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


(bambino6-il) Bambino 6

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
Bambino 6Bambino 6 airfoil
Max thickness 12% at 40% chord
Max camber 2.8% at 40% chord
Source UIUC Airfoil Coordinates Database

(e178-il) E178 (8.69%)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
E178  (8.69%)Eppler E178 low Reynolds number airfoil
Max thickness 8.7% at 29.8% chord
Max camber 2.8% at 38.8% chord
Source UIUC Airfoil Coordinates Database

(e197-il) E197 (13.49%)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
E197  (13.49%)Eppler E197 low Reynolds number airfoil
Max thickness 13.5% at 34.6% chord
Max camber 2.8% at 43.7% chord
Source UIUC Airfoil Coordinates Database

(e336-il) EPPLER 336 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 336 AIRFOILEppler E336 flying wing airfoil
Max thickness 12.8% at 28.1% chord
Max camber 2.8% at 23.4% chord
Source UIUC Airfoil Coordinates Database

(e551-il) EPPLER 551 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 551 AIRFOILEppler E551 general aviation airfoil
Max thickness 18.2% at 32.4% chord
Max camber 2.8% at 57.1% 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

(e818-il) EPPLER 818 HYDROFOIL AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 818 HYDROFOIL AIRFOILEppler E818 hydrofoil
Max thickness 9.4% at 33.1% chord
Max camber 2.8% at 67% chord
Source UIUC Airfoil Coordinates Database

(e852-il) EPPLER E852 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER E852 AIRFOILEppler E852 propeller airfoil
Max thickness 10.1% at 37.2% chord
Max camber 2.8% at 61.2% chord
Source UIUC Airfoil Coordinates Database

(e908-il) EPPLER 908 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 908 AIRFOILEppler E908 hydrofoil
Max thickness 9% at 44.8% chord
Max camber 2.8% at 66.3% chord
Source UIUC Airfoil Coordinates Database

(fx78k161-il) FX 78-K-161

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
FX 78-K-161Wortmann FX 78-K-161 airfoil for use with flaps (K)
Max thickness 16.2% at 40.2% chord
Max camber 2.8% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Page 74 of 164     64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83     Next


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