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GOE 436 AIRFOIL (goe436-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 436 AIRFOIL (goe436-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.75 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe436-il-1000000-n5.txt
Download as CSV file: xf-goe436-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 436 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -1.1138   0.03084   0.02779  -0.0832   1.0000   0.0121
 -14.250  -1.1209   0.02815   0.02490  -0.0800   1.0000   0.0124
 -14.000  -1.1059   0.02563   0.02218  -0.0806   0.9985   0.0131
 -13.750  -1.0848   0.02387   0.02025  -0.0813   0.9966   0.0137
 -13.500  -1.0614   0.02243   0.01867  -0.0819   0.9948   0.0145
 -13.250  -1.0389   0.02105   0.01717  -0.0823   0.9928   0.0155
 -13.000  -1.0152   0.01998   0.01600  -0.0824   0.9905   0.0167
 -12.750  -0.9891   0.01911   0.01503  -0.0829   0.9884   0.0176
 -12.500  -0.9614   0.01827   0.01413  -0.0835   0.9866   0.0188
 -12.250  -0.9319   0.01758   0.01337  -0.0844   0.9850   0.0200
 -12.000  -0.9028   0.01696   0.01266  -0.0851   0.9832   0.0211
 -11.750  -0.8771   0.01641   0.01206  -0.0850   0.9797   0.0220
 -11.500  -0.8481   0.01596   0.01158  -0.0855   0.9772   0.0231
 -11.250  -0.8175   0.01551   0.01108  -0.0864   0.9751   0.0240
 -11.000  -0.7859   0.01505   0.01054  -0.0874   0.9736   0.0248
 -10.750  -0.7566   0.01462   0.01003  -0.0878   0.9708   0.0254
 -10.500  -0.7293   0.01419   0.00956  -0.0879   0.9660   0.0261
 -10.250  -0.6978   0.01384   0.00919  -0.0888   0.9625   0.0269
 -10.000  -0.6653   0.01353   0.00885  -0.0899   0.9597   0.0277
  -9.750  -0.6383   0.01325   0.00851  -0.0897   0.9537   0.0284
  -9.500  -0.6081   0.01294   0.00814  -0.0902   0.9481   0.0291
  -9.250  -0.5790   0.01262   0.00776  -0.0905   0.9416   0.0297
  -9.000  -0.5506   0.01235   0.00742  -0.0906   0.9332   0.0301
  -8.750  -0.5232   0.01200   0.00700  -0.0905   0.9243   0.0309
  -8.500  -0.4954   0.01176   0.00673  -0.0905   0.9140   0.0318
  -8.250  -0.4683   0.01160   0.00652  -0.0902   0.8999   0.0325
  -8.000  -0.4418   0.01144   0.00628  -0.0898   0.8842   0.0332
  -7.500  -0.3906   0.01103   0.00567  -0.0887   0.8548   0.0342
  -7.250  -0.3651   0.01081   0.00537  -0.0881   0.8429   0.0346
  -7.000  -0.3394   0.01061   0.00508  -0.0875   0.8325   0.0351
  -6.750  -0.3136   0.01044   0.00482  -0.0870   0.8216   0.0355
  -6.500  -0.2874   0.01027   0.00458  -0.0865   0.8128   0.0358
  -6.000  -0.2360   0.00976   0.00396  -0.0854   0.7960   0.0373
  -5.750  -0.2100   0.00961   0.00376  -0.0849   0.7857   0.0379
  -5.500  -0.1838   0.00946   0.00357  -0.0844   0.7741   0.0386
  -5.250  -0.1575   0.00933   0.00340  -0.0840   0.7618   0.0392
  -5.000  -0.1314   0.00921   0.00321  -0.0834   0.7476   0.0399
  -4.750  -0.1055   0.00911   0.00303  -0.0829   0.7305   0.0406
  -4.500  -0.0801   0.00903   0.00286  -0.0822   0.7086   0.0412
  -4.250  -0.0548   0.00901   0.00273  -0.0815   0.6826   0.0419
  -4.000  -0.0294   0.00899   0.00260  -0.0809   0.6607   0.0424
  -3.750  -0.0041   0.00888   0.00240  -0.0802   0.6423   0.0434
  -3.500   0.0216   0.00881   0.00227  -0.0797   0.6256   0.0445
  -3.250   0.0476   0.00877   0.00217  -0.0792   0.6101   0.0456
  -3.000   0.0738   0.00874   0.00208  -0.0787   0.5960   0.0466
  -2.750   0.1004   0.00870   0.00200  -0.0783   0.5828   0.0477
  -2.500   0.1269   0.00867   0.00191  -0.0779   0.5687   0.0487
  -2.250   0.1532   0.00866   0.00184  -0.0774   0.5521   0.0496
  -2.000   0.1792   0.00869   0.00179  -0.0769   0.5297   0.0504
  -1.750   0.2042   0.00873   0.00170  -0.0763   0.4983   0.0519
  -1.500   0.2291   0.00881   0.00165  -0.0756   0.4667   0.0537
  -1.250   0.2547   0.00886   0.00163  -0.0750   0.4450   0.0555
  -1.000   0.2807   0.00890   0.00162  -0.0746   0.4296   0.0571
  -0.750   0.3071   0.00893   0.00160  -0.0741   0.4178   0.0588
  -0.500   0.3335   0.00897   0.00159  -0.0738   0.4075   0.0602
  -0.250   0.3601   0.00897   0.00157  -0.0734   0.3988   0.0628
   0.000   0.3864   0.00899   0.00157  -0.0730   0.3902   0.0663
   0.250   0.4132   0.00899   0.00157  -0.0727   0.3830   0.0697
   0.500   0.4398   0.00903   0.00158  -0.0723   0.3759   0.0725
   0.750   0.4664   0.00903   0.00159  -0.0720   0.3705   0.0795
   1.250   0.5193   0.00903   0.00165  -0.0713   0.3594   0.1065
   1.500   0.5455   0.00898   0.00169  -0.0709   0.3550   0.1439
   1.750   0.5713   0.00887   0.00173  -0.0704   0.3498   0.2056
   2.000   0.5943   0.00856   0.00181  -0.0696   0.3427   0.3759
   2.250   0.6120   0.00786   0.00191  -0.0678   0.3358   0.6765
   2.500   0.6613   0.00737   0.00215  -0.0723   0.3251   0.9688
   2.750   0.7118   0.00751   0.00225  -0.0773   0.3189   0.9898
   3.000   0.7574   0.00766   0.00234  -0.0812   0.3123   0.9992
   3.250   0.7860   0.00778   0.00242  -0.0814   0.3047   1.0000
   3.500   0.8087   0.00793   0.00251  -0.0803   0.2956   1.0000
   3.750   0.8324   0.00804   0.00259  -0.0794   0.2907   1.0000
   4.000   0.8559   0.00816   0.00268  -0.0785   0.2840   1.0000
   4.250   0.8790   0.00832   0.00279  -0.0775   0.2759   1.0000
   4.500   0.9023   0.00846   0.00290  -0.0765   0.2678   1.0000
   4.750   0.9257   0.00861   0.00302  -0.0756   0.2610   1.0000
   5.000   0.9491   0.00877   0.00314  -0.0746   0.2532   1.0000
   5.250   0.9722   0.00894   0.00328  -0.0737   0.2448   1.0000
   5.500   0.9948   0.00916   0.00344  -0.0726   0.2334   1.0000
   5.750   1.0167   0.00941   0.00362  -0.0715   0.2184   1.0000
   6.000   1.0364   0.00981   0.00388  -0.0700   0.1925   1.0000
   6.250   1.0545   0.01032   0.00422  -0.0682   0.1626   1.0000
   6.500   1.0738   0.01076   0.00455  -0.0667   0.1411   1.0000
   6.750   1.0936   0.01117   0.00487  -0.0652   0.1250   1.0000
   7.000   1.1143   0.01151   0.00516  -0.0640   0.1131   1.0000
   7.250   1.1346   0.01188   0.00546  -0.0626   0.1001   1.0000
   7.500   1.1484   0.01268   0.00603  -0.0603   0.0630   1.0000
   7.750   1.1683   0.01306   0.00638  -0.0589   0.0576   1.0000
   8.000   1.1886   0.01339   0.00671  -0.0576   0.0533   1.0000
   8.250   1.2098   0.01366   0.00699  -0.0565   0.0518   1.0000
   8.500   1.2306   0.01394   0.00729  -0.0553   0.0506   1.0000
   8.750   1.2507   0.01425   0.00762  -0.0540   0.0491   1.0000
   9.000   1.2698   0.01459   0.00798  -0.0525   0.0474   1.0000
   9.250   1.2873   0.01494   0.00834  -0.0507   0.0459   1.0000
   9.500   1.3033   0.01531   0.00873  -0.0487   0.0440   1.0000
   9.750   1.3203   0.01564   0.00909  -0.0469   0.0433   1.0000
  10.000   1.3382   0.01593   0.00941  -0.0453   0.0421   1.0000
  10.250   1.3551   0.01628   0.00979  -0.0435   0.0405   1.0000
  10.500   1.3711   0.01670   0.01022  -0.0417   0.0385   1.0000
  10.750   1.3859   0.01718   0.01070  -0.0398   0.0363   1.0000
  11.000   1.4021   0.01760   0.01116  -0.0381   0.0344   1.0000
  11.250   1.4157   0.01817   0.01170  -0.0362   0.0296   1.0000
  11.750   1.4346   0.01982   0.01327  -0.0315   0.0166   1.0000
  12.000   1.4450   0.02063   0.01411  -0.0294   0.0146   1.0000
  12.250   1.4550   0.02150   0.01502  -0.0274   0.0132   1.0000
  12.500   1.4661   0.02233   0.01590  -0.0257   0.0125   1.0000
  12.750   1.4760   0.02329   0.01691  -0.0240   0.0117   1.0000
  13.000   1.4847   0.02437   0.01803  -0.0223   0.0111   1.0000
  13.250   1.4919   0.02561   0.01933  -0.0206   0.0104   1.0000
  13.500   1.5011   0.02676   0.02054  -0.0193   0.0100   1.0000
  13.750   1.5089   0.02808   0.02192  -0.0180   0.0096   1.0000
  14.000   1.5155   0.02954   0.02345  -0.0168   0.0092   1.0000
  14.250   1.5209   0.03118   0.02515  -0.0157   0.0088   1.0000
  14.500   1.5247   0.03304   0.02708  -0.0147   0.0085   1.0000
  14.750   1.5266   0.03516   0.02927  -0.0138   0.0081   1.0000
  15.000   1.5274   0.03749   0.03168  -0.0132   0.0080   1.0000
  15.250   1.5295   0.03981   0.03409  -0.0128   0.0078   1.0000
  15.500   1.5310   0.04229   0.03666  -0.0126   0.0077   1.0000
  15.750   1.5308   0.04507   0.03952  -0.0125   0.0075   1.0000
  16.000   1.5284   0.04821   0.04276  -0.0127   0.0074   1.0000
  16.250   1.5258   0.05146   0.04610  -0.0131   0.0072   1.0000
  16.500   1.5208   0.05508   0.04982  -0.0136   0.0071   1.0000
  16.750   1.5148   0.05892   0.05375  -0.0143   0.0069   1.0000
  17.000   1.5073   0.06310   0.05803  -0.0152   0.0068   1.0000
  17.250   1.4973   0.06766   0.06270  -0.0163   0.0068   1.0000
  17.500   1.4879   0.07223   0.06737  -0.0175   0.0066   1.0000
  17.750   1.4773   0.07705   0.07227  -0.0188   0.0065   1.0000
  18.000   1.4649   0.08215   0.07746  -0.0203   0.0063   1.0000
  18.250   1.4537   0.08712   0.08254  -0.0218   0.0064   1.0000
  18.500   1.4407   0.09242   0.08794  -0.0235   0.0062   1.0000
  18.750   1.4285   0.09769   0.09331  -0.0253   0.0062   1.0000
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