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 (Symmetrical)

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


(sc20012-il) NASA SC(2)-0012 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
NASA SC(2)-0012 AIRFOILNASA SC(2)-0012 airfoil (NASA TP-2969)
Max thickness 12% at 37% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(sd8020-il) SD8020-010-88

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
SD8020-010-88Selig/Donovan SD8020 low Reynolds number airfoil
Max thickness 10.1% at 27.5% chord
Max camber 0% at 42.1% chord
Source UIUC Airfoil Coordinates Database

(stcyr172-il) St. CYR 172 (Royer)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
St. CYR 172 (Royer)St. CYR 172 (Royer) airfoil
Max thickness 13.6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ultimate-il) ULTIMATE

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
ULTIMATECarl Goldberg R/C Ultimate Bipe airfoil
Max thickness 12.8% at 34.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(us1000root-il) US1000ROOT

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
US1000ROOTGreat Planes R/C Ultra-Sport 1000 airfoil
Max thickness 18.6% at 27.1% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ys900-il) YS-900

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
YS-900YS900 hyrdofoil (Shen / Eppler)
Max thickness 9% at 52.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Page 14 of 14     -5 -4 -3 -2 -1 0 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.