Airfoil Tools
Search 1638 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

Airfoil database search

Search the 1638 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


(e662-il) EPPLER E662 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER E662 AIRFOILEppler E662 sailplane airfoil
Max thickness 15% at 42.8% chord
Max camber 4.1% at 47.5% chord
Source UIUC Airfoil Coordinates Database

(e715-il) EPPLER 715 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 715 AIRFOILEppler E715 tailplane airfoil
Max thickness 15% at 33.1% chord
Max camber 2.8% at 42% chord
Source UIUC Airfoil Coordinates Database

(fx67k150-il) FX 67-K-150/17 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
FX 67-K-150/17 AIRFOILWortmann FX 67-K-150/17 airfoil
Max thickness 15% at 40.2% chord
Max camber 4.8% at 43.5% 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

(fx72150a-il) WORTMANN FX 72-MS-150A AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
WORTMANN FX 72-MS-150A AIRFOILWortmann FX 72-MS-150A airfoil
Max thickness 15% at 37.1% chord
Max camber 8.3% at 46.7% chord
Source UIUC Airfoil Coordinates Database

(fx72150b-il) WORTMANN FX 72-MS-150B AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
WORTMANN FX 72-MS-150B AIRFOILWortmann FX 72-MS-150B airfoil
Max thickness 15% at 37.1% chord
Max camber 9.7% at 46.7% chord
Source UIUC Airfoil Coordinates Database

(fx84w150-il) FX 84-W-150

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
FX 84-W-150Wortmann FX 84-W-150 airfoil for use on wind turbines (W)
Max thickness 15% at 37.1% chord
Max camber 4.2% at 40.2% chord
Source UIUC Airfoil Coordinates Database
Page 39 of 164     29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48     Next


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