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GOE 514 AIRFOIL (goe514-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 514 AIRFOIL (goe514-il)
Reynolds number: 1,000,000
Max Cl/Cd: 84.13 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe514-il-1000000.txt
Download as CSV file: xf-goe514-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.4346   0.12456   0.12236  -0.0843   0.9884   0.0125
 -17.750  -0.4547   0.11590   0.11357  -0.0894   0.9876   0.0123
 -17.500  -0.4703   0.10868   0.10627  -0.0941   0.9868   0.0125
 -17.250  -0.4733   0.10357   0.10111  -0.0978   0.9861   0.0127
 -17.000  -0.4783   0.09825   0.09574  -0.1016   0.9853   0.0128
 -16.750  -0.4868   0.09232   0.08972  -0.1060   0.9847   0.0128
 -16.500  -0.4886   0.08747   0.08482  -0.1099   0.9840   0.0128
 -16.250  -0.4899   0.08269   0.08001  -0.1140   0.9835   0.0131
 -16.000  -0.4953   0.07742   0.07466  -0.1184   0.9829   0.0130
 -15.750  -0.5015   0.07304   0.07024  -0.1211   0.9807   0.0131
 -15.500  -0.5129   0.06816   0.06530  -0.1240   0.9775   0.0131
 -15.250  -0.5223   0.06270   0.05977  -0.1287   0.9754   0.0133
 -15.000  -0.5360   0.05653   0.05352  -0.1346   0.9736   0.0132
 -14.750  -0.5652   0.04759   0.04445  -0.1443   0.9716   0.0132
 -14.500  -0.6538   0.03375   0.03024  -0.1552   0.9619   0.0129
 -14.250  -0.6512   0.03002   0.02634  -0.1570   0.9593   0.0130
 -14.000  -0.6347   0.02708   0.02327  -0.1592   0.9577   0.0132
 -13.750  -0.6074   0.02485   0.02091  -0.1620   0.9567   0.0133
 -13.500  -0.5967   0.02367   0.01964  -0.1603   0.9523   0.0136
 -13.250  -0.5806   0.02247   0.01834  -0.1597   0.9488   0.0138
 -13.000  -0.5611   0.02134   0.01711  -0.1594   0.9461   0.0140
 -12.750  -0.5369   0.02036   0.01603  -0.1599   0.9438   0.0144
 -12.500  -0.5095   0.01948   0.01504  -0.1608   0.9416   0.0145
 -12.250  -0.5026   0.01902   0.01450  -0.1571   0.9370   0.0148
 -12.000  -0.4878   0.01838   0.01379  -0.1551   0.9333   0.0149
 -11.750  -0.4749   0.01734   0.01264  -0.1531   0.9299   0.0153
 -11.500  -0.4530   0.01653   0.01175  -0.1526   0.9273   0.0159
 -11.250  -0.4345   0.01604   0.01120  -0.1511   0.9240   0.0162
 -11.000  -0.4234   0.01560   0.01070  -0.1478   0.9193   0.0165
 -10.750  -0.4015   0.01513   0.01017  -0.1468   0.9155   0.0169
 -10.500  -0.3762   0.01463   0.00959  -0.1465   0.9121   0.0173
 -10.250  -0.3504   0.01426   0.00915  -0.1462   0.9084   0.0179
 -10.000  -0.3404   0.01375   0.00858  -0.1426   0.9035   0.0186
  -9.750  -0.3197   0.01328   0.00806  -0.1412   0.8991   0.0194
  -9.500  -0.2945   0.01289   0.00762  -0.1407   0.8959   0.0203
  -9.250  -0.2665   0.01257   0.00724  -0.1408   0.8923   0.0212
  -9.000  -0.2531   0.01218   0.00682  -0.1377   0.8874   0.0223
  -8.750  -0.2317   0.01181   0.00642  -0.1363   0.8827   0.0239
  -8.500  -0.2047   0.01147   0.00601  -0.1361   0.8784   0.0257
  -8.250  -0.1832   0.01112   0.00565  -0.1347   0.8735   0.0286
  -8.000  -0.1648   0.01077   0.00531  -0.1327   0.8675   0.0334
  -7.750  -0.1393   0.01039   0.00495  -0.1321   0.8622   0.0419
  -7.500  -0.1172   0.01014   0.00473  -0.1308   0.8562   0.0506
  -7.250  -0.0967   0.00994   0.00455  -0.1291   0.8485   0.0566
  -7.000  -0.0727   0.00982   0.00438  -0.1281   0.8406   0.0610
  -6.750  -0.0525   0.00962   0.00418  -0.1264   0.8304   0.0655
  -6.500  -0.0314   0.00952   0.00403  -0.1248   0.8201   0.0686
  -6.250  -0.0104   0.00939   0.00385  -0.1231   0.8078   0.0715
  -6.000   0.0086   0.00924   0.00364  -0.1211   0.7921   0.0755
  -5.750   0.0260   0.00917   0.00349  -0.1186   0.7736   0.0782
  -5.500   0.0418   0.00916   0.00336  -0.1159   0.7543   0.0809
  -5.250   0.0572   0.00907   0.00321  -0.1131   0.7372   0.0858
  -5.000   0.0739   0.00901   0.00309  -0.1105   0.7239   0.0903
  -4.750   0.0896   0.00891   0.00298  -0.1079   0.7115   0.1013
  -4.500   0.1055   0.00880   0.00295  -0.1052   0.7005   0.1265
  -4.250   0.1198   0.00879   0.00293  -0.1022   0.6896   0.1372
  -4.000   0.1352   0.00886   0.00292  -0.0993   0.6788   0.1433
  -3.750   0.1521   0.00881   0.00287  -0.0968   0.6687   0.1499
  -3.500   0.1679   0.00884   0.00285  -0.0941   0.6587   0.1544
  -3.250   0.1863   0.00886   0.00282  -0.0919   0.6484   0.1571
  -3.000   0.2033   0.00892   0.00282  -0.0895   0.6383   0.1590
  -2.750   0.2180   0.00891   0.00276  -0.0865   0.6268   0.1624
  -2.500   0.2346   0.00892   0.00274  -0.0840   0.6145   0.1657
  -2.250   0.2506   0.00897   0.00275  -0.0814   0.6015   0.1690
  -2.000   0.2652   0.00906   0.00276  -0.0785   0.5856   0.1713
  -1.750   0.2793   0.00916   0.00278  -0.0755   0.5677   0.1731
  -1.500   0.2934   0.00929   0.00281  -0.0725   0.5470   0.1745
  -1.250   0.3057   0.00948   0.00286  -0.0692   0.5225   0.1755
  -1.000   0.3173   0.00963   0.00291  -0.0658   0.4962   0.1794
  -0.750   0.3298   0.00982   0.00300  -0.0627   0.4727   0.1824
  -0.500   0.3452   0.00998   0.00307  -0.0601   0.4553   0.1851
  -0.250   0.3623   0.01011   0.00314  -0.0579   0.4417   0.1882
   0.000   0.3798   0.01023   0.00321  -0.0558   0.4310   0.1911
   0.250   0.3968   0.01036   0.00328  -0.0535   0.4210   0.1954
   0.500   0.4161   0.01042   0.00336  -0.0518   0.4142   0.2022
   0.750   0.4352   0.01051   0.00343  -0.0501   0.4076   0.2107
   1.000   0.4530   0.01063   0.00355  -0.0481   0.4011   0.2229
   1.250   0.4734   0.01068   0.00365  -0.0466   0.3964   0.2383
   1.500   0.4930   0.01078   0.00375  -0.0449   0.3913   0.2495
   1.750   0.5115   0.01095   0.00389  -0.0432   0.3855   0.2584
   2.000   0.5326   0.01103   0.00399  -0.0419   0.3814   0.2666
   2.250   0.5540   0.01113   0.00409  -0.0406   0.3773   0.2746
   2.500   0.5736   0.01127   0.00421  -0.0391   0.3728   0.2802
   2.750   0.5919   0.01144   0.00437  -0.0373   0.3683   0.2861
   3.000   0.6128   0.01156   0.00449  -0.0361   0.3651   0.2912
   3.250   0.6347   0.01167   0.00460  -0.0350   0.3618   0.2948
   3.500   0.6550   0.01178   0.00472  -0.0336   0.3584   0.3001
   3.750   0.6743   0.01194   0.00488  -0.0321   0.3548   0.3049
   4.000   0.6919   0.01217   0.00508  -0.0303   0.3502   0.3093
   4.250   0.7136   0.01229   0.00520  -0.0293   0.3477   0.3128
   4.500   0.7347   0.01239   0.00534  -0.0282   0.3450   0.3185
   4.750   0.7553   0.01254   0.00550  -0.0270   0.3418   0.3233
   5.000   0.7750   0.01272   0.00567  -0.0257   0.3388   0.3275
   5.250   0.7929   0.01295   0.00589  -0.0241   0.3352   0.3325
   5.500   0.8121   0.01315   0.00611  -0.0227   0.3321   0.3386
   5.750   0.8339   0.01328   0.00627  -0.0218   0.3300   0.3444
   6.000   0.8550   0.01342   0.00644  -0.0209   0.3269   0.3515
   6.250   0.8750   0.01361   0.00665  -0.0197   0.3238   0.3605
   6.500   0.8931   0.01385   0.00691  -0.0183   0.3200   0.3734
   6.750   0.9103   0.01413   0.00722  -0.0167   0.3164   0.3925
   7.000   0.9331   0.01411   0.00745  -0.0163   0.3145   0.4813
   7.250   1.1754   0.01412   0.00872  -0.0638   0.3066   0.9971
   7.500   1.2274   0.01459   0.00914  -0.0698   0.3018   0.9999
   7.750   1.2442   0.01487   0.00943  -0.0682   0.2993   1.0000
   8.000   1.2613   0.01508   0.00967  -0.0665   0.2977   1.0000
   8.250   1.2781   0.01532   0.00993  -0.0649   0.2958   1.0000
   8.500   1.2945   0.01559   0.01021  -0.0632   0.2934   1.0000
   8.750   1.3094   0.01593   0.01054  -0.0613   0.2904   1.0000
   9.000   1.3233   0.01632   0.01092  -0.0593   0.2872   1.0000
   9.250   1.3383   0.01670   0.01130  -0.0575   0.2834   1.0000
   9.500   1.3568   0.01694   0.01157  -0.0563   0.2807   1.0000
   9.750   1.3731   0.01728   0.01193  -0.0547   0.2776   1.0000
  10.000   1.3881   0.01769   0.01233  -0.0531   0.2739   1.0000
  10.250   1.4008   0.01822   0.01284  -0.0511   0.2694   1.0000
  10.500   1.4178   0.01857   0.01324  -0.0498   0.2671   1.0000
  10.750   1.4349   0.01894   0.01362  -0.0485   0.2634   1.0000
  11.000   1.4497   0.01942   0.01410  -0.0470   0.2592   1.0000
  11.250   1.4626   0.02001   0.01469  -0.0453   0.2549   1.0000
  11.500   1.4780   0.02049   0.01520  -0.0439   0.2516   1.0000
  11.750   1.4941   0.02096   0.01570  -0.0427   0.2477   1.0000
  12.000   1.5071   0.02159   0.01632  -0.0411   0.2424   1.0000
  12.250   1.5189   0.02232   0.01706  -0.0395   0.2376   1.0000
  12.500   1.5336   0.02291   0.01766  -0.0382   0.2315   1.0000
  12.750   1.5425   0.02384   0.01857  -0.0364   0.2244   1.0000
  13.000   1.5529   0.02472   0.01942  -0.0347   0.2143   1.0000
  13.250   1.5603   0.02579   0.02047  -0.0329   0.2052   1.0000
  13.500   1.5639   0.02715   0.02178  -0.0307   0.1920   1.0000
  13.750   1.5628   0.02888   0.02342  -0.0282   0.1756   1.0000
  14.000   1.5530   0.03129   0.02572  -0.0251   0.1555   1.0000
  14.250   1.5470   0.03355   0.02792  -0.0227   0.1407   1.0000
  14.500   1.5361   0.03633   0.03063  -0.0201   0.1253   1.0000
  14.750   1.5268   0.03912   0.03338  -0.0179   0.1134   1.0000
  15.000   1.5201   0.04180   0.03604  -0.0162   0.1052   1.0000
  15.250   1.5114   0.04477   0.03900  -0.0146   0.0953   1.0000
  15.500   1.4924   0.04884   0.04302  -0.0128   0.0787   1.0000
  15.750   1.4529   0.05520   0.04930  -0.0108   0.0559   1.0000
  16.000   1.4390   0.05924   0.05339  -0.0100   0.0492   1.0000
  16.250   1.3957   0.06680   0.06097  -0.0092   0.0313   1.0000
  16.500   1.3693   0.07279   0.06701  -0.0091   0.0218   1.0000
  16.750   1.3499   0.07812   0.07242  -0.0093   0.0182   1.0000
  17.000   1.3405   0.08225   0.07663  -0.0095   0.0175   1.0000
  17.250   1.3255   0.08717   0.08164  -0.0100   0.0157   1.0000
  17.500   1.3156   0.09150   0.08606  -0.0105   0.0152   1.0000
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