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.
(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 | |
Quabeck HQ 0/10 R/C sailplane airfoil Max thickness 10% at 33.9% chord Max camber 0% at 0% chord Max Cl/Cd 27.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database | ||
(bqm34-il) RYAN BQM-34 FIREBEE WING AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Ryan BQM-34 Firebee wing airfoil (NACA 63-014A W/NACA 0014 nose and thinned to .09899 to account for sweep) Max thickness 9.9% at 32.5% chord Max camber 0% at 0% chord Max Cl/Cd 27.1 at Re# 50,000 Source UIUC Airfoil Coordinates Database | ||
(lwk79100-il) LWK 79-100 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
LWK 79-100 symmetrical airfoil Max thickness 10% at 27.9% chord Max camber 0% at 0% chord Max Cl/Cd 27.1 at Re# 50,000 Source UIUC Airfoil Coordinates Database | ||
(rae103-il) RAE 103 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
RAE 103 airfoil Max thickness 10% at 40% chord Max camber 0% at 0% chord Max Cl/Cd 27.1 at Re# 50,000 Source UIUC Airfoil Coordinates Database | ||
(fx79l100-il) FX 79-L-100 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Wortmann FX 79-L-100 symmetrical airfoil Max thickness 10.1% at 33.9% chord Max camber 0% at 0% chord Max Cl/Cd 27 at Re# 50,000 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 | |
Selig/Donovan SD8020 low Reynolds number airfoil Max thickness 10.1% at 27.5% chord Max camber 0% at 42.1% chord Max Cl/Cd 26.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database | ||
(naca64a010-il) NACA 64A-010 10.0% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
NACA 64A010 airfoil Max thickness 10% at 40% chord Max camber 0% at 0% chord Max Cl/Cd 26.6 at Re# 50,000 Source UIUC Airfoil Coordinates Database | ||
(bqm34-il) RYAN BQM-34 FIREBEE WING AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Ryan BQM-34 Firebee wing airfoil (NACA 63-014A W/NACA 0014 nose and thinned to .09899 to account for sweep) Max thickness 9.9% at 32.5% chord Max camber 0% at 0% chord Max Cl/Cd 26.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database | ||
(lwk80100-il) LWK 80-100 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
LWK 80-100 symmetrical airfoil Max thickness 10.1% at 40.2% chord Max camber 0% at 0% chord Max Cl/Cd 26.4 at Re# 50,000 Source UIUC Airfoil Coordinates Database | ||
(n63010a-il) NACA 63A010 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
NACA 63-010A airfoil Max thickness 10% at 35% chord Max camber 0% at 0% chord Max Cl/Cd 26.4 at Re# 50,000 Source UIUC Airfoil Coordinates Database |
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