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 (H).

HQ 1.5/9 B AIRFOIL to HQ 3.0/13 AIRFOIL

Page 2 of 4     1 2 3 4     Next

(hq159b-il) HQ 1.5/9 B AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.5/9 B AIRFOILQuabeck HQ 1.5/9 B R/C sailplane airfoil
Max thickness 9% at 37.1% chord
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq17-il) HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED)Airfoil measured from an ASW22 wing
Max thickness 15.2% at 42% chord
Max camber 4.5% at 42% chord
Source UIUC Airfoil Coordinates Database

(hq2010-il) HQ 2.0/10 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.0/10 AIRFOILQuabeck HQ 2.0/10 R/C sailplane airfoil
Max thickness 10% at 35% chord
Max camber 2% at 45% chord
Source UIUC Airfoil Coordinates Database

(hq2012-il) HQ 2.0/12 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.0/12 AIRFOILQuabeck HQ 2.0/12 R/C sailplane airfoil
Max thickness 12% at 35% chord
Max camber 2% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq208-il) HQ 2.0/8 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.0/8 AIRFOILQuabeck HQ 2.0/8 R/C sailplane airfoil
Max thickness 8% at 35% chord
Max camber 2% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq209-il) HQ 2.0/9 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.0/9 AIRFOILQuabeck HQ 2.0/9 R/C sailplane airfoil
Max thickness 9% at 35% chord
Max camber 2% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq2090sm-il) HQ-2.0/9 9.0% smoothed

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ-2.0/9  9.0%   smoothedQuabeck HQ 2.0/9 R/C sailplane airfoil (smoothed)
Max thickness 9% at 35% chord
Max camber 2% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq2195-il) HQ 2.1/9.5 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.1/9.5 AIRFOILQuabeck HQ 2.1/9.5 R/C sailplane airfoil
Max thickness 9.5% at 35% chord
Max camber 2.1% at 55% chord
Source UIUC Airfoil Coordinates Database

(hq2510-il) HQ 2.5/10 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.5/10 AIRFOILQuabeck HQ 2.5/10 R/C sailplane airfoil
Max thickness 10% at 35% chord
Max camber 2.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq2511-il) HQ 2.5/11 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.5/11 AIRFOILQuabeck HQ 2.5/11 R/C sailplane airfoil
Max thickness 11% at 33.9% chord
Max camber 2.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq2512-il) HQ 2.5/12 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.5/12 AIRFOILQuabeck HQ 2.5/12 R/C sailplane airfoil
Max thickness 12% at 35% chord
Max camber 2.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq258-il) HQ 2.5/8 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.5/8 AIRFOILQuabeck HQ 2.5/8 R/C sailplane airfoil
Max thickness 8% at 35% chord
Max camber 2.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq259-il) HQ 2.5/9 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.5/9 AIRFOILQuabeck HQ 2.5/9 R/C sailplane airfoil
Max thickness 9% at 35% chord
Max camber 2.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq2590sm-il) HQ 2.5/9.0 smoothed by Eppler

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.5/9.0 smoothed by EpplerQuabeck HQ 2.5/9 R/C sailplane airfoil (smoothed)
Max thickness 9% at 35% chord
Max camber 2.5% at 55% chord
Source UIUC Airfoil Coordinates Database

(hq259b-il) HQ 2.5/9 B AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 2.5/9 B AIRFOILQuabeck HQ 2.5/9 B R/C sailplane airfoil
Max thickness 9% at 35% chord
Max camber 2.5% at 55% chord
Source UIUC Airfoil Coordinates Database

(hq300gd2-il) HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOILDFVLR/Braunschweig Horstmann and Quast HQ-300 GD(MOD 2) sailplane airfoil
Max thickness 16.6% at 39.1% chord
Max camber 3.9% at 39.1% chord
Source UIUC Airfoil Coordinates Database

(hq3010-il) HQ 3.0/10 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 3.0/10 AIRFOILQuabeck HQ 3.0/10 R/C sailplane airfoil
Max thickness 10% at 35% chord
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3011-il) HQ 3.0/11 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 3.0/11 AIRFOILQuabeck HQ 3.0/11 R/C sailplane airfoil
Max thickness 11% at 35% chord
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3012-il) HQ 3.0/12 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 3.0/12 AIRFOILQuabeck HQ 3.0/12 R/C sailplane airfoil
Max thickness 12% at 35% chord
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3013-il) HQ 3.0/13 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 3.0/13 AIRFOILQuabeck HQ 3.0/13 R/C sailplane airfoil
Max thickness 13% at 35% chord
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database
Page 2 of 4     1 2 3 4     Next

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