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GOE 758 AIRFOIL (goe758-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 758 AIRFOIL (goe758-il)
Reynolds number: 1,000,000
Max Cl/Cd: 123.12 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe758-il-1000000-n5.txt
Download as CSV file: xf-goe758-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 758 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.6438   0.03531   0.03269  -0.1158   0.9388   0.0173
 -12.500  -0.6161   0.03220   0.02928  -0.1244   0.8993   0.0174
 -12.250  -0.6209   0.03087   0.02774  -0.1224   0.8701   0.0174
 -12.000  -0.6249   0.02973   0.02645  -0.1193   0.8530   0.0175
 -11.750  -0.6180   0.02872   0.02531  -0.1177   0.8406   0.0175
 -11.500  -0.6069   0.02791   0.02437  -0.1162   0.8292   0.0176
 -11.250  -0.5905   0.02746   0.02384  -0.1152   0.8188   0.0178
 -11.000  -0.5784   0.02640   0.02264  -0.1139   0.8087   0.0179
 -10.750  -0.5628   0.02565   0.02177  -0.1127   0.7975   0.0181
 -10.500  -0.5471   0.02478   0.02075  -0.1116   0.7845   0.0182
 -10.250  -0.5316   0.02376   0.01957  -0.1104   0.7698   0.0184
 -10.000  -0.5154   0.02274   0.01835  -0.1093   0.7528   0.0187
  -9.750  -0.4988   0.02176   0.01714  -0.1081   0.7298   0.0189
  -9.500  -0.4818   0.02083   0.01596  -0.1068   0.6975   0.0192
  -9.250  -0.4637   0.01999   0.01486  -0.1056   0.6699   0.0195
  -9.000  -0.4435   0.01922   0.01389  -0.1046   0.6537   0.0198
  -8.750  -0.4218   0.01855   0.01304  -0.1039   0.6425   0.0200
  -8.500  -0.3994   0.01789   0.01223  -0.1032   0.6341   0.0202
  -8.250  -0.3763   0.01731   0.01151  -0.1026   0.6266   0.0203
  -8.000  -0.3524   0.01683   0.01091  -0.1020   0.6205   0.0204
  -7.750  -0.3296   0.01598   0.00994  -0.1014   0.6155   0.0206
  -7.500  -0.3062   0.01525   0.00912  -0.1008   0.6107   0.0209
  -7.250  -0.2817   0.01479   0.00860  -0.1004   0.6060   0.0211
  -7.000  -0.2562   0.01441   0.00818  -0.1000   0.6022   0.0213
  -6.750  -0.2306   0.01406   0.00778  -0.0997   0.5983   0.0215
  -6.500  -0.2048   0.01377   0.00744  -0.0993   0.5944   0.0217
  -6.250  -0.1793   0.01341   0.00701  -0.0989   0.5906   0.0219
  -6.000  -0.1533   0.01305   0.00661  -0.0986   0.5875   0.0221
  -5.750  -0.1272   0.01270   0.00622  -0.0983   0.5843   0.0223
  -5.500  -0.1012   0.01235   0.00582  -0.0980   0.5808   0.0225
  -5.250  -0.0752   0.01205   0.00546  -0.0976   0.5773   0.0227
  -5.000  -0.0492   0.01176   0.00512  -0.0973   0.5738   0.0229
  -4.750  -0.0227   0.01147   0.00480  -0.0970   0.5710   0.0231
  -4.500   0.0038   0.01119   0.00450  -0.0967   0.5677   0.0233
  -4.250   0.0303   0.01094   0.00421  -0.0964   0.5642   0.0235
  -4.000   0.0568   0.01072   0.00394  -0.0961   0.5605   0.0238
  -3.750   0.0833   0.01052   0.00371  -0.0958   0.5566   0.0239
  -3.500   0.1104   0.01032   0.00348  -0.0956   0.5528   0.0242
  -3.250   0.1375   0.01017   0.00331  -0.0954   0.5484   0.0244
  -3.000   0.1646   0.01006   0.00317  -0.0952   0.5440   0.0246
  -2.750   0.1908   0.00981   0.00287  -0.0949   0.5403   0.0250
  -2.500   0.2177   0.00958   0.00263  -0.0946   0.5369   0.0254
  -2.250   0.2449   0.00943   0.00247  -0.0945   0.5330   0.0257
  -2.000   0.2720   0.00931   0.00233  -0.0943   0.5286   0.0261
  -1.750   0.2990   0.00922   0.00221  -0.0941   0.5248   0.0265
  -1.500   0.3267   0.00912   0.00211  -0.0939   0.5212   0.0269
  -1.250   0.3541   0.00904   0.00201  -0.0938   0.5168   0.0274
  -1.000   0.3814   0.00898   0.00193  -0.0936   0.5120   0.0279
  -0.750   0.4087   0.00893   0.00186  -0.0935   0.5079   0.0283
  -0.500   0.4363   0.00887   0.00180  -0.0934   0.5033   0.0289
  -0.250   0.4636   0.00885   0.00175  -0.0932   0.4976   0.0293
   0.000   0.4907   0.00883   0.00171  -0.0930   0.4927   0.0302
   0.250   0.5182   0.00878   0.00167  -0.0929   0.4880   0.0320
   0.500   0.5454   0.00878   0.00164  -0.0928   0.4821   0.0335
   1.000   0.5988   0.00862   0.00163  -0.0923   0.4704   0.1000
   1.250   0.6230   0.00825   0.00164  -0.0918   0.4644   0.2570
   1.500   0.6485   0.00806   0.00168  -0.0915   0.4590   0.3463
   1.750   0.6737   0.00789   0.00174  -0.0911   0.4520   0.4391
   2.000   0.6986   0.00778   0.00183  -0.0906   0.4452   0.5226
   2.250   0.7243   0.00774   0.00191  -0.0902   0.4382   0.5783
   2.500   0.7493   0.00772   0.00200  -0.0897   0.4314   0.6285
   2.750   0.7740   0.00765   0.00208  -0.0891   0.4249   0.6883
   3.000   0.7982   0.00766   0.00218  -0.0884   0.4168   0.7336
   3.500   0.8991   0.00751   0.00250  -0.0985   0.3977   1.0000
   3.750   0.9224   0.00770   0.00262  -0.0976   0.3852   1.0000
   4.000   0.9465   0.00785   0.00273  -0.0969   0.3756   1.0000
   4.250   0.9703   0.00802   0.00285  -0.0962   0.3676   1.0000
   4.500   0.9945   0.00816   0.00297  -0.0955   0.3601   1.0000
   4.750   1.0180   0.00835   0.00311  -0.0947   0.3521   1.0000
   5.000   1.0415   0.00854   0.00326  -0.0939   0.3423   1.0000
   5.250   1.0651   0.00872   0.00341  -0.0932   0.3355   1.0000
   5.500   1.0891   0.00888   0.00356  -0.0925   0.3289   1.0000
   5.750   1.1123   0.00908   0.00372  -0.0917   0.3229   1.0000
   6.000   1.1364   0.00923   0.00388  -0.0911   0.3173   1.0000
   6.250   1.1595   0.00944   0.00406  -0.0903   0.3106   1.0000
   6.500   1.1822   0.00965   0.00425  -0.0894   0.3020   1.0000
   6.750   1.2037   0.00993   0.00448  -0.0884   0.2921   1.0000
   7.000   1.2263   0.01014   0.00468  -0.0876   0.2835   1.0000
   7.250   1.2478   0.01040   0.00491  -0.0865   0.2755   1.0000
   7.500   1.2680   0.01072   0.00517  -0.0853   0.2633   1.0000
   7.750   1.2884   0.01101   0.00543  -0.0841   0.2523   1.0000
   8.000   1.3081   0.01131   0.00570  -0.0828   0.2426   1.0000
   8.250   1.3242   0.01176   0.00606  -0.0809   0.2250   1.0000
   8.500   1.3350   0.01231   0.00649  -0.0780   0.2047   1.0000
   8.750   1.3444   0.01287   0.00696  -0.0749   0.1850   1.0000
   9.000   1.3504   0.01359   0.00755  -0.0714   0.1622   1.0000
   9.250   1.3378   0.01517   0.00881  -0.0652   0.1088   1.0000
   9.500   1.3394   0.01626   0.00979  -0.0616   0.0860   1.0000
   9.750   1.3491   0.01705   0.01056  -0.0593   0.0772   1.0000
  10.000   1.3613   0.01776   0.01127  -0.0575   0.0705   1.0000
  10.250   1.3702   0.01870   0.01219  -0.0555   0.0614   1.0000
  10.500   1.3643   0.02061   0.01393  -0.0521   0.0330   1.0000
  10.750   1.3654   0.02227   0.01554  -0.0498   0.0203   1.0000
  11.000   1.3741   0.02350   0.01678  -0.0484   0.0172   1.0000
  11.250   1.3842   0.02468   0.01800  -0.0473   0.0158   1.0000
  11.500   1.3934   0.02598   0.01934  -0.0461   0.0146   1.0000
  11.750   1.4018   0.02740   0.02080  -0.0451   0.0136   1.0000
  12.000   1.4110   0.02881   0.02226  -0.0442   0.0127   1.0000
  12.250   1.4193   0.03034   0.02384  -0.0434   0.0123   1.0000
  12.500   1.4259   0.03207   0.02562  -0.0426   0.0116   1.0000
  12.750   1.4316   0.03396   0.02756  -0.0419   0.0111   1.0000
  13.000   1.4365   0.03598   0.02964  -0.0413   0.0107   1.0000
  13.250   1.4424   0.03794   0.03167  -0.0408   0.0104   1.0000
  13.500   1.4478   0.03998   0.03377  -0.0404   0.0101   1.0000
  13.750   1.4520   0.04220   0.03604  -0.0400   0.0098   1.0000
  14.000   1.4552   0.04454   0.03845  -0.0397   0.0095   1.0000
  14.250   1.4575   0.04697   0.04094  -0.0393   0.0093   1.0000
  14.500   1.4585   0.04958   0.04362  -0.0391   0.0089   1.0000
  14.750   1.4591   0.05228   0.04637  -0.0388   0.0088   1.0000
  15.000   1.4577   0.05521   0.04936  -0.0386   0.0084   1.0000
  15.250   1.4553   0.05831   0.05253  -0.0385   0.0082   1.0000
  15.500   1.4560   0.06109   0.05539  -0.0385   0.0080   1.0000
  15.750   1.4560   0.06399   0.05836  -0.0385   0.0079   1.0000
  16.000   1.4546   0.06708   0.06153  -0.0385   0.0077   1.0000
  16.250   1.4518   0.07040   0.06492  -0.0387   0.0076   1.0000
  16.500   1.4487   0.07381   0.06841  -0.0389   0.0075   1.0000
  16.750   1.4470   0.07709   0.07176  -0.0392   0.0072   1.0000
  17.000   1.4439   0.08055   0.07529  -0.0395   0.0072   1.0000
  17.250   1.4392   0.08428   0.07910  -0.0399   0.0071   1.0000
  17.500   1.4359   0.08787   0.08275  -0.0405   0.0069   1.0000
  17.750   1.4314   0.09166   0.08661  -0.0410   0.0068   1.0000
  18.000   1.4268   0.09548   0.09051  -0.0417   0.0066   1.0000
  18.250   1.4200   0.09967   0.09478  -0.0426   0.0066   1.0000
  18.500   1.4151   0.10365   0.09883  -0.0435   0.0064   1.0000
  18.750   1.4084   0.10795   0.10321  -0.0446   0.0063   1.0000
  19.000   1.4021   0.11227   0.10760  -0.0458   0.0062   1.0000
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