.01905   0.01022  -0.0814   0.7482   0.0914
  -8.250  -0.4163   0.01870   0.00978  -0.0793   0.7382   0.0939
  -8.000  -0.4020   0.01832   0.00940  -0.0769   0.7274   0.0970
  -7.750  -0.3855   0.01799   0.00902  -0.0748   0.7183   0.1012
  -7.500  -0.3692   0.01767   0.00870  -0.0727   0.7084   0.1061
  -7.250  -0.3518   0.01737   0.00839  -0.0708   0.6998   0.1142
  -7.000  -0.3341   0.01709   0.00814  -0.0689   0.6909   0.1253
  -6.750  -0.3155   0.01687   0.00788  -0.0671   0.6821   0.1380
  -6.500  -0.2966   0.01666   0.00766  -0.0654   0.6741   0.1500
  -6.250  -0.2778   0.01645   0.00744  -0.0636   0.6659   0.1597
  -6.000  -0.2577   0.01629   0.00721  -0.0620   0.6589   0.1691
  -5.750  -0.2383   0.01611   0.00704  -0.0604   0.6510   0.1782
  -5.500  -0.2182   0.01596   0.00684  -0.0588   0.6433   0.1864
  -5.250  -0.1980   0.01581   0.00666  -0.0572   0.6362   0.1944
  -5.000  -0.1774   0.01568   0.00650  -0.0558   0.6287   0.2025
  -4.750  -0.1573   0.01554   0.00634  -0.0542   0.6221   0.2104
  -4.500  -0.1361   0.01543   0.00620  -0.0528   0.6155   0.2191
  -4.250  -0.1163   0.01529   0.00608  -0.0512   0.6083   0.2288
  -4.000  -0.0951   0.01520   0.00593  -0.0497   0.6015   0.2371
  -3.750  -0.0750   0.01507   0.00583  -0.0482   0.5945   0.2462
  -3.500  -0.0541   0.01498   0.00572  -0.0467   0.5875   0.2562
  -3.250  -0.0338   0.01487   0.00561  -0.0451   0.5814   0.2669
  -3.000  -0.0132   0.01477   0.00553  -0.0436   0.5748   0.2790
  -2.750   0.0074   0.01468   0.00545  -0.0421   0.5677   0.2931
  -2.500   0.0268   0.01456   0.00535  -0.0404   0.5614   0.3086
  -2.250   0.0462   0.01444   0.00529  -0.0386   0.5545   0.3261
  -2.000   0.0651   0.01431   0.00523  -0.0368   0.5478   0.3464
  -1.750   0.0833   0.01419   0.00516  -0.0348   0.5421   0.3716
  -1.500   0.0998   0.01403   0.00515  -0.0325   0.5358   0.4038
  -1.250   0.1147   0.01385   0.00513  -0.0298   0.5291   0.4453
  -1.000   0.1294   0.01371   0.00509  -0.0270   0.5234   0.4876
  -0.750   0.1442   0.01353   0.00510  -0.0242   0.5173   0.5323
  -0.500   0.1606   0.01336   0.00511  -0.0218   0.5113   0.5791
  -0.250   0.1829   0.01318   0.00511  -0.0205   0.5057   0.6326
   0.000   0.2307   0.01300   0.00520  -0.0246   0.4989   0.7045
   0.250   0.3543   0.01361   0.00603  -0.0439   0.4886   0.7842
   0.500   0.4146   0.01419   0.00661  -0.0499   0.4820   0.8134
   0.750   0.4510   0.01455   0.00695  -0.0512   0.4757   0.8342
   1.000   0.4771   0.01487   0.00721  -0.0505   0.4702   0.8557
   1.750   0.5550   0.01586   0.00810  -0.0486   0.4551   0.9019
   2.000   0.5793   0.01616   0.00831  -0.0477   0.4502   0.9122
   2.250   0.6114   0.01648   0.00859  -0.0485   0.4455   0.9205
   2.500   0.6440   0.01680   0.00890  -0.0493   0.4404   0.9291
   2.750   0.6708   0.01715   0.00922  -0.0490   0.4356   0.9394
   3.000   0.7115   0.01741   0.00939  -0.0517   0.4309   0.9440
   3.250   0.7439   0.01763   0.00959  -0.0527   0.4263   0.9498
   3.500   0.7706   0.01783   0.00981  -0.0526   0.4219   0.9554
   3.750   0.8054   0.01796   0.00991  -0.0542   0.4171   0.9587
   4.000   0.8356   0.01815   0.01004  -0.0549   0.4128   0.9636
   4.250   0.8659   0.01835   0.01023  -0.0556   0.4078   0.9690
   4.500   0.9021   0.01843   0.01032  -0.0575   0.4018   0.9732
   4.750   0.9301   0.01860   0.01045  -0.0578   0.3962   0.9780
   5.000   0.9579   0.01877   0.01056  -0.0581   0.3924   0.9814
   5.250   0.9896   0.01881   0.01066  -0.0593   0.3879   0.9841
   5.500   1.0187   0.01890   0.01078  -0.0599   0.3835   0.9873
   5.750   1.0460   0.01906   0.01093  -0.0602   0.3793   0.9907
   6.000   1.0746   0.01919   0.01102  -0.0607   0.3755   0.9934
   6.250   1.1057   0.01924   0.01112  -0.0618   0.3714   0.9964
   6.500   1.1369   0.01932   0.01125  -0.0629   0.3673   0.9993
   6.750   1.1561   0.01951   0.01147  -0.0616   0.3633   1.0000
   7.000   1.1703   0.01977   0.01171  -0.0593   0.3597   1.0000
   7.250   1.1843   0.02004   0.01196  -0.0570   0.3563   1.0000
   7.500   1.1978   0.02030   0.01230  -0.0546   0.3528   1.0000
   7.750   1.2102   0.02057   0.01263  -0.0520   0.3491   1.0000
   8.000   1.2212   0.02086   0.01294  -0.0491   0.3454   1.0000
   8.250   1.2313   0.02116   0.01324  -0.0462   0.3422   1.0000
   8.500   1.2378   0.02146   0.01354  -0.0425   0.3386   1.0000
   8.750   1.2418   0.02175   0.01392  -0.0384   0.3351   1.0000
   9.000   1.2457   0.02208   0.01430  -0.0344   0.3314   1.0000
   9.250   1.2503   0.02244   0.01470  -0.0306   0.3281   1.0000
   9.500   1.2550   0.02284   0.01511  -0.0269   0.3249   1.0000
   9.750   1.2602   0.02329   0.01556  -0.0234   0.3216   1.0000
  10.000   1.2649   0.02379   0.01616  -0.0201   0.3179   1.0000
  10.250   1.2702   0.02433   0.01678  -0.0169   0.3145   1.0000
  10.500   1.2750   0.02493   0.01741  -0.0138   0.3110   1.0000
  10.750   1.2795   0.02558   0.01807  -0.0108   0.3075   1.0000
  11.000   1.2848   0.02627   0.01881  -0.0081   0.3042   1.0000
  11.250   1.2887   0.02708   0.01971  -0.0053   0.3002   1.0000
  11.500   1.2913   0.02797   0.02065  -0.0025   0.2955   1.0000
  11.750   1.2942   0.02889   0.02158   0.0001   0.2913   1.0000
  12.000   1.2963   0.02995   0.02270   0.0026   0.2865   1.0000
  12.250   1.2983   0.03110   0.02393   0.0049   0.2818   1.0000
  12.500   1.2998   0.03232   0.02518   0.0072   0.2770   1.0000
  12.750   1.3012   0.03358   0.02646   0.0093   0.2723   1.0000
  13.000   1.3020   0.03504   0.02802   0.0113   0.2673   1.0000
  13.250   1.3017   0.03660   0.02964   0.0132   0.2621   1.0000
  13.500   1.3003   0.03826   0.03128   0.0150   0.2568   1.0000
  13.750   1.2991   0.04010   0.03324   0.0166   0.2513   1.0000
  14.000   1.2951   0.04218   0.03535   0.0181   0.2447   1.0000
  14.250   1.2921   0.04427   0.03749   0.0195   0.2391   1.0000
  14.500   1.2880   0.04661   0.03991   0.0207   0.2326   1.0000
  14.750   1.2809   0.04922   0.04251   0.0219   0.2256   1.0000
  15.000   1.2753   0.05192   0.04530   0.0228   0.2183   1.0000
  15.250   1.2650   0.05508   0.04846   0.0236   0.2101   1.0000
  15.500   1.2565   0.05825   0.05170   0.0242   0.2015   1.0000
  15.750   1.2447   0.06184   0.05530   0.0247   0.1926   1.0000
  16.000   1.2326   0.06558   0.05906   0.0250   0.1834   1.0000
  16.250   1.2204   0.06944   0.06294   0.0251   0.1741   1.0000
  16.500   1.2072   0.07349   0.06699   0.0251   0.1660   1.0000
  16.750   1.1961   0.07739   0.07090   0.0250   0.1586   1.0000
  17.000   1.1856   0.08128   0.07479   0.0249   0.1531   1.0000
  17.250   1.1774   0.08493   0.07845   0.0247   0.1479   1.0000
  17.500   1.1705   0.08841   0.08193   0.0245   0.1438   1.0000
  17.750   1.1664   0.09160   0.08514   0.0243   0.1403   1.0000
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