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GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 703 AIRFOIL (goe703-il)
Reynolds number: 1,000,000
Max Cl/Cd: 65.6 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe703-il-1000000-n5.txt
Download as CSV file: xf-goe703-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 703 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0820   0.07641   0.07232  -0.0745   1.0000   0.0246
 -19.500  -1.1005   0.07061   0.06639  -0.0771   1.0000   0.0247
 -19.250  -1.1142   0.06556   0.06123  -0.0793   1.0000   0.0247
 -19.000  -1.1278   0.06069   0.05625  -0.0813   1.0000   0.0247
 -18.750  -1.1387   0.05638   0.05183  -0.0828   1.0000   0.0248
 -18.500  -1.1471   0.05255   0.04790  -0.0838   1.0000   0.0248
 -18.250  -1.1524   0.04926   0.04452  -0.0845   1.0000   0.0249
 -18.000  -1.1554   0.04638   0.04156  -0.0847   1.0000   0.0251
 -17.750  -1.1578   0.04374   0.03884  -0.0846   1.0000   0.0251
 -17.500  -1.1584   0.04141   0.03643  -0.0842   1.0000   0.0252
 -17.250  -1.1584   0.03926   0.03422  -0.0836   1.0000   0.0253
 -17.000  -1.1560   0.03744   0.03233  -0.0827   1.0000   0.0254
 -16.750  -1.1548   0.03564   0.03046  -0.0815   1.0000   0.0255
 -16.500  -1.1522   0.03405   0.02881  -0.0802   1.0000   0.0256
 -16.250  -1.1486   0.03262   0.02731  -0.0787   1.0000   0.0257
 -16.000  -1.1438   0.03135   0.02599  -0.0770   1.0000   0.0258
 -15.750  -1.1387   0.03017   0.02476  -0.0752   1.0000   0.0259
 -15.500  -1.1340   0.02905   0.02358  -0.0732   1.0000   0.0259
 -15.250  -1.1281   0.02805   0.02253  -0.0712   1.0000   0.0260
 -15.000  -1.1054   0.02698   0.02141  -0.0722   0.9991   0.0261
 -14.750  -1.0836   0.02579   0.02018  -0.0732   0.9976   0.0263
 -14.500  -1.0642   0.02466   0.01901  -0.0736   0.9951   0.0266
 -14.250  -1.0510   0.02372   0.01803  -0.0724   0.9902   0.0267
 -14.000  -1.0340   0.02284   0.01712  -0.0718   0.9855   0.0269
 -13.750  -1.0178   0.02205   0.01630  -0.0710   0.9780   0.0272
 -13.500  -0.9985   0.02133   0.01555  -0.0705   0.9661   0.0274
 -13.250  -0.9677   0.02055   0.01473  -0.0723   0.9538   0.0276
 -13.000  -0.9264   0.01978   0.01393  -0.0762   0.9411   0.0279
 -12.750  -0.8784   0.01907   0.01315  -0.0815   0.9245   0.0285
 -12.500  -0.8311   0.01844   0.01242  -0.0865   0.9035   0.0288
 -12.250  -0.7855   0.01791   0.01178  -0.0911   0.8822   0.0292
 -12.000  -0.7473   0.01743   0.01120  -0.0942   0.8666   0.0295
 -11.750  -0.7165   0.01703   0.01071  -0.0957   0.8514   0.0297
 -11.250  -0.6679   0.01621   0.00975  -0.0958   0.8245   0.0305
 -11.000  -0.6458   0.01585   0.00933  -0.0953   0.8136   0.0310
 -10.750  -0.6242   0.01553   0.00897  -0.0947   0.8037   0.0314
 -10.500  -0.6030   0.01523   0.00861  -0.0938   0.7937   0.0319
 -10.250  -0.5823   0.01493   0.00827  -0.0929   0.7834   0.0324
 -10.000  -0.5621   0.01467   0.00795  -0.0918   0.7727   0.0328
  -9.750  -0.5420   0.01442   0.00765  -0.0906   0.7602   0.0332
  -9.500  -0.5218   0.01419   0.00736  -0.0894   0.7484   0.0337
  -9.250  -0.5026   0.01394   0.00706  -0.0880   0.7350   0.0346
  -9.000  -0.4829   0.01371   0.00679  -0.0866   0.7211   0.0353
  -8.750  -0.4639   0.01350   0.00652  -0.0851   0.7052   0.0363
  -8.500  -0.4449   0.01333   0.00628  -0.0836   0.6891   0.0371
  -8.250  -0.4257   0.01318   0.00605  -0.0820   0.6724   0.0381
  -8.000  -0.4063   0.01298   0.00582  -0.0806   0.6598   0.0398
  -7.750  -0.3866   0.01280   0.00560  -0.0791   0.6496   0.0416
  -7.500  -0.3666   0.01263   0.00540  -0.0777   0.6400   0.0433
  -7.250  -0.3472   0.01245   0.00519  -0.0761   0.6315   0.0459
  -7.000  -0.3269   0.01229   0.00501  -0.0748   0.6237   0.0481
  -6.750  -0.3076   0.01211   0.00482  -0.0732   0.6161   0.0515
  -6.500  -0.2873   0.01193   0.00464  -0.0718   0.6105   0.0553
  -6.250  -0.2670   0.01174   0.00446  -0.0703   0.6051   0.0604
  -6.000  -0.2477   0.01154   0.00428  -0.0688   0.5993   0.0681
  -5.500  -0.2102   0.01110   0.00394  -0.0653   0.5890   0.0932
  -5.250  -0.1912   0.01088   0.00379  -0.0636   0.5842   0.1087
  -5.000  -0.1715   0.01073   0.00366  -0.0620   0.5790   0.1195
  -4.750  -0.1519   0.01060   0.00355  -0.0604   0.5739   0.1294
  -4.500  -0.1313   0.01045   0.00344  -0.0590   0.5697   0.1389
  -4.250  -0.1099   0.01034   0.00334  -0.0576   0.5656   0.1464
  -4.000  -0.0898   0.01022   0.00325  -0.0561   0.5604   0.1554
  -3.750  -0.0697   0.01014   0.00316  -0.0545   0.5552   0.1628
  -3.500  -0.0496   0.01003   0.00308  -0.0529   0.5507   0.1725
  -3.250  -0.0294   0.00990   0.00300  -0.0513   0.5462   0.1844
  -3.000  -0.0099   0.00976   0.00292  -0.0496   0.5413   0.2006
  -2.750   0.0089   0.00965   0.00285  -0.0478   0.5364   0.2177
  -2.500   0.0276   0.00953   0.00278  -0.0459   0.5319   0.2356
  -2.250   0.0472   0.00940   0.00272  -0.0442   0.5282   0.2537
  -2.000   0.0662   0.00928   0.00266  -0.0423   0.5235   0.2721
  -1.750   0.0855   0.00921   0.00261  -0.0405   0.5186   0.2857
  -1.500   0.1039   0.00913   0.00257  -0.0385   0.5145   0.3009
  -1.250   0.1228   0.00903   0.00252  -0.0366   0.5111   0.3195
  -1.000   0.1407   0.00890   0.00247  -0.0345   0.5072   0.3429
  -0.750   0.1556   0.00873   0.00241  -0.0318   0.5029   0.3767
  -0.500   0.1647   0.00849   0.00235  -0.0279   0.4982   0.4314
  -0.250   0.1718   0.00828   0.00230  -0.0236   0.4940   0.4840
   0.000   0.1803   0.00806   0.00225  -0.0194   0.4910   0.5316
   0.250   0.1833   0.00785   0.00222  -0.0141   0.4874   0.5807
   0.500   0.1805   0.00767   0.00220  -0.0074   0.4834   0.6273
   0.750   0.1753   0.00749   0.00218  -0.0001   0.4790   0.6751
   1.000   0.1725   0.00731   0.00216   0.0067   0.4747   0.7225
   1.250   0.1758   0.00716   0.00217   0.0122   0.4704   0.7667
   1.500   0.1846   0.00708   0.00221   0.0164   0.4661   0.7986
   1.750   0.1980   0.00710   0.00226   0.0197   0.4593   0.8193
   2.000   0.2165   0.00713   0.00231   0.0218   0.4545   0.8332
   2.250   0.2349   0.00717   0.00236   0.0239   0.4484   0.8451
   2.500   0.2548   0.00726   0.00246   0.0257   0.4403   0.8580
   2.750   0.2753   0.00733   0.00254   0.0273   0.4348   0.8688
   3.000   0.2932   0.00741   0.00263   0.0295   0.4292   0.8805
   3.250   0.3191   0.00754   0.00276   0.0299   0.4231   0.8892
   3.500   0.3372   0.00763   0.00284   0.0320   0.4171   0.8962
   3.750   0.3531   0.00772   0.00291   0.0345   0.4092   0.9019
   4.000   0.3828   0.00790   0.00306   0.0340   0.4006   0.9058
   4.250   0.4059   0.00802   0.00318   0.0349   0.3930   0.9106
   4.500   0.4119   0.00813   0.00325   0.0396   0.3866   0.9176
   5.000   0.4731   0.00854   0.00360   0.0379   0.3656   0.9239
   5.250   0.4957   0.00873   0.00374   0.0387   0.3543   0.9267
   5.500   0.5128   0.00892   0.00389   0.0407   0.3441   0.9307
   5.750   0.5233   0.00905   0.00400   0.0442   0.3368   0.9353
   6.000   0.5542   0.00928   0.00419   0.0431   0.3274   0.9367
   6.250   0.5847   0.00951   0.00439   0.0421   0.3183   0.9380
   6.500   0.6151   0.00976   0.00461   0.0411   0.3094   0.9395
   6.750   0.6432   0.01004   0.00485   0.0405   0.2990   0.9412
   7.000   0.6692   0.01031   0.00508   0.0404   0.2890   0.9433
   7.250   0.6909   0.01060   0.00533   0.0411   0.2802   0.9459
   7.500   0.6995   0.01080   0.00552   0.0447   0.2734   0.9511
   7.750   0.7297   0.01116   0.00584   0.0434   0.2629   0.9521
   8.000   0.7577   0.01155   0.00618   0.0426   0.2504   0.9531
   8.250   0.7833   0.01196   0.00655   0.0422   0.2385   0.9544
   8.500   0.8052   0.01247   0.00699   0.0424   0.2244   0.9560
   8.750   0.8235   0.01309   0.00754   0.0431   0.2070   0.9581
   9.000   0.8363   0.01389   0.00823   0.0446   0.1865   0.9611
   9.250   0.8412   0.01454   0.00883   0.0479   0.1734   0.9661
   9.500   0.8604   0.01536   0.00957   0.0480   0.1589   0.9670
   9.750   0.8812   0.01604   0.01023   0.0479   0.1504   0.9680
  10.000   0.9016   0.01676   0.01092   0.0478   0.1436   0.9691
  10.250   0.9227   0.01746   0.01161   0.0477   0.1380   0.9702
  10.500   0.9421   0.01822   0.01235   0.0477   0.1330   0.9715
  10.750   0.9613   0.01892   0.01306   0.0478   0.1294   0.9730
  11.000   0.9795   0.01963   0.01378   0.0481   0.1263   0.9747
  11.250   0.9938   0.02043   0.01458   0.0490   0.1235   0.9771
  11.500   1.0039   0.02126   0.01542   0.0507   0.1209   0.9800
  11.750   1.0249   0.02207   0.01625   0.0501   0.1187   0.9807
  12.000   1.0452   0.02292   0.01712   0.0496   0.1161   0.9814
  12.250   1.0633   0.02389   0.01810   0.0493   0.1134   0.9822
  12.500   1.0793   0.02500   0.01921   0.0491   0.1103   0.9832
  12.750   1.0962   0.02603   0.02027   0.0488   0.1084   0.9841
  13.000   1.1133   0.02703   0.02131   0.0486   0.1063   0.9852
  13.250   1.1293   0.02813   0.02243   0.0484   0.1039   0.9864
  13.500   1.1425   0.02946   0.02378   0.0484   0.1011   0.9878
  13.750   1.1539   0.03089   0.02521   0.0485   0.0983   0.9892
  14.000   1.1671   0.03211   0.02647   0.0486   0.0953   0.9904
  14.250   1.1749   0.03373   0.02809   0.0490   0.0903   0.9916
  14.500   1.1769   0.03593   0.03024   0.0495   0.0774   0.9927
  14.750   1.1749   0.03880   0.03303   0.0494   0.0647   0.9938
  15.000   1.1774   0.04133   0.03556   0.0490   0.0591   0.9948
  15.250   1.1859   0.04328   0.03755   0.0486   0.0575   0.9957
  15.500   1.1912   0.04555   0.03984   0.0482   0.0555   0.9965
  15.750   1.1973   0.04774   0.04206   0.0478   0.0538   0.9972
  16.000   1.2050   0.04985   0.04422   0.0473   0.0529   0.9978
  16.250   1.2128   0.05192   0.04634   0.0468   0.0518   0.9983
  16.500   1.2185   0.05429   0.04875   0.0462   0.0509   0.9988
  16.750   1.2264   0.05649   0.05100   0.0454   0.0503   0.9992
  17.000   1.2310   0.05909   0.05364   0.0446   0.0494   0.9996
  17.250   1.2345   0.06177   0.05637   0.0439   0.0485   0.9999
  17.500   1.2342   0.06427   0.05892   0.0440   0.0478   1.0000
  17.750   1.2357   0.06640   0.06109   0.0445   0.0470   1.0000
  18.000   1.2355   0.06875   0.06350   0.0449   0.0469   1.0000
  18.250   1.2359   0.07106   0.06586   0.0452   0.0462   1.0000
  18.500   1.2346   0.07362   0.06848   0.0454   0.0456   1.0000
  18.750   1.2333   0.07619   0.07110   0.0455   0.0449   1.0000
  19.000   1.2310   0.07894   0.07390   0.0456   0.0444   1.0000
  19.250   1.2285   0.08175   0.07676   0.0455   0.0439   1.0000
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