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WORTMANN FX 049-915 AIRFOIL (fx049915-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 049-915 AIRFOIL (fx049915-il)
Reynolds number: 1,000,000
Max Cl/Cd: 155.01 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx049915-il-1000000.txt
Download as CSV file: xf-fx049915-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.6974   0.03660   0.03259  -0.0902   0.4968   0.0117
 -12.250  -0.7269   0.03248   0.02819  -0.0854   0.4962   0.0118
 -12.000  -0.7299   0.03010   0.02560  -0.0825   0.4948   0.0119
 -11.750  -0.7277   0.02804   0.02334  -0.0799   0.4931   0.0120
 -11.500  -0.7158   0.02680   0.02200  -0.0781   0.4923   0.0122
 -11.250  -0.7039   0.02542   0.02047  -0.0762   0.4915   0.0123
 -11.000  -0.6890   0.02430   0.01922  -0.0746   0.4905   0.0126
 -10.750  -0.6719   0.02334   0.01814  -0.0732   0.4893   0.0128
 -10.500  -0.6543   0.02237   0.01705  -0.0718   0.4882   0.0131
 -10.250  -0.6371   0.02129   0.01580  -0.0703   0.4870   0.0134
 -10.000  -0.6177   0.02043   0.01480  -0.0690   0.4858   0.0137
  -9.750  -0.5975   0.01964   0.01387  -0.0678   0.4845   0.0139
  -9.500  -0.5761   0.01897   0.01306  -0.0667   0.4832   0.0141
  -9.250  -0.5571   0.01796   0.01188  -0.0653   0.4819   0.0145
  -9.000  -0.5371   0.01714   0.01094  -0.0640   0.4804   0.0150
  -8.750  -0.5145   0.01664   0.01036  -0.0631   0.4786   0.0154
  -8.500  -0.4909   0.01627   0.00992  -0.0622   0.4770   0.0159
  -8.250  -0.4671   0.01578   0.00935  -0.0614   0.4764   0.0164
  -8.000  -0.4430   0.01529   0.00878  -0.0606   0.4758   0.0168
  -7.750  -0.4182   0.01491   0.00832  -0.0600   0.4749   0.0173
  -7.500  -0.3955   0.01423   0.00754  -0.0589   0.4741   0.0180
  -7.250  -0.3712   0.01380   0.00706  -0.0582   0.4732   0.0188
  -7.000  -0.3460   0.01347   0.00669  -0.0575   0.4722   0.0195
  -6.750  -0.3206   0.01316   0.00633  -0.0569   0.4712   0.0203
  -6.500  -0.2950   0.01290   0.00600  -0.0563   0.4703   0.0210
  -6.250  -0.2707   0.01246   0.00552  -0.0555   0.4694   0.0225
  -6.000  -0.2449   0.01223   0.00527  -0.0550   0.4684   0.0239
  -5.750  -0.2188   0.01204   0.00502  -0.0545   0.4675   0.0251
  -5.500  -0.1937   0.01173   0.00471  -0.0538   0.4666   0.0273
  -5.250  -0.1675   0.01157   0.00452  -0.0533   0.4656   0.0293
  -5.000  -0.1416   0.01140   0.00434  -0.0528   0.4646   0.0320
  -4.750  -0.1148   0.01136   0.00428  -0.0524   0.4632   0.0348
  -4.500  -0.0882   0.01138   0.00430  -0.0521   0.4615   0.0380
  -4.250  -0.0600   0.01140   0.00432  -0.0519   0.4610   0.0408
  -4.000  -0.0330   0.01130   0.00423  -0.0516   0.4606   0.0433
  -3.750  -0.0046   0.01137   0.00431  -0.0516   0.4600   0.0455
  -3.500   0.0238   0.01145   0.00439  -0.0515   0.4594   0.0478
  -3.250   0.0522   0.01154   0.00446  -0.0515   0.4587   0.0490
  -3.000   0.0777   0.01127   0.00420  -0.0509   0.4580   0.0515
  -2.750   0.1057   0.01131   0.00425  -0.0508   0.4573   0.0534
  -2.500   0.1333   0.01131   0.00424  -0.0506   0.4566   0.0552
  -2.250   0.1610   0.01132   0.00423  -0.0505   0.4558   0.0568
  -2.000   0.1892   0.01139   0.00429  -0.0504   0.4551   0.0578
  -1.750   0.2132   0.01096   0.00386  -0.0496   0.4543   0.0605
  -1.500   0.2401   0.01090   0.00380  -0.0493   0.4536   0.0623
  -1.250   0.2671   0.01084   0.00373  -0.0491   0.4529   0.0640
  -1.000   0.2940   0.01077   0.00365  -0.0488   0.4521   0.0656
  -0.750   0.3209   0.01069   0.00356  -0.0485   0.4513   0.0669
  -0.500   0.3478   0.01064   0.00349  -0.0482   0.4505   0.0678
  -0.250   0.3743   0.01055   0.00339  -0.0479   0.4497   0.0692
   0.000   0.3999   0.01041   0.00323  -0.0474   0.4489   0.0715
   0.250   0.4265   0.01039   0.00321  -0.0471   0.4480   0.0734
   0.500   0.4533   0.01045   0.00326  -0.0469   0.4470   0.0752
   0.750   0.4802   0.01052   0.00334  -0.0467   0.4461   0.0773
   1.000   0.5074   0.01050   0.00332  -0.0465   0.4458   0.0792
   1.250   0.5346   0.01049   0.00333  -0.0464   0.4454   0.0804
   1.500   0.5614   0.01044   0.00329  -0.0461   0.4449   0.0839
   1.750   0.5883   0.01041   0.00329  -0.0459   0.4444   0.0881
   2.000   0.6154   0.01040   0.00330  -0.0458   0.4437   0.0921
   2.250   0.6422   0.01037   0.00332  -0.0455   0.4430   0.1052
   2.500   0.6407   0.00868   0.00341  -0.0399   0.4425   0.7611
   2.750   0.7708   0.00857   0.00381  -0.0622   0.4414   0.9855
   3.000   0.8191   0.00871   0.00393  -0.0667   0.4407   0.9915
   3.250   0.8651   0.00881   0.00401  -0.0707   0.4400   0.9954
   3.500   0.9084   0.00885   0.00405  -0.0741   0.4392   0.9982
   3.750   0.9478   0.00890   0.00409  -0.0767   0.4384   1.0000
   4.000   0.9719   0.00896   0.00415  -0.0761   0.4376   1.0000
   4.250   0.9961   0.00903   0.00422  -0.0755   0.4369   1.0000
   4.500   1.0204   0.00911   0.00431  -0.0749   0.4362   1.0000
   4.750   1.0448   0.00920   0.00440  -0.0743   0.4356   1.0000
   5.000   1.0692   0.00931   0.00451  -0.0737   0.4349   1.0000
   5.250   1.0937   0.00942   0.00464  -0.0732   0.4341   1.0000
   5.500   1.1182   0.00958   0.00480  -0.0727   0.4330   1.0000
   5.750   1.1421   0.00991   0.00513  -0.0721   0.4313   1.0000
   6.000   1.1667   0.00994   0.00520  -0.0716   0.4308   1.0000
   6.250   1.1911   0.00988   0.00520  -0.0710   0.4295   1.0000
   6.500   1.2156   0.00985   0.00522  -0.0704   0.4279   1.0000
   6.750   1.2403   0.00985   0.00525  -0.0700   0.4262   1.0000
   7.000   1.2654   0.00979   0.00521  -0.0695   0.4240   1.0000
   7.250   1.2906   0.00966   0.00507  -0.0690   0.4211   1.0000
   7.500   1.3153   0.00970   0.00511  -0.0686   0.4189   1.0000
   7.750   1.3396   0.00975   0.00520  -0.0681   0.4159   1.0000
   8.000   1.3643   0.00970   0.00522  -0.0676   0.4133   1.0000
   8.250   1.3892   0.00966   0.00523  -0.0671   0.4102   1.0000
   8.500   1.4140   0.00961   0.00520  -0.0667   0.4063   1.0000
   8.750   1.4379   0.00966   0.00526  -0.0661   0.4018   1.0000
   9.000   1.4632   0.00965   0.00533  -0.0658   0.3967   1.0000
   9.250   1.4871   0.00969   0.00538  -0.0653   0.3905   1.0000
   9.500   1.5113   0.00975   0.00549  -0.0648   0.3805   1.0000
   9.750   1.5314   0.01000   0.00566  -0.0637   0.3567   1.0000
  10.000   1.5364   0.01112   0.00649  -0.0602   0.3049   1.0000
  10.250   1.5325   0.01273   0.00781  -0.0555   0.2546   1.0000
  10.500   1.5255   0.01434   0.00921  -0.0504   0.2123   1.0000
  10.750   1.5088   0.01617   0.01084  -0.0440   0.1732   1.0000
  11.000   1.4875   0.01772   0.01230  -0.0369   0.1525   1.0000
  11.250   1.4578   0.02094   0.01553  -0.0324   0.1322   1.0000
  11.500   1.4349   0.02637   0.02104  -0.0331   0.1211   1.0000
  11.750   1.4071   0.03208   0.02679  -0.0330   0.1107   1.0000
  12.000   1.3835   0.03677   0.03151  -0.0320   0.1034   1.0000
  12.250   1.3647   0.04085   0.03563  -0.0311   0.0963   1.0000
  12.500   1.3426   0.04522   0.03999  -0.0302   0.0864   1.0000
  12.750   1.3256   0.04915   0.04390  -0.0294   0.0772   1.0000
  13.000   1.3164   0.05253   0.04725  -0.0289   0.0677   1.0000
  13.250   1.3037   0.05644   0.05110  -0.0286   0.0539   1.0000
  13.500   1.2888   0.06060   0.05514  -0.0283   0.0352   1.0000
  13.750   1.2795   0.06433   0.05883  -0.0282   0.0263   1.0000
  14.000   1.2782   0.06720   0.06170  -0.0281   0.0226   1.0000
  14.250   1.2802   0.06974   0.06426  -0.0280   0.0208   1.0000
  14.500   1.2820   0.07236   0.06692  -0.0280   0.0197   1.0000
  14.750   1.2834   0.07500   0.06960  -0.0280   0.0186   1.0000
  15.000   1.2855   0.07761   0.07225  -0.0281   0.0174   1.0000
  15.250   1.2888   0.08011   0.07480  -0.0282   0.0168   1.0000
  15.500   1.2913   0.08271   0.07744  -0.0283   0.0160   1.0000
  15.750   1.2947   0.08523   0.07999  -0.0285   0.0154   1.0000
  16.000   1.2935   0.08834   0.08315  -0.0287   0.0145   1.0000
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