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

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


(fx63137-il) WORTMANN FX 63-137 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
WORTMANN FX 63-137 AIRFOILWortmann FX 63-137 human power aircraft airfoil (Liver Puffin) airfoil
Max thickness 13.7% at 30.9% chord
Max camber 6% at 53.3% chord
Max Cl/Cd 105.7 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(goe54-il) GOE 54 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 54 AIRFOILGottingen 54 airfoil
Max thickness 6.5% at 14.9% chord
Max camber 3.5% at 19.9% chord
Max Cl/Cd 105.7 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(e682-il) EPPLER 682 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
EPPLER 682 AIRFOILEppler E682 sailplane airfoil
Max thickness 15.3% at 40.4% chord
Max camber 2.9% at 40.4% chord
Max Cl/Cd 105.7 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(vr7b-il) BOEING-VERTOL VR-7 AIRFOIL WITH TAB

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
BOEING-VERTOL VR-7 AIRFOIL WITH TABBoeing-Vertol VR-7 rotorcraft airfoil with tab
Max thickness 12% at 33% chord
Max camber 3% at 29% chord
Max Cl/Cd 105.7 at Re# 1,000,000
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
Max Cl/Cd 105.7 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(goe244-il) GOE 244 (MVA PR.4) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 244 (MVA PR.4) AIRFOILGottingen 244 (MVA PR.4) airfoil
Max thickness 17.7% at 19.6% chord
Max camber 10% at 49.6% chord
Max Cl/Cd 105.6 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(goe563-il) GOE 563 AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 563 AIRFOILGottingen 563 airfoil
Max thickness 8.9% at 29.8% chord
Max camber 2.2% at 49.8% chord
Max Cl/Cd 105.6 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(sd7043-il) SD7043 (9.1%)

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
SD7043 (9.1%)Selig/Donovan SD7043 low Reynolds number airfoil
Max thickness 9.1% at 26.6% chord
Max camber 3.3% at 50.2% chord
Max Cl/Cd 105.6 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(clarkv-il) CLARK V AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
CLARK V AIRFOILCLARK V airfoil
Max thickness 11.6% at 30% chord
Max camber 3.4% at 50% chord
Max Cl/Cd 105.6 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(goe274-il) GOE 274 (DAIMLER V) AIRFOIL

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
GOE 274 (DAIMLER V) AIRFOILGottingen 274 (DAIMLER V) airfoil
Max thickness 8.7% at 29.9% chord
Max camber 4.8% at 29.9% chord
Max Cl/Cd 105.5 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database
Page 151 of 164     145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164     Next


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