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WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.73 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx79k144-il-1000000-n5.txt
Download as CSV file: xf-fx79k144-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 79-K-144/17 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0203   0.05612   0.05275  -0.0621   0.7714   0.0046
 -15.500  -1.0465   0.04832   0.04474  -0.0674   0.7711   0.0045
 -15.250  -1.0621   0.04345   0.03970  -0.0694   0.7707   0.0046
 -15.000  -1.0718   0.03988   0.03597  -0.0699   0.7703   0.0046
 -14.750  -1.0772   0.03705   0.03300  -0.0695   0.7699   0.0046
 -14.500  -1.0793   0.03468   0.03048  -0.0687   0.7695   0.0046
 -14.250  -1.0785   0.03265   0.02831  -0.0676   0.7691   0.0047
 -14.000  -1.0749   0.03088   0.02641  -0.0664   0.7687   0.0047
 -13.750  -1.0690   0.02930   0.02470  -0.0652   0.7683   0.0048
 -13.500  -1.0607   0.02789   0.02317  -0.0640   0.7680   0.0049
 -13.250  -1.0509   0.02661   0.02176  -0.0628   0.7676   0.0049
 -13.000  -1.0415   0.02553   0.02057  -0.0611   0.7672   0.0050
 -12.750  -1.0275   0.02449   0.01941  -0.0600   0.7667   0.0050
 -12.500  -1.0112   0.02351   0.01832  -0.0592   0.7662   0.0051
 -12.250  -0.9934   0.02260   0.01729  -0.0585   0.7657   0.0052
 -12.000  -0.9744   0.02176   0.01633  -0.0578   0.7651   0.0052
 -11.750  -0.9543   0.02098   0.01545  -0.0573   0.7646   0.0053
 -11.500  -0.9333   0.02025   0.01462  -0.0569   0.7641   0.0054
 -11.250  -0.9115   0.01954   0.01383  -0.0565   0.7637   0.0055
 -11.000  -0.8890   0.01889   0.01309  -0.0562   0.7633   0.0056
 -10.750  -0.8659   0.01827   0.01240  -0.0559   0.7629   0.0057
 -10.500  -0.8422   0.01770   0.01174  -0.0557   0.7624   0.0058
 -10.250  -0.8181   0.01717   0.01114  -0.0556   0.7619   0.0059
 -10.000  -0.7935   0.01667   0.01057  -0.0555   0.7614   0.0060
  -9.750  -0.7687   0.01617   0.01001  -0.0554   0.7608   0.0061
  -9.500  -0.7437   0.01567   0.00946  -0.0553   0.7602   0.0064
  -9.250  -0.7183   0.01522   0.00896  -0.0553   0.7597   0.0066
  -9.000  -0.6926   0.01479   0.00849  -0.0553   0.7592   0.0070
  -8.750  -0.6667   0.01439   0.00804  -0.0554   0.7587   0.0073
  -8.500  -0.6406   0.01400   0.00763  -0.0554   0.7582   0.0078
  -8.250  -0.6142   0.01365   0.00728  -0.0555   0.7577   0.0087
  -8.000  -0.5874   0.01337   0.00703  -0.0557   0.7572   0.0108
  -7.750  -0.5600   0.01315   0.00680  -0.0560   0.7566   0.0131
  -7.500  -0.5325   0.01294   0.00655  -0.0562   0.7560   0.0140
  -7.250  -0.5052   0.01269   0.00629  -0.0564   0.7553   0.0148
  -7.000  -0.4776   0.01247   0.00606  -0.0567   0.7548   0.0156
  -6.750  -0.4499   0.01226   0.00583  -0.0569   0.7542   0.0164
  -6.500  -0.4221   0.01205   0.00560  -0.0572   0.7534   0.0171
  -6.250  -0.3941   0.01186   0.00539  -0.0575   0.7526   0.0177
  -6.000  -0.3660   0.01169   0.00518  -0.0578   0.7519   0.0181
  -5.750  -0.3385   0.01139   0.00485  -0.0580   0.7512   0.0189
  -5.500  -0.3107   0.01114   0.00460  -0.0583   0.7505   0.0196
  -5.250  -0.2827   0.01094   0.00438  -0.0586   0.7497   0.0204
  -5.000  -0.2545   0.01073   0.00417  -0.0590   0.7488   0.0210
  -4.750  -0.2261   0.01053   0.00397  -0.0593   0.7478   0.0215
  -4.500  -0.1976   0.01034   0.00378  -0.0597   0.7467   0.0220
  -4.250  -0.1690   0.01018   0.00361  -0.0601   0.7457   0.0228
  -4.000  -0.1404   0.01000   0.00343  -0.0605   0.7446   0.0239
  -3.750  -0.1118   0.00981   0.00326  -0.0609   0.7433   0.0256
  -3.500  -0.0830   0.00963   0.00308  -0.0613   0.7419   0.0274
  -3.250  -0.0542   0.00944   0.00292  -0.0617   0.7406   0.0316
  -3.000  -0.0254   0.00922   0.00275  -0.0621   0.7393   0.0429
  -2.750   0.0033   0.00899   0.00259  -0.0626   0.7382   0.0607
  -2.500   0.0321   0.00877   0.00245  -0.0631   0.7372   0.0836
  -2.250   0.0609   0.00855   0.00232  -0.0636   0.7362   0.1116
  -2.000   0.0899   0.00835   0.00223  -0.0641   0.7349   0.1401
  -1.750   0.1189   0.00811   0.00215  -0.0647   0.7331   0.1818
  -1.250   0.1768   0.00732   0.00193  -0.0662   0.7282   0.3432
  -1.000   0.2063   0.00649   0.00173  -0.0675   0.7259   0.5325
  -0.750   0.2368   0.00603   0.00160  -0.0685   0.7237   0.6362
  -0.500   0.2664   0.00565   0.00165  -0.0691   0.7213   0.7544
  -0.250   0.2959   0.00572   0.00180  -0.0695   0.7173   0.7913
   0.000   0.3258   0.00574   0.00181  -0.0700   0.7128   0.8007
   0.250   0.3555   0.00576   0.00182  -0.0705   0.7091   0.8086
   0.500   0.3854   0.00580   0.00185  -0.0710   0.7050   0.8140
   0.750   0.4149   0.00582   0.00187  -0.0715   0.6995   0.8169
   1.000   0.4444   0.00582   0.00185  -0.0719   0.6930   0.8198
   1.250   0.4739   0.00586   0.00186  -0.0724   0.6816   0.8238
   1.500   0.5033   0.00591   0.00184  -0.0728   0.6649   0.8274
   1.750   0.5312   0.00600   0.00185  -0.0730   0.6480   0.8296
   2.000   0.5593   0.00613   0.00190  -0.0732   0.6346   0.8308
   2.500   0.6162   0.00637   0.00205  -0.0740   0.6118   0.8325
   2.750   0.6441   0.00654   0.00216  -0.0742   0.5934   0.8335
   3.000   0.6721   0.00669   0.00226  -0.0745   0.5742   0.8346
   3.250   0.6999   0.00687   0.00237  -0.0748   0.5533   0.8355
   3.500   0.7273   0.00708   0.00250  -0.0750   0.5339   0.8366
   3.750   0.7533   0.00740   0.00270  -0.0750   0.5056   0.8381
   4.000   0.7765   0.00794   0.00300  -0.0746   0.4510   0.8396
   4.250   0.7988   0.00856   0.00334  -0.0741   0.3948   0.8406
   4.500   0.8220   0.00908   0.00365  -0.0738   0.3502   0.8415
   4.750   0.8392   0.01002   0.00418  -0.0725   0.2686   0.8425
   5.000   0.8522   0.01121   0.00489  -0.0707   0.1703   0.8436
   5.250   0.8693   0.01206   0.00543  -0.0694   0.1062   0.8445
   5.500   0.8891   0.01268   0.00587  -0.0686   0.0705   0.8454
   5.750   0.9083   0.01331   0.00634  -0.0676   0.0386   0.8462
   6.000   0.9304   0.01373   0.00672  -0.0671   0.0277   0.8469
   6.250   0.9530   0.01410   0.00706  -0.0667   0.0234   0.8475
   6.500   0.9756   0.01444   0.00740  -0.0662   0.0215   0.8481
   6.750   0.9973   0.01480   0.00777  -0.0657   0.0196   0.8487
   7.000   1.0169   0.01514   0.00813  -0.0647   0.0186   0.8495
   7.250   1.0366   0.01553   0.00853  -0.0638   0.0170   0.8504
   7.500   1.0563   0.01603   0.00903  -0.0631   0.0148   0.8512
   7.750   1.0765   0.01653   0.00954  -0.0625   0.0111   0.8519
   8.000   1.0939   0.01728   0.01026  -0.0618   0.0079   0.8526
   8.250   1.1129   0.01801   0.01101  -0.0615   0.0070   0.8533
   8.500   1.1318   0.01871   0.01173  -0.0610   0.0065   0.8540
   8.750   1.1504   0.01939   0.01244  -0.0605   0.0063   0.8547
   9.000   1.1684   0.02010   0.01318  -0.0599   0.0062   0.8553
   9.250   1.1857   0.02084   0.01396  -0.0591   0.0060   0.8559
   9.500   1.2026   0.02160   0.01475  -0.0584   0.0059   0.8565
  10.000   1.2338   0.02323   0.01647  -0.0565   0.0056   0.8579
  10.250   1.2487   0.02409   0.01738  -0.0555   0.0055   0.8587
  10.500   1.2626   0.02502   0.01836  -0.0544   0.0054   0.8595
  10.750   1.2759   0.02598   0.01937  -0.0533   0.0053   0.8603
  11.000   1.2888   0.02698   0.02043  -0.0522   0.0052   0.8611
  11.250   1.3004   0.02807   0.02157  -0.0509   0.0051   0.8620
  11.500   1.3115   0.02921   0.02277  -0.0497   0.0050   0.8628
  11.750   1.3218   0.03043   0.02404  -0.0484   0.0049   0.8636
  12.000   1.3303   0.03179   0.02547  -0.0470   0.0048   0.8645
  12.250   1.3380   0.03322   0.02698  -0.0455   0.0047   0.8653
  12.500   1.3438   0.03483   0.02867  -0.0440   0.0047   0.8662
  12.750   1.3518   0.03629   0.03020  -0.0427   0.0046   0.8671
  13.000   1.3604   0.03772   0.03169  -0.0416   0.0046   0.8679
  13.250   1.3689   0.03921   0.03325  -0.0405   0.0046   0.8687
  13.500   1.3764   0.04085   0.03495  -0.0395   0.0045   0.8696
  13.750   1.3840   0.04253   0.03671  -0.0386   0.0045   0.8704
  14.000   1.3906   0.04435   0.03861  -0.0377   0.0044   0.8712
  14.250   1.3971   0.04624   0.04058  -0.0368   0.0044   0.8719
  14.500   1.4027   0.04827   0.04270  -0.0361   0.0044   0.8730
  14.750   1.4075   0.05043   0.04495  -0.0354   0.0043   0.8740
  15.000   1.4121   0.05264   0.04726  -0.0348   0.0043   0.8752
  15.250   1.4162   0.05495   0.04966  -0.0342   0.0042   0.8764
  15.500   1.4197   0.05739   0.05219  -0.0338   0.0041   0.8777
  15.750   1.4226   0.05995   0.05486  -0.0335   0.0041   0.8791
  16.000   1.4245   0.06268   0.05768  -0.0332   0.0040   0.8805
  16.250   1.4254   0.06555   0.06066  -0.0330   0.0040   0.8819
  16.500   1.4250   0.06864   0.06386  -0.0330   0.0039   0.8833
  16.750   1.4237   0.07193   0.06725  -0.0330   0.0039   0.8847
  17.000   1.4218   0.07537   0.07080  -0.0333   0.0039   0.8860
  17.500   1.4146   0.08286   0.07852  -0.0341   0.0038   0.8891
  17.750   1.4099   0.08686   0.08264  -0.0348   0.0038   0.8910
  18.000   1.4039   0.09113   0.08703  -0.0356   0.0038   0.8930
  18.250   1.3975   0.09557   0.09159  -0.0366   0.0037   0.8952
  18.500   1.3900   0.10024   0.09638  -0.0379   0.0037   0.8974
  18.750   1.3822   0.10504   0.10130  -0.0393   0.0037   0.8998
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