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WORTMANN FX 049-915 AIRFOIL (fx049915-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 049-915 AIRFOIL (fx049915-il)
Reynolds number: 500,000
Max Cl/Cd: 114.64 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx049915-il-500000-n5.txt
Download as CSV file: xf-fx049915-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 049-915 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.1851   0.09115   0.08649  -0.0636   0.4764   0.0099
 -10.500  -0.2444   0.07667   0.07215  -0.0694   0.4773   0.0103
 -10.250  -0.5385   0.03188   0.02666  -0.0812   0.4822   0.0097
 -10.000  -0.5373   0.02824   0.02263  -0.0789   0.4813   0.0098
  -9.750  -0.5269   0.02606   0.02015  -0.0771   0.4803   0.0099
  -9.500  -0.5116   0.02448   0.01831  -0.0757   0.4793   0.0101
  -9.250  -0.4950   0.02313   0.01673  -0.0743   0.4782   0.0103
  -9.000  -0.4775   0.02200   0.01543  -0.0729   0.4771   0.0106
  -8.750  -0.4572   0.02118   0.01447  -0.0718   0.4759   0.0109
  -8.500  -0.4354   0.02044   0.01362  -0.0709   0.4751   0.0112
  -8.250  -0.4132   0.01971   0.01278  -0.0700   0.4743   0.0116
  -8.000  -0.3903   0.01906   0.01202  -0.0692   0.4734   0.0122
  -7.750  -0.3671   0.01841   0.01123  -0.0684   0.4724   0.0126
  -7.500  -0.3436   0.01779   0.01046  -0.0676   0.4715   0.0131
  -7.250  -0.3198   0.01720   0.00975  -0.0668   0.4705   0.0135
  -7.000  -0.2965   0.01657   0.00904  -0.0659   0.4695   0.0142
  -6.750  -0.2719   0.01611   0.00851  -0.0653   0.4685   0.0148
  -6.500  -0.2470   0.01570   0.00802  -0.0647   0.4676   0.0155
  -6.250  -0.2218   0.01531   0.00754  -0.0641   0.4665   0.0164
  -6.000  -0.1964   0.01497   0.00710  -0.0635   0.4655   0.0173
  -5.750  -0.1715   0.01454   0.00661  -0.0628   0.4645   0.0188
  -5.500  -0.1462   0.01421   0.00624  -0.0623   0.4634   0.0205
  -5.250  -0.1206   0.01394   0.00589  -0.0617   0.4625   0.0221
  -5.000  -0.0951   0.01367   0.00555  -0.0612   0.4616   0.0246
  -4.750  -0.0691   0.01350   0.00538  -0.0607   0.4606   0.0293
  -4.500  -0.0428   0.01337   0.00521  -0.0603   0.4598   0.0335
  -4.250  -0.0153   0.01336   0.00523  -0.0601   0.4592   0.0383
  -4.000   0.0122   0.01337   0.00521  -0.0599   0.4585   0.0426
  -3.750   0.0395   0.01335   0.00513  -0.0596   0.4578   0.0454
  -3.500   0.0666   0.01330   0.00507  -0.0594   0.4571   0.0478
  -3.250   0.0944   0.01337   0.00514  -0.0593   0.4563   0.0503
  -3.000   0.1218   0.01338   0.00512  -0.0591   0.4555   0.0527
  -2.750   0.1489   0.01336   0.00505  -0.0588   0.4547   0.0549
  -2.500   0.1766   0.01342   0.00506  -0.0587   0.4540   0.0566
  -2.250   0.2027   0.01323   0.00485  -0.0583   0.4532   0.0584
  -2.000   0.2284   0.01300   0.00461  -0.0578   0.4524   0.0599
  -1.750   0.2546   0.01286   0.00445  -0.0574   0.4516   0.0610
  -1.500   0.2810   0.01274   0.00430  -0.0571   0.4507   0.0621
  -1.250   0.3073   0.01263   0.00417  -0.0567   0.4498   0.0635
  -1.000   0.3338   0.01254   0.00407  -0.0564   0.4491   0.0652
  -0.750   0.3604   0.01249   0.00399  -0.0561   0.4484   0.0671
  -0.500   0.3869   0.01243   0.00390  -0.0558   0.4477   0.0685
  -0.250   0.4135   0.01239   0.00384  -0.0555   0.4470   0.0697
   0.000   0.4402   0.01237   0.00380  -0.0552   0.4463   0.0704
   0.250   0.4665   0.01233   0.00374  -0.0549   0.4457   0.0716
   0.500   0.4929   0.01231   0.00372  -0.0547   0.4449   0.0733
   0.750   0.5195   0.01232   0.00373  -0.0544   0.4443   0.0748
   1.000   0.5462   0.01231   0.00374  -0.0542   0.4438   0.0766
   1.250   0.5730   0.01231   0.00376  -0.0540   0.4433   0.0783
   1.500   0.5997   0.01232   0.00379  -0.0538   0.4426   0.0803
   1.750   0.6263   0.01233   0.00383  -0.0536   0.4419   0.0831
   2.000   0.6529   0.01234   0.00388  -0.0534   0.4410   0.0875
   2.250   0.6795   0.01236   0.00394  -0.0532   0.4403   0.0958
   2.500   0.6991   0.01174   0.00404  -0.0520   0.4396   0.3846
   3.000   0.8484   0.01067   0.00455  -0.0728   0.4379   0.9917
   3.250   0.8899   0.01079   0.00466  -0.0759   0.4371   0.9973
   3.500   0.9280   0.01089   0.00475  -0.0783   0.4364   1.0000
   3.750   0.9524   0.01100   0.00486  -0.0778   0.4356   1.0000
   4.000   0.9768   0.01110   0.00497  -0.0772   0.4348   1.0000
   4.250   1.0013   0.01121   0.00507  -0.0767   0.4340   1.0000
   4.500   1.0258   0.01133   0.00521  -0.0762   0.4333   1.0000
   4.750   1.0504   0.01146   0.00535  -0.0757   0.4327   1.0000
   5.000   1.0750   0.01160   0.00549  -0.0752   0.4321   1.0000
   5.250   1.0997   0.01174   0.00566  -0.0747   0.4314   1.0000
   5.500   1.1245   0.01190   0.00582  -0.0743   0.4306   1.0000
   5.750   1.1492   0.01208   0.00601  -0.0739   0.4298   1.0000
   6.000   1.1737   0.01226   0.00623  -0.0735   0.4290   1.0000
   6.250   1.1978   0.01243   0.00646  -0.0729   0.4283   1.0000
   6.500   1.2218   0.01260   0.00670  -0.0724   0.4275   1.0000
   6.750   1.2456   0.01276   0.00693  -0.0719   0.4265   1.0000
   7.000   1.2695   0.01290   0.00714  -0.0713   0.4251   1.0000
   7.250   1.2934   0.01296   0.00726  -0.0708   0.4230   1.0000
   7.500   1.3177   0.01299   0.00735  -0.0703   0.4207   1.0000
   7.750   1.3421   0.01299   0.00738  -0.0698   0.4185   1.0000
   8.000   1.3666   0.01300   0.00741  -0.0694   0.4163   1.0000
   8.250   1.3897   0.01298   0.00746  -0.0687   0.4121   1.0000
   8.500   1.4126   0.01293   0.00750  -0.0679   0.4060   1.0000
   8.750   1.4361   0.01289   0.00747  -0.0673   0.4012   1.0000
   9.000   1.4590   0.01299   0.00766  -0.0666   0.3959   1.0000
   9.250   1.4809   0.01299   0.00769  -0.0658   0.3861   1.0000
   9.500   1.5018   0.01310   0.00784  -0.0648   0.3715   1.0000
   9.750   1.5172   0.01345   0.00809  -0.0630   0.3454   1.0000
  10.000   1.5162   0.01460   0.00901  -0.0587   0.3036   1.0000
  10.250   1.5025   0.01637   0.01057  -0.0528   0.2649   1.0000
  10.500   1.4831   0.01799   0.01210  -0.0460   0.2398   1.0000
  10.750   1.4649   0.02001   0.01410  -0.0409   0.2213   1.0000
  11.250   1.4120   0.02986   0.02409  -0.0392   0.1933   1.0000
  11.500   1.3798   0.03569   0.02995  -0.0384   0.1815   1.0000
  11.750   1.3509   0.04083   0.03509  -0.0373   0.1703   1.0000
  12.000   1.3234   0.04577   0.04001  -0.0363   0.1568   1.0000
  12.250   1.3004   0.05030   0.04449  -0.0354   0.1422   1.0000
  12.500   1.2842   0.05441   0.04857  -0.0348   0.1284   1.0000
  12.750   1.2700   0.05850   0.05259  -0.0344   0.1131   1.0000
  13.000   1.2603   0.06220   0.05622  -0.0342   0.0991   1.0000
  13.250   1.2513   0.06589   0.05984  -0.0340   0.0849   1.0000
  13.500   1.2468   0.06914   0.06304  -0.0339   0.0736   1.0000
  13.750   1.2435   0.07227   0.06612  -0.0338   0.0590   1.0000
  14.000   1.2233   0.07743   0.07105  -0.0338   0.0287   1.0000
  14.250   1.2232   0.08030   0.07391  -0.0338   0.0231   1.0000
  14.500   1.2264   0.08284   0.07649  -0.0339   0.0195   1.0000
  14.750   1.2288   0.08551   0.07923  -0.0340   0.0178   1.0000
  15.000   1.2311   0.08818   0.08193  -0.0341   0.0161   1.0000
  15.250   1.2346   0.09072   0.08451  -0.0343   0.0146   1.0000
  15.500   1.2385   0.09324   0.08709  -0.0344   0.0136   1.0000
  15.750   1.2410   0.09596   0.08986  -0.0347   0.0128   1.0000
  16.000   1.2438   0.09865   0.09260  -0.0350   0.0122   1.0000
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