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GOE 526 AIRFOIL (goe526-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 526 AIRFOIL (goe526-il)
Reynolds number: 1,000,000
Max Cl/Cd: 119.49 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe526-il-1000000.txt
Download as CSV file: xf-goe526-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 526 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.9593   0.03603   0.03318  -0.1015   1.0000   0.0263
 -14.250  -0.9804   0.03375   0.03078  -0.0983   1.0000   0.0264
 -14.000  -1.0061   0.03255   0.02950  -0.0916   1.0000   0.0265
 -13.750  -1.0197   0.03119   0.02804  -0.0866   0.9997   0.0266
 -13.500  -0.9972   0.02935   0.02604  -0.0883   0.9975   0.0269
 -13.250  -0.9734   0.02776   0.02430  -0.0898   0.9950   0.0272
 -13.000  -0.9485   0.02637   0.02277  -0.0911   0.9926   0.0275
 -12.750  -0.9241   0.02529   0.02156  -0.0917   0.9893   0.0278
 -12.500  -0.8956   0.02447   0.02062  -0.0928   0.9866   0.0281
 -12.250  -0.8733   0.02243   0.01837  -0.0939   0.9839   0.0285
 -12.000  -0.8461   0.02102   0.01686  -0.0951   0.9822   0.0290
 -11.750  -0.8216   0.02023   0.01602  -0.0951   0.9778   0.0293
 -11.500  -0.7924   0.01953   0.01526  -0.0959   0.9746   0.0297
 -11.250  -0.7602   0.01894   0.01463  -0.0973   0.9723   0.0301
 -11.000  -0.7272   0.01829   0.01391  -0.0988   0.9700   0.0306
 -10.750  -0.6989   0.01763   0.01316  -0.0993   0.9651   0.0310
 -10.500  -0.6709   0.01698   0.01242  -0.0996   0.9591   0.0314
 -10.250  -0.6389   0.01634   0.01168  -0.1008   0.9544   0.0318
 -10.000  -0.6146   0.01588   0.01113  -0.1002   0.9447   0.0321
  -9.750  -0.5864   0.01543   0.01058  -0.1003   0.9368   0.0323
  -9.500  -0.5669   0.01440   0.00943  -0.0991   0.9250   0.0330
  -9.250  -0.5435   0.01390   0.00887  -0.0983   0.9139   0.0335
  -9.000  -0.5186   0.01356   0.00847  -0.0976   0.9027   0.0341
  -8.750  -0.4947   0.01322   0.00806  -0.0968   0.8902   0.0345
  -8.500  -0.4705   0.01290   0.00767  -0.0960   0.8783   0.0351
  -8.250  -0.4462   0.01258   0.00725  -0.0952   0.8674   0.0356
  -8.000  -0.4217   0.01230   0.00688  -0.0944   0.8565   0.0361
  -7.750  -0.3969   0.01204   0.00654  -0.0937   0.8466   0.0366
  -7.500  -0.3719   0.01182   0.00623  -0.0929   0.8370   0.0369
  -7.250  -0.3490   0.01129   0.00563  -0.0919   0.8284   0.0377
  -7.000  -0.3244   0.01099   0.00528  -0.0912   0.8204   0.0385
  -6.750  -0.2988   0.01078   0.00504  -0.0906   0.8130   0.0394
  -6.500  -0.2732   0.01060   0.00480  -0.0900   0.8049   0.0403
  -6.250  -0.2476   0.01040   0.00455  -0.0894   0.7969   0.0411
  -6.000  -0.2216   0.01024   0.00432  -0.0888   0.7890   0.0418
  -5.750  -0.1966   0.00997   0.00399  -0.0881   0.7820   0.0428
  -5.500  -0.1709   0.00970   0.00372  -0.0875   0.7754   0.0443
  -5.250  -0.1448   0.00955   0.00353  -0.0869   0.7684   0.0455
  -5.000  -0.1184   0.00942   0.00336  -0.0865   0.7622   0.0470
  -4.750  -0.0919   0.00926   0.00317  -0.0860   0.7555   0.0484
  -4.500  -0.0663   0.00906   0.00295  -0.0854   0.7490   0.0508
  -4.250  -0.0395   0.00893   0.00281  -0.0850   0.7433   0.0529
  -4.000  -0.0128   0.00880   0.00266  -0.0845   0.7377   0.0550
  -3.750   0.0133   0.00863   0.00249  -0.0840   0.7323   0.0584
  -3.500   0.0403   0.00854   0.00238  -0.0836   0.7273   0.0612
  -3.250   0.0669   0.00837   0.00223  -0.0832   0.7221   0.0656
  -3.000   0.0937   0.00829   0.00214  -0.0828   0.7170   0.0696
  -2.750   0.1200   0.00817   0.00203  -0.0823   0.7117   0.0756
  -2.500   0.1471   0.00805   0.00194  -0.0820   0.7066   0.0817
  -2.250   0.1738   0.00796   0.00187  -0.0816   0.7009   0.0892
  -2.000   0.2002   0.00788   0.00180  -0.0811   0.6955   0.0990
  -1.750   0.2273   0.00779   0.00176  -0.0808   0.6905   0.1093
  -1.500   0.2543   0.00772   0.00172  -0.0804   0.6848   0.1191
  -1.250   0.2808   0.00770   0.00169  -0.0800   0.6785   0.1280
  -1.000   0.3078   0.00762   0.00166  -0.0796   0.6719   0.1373
  -0.750   0.3344   0.00761   0.00163  -0.0792   0.6635   0.1444
  -0.500   0.3609   0.00756   0.00160  -0.0787   0.6562   0.1538
  -0.250   0.3876   0.00754   0.00158  -0.0783   0.6480   0.1610
   0.000   0.4137   0.00750   0.00155  -0.0778   0.6393   0.1713
   0.250   0.4399   0.00749   0.00153  -0.0773   0.6289   0.1807
   0.500   0.4658   0.00745   0.00152  -0.0767   0.6180   0.1953
   0.750   0.4908   0.00742   0.00152  -0.0760   0.6047   0.2180
   1.000   0.5148   0.00734   0.00154  -0.0751   0.5899   0.2672
   1.250   0.5359   0.00707   0.00157  -0.0738   0.5744   0.3919
   1.500   0.5513   0.00656   0.00163  -0.0713   0.5576   0.6163
   1.750   0.5685   0.00592   0.00184  -0.0686   0.5385   0.9325
   2.000   0.6137   0.00620   0.00202  -0.0722   0.5103   0.9599
   2.250   0.6515   0.00650   0.00218  -0.0743   0.4827   0.9712
   2.500   0.6898   0.00683   0.00237  -0.0765   0.4593   0.9793
   2.750   0.7310   0.00711   0.00254  -0.0794   0.4410   0.9840
   3.000   0.7738   0.00734   0.00268  -0.0826   0.4262   0.9878
   3.250   0.8105   0.00753   0.00281  -0.0845   0.4140   0.9914
   3.500   0.8500   0.00773   0.00294  -0.0870   0.4037   0.9944
   3.750   0.8973   0.00790   0.00304  -0.0913   0.3921   0.9977
   4.000   0.9387   0.00803   0.00312  -0.0943   0.3808   1.0000
   4.250   0.9586   0.00820   0.00323  -0.0927   0.3712   1.0000
   4.500   0.9800   0.00830   0.00332  -0.0913   0.3630   1.0000
   4.750   0.9996   0.00847   0.00344  -0.0897   0.3539   1.0000
   5.000   1.0206   0.00857   0.00354  -0.0883   0.3469   1.0000
   5.500   1.0599   0.00887   0.00378  -0.0849   0.3294   1.0000
   5.750   1.0783   0.00906   0.00392  -0.0830   0.3195   1.0000
   6.000   1.0969   0.00923   0.00406  -0.0811   0.3084   1.0000
   6.250   1.1153   0.00941   0.00422  -0.0792   0.2982   1.0000
   6.500   1.1320   0.00965   0.00439  -0.0770   0.2840   1.0000
   6.750   1.1476   0.00993   0.00459  -0.0746   0.2663   1.0000
   7.000   1.1599   0.01033   0.00486  -0.0716   0.2408   1.0000
   7.250   1.1695   0.01084   0.00520  -0.0682   0.2091   1.0000
   7.500   1.1796   0.01134   0.00556  -0.0648   0.1864   1.0000
   7.750   1.1920   0.01171   0.00587  -0.0619   0.1749   1.0000
   8.000   1.2022   0.01206   0.00617  -0.0585   0.1661   1.0000
   8.250   1.2166   0.01231   0.00642  -0.0559   0.1614   1.0000
   8.500   1.2298   0.01264   0.00673  -0.0532   0.1554   1.0000
   8.750   1.2451   0.01295   0.00704  -0.0510   0.1501   1.0000
   9.000   1.2620   0.01323   0.00733  -0.0490   0.1458   1.0000
   9.250   1.2770   0.01360   0.00769  -0.0469   0.1401   1.0000
   9.500   1.2936   0.01394   0.00803  -0.0451   0.1349   1.0000
   9.750   1.3096   0.01433   0.00840  -0.0432   0.1276   1.0000
  10.000   1.3251   0.01475   0.00881  -0.0413   0.1198   1.0000
  10.250   1.3386   0.01530   0.00929  -0.0392   0.1084   1.0000
  10.500   1.3509   0.01593   0.00986  -0.0371   0.0969   1.0000
  10.750   1.3622   0.01664   0.01050  -0.0348   0.0875   1.0000
  11.000   1.3749   0.01730   0.01116  -0.0329   0.0819   1.0000
  11.250   1.3869   0.01803   0.01188  -0.0310   0.0768   1.0000
  11.500   1.4003   0.01872   0.01257  -0.0293   0.0730   1.0000
  11.750   1.4111   0.01958   0.01342  -0.0274   0.0689   1.0000
  12.000   1.4251   0.02027   0.01415  -0.0260   0.0665   1.0000
  12.250   1.4376   0.02109   0.01499  -0.0245   0.0635   1.0000
  12.500   1.4473   0.02211   0.01601  -0.0228   0.0602   1.0000
  12.750   1.4606   0.02293   0.01687  -0.0215   0.0585   1.0000
  13.000   1.4726   0.02386   0.01783  -0.0202   0.0561   1.0000
  13.250   1.4825   0.02497   0.01895  -0.0189   0.0539   1.0000
  13.500   1.4919   0.02614   0.02016  -0.0175   0.0517   1.0000
  13.750   1.5035   0.02718   0.02125  -0.0164   0.0502   1.0000
  14.000   1.5127   0.02843   0.02252  -0.0153   0.0483   1.0000
  14.250   1.5197   0.02988   0.02399  -0.0140   0.0463   1.0000
  14.500   1.5279   0.03126   0.02542  -0.0130   0.0450   1.0000
  14.750   1.5371   0.03261   0.02682  -0.0121   0.0438   1.0000
  15.000   1.5446   0.03413   0.02838  -0.0112   0.0422   1.0000
  15.250   1.5492   0.03592   0.03021  -0.0102   0.0408   1.0000
  15.500   1.5530   0.03785   0.03218  -0.0093   0.0393   1.0000
  15.750   1.5600   0.03954   0.03394  -0.0087   0.0386   1.0000
  16.000   1.5658   0.04138   0.03584  -0.0081   0.0373   1.0000
  16.250   1.5690   0.04350   0.03800  -0.0075   0.0363   1.0000
  16.500   1.5702   0.04588   0.04044  -0.0070   0.0353   1.0000
  16.750   1.5688   0.04863   0.04324  -0.0066   0.0342   1.0000
  17.000   1.5734   0.05079   0.04548  -0.0064   0.0335   1.0000
  17.250   1.5752   0.05329   0.04806  -0.0062   0.0327   1.0000
  17.500   1.5754   0.05602   0.05085  -0.0062   0.0318   1.0000
  17.750   1.5728   0.05916   0.05404  -0.0063   0.0308   1.0000
  18.000   1.5671   0.06275   0.05770  -0.0066   0.0301   1.0000
  18.250   1.5632   0.06618   0.06122  -0.0069   0.0294   1.0000
  18.500   1.5634   0.06914   0.06426  -0.0073   0.0287   1.0000
  18.750   1.5596   0.07269   0.06789  -0.0079   0.0280   1.0000
  19.000   1.5543   0.07648   0.07176  -0.0086   0.0274   1.0000
  19.250   1.5466   0.08061   0.07597  -0.0095   0.0268   1.0000
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