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FX 79-W-151 A (fx79w151a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 79-W-151 A (fx79w151a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.22 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx79w151a-il-1000000.txt
Download as CSV file: xf-fx79w151a-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.8007   0.08569   0.08331  -0.0482   1.0000   0.0086
 -15.750  -0.8419   0.07545   0.07293  -0.0543   1.0000   0.0084
 -15.500  -0.8882   0.06417   0.06149  -0.0612   1.0000   0.0082
 -15.250  -0.9344   0.05152   0.04864  -0.0701   1.0000   0.0082
 -15.000  -0.9596   0.04190   0.03877  -0.0789   1.0000   0.0080
 -14.750  -0.9760   0.03582   0.03252  -0.0842   1.0000   0.0082
 -14.500  -0.9836   0.03230   0.02889  -0.0860   1.0000   0.0085
 -14.250  -0.9912   0.02948   0.02591  -0.0858   0.9847   0.0084
 -14.000  -0.9644   0.02719   0.02348  -0.0905   0.9719   0.0086
 -13.750  -0.9337   0.02529   0.02143  -0.0949   0.9600   0.0088
 -13.500  -0.9012   0.02410   0.02011  -0.0981   0.9464   0.0093
 -13.250  -0.8849   0.02277   0.01860  -0.0984   0.9280   0.0093
 -13.000  -0.8768   0.02184   0.01752  -0.0961   0.9104   0.0095
 -12.750  -0.8702   0.02108   0.01662  -0.0931   0.8961   0.0095
 -12.500  -0.8593   0.02058   0.01599  -0.0906   0.8846   0.0099
 -12.250  -0.8496   0.02000   0.01530  -0.0878   0.8733   0.0102
 -12.000  -0.8367   0.01940   0.01460  -0.0856   0.8639   0.0102
 -11.500  -0.8159   0.01771   0.01263  -0.0803   0.8457   0.0109
 -11.250  -0.8014   0.01702   0.01182  -0.0783   0.8377   0.0113
 -11.000  -0.7841   0.01644   0.01117  -0.0766   0.8297   0.0118
 -10.750  -0.7654   0.01596   0.01060  -0.0752   0.8226   0.0122
 -10.500  -0.7455   0.01551   0.01007  -0.0739   0.8149   0.0126
 -10.250  -0.7253   0.01508   0.00954  -0.0726   0.8080   0.0133
 -10.000  -0.7045   0.01463   0.00902  -0.0715   0.8007   0.0139
  -9.750  -0.6856   0.01404   0.00834  -0.0700   0.7938   0.0151
  -9.500  -0.6634   0.01365   0.00791  -0.0690   0.7868   0.0166
  -9.250  -0.6405   0.01336   0.00754  -0.0681   0.7798   0.0177
  -9.000  -0.6196   0.01284   0.00700  -0.0670   0.7732   0.0204
  -8.750  -0.5957   0.01260   0.00670  -0.0663   0.7663   0.0224
  -8.500  -0.5734   0.01219   0.00626  -0.0653   0.7599   0.0252
  -8.250  -0.5494   0.01192   0.00596  -0.0646   0.7532   0.0278
  -8.000  -0.5255   0.01167   0.00564  -0.0639   0.7469   0.0300
  -7.750  -0.5018   0.01133   0.00530  -0.0632   0.7402   0.0334
  -7.500  -0.4772   0.01114   0.00504  -0.0626   0.7335   0.0358
  -7.250  -0.4529   0.01085   0.00473  -0.0619   0.7271   0.0397
  -7.000  -0.4285   0.01060   0.00447  -0.0613   0.7202   0.0436
  -6.750  -0.4038   0.01038   0.00422  -0.0607   0.7140   0.0486
  -6.500  -0.3788   0.01016   0.00400  -0.0601   0.7072   0.0542
  -6.250  -0.3541   0.00996   0.00379  -0.0595   0.7008   0.0615
  -6.000  -0.3282   0.00980   0.00362  -0.0592   0.6943   0.0674
  -5.750  -0.3032   0.00962   0.00346  -0.0586   0.6876   0.0764
  -5.500  -0.2769   0.00950   0.00331  -0.0583   0.6814   0.0824
  -5.250  -0.2512   0.00937   0.00318  -0.0579   0.6743   0.0893
  -5.000  -0.2245   0.00931   0.00307  -0.0576   0.6680   0.0928
  -4.750  -0.1989   0.00914   0.00290  -0.0572   0.6614   0.0994
  -4.500  -0.1728   0.00907   0.00279  -0.0568   0.6551   0.1044
  -4.250  -0.1460   0.00898   0.00268  -0.0566   0.6489   0.1084
  -4.000  -0.1203   0.00887   0.00255  -0.0561   0.6425   0.1149
  -3.750  -0.0937   0.00879   0.00245  -0.0559   0.6364   0.1200
  -3.500  -0.0675   0.00869   0.00234  -0.0555   0.6301   0.1264
  -3.250  -0.0414   0.00861   0.00224  -0.0552   0.6244   0.1332
  -3.000  -0.0148   0.00852   0.00215  -0.0549   0.6185   0.1408
  -2.750   0.0111   0.00845   0.00207  -0.0545   0.6124   0.1503
  -2.500   0.0373   0.00834   0.00199  -0.0542   0.6071   0.1628
  -2.250   0.0634   0.00823   0.00191  -0.0539   0.6015   0.1771
  -2.000   0.0889   0.00815   0.00185  -0.0535   0.5961   0.1965
  -1.750   0.1147   0.00800   0.00179  -0.0531   0.5907   0.2230
  -1.500   0.1399   0.00785   0.00174  -0.0526   0.5852   0.2585
  -1.250   0.1643   0.00772   0.00170  -0.0520   0.5799   0.2987
  -1.000   0.1891   0.00752   0.00166  -0.0515   0.5748   0.3490
  -0.750   0.2122   0.00728   0.00162  -0.0506   0.5695   0.4197
  -0.500   0.2347   0.00708   0.00161  -0.0496   0.5644   0.4910
  -0.250   0.2577   0.00685   0.00160  -0.0486   0.5597   0.5599
   0.000   0.2793   0.00666   0.00160  -0.0473   0.5547   0.6288
   0.250   0.2992   0.00649   0.00162  -0.0457   0.5498   0.6991
   0.500   0.3194   0.00628   0.00165  -0.0439   0.5453   0.7690
   0.750   0.3421   0.00612   0.00169  -0.0427   0.5400   0.8371
   1.000   0.3817   0.00607   0.00178  -0.0453   0.5345   0.8965
   1.250   0.4385   0.00611   0.00186  -0.0517   0.5289   0.9272
   1.500   0.4901   0.00622   0.00194  -0.0570   0.5231   0.9412
   1.750   0.5273   0.00635   0.00204  -0.0591   0.5179   0.9522
   2.000   0.5586   0.00647   0.00215  -0.0598   0.5125   0.9627
   2.250   0.5970   0.00666   0.00228  -0.0621   0.5066   0.9697
   2.500   0.6301   0.00681   0.00242  -0.0632   0.5015   0.9771
   2.750   0.6731   0.00694   0.00253  -0.0666   0.4958   0.9795
   3.000   0.7142   0.00712   0.00265  -0.0696   0.4900   0.9834
   3.250   0.7530   0.00725   0.00278  -0.0720   0.4844   0.9875
   3.500   0.7938   0.00735   0.00286  -0.0750   0.4784   0.9893
   3.750   0.8300   0.00746   0.00293  -0.0770   0.4729   0.9912
   4.000   0.8662   0.00754   0.00301  -0.0790   0.4675   0.9935
   4.250   0.9010   0.00766   0.00311  -0.0808   0.4618   0.9957
   4.500   0.9375   0.00773   0.00317  -0.0829   0.4566   0.9975
   4.750   0.9741   0.00779   0.00324  -0.0850   0.4509   0.9993
   5.000   1.0031   0.00792   0.00333  -0.0856   0.4452   1.0000
   5.250   1.0260   0.00799   0.00342  -0.0848   0.4406   1.0000
   5.500   1.0484   0.00809   0.00353  -0.0839   0.4354   1.0000
   5.750   1.0697   0.00824   0.00366  -0.0828   0.4302   1.0000
   6.000   1.0925   0.00832   0.00377  -0.0820   0.4253   1.0000
   6.250   1.1145   0.00845   0.00390  -0.0810   0.4197   1.0000
   6.500   1.1354   0.00861   0.00406  -0.0798   0.4129   1.0000
   6.750   1.1569   0.00875   0.00419  -0.0788   0.4042   1.0000
   7.000   1.1775   0.00892   0.00435  -0.0776   0.3946   1.0000
   7.250   1.1966   0.00916   0.00454  -0.0761   0.3843   1.0000
   7.500   1.2151   0.00941   0.00475  -0.0745   0.3694   1.0000
   7.750   1.2333   0.00967   0.00497  -0.0729   0.3557   1.0000
   8.000   1.2502   0.00997   0.00522  -0.0710   0.3410   1.0000
   8.250   1.2659   0.01030   0.00550  -0.0690   0.3256   1.0000
   8.500   1.2811   0.01064   0.00579  -0.0668   0.3111   1.0000
   8.750   1.2940   0.01104   0.00614  -0.0643   0.2937   1.0000
   9.000   1.3000   0.01165   0.00661  -0.0606   0.2668   1.0000
   9.250   1.2902   0.01252   0.00727  -0.0540   0.2279   1.0000
   9.500   1.2858   0.01351   0.00809  -0.0489   0.1963   1.0000
   9.750   1.2741   0.01518   0.00948  -0.0436   0.1491   1.0000
  10.000   1.2683   0.01686   0.01095  -0.0398   0.1122   1.0000
  10.250   1.2647   0.01863   0.01255  -0.0366   0.0806   1.0000
  10.500   1.2587   0.02073   0.01448  -0.0337   0.0507   1.0000
  10.750   1.2550   0.02285   0.01648  -0.0313   0.0291   1.0000
  11.000   1.2546   0.02486   0.01845  -0.0294   0.0178   1.0000
  11.250   1.2632   0.02627   0.01988  -0.0284   0.0156   1.0000
  11.500   1.2701   0.02785   0.02150  -0.0273   0.0136   1.0000
  11.750   1.2747   0.02967   0.02336  -0.0261   0.0119   1.0000
  12.000   1.2834   0.03119   0.02493  -0.0254   0.0114   1.0000
  12.250   1.2904   0.03289   0.02668  -0.0246   0.0105   1.0000
  12.500   1.2959   0.03475   0.02860  -0.0238   0.0102   1.0000
  12.750   1.2929   0.03748   0.03140  -0.0228   0.0090   1.0000
  13.000   1.3000   0.03933   0.03331  -0.0223   0.0092   1.0000
  13.250   1.3030   0.04162   0.03568  -0.0217   0.0086   1.0000
  13.500   1.3092   0.04364   0.03775  -0.0213   0.0086   1.0000
  13.750   1.3122   0.04602   0.04021  -0.0210   0.0081   1.0000
  14.000   1.3129   0.04871   0.04296  -0.0206   0.0076   1.0000
  14.250   1.3165   0.05111   0.04542  -0.0204   0.0076   1.0000
  14.500   1.3164   0.05396   0.04834  -0.0202   0.0074   1.0000
  14.750   1.3108   0.05751   0.05195  -0.0200   0.0068   1.0000
  15.000   1.3099   0.06058   0.05510  -0.0200   0.0068   1.0000
  15.250   1.3074   0.06388   0.05848  -0.0201   0.0065   1.0000
  15.500   1.3044   0.06731   0.06200  -0.0202   0.0065   1.0000
  15.750   1.3063   0.07018   0.06494  -0.0204   0.0064   1.0000
  16.000   1.3000   0.07410   0.06895  -0.0207   0.0064   1.0000
  16.250   1.3028   0.07690   0.07181  -0.0210   0.0064   1.0000
  16.500   1.3065   0.07964   0.07461  -0.0214   0.0060   1.0000
  16.750   1.3004   0.08369   0.07875  -0.0219   0.0060   1.0000
  17.000   1.3011   0.08687   0.08199  -0.0224   0.0058   1.0000
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