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 search (Symmetrical)

Search the 1636 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.

Optional
Optional
Optional
Optional. Symmetrical airfoils = 0
Optional


(ea61009-il) EPPLER EA 6(-1)-009 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER EA 6(-1)-009 AIRFOILEppler EA 6(-1)-009 airfoil
Max thickness 9% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ea61012-il) EPPLER EA 6(-1)-012 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER EA 6(-1)-012 AIRFOILEppler EA 6(-1)-012 airfoil
Max thickness 12% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ea81006-il) EPPLER EA 8(-1)-006 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER EA 8(-1)-006 AIRFOILEppler EA 8(-1)-006 airfoil
Max thickness 6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(eh0009-il) EH 0.0/9.0

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EH 0.0/9.0John Yost EH 0.0/9.0 for tailless R/C aircraft
Max thickness 9% at 28.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx71089a-il) WORTMANN FX 71-089A AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
WORTMANN FX 71-089A AIRFOILWortmann FX 71-089A airfoil
Max thickness 8.9% at 22.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx71120-il) WORTMANN FX 71-120 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
WORTMANN FX 71-120 AIRFOILWortmann FX 71-120 airfoil
Max thickness 12% at 25% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx711520-il) FX 71-L-150/20 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
FX 71-L-150/20 AIRFOILWortmann FX 71-L-150/20 airfoil
Max thickness 15% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx711525-il) FX 71-L-150/25 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
FX 71-L-150/25 AIRFOILWortmann FX 71-L-150/25 airfoil
Max thickness 15% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx711530-il) FX 71-L-150/30 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
FX 71-L-150/30 AIRFOILWortmann FX 71-L-150/30 airfoil
Max thickness 15% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx71l150-il) FX 71-L-150/30 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
FX 71-L-150/30 AIRFOILWortmann FX 71-L-150/30 airfoil
Max thickness 15% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Page 3 of 14     1 2 3 4 5 6 7 8 9 10 11 12 13 14     Next


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