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GOE 702 AIRFOIL (goe702-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 702 AIRFOIL (goe702-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.23 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe702-il-1000000.txt
Download as CSV file: xf-goe702-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 702 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.8446   0.10190   0.09935  -0.0387   1.0000   0.0335
 -17.750  -0.8780   0.09315   0.09049  -0.0442   1.0000   0.0340
 -17.500  -0.8966   0.08676   0.08403  -0.0483   1.0000   0.0342
 -17.250  -0.9124   0.08092   0.07813  -0.0520   1.0000   0.0344
 -17.000  -0.9292   0.07496   0.07211  -0.0560   1.0000   0.0346
 -16.750  -0.9516   0.06854   0.06561  -0.0605   1.0000   0.0348
 -16.500  -0.9780   0.06173   0.05871  -0.0654   1.0000   0.0349
 -16.250  -1.0074   0.05456   0.05143  -0.0709   1.0000   0.0350
 -16.000  -1.0264   0.04665   0.04338  -0.0796   0.9478   0.0351
 -15.750  -1.0051   0.03809   0.03450  -0.0965   0.9068   0.0354
 -15.500  -1.0399   0.03017   0.02621  -0.1036   0.8699   0.0354
 -15.250  -1.0528   0.02801   0.02387  -0.1020   0.8507   0.0356
 -15.000  -1.0587   0.02660   0.02233  -0.0992   0.8343   0.0358
 -14.750  -1.0591   0.02558   0.02120  -0.0961   0.8189   0.0360
 -14.500  -1.0557   0.02470   0.02019  -0.0933   0.8040   0.0363
 -14.000  -1.0313   0.02312   0.01837  -0.0897   0.7763   0.0368
 -13.750  -1.0156   0.02244   0.01757  -0.0883   0.7647   0.0371
 -13.500  -0.9983   0.02180   0.01682  -0.0869   0.7545   0.0374
 -13.250  -0.9786   0.02129   0.01620  -0.0858   0.7457   0.0376
 -13.000  -0.9654   0.02024   0.01507  -0.0841   0.7378   0.0382
 -12.750  -0.9474   0.01955   0.01430  -0.0828   0.7302   0.0387
 -12.500  -0.9265   0.01898   0.01369  -0.0818   0.7242   0.0392
 -12.250  -0.9045   0.01849   0.01314  -0.0809   0.7178   0.0396
 -12.000  -0.8821   0.01805   0.01261  -0.0800   0.7107   0.0401
 -11.750  -0.8589   0.01760   0.01211  -0.0792   0.7048   0.0406
 -11.500  -0.8353   0.01717   0.01161  -0.0785   0.6989   0.0411
 -11.250  -0.8112   0.01679   0.01115  -0.0777   0.6931   0.0416
 -11.000  -0.7866   0.01646   0.01072  -0.0770   0.6873   0.0420
 -10.750  -0.7627   0.01597   0.01018  -0.0763   0.6837   0.0425
 -10.500  -0.7401   0.01536   0.00954  -0.0754   0.6793   0.0433
 -10.250  -0.7152   0.01498   0.00912  -0.0748   0.6743   0.0440
 -10.000  -0.6897   0.01470   0.00878  -0.0742   0.6687   0.0448
  -9.750  -0.6636   0.01439   0.00844  -0.0737   0.6647   0.0455
  -9.500  -0.6372   0.01409   0.00809  -0.0732   0.6608   0.0463
  -9.250  -0.6106   0.01384   0.00778  -0.0727   0.6568   0.0469
  -9.000  -0.5854   0.01343   0.00731  -0.0721   0.6526   0.0478
  -8.750  -0.5599   0.01308   0.00692  -0.0715   0.6479   0.0489
  -8.500  -0.5330   0.01279   0.00663  -0.0710   0.6449   0.0498
  -8.250  -0.5058   0.01254   0.00635  -0.0707   0.6417   0.0509
  -8.000  -0.4784   0.01232   0.00609  -0.0703   0.6380   0.0519
  -7.750  -0.4515   0.01206   0.00578  -0.0698   0.6340   0.0530
  -7.500  -0.4250   0.01176   0.00545  -0.0694   0.6296   0.0546
  -7.250  -0.3975   0.01155   0.00522  -0.0690   0.6259   0.0561
  -7.000  -0.3695   0.01135   0.00500  -0.0687   0.6226   0.0574
  -6.750  -0.3419   0.01112   0.00474  -0.0684   0.6188   0.0590
  -6.500  -0.3146   0.01086   0.00448  -0.0680   0.6146   0.0610
  -6.250  -0.2869   0.01071   0.00429  -0.0677   0.6097   0.0629
  -6.000  -0.2587   0.01055   0.00410  -0.0674   0.6057   0.0647
  -5.750  -0.2309   0.01030   0.00388  -0.0672   0.6016   0.0677
  -5.500  -0.2026   0.01016   0.00372  -0.0669   0.5970   0.0705
  -5.250  -0.1747   0.00999   0.00355  -0.0666   0.5920   0.0739
  -5.000  -0.1464   0.00987   0.00342  -0.0664   0.5871   0.0776
  -4.750  -0.1179   0.00971   0.00328  -0.0662   0.5817   0.0816
  -4.500  -0.0894   0.00961   0.00317  -0.0660   0.5754   0.0859
  -4.250  -0.0612   0.00952   0.00306  -0.0658   0.5690   0.0904
  -4.000  -0.0323   0.00943   0.00299  -0.0656   0.5627   0.0947
  -3.750  -0.0040   0.00935   0.00288  -0.0654   0.5547   0.0986
  -3.500   0.0245   0.00927   0.00280  -0.0652   0.5465   0.1026
  -3.250   0.0530   0.00925   0.00273  -0.0650   0.5352   0.1056
  -3.000   0.0811   0.00917   0.00262  -0.0648   0.5228   0.1097
  -2.750   0.1091   0.00913   0.00255  -0.0646   0.5081   0.1132
  -2.500   0.1370   0.00916   0.00251  -0.0643   0.4915   0.1163
  -2.250   0.1646   0.00918   0.00245  -0.0640   0.4750   0.1196
  -2.000   0.1919   0.00919   0.00241  -0.0637   0.4599   0.1237
  -1.750   0.2197   0.00921   0.00239  -0.0635   0.4480   0.1274
  -1.500   0.2476   0.00925   0.00237  -0.0632   0.4379   0.1303
  -1.250   0.2751   0.00923   0.00234  -0.0630   0.4293   0.1362
  -1.000   0.3028   0.00925   0.00234  -0.0627   0.4221   0.1416
  -0.750   0.3308   0.00922   0.00232  -0.0625   0.4166   0.1491
  -0.500   0.3584   0.00922   0.00232  -0.0623   0.4109   0.1588
  -0.250   0.3854   0.00919   0.00234  -0.0620   0.4051   0.1785
   0.000   0.4130   0.00908   0.00235  -0.0617   0.4015   0.2117
   0.250   0.4405   0.00904   0.00239  -0.0615   0.3971   0.2418
   0.500   0.4680   0.00907   0.00245  -0.0613   0.3923   0.2616
   0.750   0.4951   0.00914   0.00253  -0.0610   0.3871   0.2769
   1.000   0.5235   0.00914   0.00257  -0.0608   0.3847   0.2893
   1.250   0.5516   0.00916   0.00261  -0.0607   0.3816   0.3012
   1.500   0.5793   0.00920   0.00267  -0.0605   0.3781   0.3132
   1.750   0.6068   0.00928   0.00274  -0.0603   0.3744   0.3227
   2.000   0.6334   0.00938   0.00284  -0.0599   0.3698   0.3346
   2.250   0.6615   0.00940   0.00290  -0.0598   0.3674   0.3453
   2.500   0.6893   0.00941   0.00296  -0.0596   0.3647   0.3585
   2.750   0.7168   0.00945   0.00303  -0.0594   0.3617   0.3727
   3.000   0.7438   0.00951   0.00311  -0.0592   0.3586   0.3898
   3.250   0.7702   0.00958   0.00322  -0.0588   0.3552   0.4104
   3.500   0.7960   0.00968   0.00336  -0.0584   0.3513   0.4366
   3.750   0.8226   0.00961   0.00345  -0.0581   0.3497   0.4843
   4.000   0.8721   0.00863   0.00372  -0.0626   0.3469   0.9695
   4.250   0.9224   0.00879   0.00385  -0.0672   0.3435   0.9886
   4.500   0.9706   0.00897   0.00398  -0.0714   0.3398   0.9969
   4.750   1.0141   0.00919   0.00413  -0.0747   0.3358   1.0000
   5.000   1.0377   0.00934   0.00427  -0.0738   0.3334   1.0000
   5.250   1.0621   0.00943   0.00438  -0.0731   0.3318   1.0000
   5.500   1.0863   0.00954   0.00449  -0.0723   0.3296   1.0000
   5.750   1.1101   0.00967   0.00461  -0.0715   0.3271   1.0000
   6.000   1.1333   0.00983   0.00475  -0.0706   0.3245   1.0000
   6.250   1.1559   0.01001   0.00491  -0.0696   0.3218   1.0000
   6.500   1.1775   0.01025   0.00513  -0.0685   0.3186   1.0000
   6.750   1.2003   0.01043   0.00530  -0.0676   0.3165   1.0000
   7.000   1.2242   0.01055   0.00544  -0.0668   0.3148   1.0000
   7.250   1.2477   0.01068   0.00559  -0.0660   0.3127   1.0000
   7.500   1.2707   0.01084   0.00576  -0.0651   0.3105   1.0000
   7.750   1.2930   0.01103   0.00594  -0.0642   0.3082   1.0000
   8.000   1.3146   0.01124   0.00615  -0.0631   0.3057   1.0000
   8.250   1.3344   0.01154   0.00641  -0.0618   0.3024   1.0000
   8.500   1.3554   0.01177   0.00666  -0.0607   0.3002   1.0000
   8.750   1.3781   0.01192   0.00684  -0.0598   0.2985   1.0000
   9.000   1.4005   0.01207   0.00702  -0.0589   0.2958   1.0000
   9.250   1.4212   0.01227   0.00722  -0.0578   0.2925   1.0000
   9.500   1.4397   0.01255   0.00749  -0.0564   0.2894   1.0000
   9.750   1.4532   0.01292   0.00784  -0.0541   0.2860   1.0000
  10.000   1.4681   0.01318   0.00813  -0.0520   0.2837   1.0000
  10.250   1.4861   0.01340   0.00839  -0.0505   0.2816   1.0000
  10.500   1.5032   0.01369   0.00871  -0.0490   0.2792   1.0000
  10.750   1.5193   0.01407   0.00912  -0.0475   0.2768   1.0000
  11.000   1.5343   0.01457   0.00962  -0.0462   0.2739   1.0000
  11.250   1.5474   0.01523   0.01028  -0.0447   0.2704   1.0000
  11.500   1.5651   0.01571   0.01080  -0.0438   0.2675   1.0000
  11.750   1.5839   0.01616   0.01128  -0.0431   0.2653   1.0000
  12.000   1.6013   0.01669   0.01185  -0.0423   0.2624   1.0000
  12.250   1.6164   0.01740   0.01257  -0.0414   0.2587   1.0000
  12.500   1.6278   0.01835   0.01351  -0.0403   0.2544   1.0000
  12.750   1.6456   0.01894   0.01415  -0.0397   0.2519   1.0000
  13.000   1.6625   0.01960   0.01485  -0.0391   0.2490   1.0000
  13.250   1.6772   0.02041   0.01569  -0.0384   0.2456   1.0000
  13.500   1.6889   0.02146   0.01675  -0.0376   0.2419   1.0000
  13.750   1.6999   0.02259   0.01790  -0.0368   0.2378   1.0000
  14.000   1.7152   0.02341   0.01877  -0.0363   0.2342   1.0000
  14.250   1.7250   0.02466   0.02003  -0.0355   0.2288   1.0000
  14.500   1.7311   0.02622   0.02159  -0.0346   0.2238   1.0000
  14.750   1.7432   0.02731   0.02272  -0.0341   0.2188   1.0000
  15.000   1.7480   0.02899   0.02440  -0.0332   0.2129   1.0000
  15.250   1.7523   0.03075   0.02618  -0.0325   0.2063   1.0000
  15.500   1.7558   0.03257   0.02802  -0.0317   0.2002   1.0000
  15.750   1.7545   0.03488   0.03032  -0.0309   0.1917   1.0000
  16.000   1.7507   0.03750   0.03294  -0.0302   0.1842   1.0000
  16.250   1.7464   0.04023   0.03567  -0.0295   0.1755   1.0000
  16.500   1.7350   0.04371   0.03915  -0.0289   0.1658   1.0000
  16.750   1.7207   0.04759   0.04302  -0.0284   0.1567   1.0000
  17.000   1.7052   0.05174   0.04717  -0.0281   0.1466   1.0000
  17.250   1.6883   0.05615   0.05159  -0.0280   0.1375   1.0000
  17.500   1.6663   0.06128   0.05673  -0.0281   0.1282   1.0000
  17.750   1.6404   0.06705   0.06252  -0.0285   0.1196   1.0000
  18.000   1.6125   0.07320   0.06870  -0.0291   0.1111   1.0000
  18.250   1.5857   0.07938   0.07490  -0.0299   0.1028   1.0000
  18.500   1.5652   0.08488   0.08045  -0.0307   0.0978   1.0000
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