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 list (S).

S2060 8% to S4110

Page 2 of 9     1 2 3 4 5 6 7 8 9     Next

(s2060-il) S2060 8%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S2060 8%Selig S2060 low Reynolds number airfoil
Max thickness 8% at 30.2% chord
Max camber 1.6% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(s2062-il) S2062 8%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S2062 8%Selig S2062 low Reynolds number airfoil
Max thickness 8% at 30.1% chord
Max camber 1.5% at 49.6% chord
Source UIUC Airfoil Coordinates Database

(s2091-il) S2091-101-83

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S2091-101-83Selig S2091 low Reynolds number airfoil
Max thickness 10.1% at 26% chord
Max camber 3.7% at 39.5% chord
Source UIUC Airfoil Coordinates Database

(s3-il) REPUBLIC S-3 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
REPUBLIC S-3 AIRFOILRepublic S-3 airfoil (P-47 wing airfoil)
Max thickness 11% at 30% chord
Max camber 1.8% at 15% chord
Source UIUC Airfoil Coordinates Database

(s3002-il) SELIG 3002-099-83

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
SELIG 3002-099-83Selig S3002 low Reynolds number airfoil
Max thickness 9.9% at 30.6% chord
Max camber 2.3% at 49.8% chord
Source UIUC Airfoil Coordinates Database

(s3010-il) S3010-103-84

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S3010-103-84Selig S3010 low Reynolds number airfoil
Max thickness 10.3% at 25% chord
Max camber 2.3% at 43.3% chord
Source UIUC Airfoil Coordinates Database

(s3014-il) S3014-095-85

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S3014-095-85Selig S3014 low Reynolds number airfoil
Max thickness 9.5% at 29.4% chord
Max camber 2.6% at 38.6% chord
Source UIUC Airfoil Coordinates Database

(s3016-il) S3016-095-87

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S3016-095-87Selig S3016 low Reynolds number airfoil
Max thickness 9.5% at 28.9% chord
Max camber 1.8% at 43.1% chord
Source UIUC Airfoil Coordinates Database

(s3021-il) S3021-095-84

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S3021-095-84Selig S3021 low Reynolds number airfoil
Max thickness 9.5% at 30% chord
Max camber 2.5% at 39.2% chord
Source UIUC Airfoil Coordinates Database

(s3024-il) AIRFOIL 3024 9.84%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
AIRFOIL 3024    9.84%Selig S3024 low Reynolds number airfoil
Max thickness 9.8% at 30.7% chord
Max camber 3% at 44.7% chord
Source UIUC Airfoil Coordinates Database

(s3025-il) S3025 9.38%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S3025 9.38%Selig S3025 low Reynolds number airfoil
Max thickness 9.4% at 30.9% chord
Max camber 3% at 44.9% chord
Source UIUC Airfoil Coordinates Database

(s4022-il) S4022

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4022Selig S4022 low Reynolds number airfoil
Max thickness 11.3% at 34.1% chord
Max camber 4.3% at 57.8% chord
Source UIUC Airfoil Coordinates Database

(s4053-il) S4053

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4053Selig S4053 low Reynolds number airfoil
Max thickness 8.9% at 30.9% chord
Max camber 3% at 45% chord
Source UIUC Airfoil Coordinates Database

(s4061-il) S4061-096-84

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4061-096-84Selig S4061 low Reynolds number airfoil
Max thickness 9.6% at 30.9% chord
Max camber 3.3% at 44.7% chord
Source UIUC Airfoil Coordinates Database

(s4062-il) S4062-095-87

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4062-095-87Selig S4062 low Reynolds number airfoil
Max thickness 9.5% at 31.7% chord
Max camber 4% at 50.4% chord
Source UIUC Airfoil Coordinates Database

(s4083-il) S4083 (8%)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4083 (8%)Selig S4083 low Reynolds number airfoil
Max thickness 8% at 22.5% chord
Max camber 3.4% at 35.5% chord
Source UIUC Airfoil Coordinates Database

(s4094-il) S4094 (root airfoil designed for and used on the E-flite UMX ASK-21 scale RC sailplane)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4094 (root airfoil designed for and used on the E-flite UMX ASK-21 scale RC sailplane)Selig airfoil for micro RC soaring. Used on the E-flite UMX ASK-21 scale RC sailplane.
Max thickness 9.9% at 29.1% chord
Max camber 1.8% at 33.6% chord
Source UIUC Airfoil Coordinates Database

(s4095-il) S4095 (designed for the E-flite UMX ASK-21 scale RC sailplane)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4095 (designed for the E-flite UMX ASK-21 scale RC sailplane)Selig airfoil for micro RC soaring. Used on the E-flite UMX ASK-21 scale RC sailplane.
Max thickness 9.7% at 29.1% chord
Max camber 1.7% at 33.7% chord
Source UIUC Airfoil Coordinates Database

(s4096-il) S4096 (designed for the E-flite UMX ASK-21 scale RC sailplane)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4096 (designed for the E-flite UMX ASK-21 scale RC sailplane)Selig airfoil for micro RC soaring. Used on the E-flite UMX ASK-21 scale RC sailplane.
Max thickness 12.5% at 34% chord
Max camber 1.2% at 34% chord
Source UIUC Airfoil Coordinates Database

(s4110-il) S4110

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
S4110Selig S4110 low Reynolds number airfoil
Max thickness 8.4% at 26.6% chord
Max camber 3.1% at 45.4% chord
Source UIUC Airfoil Coordinates Database
Page 2 of 9     1 2 3 4 5 6 7 8 9     Next

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