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

EPPLER 360 AIRFOIL (e360-il)

EPPLER 360 AIRFOIL - Eppler E360 rotorcraft airfoil


Airfoil e360-il
Details Dat file Parser  
(e360-il) EPPLER 360 AIRFOIL
Eppler E360 rotorcraft airfoil
Max thickness 12.2% at 36.9% chord.
Max camber 1.6% at 27.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 360 AIRFOIL
       34.       39.

 0.0000100 -.0005100
 0.0000400 0.0010500
 0.0004000 0.0035100
 0.0011800 0.0062200
 0.0063900 0.0152700
 0.0156500 0.0245600
 0.0291000 0.0335500
 0.0467900 0.0418700
 0.0688200 0.0492500
 0.0952700 0.0556900
 0.1259300 0.0613400
 0.1603900 0.0662000
 0.1982200 0.0702100
 0.2389900 0.0732700
 0.2822200 0.0753000
 0.3274200 0.0761300
 0.3742000 0.0755500
 0.4223000 0.0734600
 0.4714600 0.0698500
 0.5215100 0.0649100
 0.5720600 0.0590300
 0.6225400 0.0525700
 0.6723500 0.0458300
 0.7208400 0.0390600
 0.7673600 0.0324600
 0.8112400 0.0263100
 0.8518300 0.0206800
 0.8884900 0.0157000
 0.9206300 0.0113900
 0.9477000 0.0076900
 0.9694500 0.0044300
 0.9858300 0.0018400
 0.9963300 0.0003900
 1.0000000 0.0000000

 0.0000100 -.0005100
 0.0001600 -.0019700
 0.0003000 -.0026600
 0.0004900 -.0033100
 0.0007600 -.0039200
 0.0011100 -.0044900
 0.0015500 -.0050600
 0.0020700 -.0056300
 0.0033200 -.0067700
 0.0048300 -.0079100
 0.0075300 -.0096100
 0.0155600 -.0134700
 0.0317700 -.0188000
 0.0532200 -.0237000
 0.0796200 -.0282200
 0.1106200 -.0323400
 0.1458300 -.0360300
 0.1848400 -.0392500
 0.2271800 -.0419600
 0.2723800 -.0441200
 0.3199200 -.0457100
 0.3692500 -.0466800
 0.4198300 -.0470000
 0.4710700 -.0466300
 0.5224000 -.0454900
 0.5733200 -.0434500
 0.6234700 -.0405100
 0.6724401 -.0367200
 0.7198400 -.0322200
 0.7653100 -.0271800
 0.8084800 -.0219200
 0.8488200 -.0168500
 0.8856600 -.0122800
 0.9183200 -.0083700
 0.9461901 -.0051900
 0.9687700 -.0027000
 0.9856700 -.0009900
 0.9963300 -.0001800
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

EPPLER 361 AIRFOILPreviewDetails
NASA/LANGLEY RC-12(N)1 AIRFOILPreviewDetails
EPPLER 485 AIRFOILPreviewDetails
S4096 (designed for the E-flite UMXPreviewDetails
NASA/LANGLEY RC-12(B)3 AIRFOILPreviewDetails
NASA/LANGLEY RC12-64C AIRFOILPreviewDetails
ONERA OA212 AIRFOILPreviewDetails
GOE 676 (= M 12) AIRFOILPreviewDetails
NACA M12 AIRFOILPreviewDetails
NACA M12PreviewDetails

Polars for EPPLER 360 AIRFOIL (e360-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e360-il50,000930.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e360-il50,000531.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e360-il100,000947.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e360-il100,000546 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e360-il200,000963.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e360-il200,000552.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e360-il500,000969.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e360-il500,000569 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e360-il1,000,000986 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e360-il1,000,000584 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit