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FX 79-W-151 A (fx79w151a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 79-W-151 A (fx79w151a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 126.12 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx79w151a-il-1000000-n5.txt
Download as CSV file: xf-fx79w151a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 79-W-151 A                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8167   0.08778   0.08527  -0.0471   1.0000   0.0061
 -16.000  -0.9026   0.07038   0.06765  -0.0576   1.0000   0.0058
 -15.500  -1.0364   0.03786   0.03444  -0.0825   0.9788   0.0055
 -15.250  -1.0194   0.03298   0.02933  -0.0915   0.9603   0.0056
 -15.000  -1.0012   0.02896   0.02505  -0.0988   0.9427   0.0057
 -14.750  -0.9806   0.02692   0.02284  -0.1021   0.9234   0.0059
 -14.500  -0.9692   0.02545   0.02122  -0.1023   0.9037   0.0063
 -14.250  -0.9644   0.02422   0.01981  -0.1006   0.8864   0.0063
 -14.000  -0.9584   0.02328   0.01875  -0.0983   0.8726   0.0064
 -13.750  -0.9549   0.02232   0.01764  -0.0953   0.8603   0.0065
 -13.500  -0.9455   0.02170   0.01693  -0.0929   0.8497   0.0067
 -13.000  -0.9312   0.02033   0.01533  -0.0868   0.8300   0.0068
 -12.750  -0.9195   0.01973   0.01462  -0.0844   0.8219   0.0068
 -12.500  -0.9046   0.01917   0.01397  -0.0826   0.8141   0.0072
 -12.250  -0.8892   0.01862   0.01332  -0.0807   0.8061   0.0074
 -12.000  -0.8723   0.01811   0.01272  -0.0791   0.7982   0.0074
 -11.750  -0.8555   0.01756   0.01207  -0.0775   0.7911   0.0076
 -11.500  -0.8371   0.01706   0.01149  -0.0760   0.7834   0.0078
 -11.250  -0.8190   0.01654   0.01086  -0.0745   0.7762   0.0082
 -11.000  -0.7999   0.01602   0.01027  -0.0732   0.7689   0.0085
 -10.750  -0.7801   0.01557   0.00975  -0.0719   0.7622   0.0089
 -10.500  -0.7589   0.01517   0.00928  -0.0709   0.7553   0.0092
 -10.250  -0.7378   0.01477   0.00881  -0.0698   0.7485   0.0098
 -10.000  -0.7156   0.01442   0.00838  -0.0689   0.7421   0.0103
  -9.750  -0.6936   0.01404   0.00794  -0.0679   0.7353   0.0109
  -9.500  -0.6716   0.01365   0.00750  -0.0670   0.7288   0.0121
  -9.250  -0.6486   0.01332   0.00712  -0.0661   0.7217   0.0131
  -9.000  -0.6257   0.01300   0.00675  -0.0653   0.7154   0.0145
  -8.750  -0.6024   0.01267   0.00639  -0.0645   0.7087   0.0164
  -8.500  -0.5785   0.01242   0.00608  -0.0638   0.7021   0.0177
  -8.250  -0.5547   0.01210   0.00574  -0.0631   0.6961   0.0199
  -8.000  -0.5305   0.01185   0.00545  -0.0625   0.6897   0.0218
  -7.750  -0.5060   0.01162   0.00517  -0.0619   0.6834   0.0236
  -7.500  -0.4816   0.01136   0.00489  -0.0613   0.6764   0.0260
  -7.250  -0.4569   0.01116   0.00464  -0.0607   0.6701   0.0283
  -7.000  -0.4318   0.01094   0.00440  -0.0602   0.6634   0.0308
  -6.750  -0.4072   0.01072   0.00415  -0.0596   0.6566   0.0343
  -6.500  -0.3816   0.01054   0.00394  -0.0592   0.6506   0.0369
  -6.250  -0.3569   0.01032   0.00371  -0.0586   0.6439   0.0424
  -6.000  -0.3317   0.01013   0.00351  -0.0581   0.6381   0.0478
  -5.750  -0.3063   0.00994   0.00333  -0.0577   0.6316   0.0549
  -5.250  -0.2552   0.00963   0.00301  -0.0568   0.6192   0.0688
  -5.000  -0.2295   0.00949   0.00287  -0.0564   0.6128   0.0751
  -4.750  -0.2031   0.00940   0.00274  -0.0561   0.6074   0.0791
  -4.500  -0.1770   0.00928   0.00262  -0.0558   0.6014   0.0847
  -4.000  -0.1241   0.00912   0.00241  -0.0552   0.5905   0.0934
  -3.750  -0.0980   0.00902   0.00231  -0.0549   0.5845   0.0998
  -3.500  -0.0716   0.00896   0.00222  -0.0546   0.5790   0.1049
  -3.250  -0.0448   0.00889   0.00213  -0.0543   0.5738   0.1091
  -3.000  -0.0186   0.00881   0.00205  -0.0540   0.5680   0.1159
  -2.500   0.0345   0.00867   0.00191  -0.0535   0.5577   0.1293
  -2.250   0.0611   0.00863   0.00185  -0.0533   0.5525   0.1351
  -2.000   0.0875   0.00857   0.00179  -0.0530   0.5480   0.1430
  -1.500   0.1403   0.00845   0.00170  -0.0525   0.5372   0.1658
  -1.250   0.1665   0.00839   0.00166  -0.0522   0.5326   0.1797
  -1.000   0.1928   0.00832   0.00163  -0.0519   0.5273   0.1968
  -0.750   0.2183   0.00823   0.00160  -0.0515   0.5220   0.2218
  -0.500   0.2441   0.00816   0.00158  -0.0511   0.5173   0.2456
  -0.250   0.2700   0.00807   0.00157  -0.0508   0.5126   0.2730
   0.000   0.2953   0.00798   0.00156  -0.0503   0.5077   0.3044
   0.250   0.3204   0.00789   0.00156  -0.0499   0.5032   0.3405
   0.500   0.3448   0.00774   0.00156  -0.0493   0.4983   0.3941
   0.750   0.3685   0.00760   0.00157  -0.0485   0.4928   0.4522
   1.000   0.3922   0.00748   0.00159  -0.0478   0.4881   0.5061
   1.250   0.4161   0.00736   0.00162  -0.0470   0.4834   0.5584
   1.500   0.4390   0.00724   0.00165  -0.0461   0.4786   0.6128
   1.750   0.4598   0.00711   0.00170  -0.0446   0.4741   0.6790
   2.000   0.4814   0.00698   0.00174  -0.0433   0.4698   0.7360
   2.250   0.5025   0.00687   0.00180  -0.0419   0.4646   0.7929
   2.500   0.5397   0.00669   0.00194  -0.0440   0.4592   0.8956
   2.750   0.6238   0.00679   0.00211  -0.0566   0.4524   0.9399
   3.000   0.6674   0.00695   0.00224  -0.0602   0.4469   0.9537
   3.250   0.6979   0.00710   0.00237  -0.0608   0.4422   0.9667
   3.500   0.7256   0.00723   0.00250  -0.0608   0.4373   0.9765
   3.750   0.7605   0.00737   0.00261  -0.0625   0.4318   0.9781
   4.000   0.7948   0.00750   0.00272  -0.0641   0.4268   0.9802
   4.250   0.8277   0.00761   0.00283  -0.0654   0.4220   0.9827
   4.500   0.8576   0.00775   0.00296  -0.0660   0.4172   0.9861
   4.750   0.8914   0.00788   0.00308  -0.0676   0.4128   0.9878
   5.000   0.9276   0.00800   0.00320  -0.0696   0.4077   0.9894
   5.250   0.9621   0.00814   0.00333  -0.0713   0.4028   0.9913
   5.500   0.9946   0.00829   0.00347  -0.0726   0.3979   0.9932
   5.750   1.0259   0.00841   0.00362  -0.0736   0.3934   0.9949
   6.000   1.0567   0.00856   0.00376  -0.0745   0.3881   0.9966
   6.250   1.0882   0.00872   0.00392  -0.0756   0.3829   0.9981
   6.500   1.1199   0.00888   0.00408  -0.0768   0.3748   0.9993
   6.750   1.1480   0.00911   0.00427  -0.0773   0.3632   1.0000
   7.000   1.1666   0.00936   0.00447  -0.0757   0.3497   1.0000
   7.250   1.1847   0.00964   0.00470  -0.0741   0.3363   1.0000
   7.500   1.1983   0.01009   0.00503  -0.0717   0.3115   1.0000
   7.750   1.2089   0.01064   0.00542  -0.0687   0.2821   1.0000
   8.000   1.2135   0.01137   0.00594  -0.0648   0.2435   1.0000
   8.250   1.2022   0.01255   0.00680  -0.0580   0.1900   1.0000
   8.500   1.1936   0.01332   0.00743  -0.0516   0.1616   1.0000
   8.750   1.1881   0.01439   0.00832  -0.0466   0.1289   1.0000
   9.000   1.1888   0.01550   0.00929  -0.0430   0.1011   1.0000
   9.250   1.1870   0.01694   0.01056  -0.0395   0.0686   1.0000
   9.500   1.1992   0.01774   0.01136  -0.0379   0.0610   1.0000
   9.750   1.2001   0.01930   0.01279  -0.0354   0.0379   1.0000
  10.000   1.2063   0.02063   0.01407  -0.0336   0.0259   1.0000
  10.250   1.2154   0.02184   0.01526  -0.0322   0.0193   1.0000
  10.500   1.2249   0.02308   0.01651  -0.0309   0.0148   1.0000
  10.750   1.2342   0.02436   0.01780  -0.0298   0.0118   1.0000
  11.000   1.2451   0.02557   0.01905  -0.0288   0.0105   1.0000
  11.250   1.2564   0.02678   0.02030  -0.0280   0.0101   1.0000
  11.500   1.2651   0.02823   0.02177  -0.0271   0.0089   1.0000
  11.750   1.2748   0.02963   0.02322  -0.0263   0.0082   1.0000
  12.000   1.2836   0.03114   0.02477  -0.0255   0.0078   1.0000
  12.250   1.2909   0.03280   0.02647  -0.0248   0.0071   1.0000
  12.500   1.2986   0.03445   0.02816  -0.0241   0.0070   1.0000
  12.750   1.3046   0.03632   0.03008  -0.0234   0.0064   1.0000
  13.000   1.3116   0.03814   0.03196  -0.0229   0.0064   1.0000
  13.250   1.3186   0.04000   0.03388  -0.0224   0.0060   1.0000
  13.500   1.3245   0.04201   0.03595  -0.0220   0.0060   1.0000
  13.750   1.3294   0.04415   0.03815  -0.0216   0.0057   1.0000
  14.000   1.3322   0.04656   0.04060  -0.0212   0.0052   1.0000
  14.250   1.3378   0.04871   0.04281  -0.0210   0.0053   1.0000
  14.500   1.3394   0.05130   0.04546  -0.0207   0.0050   1.0000
  14.750   1.3408   0.05399   0.04820  -0.0206   0.0046   1.0000
  15.000   1.3415   0.05680   0.05109  -0.0205   0.0046   1.0000
  15.250   1.3471   0.05909   0.05344  -0.0205   0.0045   1.0000
  15.500   1.3496   0.06171   0.05613  -0.0205   0.0044   1.0000
  15.750   1.3521   0.06440   0.05888  -0.0206   0.0043   1.0000
  16.000   1.3504   0.06766   0.06222  -0.0207   0.0043   1.0000
  16.250   1.3536   0.07033   0.06495  -0.0209   0.0042   1.0000
  16.500   1.3562   0.07310   0.06777  -0.0212   0.0040   1.0000
  16.750   1.3534   0.07657   0.07132  -0.0215   0.0039   1.0000
  17.000   1.3533   0.07975   0.07458  -0.0219   0.0038   1.0000
  17.250   1.3528   0.08301   0.07790  -0.0224   0.0037   1.0000
  17.500   1.3535   0.08616   0.08112  -0.0229   0.0038   1.0000
  17.750   1.3524   0.08953   0.08455  -0.0235   0.0036   1.0000
  18.000   1.3519   0.09287   0.08795  -0.0241   0.0035   1.0000
  18.250   1.3513   0.09624   0.09138  -0.0248   0.0033   1.0000
  18.500   1.3505   0.09968   0.09490  -0.0256   0.0034   1.0000
  18.750   1.3464   0.10366   0.09896  -0.0265   0.0034   1.0000
  19.000   1.3420   0.10769   0.10305  -0.0275   0.0033   1.0000
  19.250   1.3381   0.11164   0.10707  -0.0286   0.0030   1.0000
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