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GOE 525 AIRFOIL (goe525-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 525 AIRFOIL (goe525-il)
Reynolds number: 500,000
Max Cl/Cd: 102.14 at α=0.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe525-il-500000.txt
Download as CSV file: xf-goe525-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 525 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250   0.3305   0.10439   0.10170  -0.1667   0.9428   0.0299
 -13.000   0.3246   0.09989   0.09718  -0.1721   0.9416   0.0316
 -12.750   0.3294   0.09773   0.09503  -0.1702   0.9357   0.0317
 -12.500   0.3486   0.09512   0.09242  -0.1710   0.9331   0.0320
 -12.250   0.3645   0.09244   0.08973  -0.1729   0.9309   0.0323
 -12.000   0.3807   0.08969   0.08696  -0.1752   0.9290   0.0329
 -11.750   0.3961   0.08668   0.08393  -0.1778   0.9271   0.0337
 -11.500   0.4040   0.08419   0.08144  -0.1786   0.9230   0.0346
 -11.250   0.3889   0.08001   0.07725  -0.1808   0.9168   0.0363
 -11.000   0.4106   0.07748   0.07469  -0.1816   0.9139   0.0366
 -10.750   0.4301   0.07495   0.07214  -0.1835   0.9111   0.0370
 -10.500   0.4378   0.07308   0.07027  -0.1831   0.9053   0.0376
 -10.250   0.4103   0.08297   0.08006  -0.1906   0.9238   0.0372
 -10.000   0.4182   0.08126   0.07836  -0.1903   0.9172   0.0377
  -9.750   0.4356   0.07875   0.07582  -0.1930   0.9131   0.0388
  -9.500   0.4212   0.07404   0.07109  -0.1978   0.9042   0.0413
  -9.250   0.4383   0.07207   0.06910  -0.1979   0.8984   0.0416
  -9.000   0.4671   0.07028   0.06724  -0.2001   0.8940   0.0421
  -8.750   0.4717   0.06916   0.06614  -0.1981   0.8859   0.0427
  -8.500   0.4863   0.06725   0.06420  -0.1994   0.8799   0.0437
  -8.250   0.4933   0.06531   0.06224  -0.1998   0.8729   0.0448
  -8.000   0.4747   0.06029   0.05719  -0.2030   0.8628   0.0472
  -7.750   0.4870   0.05923   0.05612  -0.2018   0.8562   0.0475
  -7.500   0.4980   0.05811   0.05500  -0.2007   0.8488   0.0480
  -7.250   0.5108   0.05666   0.05351  -0.2009   0.8418   0.0486
  -7.000   0.5135   0.05537   0.05222  -0.1993   0.8327   0.0495
  -6.750   0.4462   0.02168   0.01723  -0.2508   0.8117   0.0410
  -6.500   0.4776   0.01944   0.01473  -0.2543   0.8040   0.0408
  -6.250   0.5126   0.01783   0.01281  -0.2574   0.7965   0.0408
  -6.000   0.5452   0.01674   0.01147  -0.2593   0.7888   0.0410
  -5.750   0.5770   0.01557   0.01008  -0.2610   0.7800   0.0415
  -5.500   0.6060   0.01470   0.00913  -0.2618   0.7708   0.0422
  -5.250   0.6352   0.01412   0.00843  -0.2623   0.7608   0.0426
  -5.000   0.6625   0.01365   0.00788  -0.2624   0.7498   0.0431
  -4.750   0.6909   0.01326   0.00737  -0.2627   0.7392   0.0437
  -4.500   0.7180   0.01294   0.00694  -0.2627   0.7271   0.0443
  -4.250   0.7447   0.01266   0.00657  -0.2625   0.7149   0.0450
  -4.000   0.7717   0.01245   0.00624  -0.2624   0.7032   0.0457
  -3.750   0.7983   0.01230   0.00597  -0.2622   0.6917   0.0465
  -3.500   0.8262   0.01203   0.00565  -0.2624   0.6813   0.0477
  -3.250   0.8537   0.01192   0.00546  -0.2625   0.6717   0.0493
  -3.000   0.8808   0.01183   0.00533  -0.2625   0.6622   0.0508
  -2.750   0.9080   0.01181   0.00520  -0.2624   0.6535   0.0524
  -2.500   0.9362   0.01169   0.00504  -0.2627   0.6451   0.0546
  -2.250   0.9638   0.01170   0.00497  -0.2627   0.6374   0.0578
  -2.000   0.9916   0.01163   0.00488  -0.2628   0.6303   0.0628
  -1.750   1.0192   0.01160   0.00482  -0.2629   0.6227   0.0751
  -1.500   1.0485   0.01145   0.00485  -0.2635   0.6157   0.1378
  -1.250   1.0737   0.01147   0.00489  -0.2631   0.6084   0.1672
  -1.000   1.0992   0.01156   0.00496  -0.2628   0.6015   0.1950
  -0.750   1.1240   0.01155   0.00506  -0.2624   0.5948   0.2383
  -0.500   1.1477   0.01163   0.00518  -0.2617   0.5874   0.2816
   0.000   1.1942   0.01185   0.00545  -0.2600   0.5732   0.3442
   0.250   1.2166   0.01202   0.00563  -0.2591   0.5659   0.3786
   0.500   1.2393   0.01215   0.00582  -0.2581   0.5586   0.4137
   0.750   1.2604   0.01234   0.00603  -0.2569   0.5506   0.4435
   1.000   1.2814   0.01256   0.00624  -0.2556   0.5430   0.4654
   1.250   1.3022   0.01277   0.00645  -0.2543   0.5346   0.4836
   1.500   1.3216   0.01306   0.00669  -0.2528   0.5264   0.5004
   1.750   1.3417   0.01331   0.00693  -0.2514   0.5175   0.5166
   2.000   1.3603   0.01365   0.00722  -0.2498   0.5091   0.5307
   2.250   1.3804   0.01392   0.00749  -0.2484   0.5003   0.5425
   2.500   1.3981   0.01432   0.00781  -0.2467   0.4922   0.5551
   2.750   1.4186   0.01461   0.00811  -0.2455   0.4844   0.5654
   3.000   1.4370   0.01502   0.00845  -0.2439   0.4769   0.5750
   3.250   1.4572   0.01535   0.00879  -0.2427   0.4703   0.5841
   3.500   1.4765   0.01574   0.00914  -0.2413   0.4636   0.5934
   3.750   1.4943   0.01620   0.00956  -0.2397   0.4573   0.6017
   4.000   1.5154   0.01653   0.00989  -0.2387   0.4515   0.6109
   4.250   1.5340   0.01695   0.01031  -0.2373   0.4454   0.6179
   4.500   1.5516   0.01747   0.01077  -0.2358   0.4397   0.6259
   4.750   1.5725   0.01780   0.01114  -0.2348   0.4348   0.6318
   5.000   1.5919   0.01822   0.01156  -0.2336   0.4296   0.6380
   5.250   1.6097   0.01876   0.01204  -0.2322   0.4246   0.6448
   5.500   1.6289   0.01920   0.01251  -0.2310   0.4202   0.6505
   5.750   1.6487   0.01961   0.01296  -0.2300   0.4157   0.6565
   6.000   1.6673   0.02011   0.01344  -0.2288   0.4111   0.6626
   6.250   1.6843   0.02070   0.01401  -0.2274   0.4065   0.6679
   6.500   1.7031   0.02119   0.01453  -0.2262   0.4024   0.6742
   6.750   1.7218   0.02168   0.01506  -0.2251   0.3979   0.6812
   7.000   1.7384   0.02227   0.01566  -0.2237   0.3929   0.6885
   7.250   1.7533   0.02303   0.01638  -0.2221   0.3876   0.6968
   7.500   1.7713   0.02353   0.01697  -0.2210   0.3833   0.7040
   7.750   1.7885   0.02413   0.01760  -0.2197   0.3787   0.7108
   8.000   1.8043   0.02484   0.01831  -0.2184   0.3743   0.7166
   8.250   1.8189   0.02565   0.01913  -0.2169   0.3698   0.7232
   8.500   1.8365   0.02625   0.01980  -0.2158   0.3658   0.7306
   8.750   1.8525   0.02696   0.02057  -0.2146   0.3610   0.7377
   9.000   1.8657   0.02788   0.02149  -0.2131   0.3564   0.7455
   9.250   1.8803   0.02876   0.02241  -0.2118   0.3521   0.7542
   9.500   1.8973   0.02949   0.02323  -0.2108   0.3478   0.7656
   9.750   1.9113   0.03043   0.02424  -0.2095   0.3429   0.7810
  10.000   1.9225   0.03149   0.02537  -0.2079   0.3380   0.8199
  10.250   1.9336   0.03230   0.02632  -0.2061   0.3336   1.0000
  10.500   1.9468   0.03336   0.02742  -0.2048   0.3283   1.0000
  10.750   1.9567   0.03471   0.02874  -0.2033   0.3228   1.0000
  11.000   1.9674   0.03602   0.03007  -0.2018   0.3177   1.0000
  11.250   1.9800   0.03720   0.03130  -0.2006   0.3125   1.0000
  11.500   1.9885   0.03874   0.03284  -0.1991   0.3073   1.0000
  11.750   1.9972   0.04029   0.03440  -0.1976   0.3025   1.0000
  12.000   2.0090   0.04161   0.03579  -0.1965   0.2978   1.0000
  12.250   2.0169   0.04329   0.03749  -0.1951   0.2926   1.0000
  12.500   2.0216   0.04531   0.03951  -0.1935   0.2874   1.0000
  12.750   2.0325   0.04679   0.04106  -0.1925   0.2826   1.0000
  13.000   2.0394   0.04869   0.04298  -0.1913   0.2776   1.0000
  13.250   2.0429   0.05095   0.04525  -0.1898   0.2729   1.0000
  13.500   2.0518   0.05271   0.04709  -0.1888   0.2691   1.0000
  13.750   2.0593   0.05465   0.04909  -0.1878   0.2646   1.0000
  14.000   2.0625   0.05708   0.05155  -0.1867   0.2600   1.0000
  14.250   2.0656   0.05957   0.05407  -0.1856   0.2555   1.0000
  14.500   2.0719   0.06176   0.05634  -0.1848   0.2507   1.0000
  14.750   2.0739   0.06446   0.05908  -0.1838   0.2458   1.0000
  15.000   2.0730   0.06756   0.06220  -0.1828   0.2410   1.0000
  15.250   2.0788   0.06991   0.06465  -0.1822   0.2368   1.0000
  15.500   2.0802   0.07282   0.06762  -0.1815   0.2318   1.0000
  15.750   2.0762   0.07646   0.07127  -0.1807   0.2268   1.0000
  16.000   2.0790   0.07927   0.07418  -0.1803   0.2217   1.0000
  16.250   2.0756   0.08292   0.07788  -0.1797   0.2156   1.0000
  16.500   2.0713   0.08675   0.08175  -0.1793   0.2100   1.0000
  16.750   2.0682   0.09047   0.08555  -0.1790   0.2031   1.0000
  17.000   2.0590   0.09508   0.09019  -0.1788   0.1967   1.0000
  17.250   2.0525   0.09935   0.09451  -0.1788   0.1873   1.0000
  17.500   2.0407   0.10443   0.09962  -0.1789   0.1770   1.0000
  17.750   2.0212   0.11076   0.10594  -0.1794   0.1624   1.0000
  18.000   1.9924   0.11861   0.11375  -0.1804   0.1439   1.0000
  18.250   1.9546   0.12798   0.12304  -0.1821   0.1210   1.0000
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