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GOE 514 AIRFOIL (goe514-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 514 AIRFOIL (goe514-il)
Reynolds number: 500,000
Max Cl/Cd: 69.2 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe514-il-500000.txt
Download as CSV file: xf-goe514-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 514 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.4908   0.08378   0.08077  -0.0982   0.9834   0.0185
 -14.750  -0.5119   0.07508   0.07192  -0.1060   0.9825   0.0185
 -14.500  -0.5499   0.06690   0.06358  -0.1107   0.9769   0.0184
 -14.250  -0.5694   0.05964   0.05617  -0.1176   0.9740   0.0183
 -14.000  -0.5897   0.05102   0.04736  -0.1276   0.9715   0.0182
 -13.750  -0.6073   0.04351   0.03964  -0.1363   0.9660   0.0180
 -13.500  -0.6205   0.03869   0.03462  -0.1387   0.9612   0.0182
 -13.250  -0.6181   0.03576   0.03154  -0.1396   0.9586   0.0184
 -13.000  -0.6085   0.03358   0.02922  -0.1402   0.9569   0.0186
 -12.750  -0.6269   0.03269   0.02826  -0.1336   0.9491   0.0188
 -12.500  -0.6193   0.03134   0.02681  -0.1319   0.9457   0.0190
 -12.250  -0.6067   0.02988   0.02525  -0.1309   0.9435   0.0194
 -12.000  -0.5860   0.02845   0.02370  -0.1310   0.9421   0.0196
 -11.750  -0.5996   0.02793   0.02310  -0.1239   0.9335   0.0198
 -11.500  -0.5814   0.02673   0.02178  -0.1230   0.9307   0.0203
 -11.250  -0.5583   0.02556   0.02048  -0.1230   0.9290   0.0207
 -11.000  -0.5323   0.02444   0.01921  -0.1233   0.9279   0.0211
 -10.750  -0.5067   0.02313   0.01780  -0.1237   0.9269   0.0217
 -10.500  -0.5162   0.02276   0.01738  -0.1167   0.9179   0.0220
 -10.250  -0.4927   0.02181   0.01639  -0.1163   0.9155   0.0228
 -10.000  -0.4629   0.02095   0.01546  -0.1170   0.9140   0.0238
  -9.750  -0.4285   0.02006   0.01446  -0.1185   0.9130   0.0248
  -9.500  -0.3921   0.01890   0.01322  -0.1207   0.9119   0.0259
  -9.250  -0.3523   0.01792   0.01219  -0.1233   0.9108   0.0273
  -9.000  -0.3454   0.01754   0.01175  -0.1190   0.9035   0.0283
  -8.750  -0.3180   0.01679   0.01092  -0.1189   0.8997   0.0300
  -8.500  -0.2840   0.01601   0.01011  -0.1202   0.8974   0.0325
  -8.250  -0.2455   0.01522   0.00927  -0.1225   0.8954   0.0364
  -8.000  -0.2056   0.01449   0.00854  -0.1250   0.8936   0.0434
  -7.750  -0.2018   0.01425   0.00830  -0.1198   0.8850   0.0483
  -7.500  -0.1669   0.01378   0.00784  -0.1212   0.8812   0.0580
  -7.250  -0.1268   0.01332   0.00735  -0.1236   0.8781   0.0661
  -7.000  -0.1090   0.01313   0.00711  -0.1213   0.8711   0.0705
  -6.750  -0.0832   0.01268   0.00665  -0.1207   0.8647   0.0766
  -6.500  -0.0454   0.01225   0.00614  -0.1227   0.8603   0.0825
  -6.250  -0.0362   0.01198   0.00589  -0.1186   0.8503   0.0868
  -6.000  -0.0030   0.01160   0.00546  -0.1196   0.8444   0.0934
  -5.750   0.0095   0.01137   0.00526  -0.1161   0.8338   0.0999
  -5.500   0.0413   0.01107   0.00499  -0.1168   0.8264   0.1134
  -5.250   0.0579   0.01095   0.00489  -0.1142   0.8147   0.1274
  -5.000   0.0800   0.01088   0.00482  -0.1128   0.8035   0.1410
  -4.750   0.1051   0.01080   0.00470  -0.1120   0.7917   0.1521
  -4.500   0.1309   0.01082   0.00458  -0.1113   0.7786   0.1596
  -4.250   0.1519   0.01069   0.00443  -0.1097   0.7644   0.1664
  -4.000   0.1737   0.01070   0.00433  -0.1082   0.7504   0.1718
  -3.750   0.1958   0.01075   0.00425  -0.1068   0.7377   0.1756
  -3.500   0.2172   0.01065   0.00411  -0.1053   0.7257   0.1806
  -3.250   0.2374   0.01066   0.00405  -0.1036   0.7135   0.1847
  -3.000   0.2549   0.01068   0.00400  -0.1012   0.7016   0.1884
  -2.750   0.2727   0.01071   0.00393  -0.0989   0.6902   0.1910
  -2.500   0.2885   0.01068   0.00384  -0.0962   0.6787   0.1943
  -2.250   0.3021   0.01064   0.00379  -0.0931   0.6674   0.1980
  -2.000   0.3175   0.01065   0.00375  -0.0903   0.6561   0.2013
  -1.750   0.3317   0.01069   0.00372  -0.0873   0.6437   0.2046
  -1.500   0.3448   0.01072   0.00369  -0.0840   0.6301   0.2073
  -1.250   0.3577   0.01076   0.00367  -0.0808   0.6159   0.2102
  -1.000   0.3694   0.01082   0.00369  -0.0773   0.5997   0.2143
  -0.750   0.3798   0.01093   0.00373  -0.0735   0.5808   0.2179
  -0.500   0.3904   0.01107   0.00378  -0.0699   0.5606   0.2220
  -0.250   0.3993   0.01126   0.00386  -0.0659   0.5378   0.2270
   0.000   0.4089   0.01146   0.00398  -0.0622   0.5135   0.2336
   0.250   0.4196   0.01171   0.00410  -0.0587   0.4919   0.2403
   0.500   0.4316   0.01191   0.00424  -0.0556   0.4746   0.2476
   0.750   0.4465   0.01213   0.00438  -0.0530   0.4609   0.2565
   1.000   0.4622   0.01233   0.00453  -0.0506   0.4498   0.2653
   1.250   0.4791   0.01255   0.00469  -0.0485   0.4398   0.2751
   1.500   0.4968   0.01271   0.00482  -0.0465   0.4319   0.2833
   1.750   0.5153   0.01290   0.00497  -0.0448   0.4247   0.2911
   2.000   0.5331   0.01311   0.00512  -0.0429   0.4186   0.2978
   2.250   0.5535   0.01321   0.00525  -0.0415   0.4131   0.3045
   2.500   0.5730   0.01340   0.00539  -0.0400   0.4076   0.3107
   2.750   0.5906   0.01360   0.00555  -0.0381   0.4024   0.3165
   3.000   0.6108   0.01372   0.00569  -0.0368   0.3980   0.3224
   3.250   0.6309   0.01387   0.00584  -0.0354   0.3931   0.3280
   3.500   0.6497   0.01403   0.00598  -0.0338   0.3888   0.3334
   3.750   0.6688   0.01426   0.00617  -0.0323   0.3843   0.3392
   4.000   0.6895   0.01439   0.00633  -0.0311   0.3809   0.3451
   4.250   0.7091   0.01451   0.00648  -0.0297   0.3773   0.3508
   4.500   0.7286   0.01467   0.00666  -0.0283   0.3737   0.3578
   4.750   0.7479   0.01489   0.00684  -0.0269   0.3701   0.3645
   5.000   0.7681   0.01510   0.00705  -0.0258   0.3663   0.3717
   5.250   0.7876   0.01522   0.00724  -0.0244   0.3632   0.3820
   5.500   0.8070   0.01536   0.00744  -0.0231   0.3600   0.3934
   5.750   0.8262   0.01551   0.00765  -0.0218   0.3570   0.4101
   6.000   0.8433   0.01545   0.00784  -0.0202   0.3541   0.5055
   6.250   1.1148   0.01611   0.00966  -0.0735   0.3440   1.0000
   6.500   1.1291   0.01633   0.00988  -0.0712   0.3408   1.0000
   6.750   1.1431   0.01660   0.01012  -0.0690   0.3377   1.0000
   7.000   1.1579   0.01694   0.01040  -0.0669   0.3338   1.0000
   7.250   1.1735   0.01719   0.01068  -0.0650   0.3312   1.0000
   7.500   1.1895   0.01744   0.01096  -0.0632   0.3289   1.0000
   7.750   1.2054   0.01771   0.01125  -0.0613   0.3265   1.0000
   8.000   1.2212   0.01800   0.01156  -0.0595   0.3240   1.0000
   8.250   1.2371   0.01832   0.01187  -0.0578   0.3215   1.0000
   8.500   1.2529   0.01869   0.01221  -0.0561   0.3184   1.0000
   8.750   1.2695   0.01905   0.01257  -0.0546   0.3154   1.0000
   9.000   1.2851   0.01937   0.01295  -0.0529   0.3133   1.0000
   9.250   1.3012   0.01971   0.01333  -0.0513   0.3110   1.0000
   9.500   1.3171   0.02007   0.01371  -0.0497   0.3085   1.0000
   9.750   1.3321   0.02048   0.01414  -0.0481   0.3058   1.0000
  10.000   1.3460   0.02095   0.01458  -0.0463   0.3023   1.0000
  10.250   1.3609   0.02141   0.01506  -0.0447   0.2988   1.0000
  10.500   1.3748   0.02185   0.01558  -0.0430   0.2958   1.0000
  10.750   1.3881   0.02234   0.01612  -0.0413   0.2922   1.0000
  11.000   1.4017   0.02288   0.01666  -0.0397   0.2889   1.0000
  11.250   1.4148   0.02348   0.01724  -0.0381   0.2857   1.0000
  11.500   1.4284   0.02405   0.01788  -0.0366   0.2824   1.0000
  11.750   1.4420   0.02462   0.01853  -0.0352   0.2788   1.0000
  12.000   1.4545   0.02528   0.01922  -0.0336   0.2750   1.0000
  12.250   1.4655   0.02604   0.01998  -0.0320   0.2711   1.0000
  12.500   1.4770   0.02682   0.02079  -0.0305   0.2673   1.0000
  12.750   1.4900   0.02753   0.02159  -0.0293   0.2625   1.0000
  13.000   1.5010   0.02840   0.02249  -0.0278   0.2584   1.0000
  13.250   1.5096   0.02944   0.02352  -0.0263   0.2543   1.0000
  13.500   1.5218   0.03030   0.02447  -0.0251   0.2493   1.0000
  13.750   1.5304   0.03142   0.02563  -0.0237   0.2430   1.0000
  14.000   1.5371   0.03271   0.02693  -0.0223   0.2367   1.0000
  14.250   1.5471   0.03383   0.02811  -0.0212   0.2308   1.0000
  14.500   1.5497   0.03551   0.02978  -0.0196   0.2239   1.0000
  14.750   1.5559   0.03700   0.03131  -0.0185   0.2142   1.0000
  15.000   1.5580   0.03883   0.03316  -0.0171   0.2055   1.0000
  15.250   1.5552   0.04114   0.03546  -0.0156   0.1953   1.0000
  15.500   1.5473   0.04399   0.03827  -0.0140   0.1804   1.0000
  15.750   1.5332   0.04752   0.04175  -0.0124   0.1642   1.0000
  16.000   1.5222   0.05087   0.04509  -0.0111   0.1539   1.0000
  16.250   1.5006   0.05544   0.04963  -0.0098   0.1392   1.0000
  16.500   1.4828   0.05984   0.05405  -0.0089   0.1301   1.0000
  16.750   1.4686   0.06399   0.05823  -0.0084   0.1226   1.0000
  17.000   1.4521   0.06854   0.06283  -0.0081   0.1171   1.0000
  17.250   1.4324   0.07365   0.06799  -0.0080   0.1092   1.0000
  17.500   1.4108   0.07915   0.07353  -0.0082   0.1013   1.0000
  17.750   1.3905   0.08462   0.07906  -0.0087   0.0951   1.0000
  18.000   1.3674   0.09057   0.08503  -0.0094   0.0841   1.0000
  18.250   1.3420   0.09692   0.09140  -0.0103   0.0726   1.0000
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