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

Airfoil database list (E).

EH 2.0/7.0 to ESA40

Page 11 of 11     -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9 10 11     Next

(eh2070-il) EH 2.0/7.0

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EH 2.0/7.0John Yost EH 2.0/7.0 for tailless R/C aircraft
Max thickness 7% at 28.7% chord
Max camber 2% at 25.9% chord
Source UIUC Airfoil Coordinates Database

(eh2510-il) EH 2.5/10

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EH 2.5/10John Yost EH 2.5/10 for tailless R/C aircraft
Max thickness 10% at 30% chord
Max camber 2.5% at 25% chord
Source UIUC Airfoil Coordinates Database

(eh3012-il) EH 3.0/12

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EH 3.0/12John Yost EH 3.0/12 for tailless R/C aircraft
Max thickness 12% at 30% chord
Max camber 2.9% at 25% chord
Source UIUC Airfoil Coordinates Database

(eiffel10-il) Eiffel 10 (Wright) - 1903 Wright Flyer airfoil

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
Eiffel 10 (Wright) - 1903 Wright Flyer airfoilEiffel 10 (Wright) - 1903 Wright Flyer airfoil
Max thickness 2.7% at 0% chord
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(eiffel371-il) Eiffel 371 (Monge)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
Eiffel 371 (Monge)Eiffel 371 (Monge) airfoil
Max thickness 14.4% at 30% chord
Max camber 3.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(eiffel385-il) Eiffel 385 (S.T. Ae)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
Eiffel 385 (S.T. Ae)Eiffel 385 (S.T. Ae) airfoil
Max thickness 13.4% at 20% chord
Max camber 4.4% at 50% chord
Source UIUC Airfoil Coordinates Database

(eiffel428-il) Eiffel 428 (Bleriot)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
Eiffel 428 (Bleriot)Eiffel 428 (Bleriot) airfoil
Max thickness 9% at 30% chord
Max camber 4.2% at 40% chord
Source UIUC Airfoil Coordinates Database

(eiffel430-il) Eiffel 430 (Lachassgne)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
Eiffel 430 (Lachassgne)Eiffel 430 (Lachassgne) airfoil
Max thickness 9.7% at 15% chord
Max camber 4.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(esa40-il) ESA40

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
ESA40Evans Simitar Airfoil ESA40 for R/C tailless aircraft
Max thickness 10.7% at 27.1% chord
Max camber 2% at 12% chord
Source UIUC Airfoil Coordinates Database
Page 11 of 11     -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9 10 11     Next

Please see the source web site or designer for any license conditions.