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GOE 546 AIRFOIL (goe546-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 546 AIRFOIL (goe546-il)
Reynolds number: 500,000
Max Cl/Cd: 93.53 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe546-il-500000-n5.txt
Download as CSV file: xf-goe546-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.8554   0.03791   0.03512  -0.0807   1.0000   0.0108
 -12.000  -0.8643   0.03302   0.02987  -0.0826   0.9981   0.0110
 -11.750  -0.8465   0.02923   0.02568  -0.0863   0.9938   0.0114
 -11.500  -0.8260   0.02672   0.02290  -0.0883   0.9894   0.0118
 -11.250  -0.7989   0.02545   0.02152  -0.0900   0.9865   0.0123
 -11.000  -0.7733   0.02437   0.02032  -0.0909   0.9825   0.0127
 -10.750  -0.7470   0.02326   0.01905  -0.0919   0.9783   0.0133
 -10.500  -0.7189   0.02196   0.01755  -0.0933   0.9754   0.0139
 -10.250  -0.6959   0.02069   0.01606  -0.0935   0.9685   0.0146
  -9.750  -0.6398   0.01919   0.01437  -0.0950   0.9587   0.0158
  -9.500  -0.6086   0.01880   0.01391  -0.0961   0.9544   0.0166
  -9.250  -0.5755   0.01822   0.01321  -0.0977   0.9513   0.0176
  -9.000  -0.5459   0.01740   0.01219  -0.0986   0.9457   0.0186
  -8.750  -0.5140   0.01674   0.01144  -0.0999   0.9412   0.0194
  -8.500  -0.4794   0.01639   0.01103  -0.1017   0.9373   0.0202
  -8.250  -0.4472   0.01608   0.01066  -0.1028   0.9314   0.0212
  -8.000  -0.4144   0.01559   0.01005  -0.1041   0.9256   0.0224
  -7.750  -0.3827   0.01509   0.00938  -0.1052   0.9201   0.0233
  -7.500  -0.3546   0.01444   0.00861  -0.1056   0.9136   0.0242
  -7.250  -0.3248   0.01410   0.00823  -0.1062   0.9081   0.0252
  -7.000  -0.2971   0.01382   0.00789  -0.1064   0.9026   0.0261
  -6.750  -0.2698   0.01347   0.00746  -0.1064   0.8969   0.0271
  -6.500  -0.2418   0.01312   0.00701  -0.1065   0.8917   0.0281
  -6.250  -0.2157   0.01282   0.00661  -0.1062   0.8860   0.0290
  -6.000  -0.1889   0.01252   0.00622  -0.1060   0.8804   0.0295
  -5.500  -0.1378   0.01155   0.00517  -0.1053   0.8703   0.0317
  -5.250  -0.1114   0.01127   0.00484  -0.1051   0.8648   0.0326
  -5.000  -0.0846   0.01099   0.00449  -0.1049   0.8599   0.0335
  -4.750  -0.0587   0.01071   0.00418  -0.1045   0.8543   0.0344
  -4.500  -0.0321   0.01048   0.00390  -0.1042   0.8489   0.0355
  -4.250  -0.0053   0.01027   0.00363  -0.1039   0.8437   0.0364
  -4.000   0.0209   0.01006   0.00337  -0.1035   0.8374   0.0369
  -3.750   0.0472   0.00977   0.00302  -0.1032   0.8311   0.0383
  -3.500   0.0733   0.00954   0.00277  -0.1027   0.8230   0.0399
  -3.250   0.0998   0.00938   0.00256  -0.1024   0.8142   0.0416
  -3.000   0.1261   0.00923   0.00238  -0.1020   0.8049   0.0437
  -2.750   0.1529   0.00911   0.00221  -0.1016   0.7973   0.0460
  -2.500   0.1794   0.00894   0.00205  -0.1013   0.7886   0.0511
  -2.250   0.2061   0.00883   0.00192  -0.1009   0.7801   0.0569
  -2.000   0.2326   0.00870   0.00180  -0.1006   0.7706   0.0683
  -1.750   0.2589   0.00855   0.00168  -0.1002   0.7606   0.0884
  -1.500   0.2846   0.00831   0.00158  -0.0998   0.7498   0.1391
  -1.250   0.3095   0.00797   0.00149  -0.0993   0.7379   0.2346
  -1.000   0.3349   0.00775   0.00145  -0.0989   0.7254   0.3046
  -0.750   0.3603   0.00761   0.00143  -0.0984   0.7120   0.3618
  -0.500   0.3852   0.00746   0.00145  -0.0978   0.6977   0.4322
  -0.250   0.4097   0.00735   0.00148  -0.0971   0.6829   0.5032
   0.000   0.4341   0.00726   0.00151  -0.0963   0.6684   0.5603
   0.250   0.4585   0.00722   0.00154  -0.0955   0.6537   0.6062
   0.500   0.4832   0.00720   0.00158  -0.0948   0.6406   0.6465
   0.750   0.5077   0.00717   0.00163  -0.0940   0.6296   0.6887
   1.000   0.5310   0.00705   0.00170  -0.0929   0.6191   0.7567
   1.250   0.5529   0.00688   0.00179  -0.0912   0.6091   0.8647
   1.500   0.6002   0.00690   0.00186  -0.0954   0.5932   0.9560
   1.750   0.6395   0.00708   0.00193  -0.0980   0.5693   1.0000
   2.000   0.6631   0.00723   0.00199  -0.0970   0.5507   1.0000
   2.250   0.6865   0.00739   0.00206  -0.0960   0.5286   1.0000
   2.500   0.7091   0.00761   0.00215  -0.0949   0.5020   1.0000
   3.000   0.7548   0.00807   0.00238  -0.0929   0.4528   1.0000
   3.250   0.7772   0.00834   0.00253  -0.0918   0.4277   1.0000
   3.500   0.8002   0.00861   0.00269  -0.0908   0.4043   1.0000
   3.750   0.8215   0.00897   0.00290  -0.0896   0.3700   1.0000
   4.000   0.8417   0.00943   0.00313  -0.0882   0.3240   1.0000
   4.250   0.8606   0.01001   0.00343  -0.0867   0.2700   1.0000
   4.500   0.8810   0.01049   0.00373  -0.0854   0.2351   1.0000
   4.750   0.9025   0.01090   0.00403  -0.0842   0.2094   1.0000
   5.000   0.9234   0.01134   0.00433  -0.0831   0.1796   1.0000
   5.250   0.9397   0.01212   0.00478  -0.0812   0.1186   1.0000
   5.500   0.9577   0.01278   0.00525  -0.0795   0.0827   1.0000
   5.750   0.9766   0.01336   0.00567  -0.0780   0.0532   1.0000
   6.000   0.9969   0.01382   0.00605  -0.0767   0.0426   1.0000
   6.250   1.0184   0.01418   0.00641  -0.0756   0.0397   1.0000
   6.500   1.0396   0.01455   0.00679  -0.0745   0.0375   1.0000
   6.750   1.0605   0.01493   0.00719  -0.0733   0.0359   1.0000
   7.000   1.0815   0.01528   0.00758  -0.0721   0.0354   1.0000
   7.250   1.1019   0.01565   0.00800  -0.0709   0.0348   1.0000
   7.500   1.1216   0.01605   0.00845  -0.0695   0.0339   1.0000
   7.750   1.1399   0.01646   0.00890  -0.0679   0.0332   1.0000
   8.000   1.1570   0.01690   0.00939  -0.0661   0.0325   1.0000
   8.250   1.1732   0.01738   0.00991  -0.0641   0.0318   1.0000
   8.500   1.1886   0.01791   0.01048  -0.0621   0.0309   1.0000
   8.750   1.2029   0.01850   0.01112  -0.0600   0.0300   1.0000
   9.000   1.2152   0.01922   0.01188  -0.0576   0.0290   1.0000
   9.250   1.2246   0.02010   0.01282  -0.0548   0.0280   1.0000
   9.500   1.2413   0.02058   0.01336  -0.0533   0.0276   1.0000
   9.750   1.2562   0.02117   0.01401  -0.0515   0.0270   1.0000
  10.000   1.2708   0.02178   0.01470  -0.0498   0.0263   1.0000
  10.250   1.2849   0.02244   0.01542  -0.0481   0.0255   1.0000
  10.500   1.2975   0.02321   0.01625  -0.0462   0.0248   1.0000
  10.750   1.3105   0.02397   0.01706  -0.0445   0.0239   1.0000
  11.000   1.3231   0.02478   0.01791  -0.0429   0.0231   1.0000
  11.250   1.3329   0.02580   0.01898  -0.0410   0.0225   1.0000
  11.500   1.3395   0.02709   0.02034  -0.0390   0.0216   1.0000
  11.750   1.3537   0.02786   0.02120  -0.0377   0.0211   1.0000
  12.000   1.3659   0.02880   0.02223  -0.0364   0.0204   1.0000
  12.250   1.3784   0.02973   0.02323  -0.0351   0.0194   1.0000
  12.500   1.3895   0.03080   0.02437  -0.0339   0.0187   1.0000
  12.750   1.4016   0.03181   0.02543  -0.0328   0.0179   1.0000
  13.000   1.4117   0.03300   0.02667  -0.0316   0.0172   1.0000
  13.250   1.4202   0.03437   0.02811  -0.0305   0.0165   1.0000
  13.500   1.4279   0.03586   0.02971  -0.0293   0.0158   1.0000
  13.750   1.4364   0.03732   0.03124  -0.0284   0.0150   1.0000
  14.000   1.4454   0.03876   0.03274  -0.0276   0.0142   1.0000
  14.250   1.4519   0.04048   0.03452  -0.0268   0.0137   1.0000
  14.500   1.4569   0.04241   0.03651  -0.0260   0.0131   1.0000
  14.750   1.4600   0.04462   0.03883  -0.0254   0.0127   1.0000
  15.000   1.4624   0.04697   0.04131  -0.0249   0.0122   1.0000
  15.250   1.4644   0.04945   0.04389  -0.0246   0.0118   1.0000
  15.500   1.4672   0.05194   0.04647  -0.0244   0.0112   1.0000
  15.750   1.4679   0.05476   0.04938  -0.0245   0.0109   1.0000
  16.000   1.4670   0.05785   0.05256  -0.0247   0.0105   1.0000
  16.250   1.4645   0.06127   0.05608  -0.0251   0.0101   1.0000
  16.500   1.4618   0.06481   0.05974  -0.0257   0.0098   1.0000
  16.750   1.4580   0.06861   0.06366  -0.0265   0.0096   1.0000
  17.000   1.4532   0.07265   0.06784  -0.0275   0.0094   1.0000
  17.250   1.4475   0.07698   0.07230  -0.0287   0.0091   1.0000
  17.500   1.4411   0.08154   0.07699  -0.0302   0.0089   1.0000
  17.750   1.4336   0.08641   0.08199  -0.0320   0.0088   1.0000
  18.000   1.4250   0.09159   0.08730  -0.0341   0.0085   1.0000
  18.250   1.4156   0.09706   0.09290  -0.0364   0.0085   1.0000
  18.500   1.4051   0.10286   0.09882  -0.0390   0.0083   1.0000
  18.750   1.3935   0.10898   0.10507  -0.0420   0.0082   1.0000
  19.000   1.3811   0.11539   0.11162  -0.0452   0.0081   1.0000
  19.250   1.3681   0.12209   0.11845  -0.0487   0.0080   1.0000
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