Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

NACA 64(2)-415 (naca642415-il)

NACA 64(2)-415 - NACA 64(2)-415 airfoil


Airfoil naca642415-il
Details Dat file Parser  
(naca642415-il) NACA 64(2)-415
NACA 64(2)-415 airfoil
Max thickness 15% at 34.9% chord.
Max camber 2.2% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
NACA 64(2)-415
1.00000     0.00000
0.95032     0.00976
0.90066     0.01982
0.85092     0.03020
0.80109     0.04062
0.75115     0.05084
0.70111     0.06055
0.65096     0.06954
0.60087     0.07762
0.55040     0.08456
0.50000     0.09016
0.44954     0.09414
0.39904     0.09614
0.34853     0.09541
0.29803     0.09260
0.24756     0.08771
0.19714     0.08066
0.14681     0.07122
0.09662     0.05864
0.07162     0.05075
0.04673     0.04121
0.02207     0.02883
0.00996     0.02038
0.00526     0.01579
0.00299     0.01291
0.00000     0.00000
0.00701     -0.01091
0.00974     -0.01299
0.01504     -0.01610
0.02793     -0.02139
0.05327     -0.02857
0.07838     -0.03379
0.10338     -0.03796
0.15319     -0.04430
0.20286     -0.04882
0.25244     -0.05191
0.30197     -0.05372
0.35147     -0.05421
0.40096     -0.05330
0.45046     -0.05034
0.50000     -0.04604
0.54960     -0.04076
0.59928     -0.03478
0.64904     -0.02834
0.69889     -0.02167
0.74885     -0.01504
0.79897     -0.00878
0.84908     -0.00328
0.89934     0.00086
0.94968     0.00288
1.00000     0.00000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

NACA 63-415 AIRFOILPreviewDetails
NACA 65(2)-415PreviewDetails
HQ 3.0/15 AIRFOILPreviewDetails
EPPLER 715 AIRFOILPreviewDetails
MRC-20PreviewDetails
NACA 63-215 AIRFOILPreviewDetails
NACA 64-215 AIRFOILPreviewDetails
NACA 64(2)-215PreviewDetails
NACA 63(2)-615PreviewDetails
NACA 65(2)-415 a=0.5PreviewDetails

Polars for NACA 64(2)-415 (naca642415-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   naca642415-il50,000927.2 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca642415-il50,000525.9 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   naca642415-il100,000951.9 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   naca642415-il100,000551.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   naca642415-il200,000975.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   naca642415-il200,000570 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   naca642415-il500,0009101.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   naca642415-il500,000590.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   naca642415-il1,000,0009120.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   naca642415-il1,000,0005103.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit