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WORTMANN FX 049-915 AIRFOIL (fx049915-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 049-915 AIRFOIL (fx049915-il)
Reynolds number: 1,000,000
Max Cl/Cd: 152.65 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx049915-il-1000000-n5.txt
Download as CSV file: xf-fx049915-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.3610   0.08069   0.07679  -0.0715   0.4685   0.0074
 -12.250  -0.6790   0.03802   0.03376  -0.0893   0.4735   0.0067
 -12.000  -0.7044   0.03169   0.02705  -0.0860   0.4732   0.0066
 -11.750  -0.7069   0.02767   0.02275  -0.0836   0.4724   0.0067
 -11.500  -0.6962   0.02548   0.02038  -0.0820   0.4714   0.0068
 -11.250  -0.6829   0.02386   0.01859  -0.0803   0.4703   0.0069
 -11.000  -0.6650   0.02277   0.01737  -0.0791   0.4693   0.0071
 -10.750  -0.6474   0.02167   0.01612  -0.0778   0.4681   0.0072
 -10.500  -0.6289   0.02064   0.01494  -0.0765   0.4670   0.0074
 -10.250  -0.6085   0.01982   0.01400  -0.0754   0.4659   0.0075
 -10.000  -0.5879   0.01904   0.01307  -0.0743   0.4647   0.0076
  -9.750  -0.5665   0.01833   0.01224  -0.0732   0.4635   0.0077
  -9.500  -0.5448   0.01764   0.01143  -0.0722   0.4624   0.0078
  -9.250  -0.5233   0.01691   0.01059  -0.0712   0.4611   0.0081
  -9.000  -0.5005   0.01632   0.00991  -0.0703   0.4599   0.0084
  -8.750  -0.4767   0.01582   0.00935  -0.0695   0.4593   0.0086
  -8.500  -0.4526   0.01535   0.00882  -0.0688   0.4587   0.0089
  -8.250  -0.4282   0.01491   0.00830  -0.0681   0.4580   0.0091
  -8.000  -0.4035   0.01450   0.00783  -0.0674   0.4572   0.0095
  -7.750  -0.3785   0.01413   0.00738  -0.0668   0.4564   0.0098
  -7.500  -0.3533   0.01379   0.00697  -0.0662   0.4556   0.0100
  -7.250  -0.3279   0.01346   0.00658  -0.0656   0.4547   0.0103
  -7.000  -0.3032   0.01303   0.00611  -0.0649   0.4538   0.0110
  -6.750  -0.2777   0.01272   0.00576  -0.0643   0.4528   0.0116
  -6.500  -0.2520   0.01244   0.00543  -0.0638   0.4519   0.0122
  -6.250  -0.2262   0.01219   0.00512  -0.0633   0.4507   0.0128
  -6.000  -0.2002   0.01196   0.00485  -0.0628   0.4498   0.0133
  -5.750  -0.1746   0.01168   0.00453  -0.0622   0.4488   0.0142
  -5.500  -0.1490   0.01142   0.00425  -0.0617   0.4479   0.0154
  -5.250  -0.1230   0.01122   0.00401  -0.0612   0.4470   0.0166
  -5.000  -0.0969   0.01105   0.00380  -0.0607   0.4460   0.0176
  -4.750  -0.0714   0.01083   0.00357  -0.0601   0.4450   0.0204
  -4.500  -0.0453   0.01066   0.00339  -0.0596   0.4442   0.0229
  -4.250  -0.0190   0.01050   0.00325  -0.0592   0.4438   0.0289
  -4.000   0.0077   0.01037   0.00314  -0.0589   0.4433   0.0337
  -3.750   0.0352   0.01033   0.00314  -0.0587   0.4428   0.0401
  -3.500   0.0626   0.01029   0.00309  -0.0584   0.4422   0.0435
  -3.250   0.0900   0.01024   0.00302  -0.0582   0.4416   0.0450
  -3.000   0.1173   0.01020   0.00296  -0.0580   0.4410   0.0459
  -2.750   0.1443   0.01011   0.00287  -0.0577   0.4404   0.0483
  -2.500   0.1717   0.01007   0.00284  -0.0575   0.4397   0.0500
  -2.250   0.1995   0.01008   0.00285  -0.0574   0.4390   0.0521
  -2.000   0.2271   0.01007   0.00283  -0.0572   0.4383   0.0541
  -1.750   0.2544   0.01003   0.00277  -0.0570   0.4375   0.0551
  -1.500   0.2815   0.00996   0.00268  -0.0568   0.4366   0.0558
  -1.250   0.3086   0.00991   0.00261  -0.0565   0.4359   0.0565
  -1.000   0.3357   0.00987   0.00256  -0.0563   0.4352   0.0569
  -0.750   0.3625   0.00979   0.00246  -0.0560   0.4345   0.0579
  -0.500   0.3890   0.00970   0.00236  -0.0557   0.4338   0.0606
  -0.250   0.4160   0.00966   0.00233  -0.0555   0.4331   0.0623
   0.000   0.4430   0.00964   0.00229  -0.0553   0.4325   0.0634
   0.250   0.4701   0.00962   0.00227  -0.0551   0.4318   0.0645
   0.500   0.4971   0.00962   0.00226  -0.0549   0.4310   0.0657
   0.750   0.5240   0.00963   0.00226  -0.0547   0.4302   0.0667
   1.000   0.5510   0.00965   0.00228  -0.0545   0.4293   0.0679
   1.250   0.5782   0.00964   0.00229  -0.0544   0.4289   0.0688
   1.500   0.6056   0.00964   0.00229  -0.0543   0.4285   0.0698
   1.750   0.6329   0.00964   0.00231  -0.0542   0.4280   0.0705
   2.000   0.6600   0.00962   0.00232  -0.0541   0.4275   0.0728
   2.250   0.6871   0.00962   0.00235  -0.0540   0.4269   0.0759
   2.500   0.7143   0.00963   0.00239  -0.0539   0.4264   0.0790
   2.750   0.7413   0.00964   0.00244  -0.0538   0.4258   0.0847
   3.000   0.7681   0.00963   0.00249  -0.0536   0.4253   0.1015
   3.250   0.7672   0.00805   0.00263  -0.0481   0.4248   0.7797
   3.750   0.9255   0.00800   0.00304  -0.0710   0.4232   0.9885
   4.250   0.9990   0.00818   0.00321  -0.0752   0.4215   0.9957
   4.500   1.0403   0.00824   0.00328  -0.0783   0.4209   0.9985
   4.750   1.0771   0.00831   0.00336  -0.0805   0.4202   1.0000
   5.000   1.1019   0.00839   0.00345  -0.0800   0.4196   1.0000
   5.250   1.1266   0.00847   0.00355  -0.0795   0.4188   1.0000
   5.500   1.1514   0.00856   0.00364  -0.0791   0.4180   1.0000
   5.750   1.1761   0.00866   0.00375  -0.0786   0.4171   1.0000
   6.000   1.2007   0.00877   0.00388  -0.0781   0.4161   1.0000
   6.250   1.2251   0.00891   0.00401  -0.0776   0.4144   1.0000
   6.500   1.2503   0.00894   0.00410  -0.0773   0.4131   1.0000
   6.750   1.2757   0.00895   0.00417  -0.0770   0.4107   1.0000
   7.000   1.3010   0.00900   0.00425  -0.0766   0.4083   1.0000
   7.250   1.3260   0.00905   0.00434  -0.0763   0.4057   1.0000
   7.500   1.3502   0.00911   0.00438  -0.0758   0.4012   1.0000
   7.750   1.3753   0.00916   0.00448  -0.0755   0.3964   1.0000
   8.000   1.4001   0.00923   0.00458  -0.0751   0.3910   1.0000
   8.250   1.4237   0.00935   0.00470  -0.0745   0.3849   1.0000
   8.500   1.4471   0.00948   0.00483  -0.0740   0.3730   1.0000
   8.750   1.4646   0.00993   0.00515  -0.0724   0.3441   1.0000
   9.000   1.4691   0.01114   0.00608  -0.0689   0.2937   1.0000
   9.250   1.4711   0.01245   0.00717  -0.0650   0.2524   1.0000
   9.500   1.4683   0.01389   0.00839  -0.0604   0.2107   1.0000
   9.750   1.4480   0.01595   0.01018  -0.0533   0.1603   1.0000
  10.000   1.4195   0.01776   0.01187  -0.0451   0.1312   1.0000
  10.250   1.3965   0.02042   0.01452  -0.0406   0.1137   1.0000
  10.500   1.3778   0.02499   0.01917  -0.0406   0.1038   1.0000
  10.750   1.3704   0.02889   0.02315  -0.0410   0.0992   1.0000
  11.000   1.3443   0.03417   0.02846  -0.0403   0.0895   1.0000
  11.250   1.3340   0.03758   0.03194  -0.0396   0.0862   1.0000
  11.500   1.3179   0.04145   0.03583  -0.0386   0.0799   1.0000
  11.750   1.3063   0.04489   0.03929  -0.0378   0.0742   1.0000
  12.000   1.2975   0.04807   0.04248  -0.0371   0.0671   1.0000
  12.250   1.2840   0.05183   0.04621  -0.0365   0.0549   1.0000
  12.500   1.2632   0.05654   0.05079  -0.0360   0.0320   1.0000
  12.750   1.2590   0.05965   0.05391  -0.0357   0.0250   1.0000
  13.000   1.2591   0.06232   0.05657  -0.0355   0.0188   1.0000
  13.250   1.2617   0.06477   0.05906  -0.0353   0.0169   1.0000
  13.500   1.2636   0.06733   0.06164  -0.0352   0.0149   1.0000
  13.750   1.2687   0.06952   0.06387  -0.0352   0.0139   1.0000
  14.000   1.2728   0.07184   0.06620  -0.0351   0.0126   1.0000
  14.250   1.2756   0.07436   0.06877  -0.0351   0.0116   1.0000
  14.500   1.2797   0.07675   0.07120  -0.0351   0.0109   1.0000
  14.750   1.2846   0.07901   0.07348  -0.0352   0.0100   1.0000
  15.000   1.2900   0.08122   0.07573  -0.0352   0.0097   1.0000
  15.250   1.2933   0.08374   0.07828  -0.0353   0.0091   1.0000
  15.500   1.2962   0.08635   0.08093  -0.0355   0.0084   1.0000
  15.750   1.3015   0.08864   0.08325  -0.0356   0.0080   1.0000
  16.000   1.3063   0.09096   0.08561  -0.0358   0.0077   1.0000
  16.250   1.3095   0.09353   0.08822  -0.0360   0.0073   1.0000
  16.500   1.3121   0.09622   0.09095  -0.0363   0.0069   1.0000
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