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).

HUGHES HELICOPTERS HH-02 AIRFOIL to HQ 1.5/9 AIRFOIL

Page 1 of 4     1 2 3 4     Next

(hh02-il) HUGHES HELICOPTERS HH-02 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HUGHES HELICOPTERS HH-02 AIRFOILHughes helicopters HH-02 rotorcraft airfoil
Max thickness 9.6% at 30% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database

(hobie-il) HOBIE

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HOBIEHobie Hawk airfoil (Hobie Hawk R/C sailplane)
Max thickness 8.5% at 25% chord
Max camber 4% at 45% chord
Source UIUC Airfoil Coordinates Database

(hobiesm-il) HOBIESMO1.DAT

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HOBIESMO1.DATHobie Hawk airfoil (Hobie Hawk R/C sailplane)
Max thickness 8.6% at 25% chord
Max camber 3.8% at 45% chord
Source UIUC Airfoil Coordinates Database

(hor04-il) ONERA HOR04 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
ONERA HOR04 AIRFOILOnera propeller blade airfoils from US Patent 4
Max thickness 4.1% at 33.2% chord
Max camber 1.4% at 38.3% chord
Source UIUC Airfoil Coordinates Database

(hor07-il) ONERA HOR07 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
ONERA HOR07 AIRFOILOnera propeller blade airfoils from US Patent 4
Max thickness 7.2% at 23.2% chord
Max camber 4.5% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(hor12-il) ONERA HOR12 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
ONERA HOR12 AIRFOILOnera propeller blade airfoils from US Patent 4
Max thickness 11.9% at 22.8% chord
Max camber 3.7% at 46.2% chord
Source UIUC Airfoil Coordinates Database

(hor20-il) ONERA HOR20 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
ONERA HOR20 AIRFOILOnera propeller blade airfoils from US Patent 4
Max thickness 20.4% at 24.3% chord
Max camber 3.3% at 51.3% chord
Source UIUC Airfoil Coordinates Database

(hq010-il) HQ 0/10 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 0/10 AIRFOILQuabeck HQ 0/10 R/C sailplane airfoil
Max thickness 10% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(hq07-il) HQ 0/7 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 0/7 AIRFOILQuabeck HQ 0/7 R/C sailplane airfoil
Max thickness 7% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(hq09-il) HQ 0/9 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 0/9 AIRFOILQuabeck HQ 0/9 R/C sailplane airfoil
Max thickness 8.1% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(hq1010-il) HQ 1.0/10 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.0/10 AIRFOILQuabeck HQ 1.0/10 R/C sailplane airfoil
Max thickness 10% at 35% chord
Max camber 1% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq1012-il) HQ 1.0/12 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.0/12 AIRFOILQuabeck HQ 1.0/12 R/C sailplane airfoil
Max thickness 12% at 35% chord
Max camber 1% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq108-il) HQ 1.0/8 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.0/8 AIRFOILQuabeck HQ 1.0/8 R/C sailplane airfoil
Max thickness 8% at 35% chord
Max camber 1% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq109-il) HQ 1.0/9 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.0/9 AIRFOILQuabeck HQ 1.0/9 R/C sailplane airfoil
Max thickness 9% at 35% chord
Max camber 1% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq1510-il) HQ 1.5/10 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.5/10 AIRFOILQuabeck HQ 1.5/10 R/C sailplane airfoil
Max thickness 10% at 35% chord
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq1511-il) HQ 1.5/11 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.5/11 AIRFOILQuabeck HQ 1.5/11 R/C sailplane airfoil
Max thickness 11% at 33.9% chord
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq1512-il) HQ 1.5/12 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.5/12 AIRFOILQuabeck HQ 1.5/12 R/C sailplane airfoil
Max thickness 12% at 35% chord
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq158-il) HQ 1.5/8 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.5/8 AIRFOILQuabeck HQ 1.5/8 R/C sailplane airfoil
Max thickness 8% at 32.5% chord
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq1585-il) HQ 1.5/8.5 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
HQ 1.5/8.5 AIRFOILQuabeck HQ 1.5/8.5 R/C sailplane airfoil
Max thickness 8.6% at 35% chord
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq159-il) HQ 1.5/9 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 AIRFOILQuabeck HQ 1.5/9 R/C sailplane airfoil
Max thickness 9% at 35% chord
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database
Page 1 of 4     1 2 3 4     Next

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