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GOE 460 AIRFOIL (goe460-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 460 AIRFOIL (goe460-il)
Reynolds number: 100,000
Max Cl/Cd: 34.06 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe460-il-100000-n5.txt
Download as CSV file: xf-goe460-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 460 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.7995   0.12857   0.12171  -0.0450   1.0000   0.0862
 -19.250  -0.7700   0.13080   0.12402  -0.0435   1.0000   0.0874
 -19.000  -0.7829   0.12507   0.11824  -0.0461   1.0000   0.0900
 -18.750  -0.8630   0.10773   0.10052  -0.0545   1.0000   0.0938
 -18.500  -0.8844   0.10114   0.09378  -0.0572   1.0000   0.0962
 -18.250  -0.8780   0.09922   0.09190  -0.0575   1.0000   0.0986
 -18.000  -0.8880   0.09468   0.08727  -0.0591   1.0000   0.1014
 -17.750  -0.9077   0.08871   0.08111  -0.0613   1.0000   0.1044
 -17.500  -0.9150   0.08480   0.07711  -0.0624   1.0000   0.1071
 -17.250  -0.9131   0.08238   0.07472  -0.0627   1.0000   0.1102
 -17.000  -0.9203   0.07863   0.07090  -0.0636   1.0000   0.1135
 -16.750  -0.9330   0.07417   0.06625  -0.0647   1.0000   0.1169
 -16.500  -0.9316   0.07184   0.06398  -0.0648   1.0000   0.1202
 -16.250  -0.9354   0.06885   0.06097  -0.0651   1.0000   0.1237
 -16.000  -0.9426   0.06545   0.05745  -0.0655   1.0000   0.1276
 -15.750  -0.9459   0.06265   0.05462  -0.0655   1.0000   0.1313
 -15.500  -0.9483   0.06013   0.05211  -0.0653   1.0000   0.1349
 -15.250  -0.9530   0.05734   0.04925  -0.0652   1.0000   0.1390
 -15.000  -0.9562   0.05480   0.04663  -0.0648   1.0000   0.1429
 -14.750  -0.9582   0.05261   0.04446  -0.0642   1.0000   0.1467
 -14.500  -0.9608   0.05036   0.04215  -0.0635   1.0000   0.1510
 -14.250  -0.9630   0.04822   0.03992  -0.0626   1.0000   0.1556
 -14.000  -0.9646   0.04638   0.03808  -0.0614   1.0000   0.1598
 -13.750  -0.9660   0.04455   0.03618  -0.0601   1.0000   0.1647
 -13.500  -0.9666   0.04289   0.03443  -0.0586   1.0000   0.1696
 -13.250  -0.9670   0.04142   0.03296  -0.0569   1.0000   0.1741
 -13.000  -0.9673   0.03998   0.03143  -0.0550   1.0000   0.1793
 -12.750  -0.9673   0.03866   0.03004  -0.0529   1.0000   0.1844
 -12.500  -0.9667   0.03752   0.02890  -0.0506   1.0000   0.1892
 -12.250  -0.9672   0.03638   0.02767  -0.0481   1.0000   0.1947
 -12.000  -0.9678   0.03533   0.02654  -0.0453   1.0000   0.2001
 -11.750  -0.9676   0.03444   0.02569  -0.0424   1.0000   0.2052
 -11.500  -0.9699   0.03355   0.02474  -0.0390   1.0000   0.2110
 -11.250  -0.9726   0.03273   0.02384  -0.0354   1.0000   0.2167
 -11.000  -0.9737   0.03205   0.02323  -0.0318   1.0000   0.2220
 -10.750  -0.9778   0.03140   0.02254  -0.0277   1.0000   0.2278
 -10.250  -0.9847   0.03028   0.02140  -0.0192   1.0000   0.2384
 -10.000  -0.9892   0.02981   0.02093  -0.0146   1.0000   0.2434
  -9.750  -0.9940   0.02938   0.02043  -0.0099   1.0000   0.2484
  -9.500  -0.9816   0.02885   0.01990  -0.0082   0.9976   0.2544
  -9.250  -0.9526   0.02829   0.01933  -0.0096   0.9921   0.2617
  -9.000  -0.9269   0.02774   0.01866  -0.0103   0.9859   0.2690
  -8.750  -0.8981   0.02723   0.01821  -0.0115   0.9807   0.2757
  -8.500  -0.8737   0.02675   0.01769  -0.0117   0.9743   0.2832
  -8.250  -0.8471   0.02628   0.01722  -0.0124   0.9682   0.2907
  -8.000  -0.8204   0.02585   0.01679  -0.0130   0.9626   0.2987
  -7.750  -0.7977   0.02543   0.01633  -0.0126   0.9550   0.3065
  -7.500  -0.7676   0.02500   0.01594  -0.0138   0.9502   0.3150
  -7.250  -0.7499   0.02464   0.01556  -0.0124   0.9413   0.3239
  -7.000  -0.7228   0.02423   0.01518  -0.0128   0.9353   0.3345
  -6.750  -0.7035   0.02388   0.01486  -0.0116   0.9272   0.3451
  -6.500  -0.6799   0.02349   0.01446  -0.0112   0.9198   0.3585
  -6.250  -0.6471   0.02304   0.01406  -0.0125   0.9155   0.3730
  -6.000  -0.6355   0.02276   0.01383  -0.0096   0.9041   0.3848
  -5.750  -0.6035   0.02233   0.01342  -0.0107   0.8992   0.4002
  -5.500  -0.5888   0.02206   0.01313  -0.0083   0.8888   0.4138
  -5.250  -0.5580   0.02168   0.01281  -0.0090   0.8828   0.4286
  -5.000  -0.5320   0.02137   0.01254  -0.0086   0.8754   0.4423
  -4.750  -0.5091   0.02110   0.01228  -0.0077   0.8664   0.4562
  -4.500  -0.4745   0.02072   0.01188  -0.0089   0.8614   0.4714
  -4.250  -0.4577   0.02057   0.01178  -0.0067   0.8501   0.4825
  -4.000  -0.4243   0.02025   0.01146  -0.0077   0.8440   0.4953
  -3.750  -0.4036   0.02006   0.01125  -0.0062   0.8340   0.5071
  -3.500  -0.3728   0.01982   0.01104  -0.0066   0.8262   0.5183
  -3.250  -0.3433   0.01957   0.01075  -0.0068   0.8189   0.5304
  -3.000  -0.3208   0.01943   0.01064  -0.0056   0.8082   0.5410
  -2.750  -0.2840   0.01914   0.01034  -0.0071   0.8021   0.5530
  -2.500  -0.2693   0.01908   0.01028  -0.0044   0.7894   0.5640
  -2.250  -0.2327   0.01885   0.01007  -0.0059   0.7825   0.5754
  -2.000  -0.2187   0.01878   0.00997  -0.0031   0.7700   0.5868
  -1.750  -0.1808   0.01859   0.00982  -0.0048   0.7626   0.5975
  -1.500  -0.1648   0.01853   0.00977  -0.0024   0.7502   0.6084
  -1.250  -0.1281   0.01837   0.00963  -0.0037   0.7424   0.6200
  -1.000  -0.1094   0.01838   0.00969  -0.0018   0.7301   0.6322
  -0.750  -0.0814   0.01827   0.00958  -0.0015   0.7211   0.6472
  -0.500  -0.0559   0.01831   0.00970  -0.0007   0.7094   0.6603
  -0.250  -0.0264   0.01830   0.00972  -0.0007   0.6985   0.6732
   0.000  -0.0001   0.01825   0.00965   0.0000   0.6869   0.6868
   0.250   0.0265   0.01831   0.00972   0.0006   0.6735   0.6984
   0.500   0.0560   0.01831   0.00969   0.0007   0.6604   0.7093
   0.750   0.0813   0.01827   0.00958   0.0015   0.6473   0.7212
   1.000   0.1095   0.01838   0.00969   0.0018   0.6322   0.7301
   1.250   0.1280   0.01837   0.00963   0.0038   0.6199   0.7424
   1.500   0.1648   0.01853   0.00976   0.0024   0.6084   0.7501
   1.750   0.1808   0.01859   0.00982   0.0047   0.5975   0.7626
   2.000   0.2188   0.01878   0.00997   0.0031   0.5869   0.7700
   2.250   0.2326   0.01884   0.01006   0.0059   0.5754   0.7825
   2.500   0.2693   0.01908   0.01028   0.0045   0.5639   0.7895
   2.750   0.2841   0.01914   0.01035   0.0071   0.5530   0.8021
   3.000   0.3208   0.01943   0.01064   0.0056   0.5409   0.8082
   3.250   0.3434   0.01957   0.01075   0.0068   0.5304   0.8188
   3.500   0.3729   0.01982   0.01104   0.0066   0.5183   0.8262
   3.750   0.4036   0.02006   0.01125   0.0062   0.5071   0.8341
   4.000   0.4244   0.02025   0.01146   0.0076   0.4953   0.8440
   4.250   0.4577   0.02057   0.01178   0.0067   0.4824   0.8501
   4.500   0.4746   0.02072   0.01189   0.0089   0.4714   0.8614
   4.750   0.5091   0.02109   0.01227   0.0077   0.4561   0.8665
   5.000   0.5320   0.02137   0.01253   0.0086   0.4424   0.8753
   5.250   0.5582   0.02168   0.01280   0.0089   0.4287   0.8828
   5.500   0.5887   0.02206   0.01312   0.0083   0.4137   0.8888
   5.750   0.6037   0.02233   0.01341   0.0106   0.4001   0.8992
   6.000   0.6357   0.02276   0.01383   0.0096   0.3847   0.9042
   6.250   0.6475   0.02304   0.01406   0.0125   0.3732   0.9155
   6.500   0.6799   0.02349   0.01445   0.0112   0.3583   0.9198
   6.750   0.7037   0.02387   0.01485   0.0116   0.3451   0.9273
   7.000   0.7231   0.02422   0.01518   0.0127   0.3344   0.9353
   7.250   0.7501   0.02464   0.01555   0.0123   0.3238   0.9413
   7.500   0.7681   0.02499   0.01594   0.0137   0.3151   0.9502
   7.750   0.7982   0.02542   0.01633   0.0126   0.3064   0.9550
   8.000   0.8205   0.02584   0.01678   0.0129   0.2985   0.9627
   8.250   0.8474   0.02628   0.01721   0.0123   0.2905   0.9683
   8.500   0.8741   0.02674   0.01768   0.0117   0.2831   0.9744
   8.750   0.8987   0.02722   0.01820   0.0114   0.2756   0.9808
   9.000   0.9276   0.02773   0.01865   0.0102   0.2689   0.9860
   9.250   0.9535   0.02828   0.01932   0.0095   0.2617   0.9921
   9.500   0.9824   0.02884   0.01988   0.0081   0.2543   0.9977
   9.750   0.9940   0.02936   0.02041   0.0098   0.2484   1.0000
  10.000   0.9891   0.02979   0.02091   0.0146   0.2433   1.0000
  10.250   0.9849   0.03026   0.02138   0.0191   0.2384   1.0000
  10.500   0.9840   0.03077   0.02178   0.0231   0.2333   1.0000
  10.750   0.9780   0.03138   0.02251   0.0277   0.2277   1.0000
  11.000   0.9740   0.03203   0.02321   0.0318   0.2220   1.0000
  11.250   0.9729   0.03271   0.02381   0.0354   0.2166   1.0000
  11.500   0.9703   0.03353   0.02471   0.0390   0.2110   1.0000
  11.750   0.9681   0.03441   0.02566   0.0423   0.2052   1.0000
  12.000   0.9686   0.03529   0.02650   0.0452   0.2002   1.0000
  12.250   0.9684   0.03633   0.02761   0.0480   0.1949   1.0000
  12.500   0.9675   0.03748   0.02886   0.0505   0.1892   1.0000
  12.750   0.9679   0.03863   0.02999   0.0528   0.1844   1.0000
  13.000   0.9684   0.03993   0.03137   0.0549   0.1794   1.0000
  13.250   0.9679   0.04138   0.03291   0.0568   0.1740   1.0000
  13.500   0.9678   0.04283   0.03436   0.0585   0.1696   1.0000
  13.750   0.9673   0.04450   0.03611   0.0600   0.1647   1.0000
  14.000   0.9654   0.04634   0.03804   0.0613   0.1596   1.0000
  14.250   0.9643   0.04815   0.03985   0.0625   0.1555   1.0000
  14.500   0.9621   0.05031   0.04209   0.0634   0.1508   1.0000
  14.750   0.9595   0.05254   0.04439   0.0641   0.1466   1.0000
  15.000   0.9580   0.05470   0.04653   0.0647   0.1429   1.0000
  15.250   0.9542   0.05731   0.04921   0.0650   0.1387   1.0000
  15.500   0.9499   0.06005   0.05203   0.0652   0.1347   1.0000
  15.750   0.9478   0.06255   0.05450   0.0653   0.1311   1.0000
  16.000   0.9440   0.06542   0.05743   0.0653   0.1273   1.0000
  16.250   0.9373   0.06877   0.06088   0.0649   0.1236   1.0000
  16.500   0.9339   0.07171   0.06384   0.0646   0.1201   1.0000
  16.750   0.9354   0.07404   0.06612   0.0645   0.1168   1.0000
  17.000   0.9224   0.07854   0.07080   0.0634   0.1133   1.0000
  17.250   0.9159   0.08221   0.07454   0.0625   0.1100   1.0000
  17.500   0.9185   0.08453   0.07682   0.0622   0.1070   1.0000
  17.750   0.9088   0.08882   0.08123   0.0610   0.1041   1.0000
  18.000   0.8907   0.09456   0.08715   0.0589   0.1012   1.0000
  18.250   0.8811   0.09905   0.09172   0.0573   0.0984   1.0000
  18.500   0.8888   0.10076   0.09338   0.0571   0.0960   1.0000
  18.750   0.8642   0.10791   0.10071   0.0541   0.0937   1.0000
  19.000   0.7898   0.12424   0.11739   0.0462   0.0899   1.0000
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