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NACA 64-108 AIRFOIL (n64108-il)

NACA 64-108 AIRFOIL - NACA 64-108 airfoil


Airfoil n64108-il
Details Dat file Parser  
(n64108-il) NACA 64-108 AIRFOIL
NACA 64-108 airfoil
Max thickness 8% at 40% chord.
Max camber 0.6% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NACA 64-108 AIRFOIL
       26.       26.

  0.000000  0.000000
  0.004720  0.006820
  0.007190  0.008280
  0.012150  0.010580
  0.024600  0.014570
  0.049560  0.020320
  0.074550  0.024710
  0.099550  0.028320
  0.149580  0.034050
  0.199620  0.038350
  0.249680  0.041520
  0.299740  0.043700
  0.349800  0.044940
  0.399870  0.045280
  0.449940  0.044310
  0.500000  0.042360
  0.550050  0.039590
  0.600100  0.036170
  0.650130  0.032190
  0.700150  0.027770
  0.750160  0.023020
  0.800150  0.018020
  0.850130  0.012970
  0.900100  0.008080
  0.950050  0.003640
  1.000000  0.000000

  0.000000  0.000000
  0.005280 -0.006320
  0.007810 -0.007580
  0.012850 -0.009500
  0.025400 -0.012710
  0.050440 -0.017160
  0.075450 -0.020470
  0.100450 -0.023160
  0.150420 -0.027330
  0.200380 -0.030390
  0.250320 -0.032560
  0.300260 -0.033980
  0.350200 -0.034640
  0.400130 -0.034560
  0.450060 -0.033350
  0.500000 -0.031320
  0.549950 -0.028630
  0.599900 -0.025450
  0.649870 -0.021890
  0.699850 -0.018050
  0.749840 -0.014060
  0.799850 -0.010060
  0.849870 -0.006250
  0.899900 -0.002920
  0.949950 -0.000480
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for NACA 64-108 AIRFOIL (n64108-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n64108-il50,000926.4 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   n64108-il50,000527.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n64108-il100,000939 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64108-il100,000536.2 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64108-il200,000949.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   n64108-il200,000543.5 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n64108-il500,000960 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64108-il500,000550.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64108-il1,000,000963.1 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n64108-il1,000,000565.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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