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GOE 546 AIRFOIL (goe546-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 546 AIRFOIL (goe546-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.65 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe546-il-1000000.txt
Download as CSV file: xf-goe546-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 546 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.7443   0.06960   0.06777  -0.0585   1.0000   0.0130
 -13.000  -0.9214   0.03592   0.03357  -0.0837   1.0000   0.0121
 -12.750  -0.9340   0.03314   0.03063  -0.0820   1.0000   0.0122
 -12.500  -0.9424   0.03058   0.02788  -0.0798   1.0000   0.0123
 -12.250  -0.9441   0.02873   0.02587  -0.0773   1.0000   0.0124
 -12.000  -0.9175   0.02674   0.02364  -0.0798   0.9982   0.0126
 -11.750  -0.8958   0.02337   0.01993  -0.0829   0.9955   0.0132
 -11.500  -0.8646   0.02250   0.01900  -0.0847   0.9941   0.0136
 -11.250  -0.8349   0.02195   0.01841  -0.0859   0.9917   0.0139
 -11.000  -0.8034   0.02143   0.01784  -0.0873   0.9893   0.0144
 -10.750  -0.7716   0.02070   0.01701  -0.0889   0.9871   0.0149
 -10.500  -0.7394   0.01988   0.01604  -0.0906   0.9854   0.0155
 -10.250  -0.7063   0.01923   0.01527  -0.0923   0.9841   0.0158
 -10.000  -0.6844   0.01745   0.01330  -0.0926   0.9783   0.0165
  -9.750  -0.6522   0.01715   0.01299  -0.0938   0.9757   0.0171
  -9.500  -0.6191   0.01688   0.01269  -0.0952   0.9737   0.0177
  -9.250  -0.5861   0.01634   0.01207  -0.0967   0.9721   0.0183
  -9.000  -0.5601   0.01580   0.01143  -0.0966   0.9651   0.0189
  -8.750  -0.5267   0.01551   0.01105  -0.0979   0.9619   0.0194
  -8.500  -0.4940   0.01429   0.00971  -0.0998   0.9592   0.0205
  -8.250  -0.4628   0.01410   0.00952  -0.1006   0.9528   0.0212
  -8.000  -0.4288   0.01379   0.00916  -0.1021   0.9482   0.0220
  -7.750  -0.3950   0.01338   0.00866  -0.1036   0.9436   0.0229
  -7.500  -0.3638   0.01308   0.00828  -0.1044   0.9369   0.0236
  -7.250  -0.3336   0.01226   0.00732  -0.1053   0.9307   0.0245
  -7.000  -0.3065   0.01179   0.00682  -0.1053   0.9232   0.0255
  -6.750  -0.2774   0.01154   0.00652  -0.1057   0.9167   0.0263
  -6.500  -0.2508   0.01125   0.00618  -0.1055   0.9102   0.0272
  -6.250  -0.2237   0.01099   0.00585  -0.1053   0.9043   0.0281
  -6.000  -0.1959   0.01084   0.00563  -0.1053   0.8990   0.0289
  -5.750  -0.1697   0.01066   0.00540  -0.1049   0.8933   0.0294
  -5.500  -0.1463   0.00977   0.00443  -0.1042   0.8874   0.0307
  -5.250  -0.1199   0.00950   0.00414  -0.1040   0.8823   0.0317
  -5.000  -0.0937   0.00930   0.00392  -0.1036   0.8769   0.0328
  -4.750  -0.0671   0.00907   0.00364  -0.1033   0.8716   0.0338
  -4.500  -0.0406   0.00887   0.00339  -0.1029   0.8657   0.0347
  -4.250  -0.0145   0.00868   0.00316  -0.1025   0.8586   0.0354
  -4.000   0.0117   0.00843   0.00285  -0.1021   0.8518   0.0364
  -3.750   0.0372   0.00808   0.00247  -0.1015   0.8453   0.0383
  -3.500   0.0640   0.00792   0.00226  -0.1012   0.8394   0.0398
  -3.250   0.0909   0.00777   0.00210  -0.1009   0.8335   0.0414
  -3.000   0.1178   0.00764   0.00194  -0.1006   0.8270   0.0431
  -2.750   0.1447   0.00749   0.00175  -0.1003   0.8208   0.0460
  -2.500   0.1714   0.00732   0.00160  -0.0999   0.8136   0.0508
  -2.250   0.1982   0.00720   0.00146  -0.0996   0.8065   0.0587
  -2.000   0.2248   0.00701   0.00134  -0.0993   0.7985   0.0785
  -1.750   0.2500   0.00666   0.00121  -0.0988   0.7906   0.1546
  -1.500   0.2745   0.00620   0.00114  -0.0983   0.7811   0.2785
  -1.250   0.3001   0.00599   0.00109  -0.0978   0.7704   0.3453
  -1.000   0.3256   0.00585   0.00106  -0.0973   0.7581   0.4018
  -0.750   0.3513   0.00577   0.00105  -0.0968   0.7437   0.4467
  -0.500   0.3770   0.00573   0.00104  -0.0962   0.7277   0.4815
  -0.250   0.4024   0.00569   0.00104  -0.0956   0.7100   0.5173
   0.000   0.4272   0.00563   0.00107  -0.0949   0.6933   0.5688
   0.250   0.4512   0.00551   0.00111  -0.0941   0.6780   0.6409
   0.500   0.4735   0.00532   0.00116  -0.0928   0.6642   0.7382
   0.750   0.4925   0.00504   0.00126  -0.0905   0.6516   0.8826
   1.000   0.5382   0.00504   0.00132  -0.0943   0.6371   0.9618
   1.250   0.5870   0.00518   0.00136  -0.0990   0.6161   0.9900
   1.500   0.6193   0.00533   0.00142  -0.1000   0.5979   1.0000
   1.750   0.6434   0.00543   0.00146  -0.0992   0.5862   1.0000
   2.000   0.6675   0.00554   0.00152  -0.0983   0.5740   1.0000
   2.250   0.6915   0.00566   0.00157  -0.0974   0.5592   1.0000
   2.500   0.7155   0.00578   0.00164  -0.0965   0.5423   1.0000
   2.750   0.7392   0.00593   0.00171  -0.0956   0.5218   1.0000
   3.000   0.7621   0.00613   0.00180  -0.0945   0.4966   1.0000
   3.250   0.7841   0.00639   0.00192  -0.0933   0.4642   1.0000
   3.500   0.8057   0.00669   0.00207  -0.0920   0.4297   1.0000
   3.750   0.8280   0.00698   0.00222  -0.0909   0.3995   1.0000
   4.000   0.8498   0.00732   0.00240  -0.0897   0.3647   1.0000
   4.250   0.8694   0.00781   0.00264  -0.0882   0.3104   1.0000
   4.500   0.8872   0.00845   0.00296  -0.0864   0.2480   1.0000
   4.750   0.9068   0.00898   0.00327  -0.0849   0.2050   1.0000
   5.000   0.9227   0.00978   0.00369  -0.0828   0.1320   1.0000
   5.250   0.9384   0.01061   0.00420  -0.0807   0.0731   1.0000
   5.500   0.9575   0.01119   0.00459  -0.0791   0.0422   1.0000
   5.750   0.9802   0.01151   0.00489  -0.0781   0.0389   1.0000
   6.000   1.0026   0.01183   0.00522  -0.0771   0.0363   1.0000
   6.250   1.0248   0.01217   0.00558  -0.0761   0.0347   1.0000
   6.500   1.0476   0.01246   0.00588  -0.0751   0.0339   1.0000
   6.750   1.0697   0.01278   0.00623  -0.0741   0.0332   1.0000
   7.000   1.0913   0.01312   0.00660  -0.0730   0.0323   1.0000
   7.250   1.1123   0.01349   0.00700  -0.0718   0.0314   1.0000
   7.500   1.1323   0.01391   0.00744  -0.0705   0.0304   1.0000
   7.750   1.1508   0.01442   0.00797  -0.0688   0.0293   1.0000
   8.000   1.1645   0.01518   0.00882  -0.0664   0.0281   1.0000
   8.250   1.1833   0.01556   0.00923  -0.0648   0.0276   1.0000
   8.500   1.2010   0.01592   0.00962  -0.0631   0.0272   1.0000
   8.750   1.2173   0.01634   0.01008  -0.0611   0.0266   1.0000
   9.000   1.2333   0.01677   0.01056  -0.0591   0.0260   1.0000
   9.250   1.2493   0.01722   0.01103  -0.0571   0.0252   1.0000
   9.500   1.2650   0.01769   0.01152  -0.0552   0.0244   1.0000
   9.750   1.2786   0.01828   0.01214  -0.0530   0.0238   1.0000
  10.000   1.2882   0.01911   0.01301  -0.0503   0.0230   1.0000
  10.250   1.2897   0.02046   0.01445  -0.0466   0.0222   1.0000
  10.500   1.3095   0.02072   0.01474  -0.0455   0.0218   1.0000
  10.750   1.3255   0.02122   0.01529  -0.0440   0.0213   1.0000
  11.000   1.3412   0.02176   0.01587  -0.0425   0.0206   1.0000
  11.250   1.3561   0.02235   0.01651  -0.0410   0.0200   1.0000
  11.500   1.3699   0.02303   0.01722  -0.0394   0.0194   1.0000
  11.750   1.3833   0.02375   0.01797  -0.0379   0.0189   1.0000
  12.000   1.3927   0.02476   0.01901  -0.0360   0.0184   1.0000
  12.250   1.3948   0.02636   0.02068  -0.0335   0.0176   1.0000
  12.500   1.4099   0.02703   0.02141  -0.0324   0.0173   1.0000
  12.750   1.4231   0.02787   0.02232  -0.0312   0.0168   1.0000
  13.000   1.4361   0.02875   0.02326  -0.0300   0.0163   1.0000
  13.250   1.4492   0.02963   0.02418  -0.0289   0.0158   1.0000
  13.500   1.4601   0.03072   0.02531  -0.0277   0.0154   1.0000
  13.750   1.4718   0.03176   0.02638  -0.0267   0.0149   1.0000
  14.000   1.4769   0.03340   0.02807  -0.0254   0.0145   1.0000
  14.250   1.4717   0.03602   0.03079  -0.0236   0.0140   1.0000
  14.500   1.4819   0.03734   0.03219  -0.0228   0.0138   1.0000
  14.750   1.4889   0.03900   0.03394  -0.0220   0.0135   1.0000
  15.000   1.4974   0.04054   0.03555  -0.0214   0.0130   1.0000
  15.250   1.5028   0.04247   0.03756  -0.0208   0.0127   1.0000
  15.500   1.5101   0.04426   0.03941  -0.0204   0.0124   1.0000
  15.750   1.5168   0.04616   0.04136  -0.0202   0.0120   1.0000
  16.000   1.5188   0.04864   0.04391  -0.0199   0.0117   1.0000
  16.250   1.5184   0.05150   0.04684  -0.0199   0.0115   1.0000
  16.500   1.5103   0.05540   0.05085  -0.0201   0.0112   1.0000
  16.750   1.5006   0.05964   0.05521  -0.0205   0.0109   1.0000
  17.000   1.5004   0.06282   0.05849  -0.0210   0.0108   1.0000
  17.250   1.4993   0.06619   0.06197  -0.0217   0.0107   1.0000
  17.500   1.4950   0.07010   0.06600  -0.0227   0.0105   1.0000
  17.750   1.4904   0.07416   0.07017  -0.0238   0.0104   1.0000
  18.000   1.4845   0.07853   0.07466  -0.0252   0.0102   1.0000
  18.250   1.4774   0.08323   0.07946  -0.0269   0.0101   1.0000
  18.500   1.4717   0.08785   0.08419  -0.0287   0.0098   1.0000
  18.750   1.4611   0.09332   0.08978  -0.0309   0.0098   1.0000
  19.000   1.4512   0.09887   0.09544  -0.0334   0.0097   1.0000
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