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

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


(b737a-il) BOEING 737 ROOT AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
BOEING 737 ROOT AIRFOILBoeing Commercial Airplane Company model 737 airfoils
Max thickness 15.4% at 19.6% chord
Max camber 0.2% at 5% chord
Source UIUC Airfoil Coordinates Database

(b737b-il) BOEING 737 MIDSPAN AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
BOEING 737 MIDSPAN AIRFOILBoeing Commercial Airplane Company model 737 airfoils
Max thickness 12.5% at 29.7% chord
Max camber 0.8% at 10% chord
Source UIUC Airfoil Coordinates Database

(b737c-il) BOEING 737 MIDSPAN AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
BOEING 737 MIDSPAN AIRFOILBoeing Commercial Airplane Company model 737 airfoils
Max thickness 10% at 39.9% chord
Max camber 1.5% at 20.4% chord
Source UIUC Airfoil Coordinates Database

(b737d-il) BOEING 737 OUTBOARD AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
BOEING 737 OUTBOARD AIRFOILBoeing Commercial Airplane Company model 737 airfoils
Max thickness 10.8% at 40% chord
Max camber 1.6% at 20% chord
Source UIUC Airfoil Coordinates Database
Page 1 of 1     


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