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GOE 702 AIRFOIL (goe702-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 702 AIRFOIL (goe702-il)
Reynolds number: 500,000
Max Cl/Cd: 89.74 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe702-il-500000-n5.txt
Download as CSV file: xf-goe702-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.7360   0.07986   0.07620  -0.0656   0.9021   0.0362
 -16.000  -0.7638   0.07120   0.06727  -0.0727   0.8805   0.0364
 -15.750  -0.7903   0.06459   0.06047  -0.0772   0.8630   0.0366
 -15.500  -0.8127   0.05911   0.05486  -0.0804   0.8472   0.0367
 -15.000  -0.8696   0.04736   0.04284  -0.0870   0.8160   0.0369
 -14.750  -0.9042   0.04064   0.03594  -0.0911   0.7998   0.0370
 -14.500  -0.9403   0.03255   0.02755  -0.0982   0.7835   0.0370
 -14.250  -0.9529   0.03014   0.02497  -0.0969   0.7705   0.0371
 -14.000  -0.9577   0.02862   0.02333  -0.0944   0.7591   0.0373
 -13.750  -0.9564   0.02754   0.02213  -0.0918   0.7498   0.0376
 -13.500  -0.9473   0.02651   0.02099  -0.0902   0.7410   0.0379
 -13.250  -0.9352   0.02560   0.01997  -0.0886   0.7330   0.0383
 -13.000  -0.9203   0.02478   0.01905  -0.0874   0.7262   0.0387
 -12.750  -0.9040   0.02400   0.01817  -0.0861   0.7197   0.0391
 -12.500  -0.8867   0.02326   0.01731  -0.0849   0.7139   0.0395
 -12.250  -0.8680   0.02257   0.01651  -0.0839   0.7089   0.0400
 -12.000  -0.8482   0.02190   0.01574  -0.0829   0.7041   0.0404
 -11.750  -0.8275   0.02129   0.01502  -0.0819   0.6991   0.0408
 -11.500  -0.8072   0.02064   0.01429  -0.0809   0.6941   0.0413
 -11.250  -0.7862   0.02004   0.01361  -0.0800   0.6891   0.0417
 -11.000  -0.7638   0.01949   0.01302  -0.0792   0.6834   0.0423
 -10.750  -0.7408   0.01900   0.01246  -0.0784   0.6775   0.0428
 -10.500  -0.7174   0.01855   0.01192  -0.0777   0.6722   0.0434
 -10.250  -0.6934   0.01811   0.01141  -0.0770   0.6679   0.0441
 -10.000  -0.6688   0.01769   0.01092  -0.0764   0.6635   0.0449
  -9.750  -0.6439   0.01731   0.01045  -0.0758   0.6585   0.0456
  -9.500  -0.6197   0.01686   0.00994  -0.0751   0.6536   0.0463
  -9.250  -0.5950   0.01646   0.00948  -0.0745   0.6489   0.0471
  -9.000  -0.5694   0.01608   0.00907  -0.0739   0.6440   0.0479
  -8.750  -0.5436   0.01573   0.00868  -0.0734   0.6392   0.0489
  -8.500  -0.5176   0.01542   0.00829  -0.0729   0.6350   0.0498
  -8.250  -0.4914   0.01514   0.00792  -0.0724   0.6313   0.0507
  -8.000  -0.4654   0.01479   0.00754  -0.0719   0.6276   0.0517
  -7.750  -0.4389   0.01446   0.00720  -0.0715   0.6235   0.0529
  -7.500  -0.4122   0.01418   0.00689  -0.0711   0.6188   0.0543
  -7.250  -0.3853   0.01394   0.00659  -0.0707   0.6145   0.0557
  -7.000  -0.3584   0.01370   0.00628  -0.0702   0.6106   0.0570
  -6.750  -0.3314   0.01341   0.00599  -0.0699   0.6067   0.0586
  -6.500  -0.3041   0.01317   0.00573  -0.0695   0.6019   0.0603
  -6.250  -0.2767   0.01296   0.00548  -0.0692   0.5965   0.0621
  -6.000  -0.2495   0.01275   0.00523  -0.0688   0.5915   0.0640
  -5.750  -0.2218   0.01254   0.00501  -0.0685   0.5870   0.0665
  -5.500  -0.1940   0.01236   0.00481  -0.0682   0.5815   0.0693
  -5.250  -0.1664   0.01218   0.00462  -0.0679   0.5754   0.0723
  -5.000  -0.1387   0.01203   0.00445  -0.0676   0.5691   0.0758
  -4.750  -0.1107   0.01188   0.00429  -0.0674   0.5618   0.0793
  -4.500  -0.0828   0.01177   0.00415  -0.0671   0.5542   0.0836
  -4.250  -0.0548   0.01165   0.00402  -0.0669   0.5467   0.0875
  -4.000  -0.0268   0.01156   0.00390  -0.0666   0.5373   0.0917
  -3.750   0.0011   0.01147   0.00377  -0.0663   0.5269   0.0952
  -3.500   0.0287   0.01141   0.00366  -0.0660   0.5141   0.0992
  -3.250   0.0564   0.01138   0.00356  -0.0657   0.4991   0.1027
  -3.000   0.0838   0.01134   0.00345  -0.0654   0.4846   0.1059
  -2.750   0.1111   0.01131   0.00338  -0.0651   0.4714   0.1097
  -2.500   0.1385   0.01132   0.00332  -0.0648   0.4594   0.1131
  -2.250   0.1659   0.01133   0.00326  -0.0645   0.4484   0.1160
  -2.000   0.1931   0.01130   0.00321  -0.0641   0.4393   0.1200
  -1.750   0.2204   0.01131   0.00318  -0.0639   0.4305   0.1240
  -1.500   0.2478   0.01134   0.00315  -0.0636   0.4235   0.1274
  -1.250   0.2754   0.01130   0.00312  -0.0633   0.4178   0.1323
  -1.000   0.3028   0.01130   0.00311  -0.0630   0.4122   0.1378
  -0.750   0.3299   0.01132   0.00311  -0.0627   0.4070   0.1445
  -0.500   0.3574   0.01128   0.00310  -0.0625   0.4027   0.1550
  -0.250   0.3847   0.01124   0.00311  -0.0622   0.3980   0.1683
   0.000   0.4117   0.01123   0.00313  -0.0619   0.3932   0.1845
   0.250   0.4383   0.01124   0.00318  -0.0615   0.3889   0.2064
   0.500   0.4655   0.01122   0.00324  -0.0613   0.3857   0.2297
   0.750   0.4930   0.01122   0.00329  -0.0610   0.3824   0.2481
   1.000   0.5204   0.01126   0.00336  -0.0608   0.3789   0.2632
   1.250   0.5474   0.01131   0.00343  -0.0605   0.3753   0.2771
   1.500   0.5740   0.01139   0.00351  -0.0601   0.3715   0.2891
   2.000   0.6282   0.01150   0.00367  -0.0596   0.3652   0.3129
   2.250   0.6553   0.01157   0.00375  -0.0593   0.3622   0.3231
   2.500   0.6820   0.01163   0.00385  -0.0590   0.3591   0.3344
   2.750   0.7085   0.01172   0.00395  -0.0586   0.3561   0.3451
   3.000   0.7345   0.01182   0.00406  -0.0582   0.3531   0.3580
   3.250   0.7602   0.01191   0.00419  -0.0578   0.3503   0.3761
   3.500   0.7866   0.01193   0.00431  -0.0574   0.3479   0.4025
   3.750   0.8124   0.01196   0.00443  -0.0570   0.3451   0.4311
   4.000   0.8375   0.01198   0.00457  -0.0565   0.3421   0.4683
   4.250   0.8581   0.01171   0.00471  -0.0552   0.3395   0.6080
   4.750   0.9731   0.01153   0.00528  -0.0674   0.3327   0.9948
   5.000   1.0098   0.01169   0.00545  -0.0692   0.3305   1.0000
   5.250   1.0331   0.01185   0.00560  -0.0684   0.3281   1.0000
   5.500   1.0561   0.01202   0.00576  -0.0674   0.3254   1.0000
   5.750   1.0787   0.01221   0.00594  -0.0665   0.3227   1.0000
   6.000   1.1007   0.01242   0.00613  -0.0654   0.3202   1.0000
   6.250   1.1223   0.01265   0.00633  -0.0643   0.3179   1.0000
   6.500   1.1435   0.01290   0.00656  -0.0632   0.3156   1.0000
   6.750   1.1662   0.01307   0.00676  -0.0623   0.3138   1.0000
   7.000   1.1882   0.01327   0.00697  -0.0613   0.3115   1.0000
   7.250   1.2096   0.01348   0.00720  -0.0602   0.3091   1.0000
   7.500   1.2303   0.01371   0.00744  -0.0590   0.3066   1.0000
   7.750   1.2501   0.01397   0.00769  -0.0577   0.3044   1.0000
   8.000   1.2690   0.01425   0.00797  -0.0563   0.3022   1.0000
   8.250   1.2864   0.01458   0.00828  -0.0547   0.2999   1.0000
   8.500   1.3041   0.01485   0.00858  -0.0531   0.2979   1.0000
   8.750   1.3205   0.01510   0.00887  -0.0512   0.2960   1.0000
   9.000   1.3362   0.01540   0.00921  -0.0493   0.2939   1.0000
   9.250   1.3516   0.01575   0.00958  -0.0476   0.2917   1.0000
   9.500   1.3666   0.01616   0.01001  -0.0459   0.2893   1.0000
   9.750   1.3811   0.01665   0.01051  -0.0443   0.2869   1.0000
  10.000   1.3949   0.01722   0.01107  -0.0428   0.2844   1.0000
  10.250   1.4106   0.01775   0.01164  -0.0416   0.2814   1.0000
  10.500   1.4272   0.01826   0.01219  -0.0406   0.2779   1.0000
  10.750   1.4419   0.01889   0.01285  -0.0395   0.2737   1.0000
  11.000   1.4558   0.01960   0.01357  -0.0384   0.2707   1.0000
  11.250   1.4682   0.02044   0.01441  -0.0372   0.2676   1.0000
  11.500   1.4848   0.02107   0.01510  -0.0364   0.2652   1.0000
  11.750   1.5003   0.02178   0.01587  -0.0356   0.2620   1.0000
  12.000   1.5138   0.02265   0.01676  -0.0348   0.2584   1.0000
  12.250   1.5256   0.02365   0.01777  -0.0339   0.2549   1.0000
  12.500   1.5363   0.02475   0.01889  -0.0330   0.2520   1.0000
  12.750   1.5510   0.02561   0.01982  -0.0324   0.2488   1.0000
  13.000   1.5634   0.02665   0.02091  -0.0317   0.2447   1.0000
  13.250   1.5723   0.02797   0.02224  -0.0309   0.2404   1.0000
  13.500   1.5797   0.02941   0.02370  -0.0302   0.2363   1.0000
  13.750   1.5912   0.03057   0.02493  -0.0296   0.2322   1.0000
  14.000   1.5991   0.03204   0.02644  -0.0289   0.2279   1.0000
  14.250   1.6038   0.03376   0.02818  -0.0282   0.2237   1.0000
  14.500   1.6114   0.03529   0.02976  -0.0276   0.2201   1.0000
  14.750   1.6175   0.03701   0.03153  -0.0271   0.2148   1.0000
  15.000   1.6182   0.03925   0.03379  -0.0265   0.2096   1.0000
  15.250   1.6220   0.04127   0.03586  -0.0261   0.2046   1.0000
  15.500   1.6233   0.04356   0.03819  -0.0257   0.1987   1.0000
  15.750   1.6203   0.04632   0.04098  -0.0254   0.1931   1.0000
  16.000   1.6180   0.04910   0.04379  -0.0251   0.1864   1.0000
  16.250   1.6094   0.05259   0.04732  -0.0250   0.1801   1.0000
  16.500   1.5986   0.05642   0.05116  -0.0250   0.1711   1.0000
  16.750   1.5872   0.06040   0.05518  -0.0251   0.1645   1.0000
  17.000   1.5703   0.06513   0.05993  -0.0254   0.1564   1.0000
  17.250   1.5537   0.06993   0.06477  -0.0258   0.1483   1.0000
  17.500   1.5312   0.07556   0.07042  -0.0266   0.1396   1.0000
  17.750   1.5067   0.08155   0.07644  -0.0275   0.1313   1.0000
  18.000   1.4843   0.08741   0.08232  -0.0285   0.1225   1.0000
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