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NACA 64A210 (naca64a210-il)

NACA 64A210 - NACA 64A210 airfoil


Airfoil naca64a210-il
Details Dat file Parser  
(naca64a210-il) NACA 64A210
NACA 64A210 airfoil
Max thickness 10% at 40% chord.
Max camber 1.3% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
NACA 64A210
1.00000     0.00021
0.95027     0.00785
0.90052     0.01551
0.85074     0.02301
0.80076     0.03037
0.75063     0.03702
0.70054     0.04310
0.65042     0.04852
0.60028     0.05323
0.55012     0.05714
0.49994     0.06014
0.44975     0.06208
0.39955     0.06274
0.34935     0.06192
0.29917     0.05984
0.24900     0.05656
0.19885     0.05200
0.14874     0.04592
0.09868     0.03792
0.07369     0.03288
0.04874     0.02685
0.02387     0.01895
0.01153     0.01342
0.00665     0.01044
0.00424     0.00856
0.00000     0.00000
0.00576     -0.00744
0.00835     -0.00886
0.01347     -0.01100
0.02613     -0.01473
0.05126     -0.01963
0.07631     -0.02316
0.10132     -0.02600
0.15126     -0.03030
0.20115     -0.03340
0.25100     -0.03554
0.30083     -0.03688
0.35065     -0.03744
0.40045     -0.03716
0.45025     -0.03580
0.50006     -0.03354
0.54988     -0.03062
0.59972     -0.02719
0.64958     -0.02342
0.69946     -0.01944
0.74937     -0.01542
0.79924     -0.01167
0.84926     -0.00859
0.89948     -0.00571
0.94974     -0.00295
1.00000     -0.00021
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Lednicer format dat file
Selig format dat file

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Polars for NACA 64A210 (naca64a210-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   naca64a210-il50,000933.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca64a210-il50,000532.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   naca64a210-il100,000949.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   naca64a210-il100,000546.5 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   naca64a210-il200,000965.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca64a210-il200,000559.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   naca64a210-il500,000985 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   naca64a210-il500,000568.5 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   naca64a210-il1,000,000993.1 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca64a210-il1,000,000573.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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