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GOE 683 AIRFOIL (goe683-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 683 AIRFOIL (goe683-il)
Reynolds number: 200,000
Max Cl/Cd: 58.11 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe683-il-200000.txt
Download as CSV file: xf-goe683-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6958   0.08071   0.07602  -0.0774   1.0000   0.0748
 -15.500  -0.7723   0.06813   0.06313  -0.0848   1.0000   0.0742
 -15.250  -0.8164   0.06133   0.05609  -0.0873   1.0000   0.0740
 -15.000  -0.8536   0.05630   0.05081  -0.0874   1.0000   0.0740
 -14.750  -0.8843   0.05263   0.04692  -0.0859   1.0000   0.0742
 -14.500  -0.9102   0.04972   0.04378  -0.0831   1.0000   0.0744
 -14.250  -0.9342   0.04738   0.04123  -0.0793   1.0000   0.0747
 -14.000  -0.9550   0.04554   0.03918  -0.0747   1.0000   0.0749
 -13.750  -0.9778   0.04411   0.03754  -0.0689   1.0000   0.0752
 -13.500  -0.9756   0.04179   0.03515  -0.0666   1.0000   0.0759
 -13.250  -0.9645   0.04027   0.03366  -0.0649   1.0000   0.0769
 -13.000  -0.9636   0.03924   0.03261  -0.0615   1.0000   0.0777
 -12.750  -0.9673   0.03843   0.03180  -0.0572   1.0000   0.0786
 -12.500  -0.9945   0.03829   0.03164  -0.0490   1.0000   0.0787
 -12.250  -0.9753   0.03696   0.03019  -0.0492   0.9948   0.0803
 -12.000  -0.9507   0.03532   0.02830  -0.0504   0.9855   0.0818
 -11.750  -0.9273   0.03389   0.02657  -0.0511   0.9760   0.0831
 -11.500  -0.8855   0.03165   0.02432  -0.0548   0.9703   0.0850
 -11.250  -0.8437   0.03027   0.02298  -0.0582   0.9650   0.0873
 -11.000  -0.8122   0.02907   0.02167  -0.0597   0.9551   0.0895
 -10.750  -0.7749   0.02778   0.02018  -0.0622   0.9487   0.0915
 -10.500  -0.7316   0.02616   0.01858  -0.0658   0.9404   0.0941
 -10.250  -0.6832   0.02498   0.01744  -0.0703   0.9340   0.0971
 -10.000  -0.6387   0.02390   0.01624  -0.0741   0.9240   0.1004
  -9.750  -0.5861   0.02258   0.01490  -0.0795   0.9151   0.1037
  -9.500  -0.5410   0.02171   0.01403  -0.0834   0.9012   0.1075
  -9.250  -0.5000   0.02099   0.01317  -0.0864   0.8869   0.1115
  -9.000  -0.4636   0.02023   0.01242  -0.0885   0.8724   0.1154
  -8.750  -0.4385   0.01983   0.01194  -0.0882   0.8567   0.1193
  -8.500  -0.4187   0.01952   0.01150  -0.0867   0.8416   0.1237
  -8.250  -0.3995   0.01910   0.01111  -0.0853   0.8287   0.1283
  -8.000  -0.3797   0.01881   0.01072  -0.0837   0.8165   0.1338
  -7.750  -0.3645   0.01845   0.01039  -0.0814   0.8041   0.1398
  -7.500  -0.3445   0.01821   0.01002  -0.0798   0.7940   0.1489
  -7.250  -0.3323   0.01784   0.00975  -0.0769   0.7825   0.1585
  -7.000  -0.3149   0.01751   0.00939  -0.0749   0.7736   0.1718
  -6.750  -0.3031   0.01725   0.00918  -0.0718   0.7629   0.1862
  -6.500  -0.2864   0.01704   0.00891  -0.0695   0.7544   0.2008
  -6.250  -0.2723   0.01698   0.00877  -0.0667   0.7444   0.2126
  -6.000  -0.2547   0.01675   0.00856  -0.0646   0.7360   0.2234
  -5.750  -0.2367   0.01663   0.00839  -0.0626   0.7275   0.2333
  -5.500  -0.2189   0.01649   0.00824  -0.0605   0.7187   0.2426
  -5.250  -0.1971   0.01635   0.00801  -0.0592   0.7113   0.2519
  -5.000  -0.1791   0.01620   0.00790  -0.0572   0.7020   0.2605
  -4.750  -0.1568   0.01607   0.00766  -0.0559   0.6944   0.2704
  -4.500  -0.1369   0.01590   0.00755  -0.0543   0.6861   0.2800
  -4.250  -0.1153   0.01575   0.00737  -0.0529   0.6780   0.2910
  -4.000  -0.0926   0.01560   0.00718  -0.0518   0.6710   0.3035
  -3.750  -0.0725   0.01539   0.00706  -0.0502   0.6622   0.3158
  -3.500  -0.0497   0.01520   0.00684  -0.0491   0.6546   0.3310
  -3.250  -0.0299   0.01504   0.00674  -0.0475   0.6467   0.3489
  -3.000  -0.0111   0.01481   0.00661  -0.0456   0.6388   0.3707
  -2.750   0.0083   0.01458   0.00647  -0.0438   0.6324   0.3999
  -2.500   0.0209   0.01439   0.00648  -0.0407   0.6244   0.4352
  -2.250   0.0340   0.01413   0.00640  -0.0376   0.6171   0.4808
  -2.000   0.0474   0.01390   0.00634  -0.0345   0.6108   0.5367
  -1.500   0.0901   0.01329   0.00636  -0.0313   0.5960   0.6818
  -1.250   0.2108   0.01371   0.00711  -0.0495   0.5853   0.7795
  -1.000   0.2739   0.01441   0.00777  -0.0557   0.5767   0.8121
  -0.750   0.3110   0.01495   0.00822  -0.0568   0.5699   0.8352
  -0.500   0.3377   0.01540   0.00866  -0.0559   0.5625   0.8554
  -0.250   0.3743   0.01591   0.00904  -0.0569   0.5559   0.8678
   0.000   0.4074   0.01638   0.00944  -0.0574   0.5494   0.8806
   0.250   0.4364   0.01679   0.00981  -0.0572   0.5423   0.8941
   0.500   0.4807   0.01722   0.01012  -0.0601   0.5361   0.9021
   0.750   0.5188   0.01769   0.01052  -0.0617   0.5297   0.9129
   1.000   0.5552   0.01813   0.01093  -0.0630   0.5228   0.9254
   1.250   0.6081   0.01841   0.01109  -0.0677   0.5166   0.9324
   1.500   0.6463   0.01870   0.01133  -0.0697   0.5108   0.9419
   1.750   0.6867   0.01884   0.01145  -0.0722   0.5041   0.9502
   2.000   0.7310   0.01889   0.01141  -0.0755   0.4984   0.9580
   2.250   0.7768   0.01904   0.01149  -0.0792   0.4928   0.9689
   2.500   0.8245   0.01901   0.01148  -0.0833   0.4863   0.9805
   2.750   0.8739   0.01862   0.01101  -0.0879   0.4805   0.9880
   3.000   0.9195   0.01838   0.01066  -0.0919   0.4753   0.9956
   3.250   0.9527   0.01815   0.01050  -0.0935   0.4699   1.0000
   3.500   0.9700   0.01825   0.01059  -0.0919   0.4652   1.0000
   3.750   0.9890   0.01835   0.01062  -0.0905   0.4608   1.0000
   4.000   1.0086   0.01856   0.01076  -0.0893   0.4565   1.0000
   4.250   1.0232   0.01868   0.01097  -0.0871   0.4509   1.0000
   4.500   1.0411   0.01881   0.01108  -0.0855   0.4460   1.0000
   4.750   1.0612   0.01896   0.01116  -0.0843   0.4418   1.0000
   5.000   1.0809   0.01922   0.01139  -0.0830   0.4376   1.0000
   5.250   1.0961   0.01944   0.01170  -0.0809   0.4331   1.0000
   5.500   1.1139   0.01964   0.01192  -0.0792   0.4287   1.0000
   5.750   1.1337   0.01982   0.01207  -0.0779   0.4247   1.0000
   6.000   1.1571   0.02012   0.01224  -0.0773   0.4205   1.0000
   6.250   1.1695   0.02037   0.01264  -0.0747   0.4162   1.0000
   6.500   1.1853   0.02061   0.01294  -0.0727   0.4116   1.0000
   6.750   1.2042   0.02084   0.01316  -0.0712   0.4077   1.0000
   7.000   1.2256   0.02109   0.01336  -0.0702   0.4042   1.0000
   7.250   1.2445   0.02148   0.01376  -0.0688   0.4007   1.0000
   7.500   1.2565   0.02184   0.01424  -0.0662   0.3968   1.0000
   7.750   1.2719   0.02215   0.01462  -0.0641   0.3928   1.0000
   8.000   1.2901   0.02241   0.01487  -0.0626   0.3891   1.0000
   8.250   1.3127   0.02265   0.01503  -0.0618   0.3852   1.0000
   8.500   1.3238   0.02305   0.01553  -0.0590   0.3811   1.0000
   8.750   1.3333   0.02341   0.01600  -0.0560   0.3769   1.0000
   9.000   1.3476   0.02372   0.01634  -0.0537   0.3730   1.0000
   9.250   1.3662   0.02395   0.01655  -0.0522   0.3694   1.0000
   9.500   1.3911   0.02432   0.01685  -0.0520   0.3661   1.0000
   9.750   1.3923   0.02484   0.01755  -0.0476   0.3627   1.0000
  10.000   1.3973   0.02526   0.01808  -0.0438   0.3587   1.0000
  10.250   1.4074   0.02556   0.01840  -0.0409   0.3548   1.0000
  10.500   1.4244   0.02574   0.01855  -0.0392   0.3510   1.0000
  10.750   1.4390   0.02617   0.01899  -0.0372   0.3475   1.0000
  11.000   1.4276   0.02668   0.01965  -0.0307   0.3440   1.0000
  11.250   1.4205   0.02707   0.02013  -0.0249   0.3403   1.0000
  11.500   1.4236   0.02735   0.02043  -0.0210   0.3365   1.0000
  11.750   1.4404   0.02753   0.02056  -0.0193   0.3327   1.0000
  12.000   1.4347   0.02818   0.02130  -0.0144   0.3289   1.0000
  12.250   1.4218   0.02902   0.02227  -0.0088   0.3249   1.0000
  12.500   1.4210   0.02965   0.02296  -0.0052   0.3206   1.0000
  12.750   1.4332   0.02991   0.02315  -0.0032   0.3160   1.0000
  13.000   1.4288   0.03090   0.02424   0.0005   0.3118   1.0000
  13.250   1.4159   0.03227   0.02576   0.0047   0.3071   1.0000
  13.500   1.4162   0.03320   0.02672   0.0074   0.3024   1.0000
  13.750   1.4334   0.03344   0.02687   0.0086   0.2975   1.0000
  14.000   1.4108   0.03572   0.02936   0.0127   0.2924   1.0000
  14.250   1.4039   0.03732   0.03103   0.0153   0.2867   1.0000
  14.500   1.4142   0.03793   0.03155   0.0167   0.2808   1.0000
  14.750   1.3921   0.04087   0.03469   0.0195   0.2746   1.0000
  15.000   1.3898   0.04251   0.03634   0.0212   0.2681   1.0000
  15.250   1.3810   0.04484   0.03873   0.0229   0.2613   1.0000
  15.500   1.3690   0.04760   0.04156   0.0244   0.2536   1.0000
  15.750   1.3610   0.05015   0.04413   0.0255   0.2457   1.0000
  16.000   1.3502   0.05311   0.04711   0.0265   0.2369   1.0000
  16.250   1.3350   0.05672   0.05078   0.0273   0.2276   1.0000
  16.500   1.3326   0.05898   0.05292   0.0281   0.2188   1.0000
  16.750   1.3137   0.06333   0.05738   0.0284   0.2097   1.0000
  17.000   1.3097   0.06598   0.05997   0.0289   0.2022   1.0000
  17.250   1.2972   0.06979   0.06382   0.0290   0.1944   1.0000
  17.500   1.2958   0.07225   0.06622   0.0293   0.1882   1.0000
  17.750   1.2855   0.07598   0.07003   0.0292   0.1820   1.0000
  18.000   1.2904   0.07766   0.07158   0.0297   0.1765   1.0000
  18.250   1.2788   0.08173   0.07577   0.0293   0.1714   1.0000
  18.500   1.2763   0.08458   0.07863   0.0292   0.1667   1.0000
  18.750   1.2815   0.08629   0.08024   0.0295   0.1619   1.0000
  19.000   1.2713   0.09029   0.08437   0.0290   0.1575   1.0000
  19.250   1.2707   0.09290   0.08697   0.0288   0.1530   1.0000
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