Airfoil database search
Online search of airfoils (aerofoil) in the databases filtering by name, thickness and camber
NACA 4412 (naca4412-il) - Airfoil Tools
Details: Dat file: Parser (naca4412-il) NACA 4412 NACA 4412 airfoil Max thickness 12% at 30% chord. Max camber 4% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file
NACA 6 series Airfoil database search
Airfoil database search (NACA 6 series) Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview …
NACA 4 digit Airfoil database search
(naca0006-il) NACA 0006: Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file: NACA 0006 airfoil Max thickness 6% at 30% chord …
NACA 0018 (naca0018-il) - Airfoil Tools
Details: Dat file: Parser (naca0018-il) NACA 0018 NACA 0018 airfoil Max thickness 18% at 30% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file …
E387 (e387-il) - Airfoil Tools
Details: Dat file: Parser (e387-il) E387 Eppler E387 low Reynolds number airfoil Max thickness 9.1% at 31.1% chord. Max camber 3.2% at 44.8% chord Source UIUC Airfoil Coordinates …
NASA/LANGLEY LS (1)-0421 AIRFOIL (ls421-il)
Details: Dat file: Parser (ls421-il) NASA/LANGLEY LS(1)-0421 AIRFOIL NASA/Langley LS(1)-0421 general aviation airfoil Max thickness 20.9% at 40% chord.
S1223 (s1223-il) - Airfoil Tools
Details: Dat file: Parser (s1223-il) S1223 Selig S1223 high lift low Reynolds number airfoil Max thickness 12.1% at 19.8% chord. Max camber 8.1% at 49% chord
RAE 2822 AIRFOIL (rae2822-il)
Details: Dat file: Parser (rae2822-il) RAE 2822 AIRFOIL RAE 2822 transonic airfoil Max thickness 12.1% at 37.9% chord. Max camber 1.3% at 75.7% chord
NACA 0012 AIRFOILS (n0012-il)
Details: Dat file: Parser (n0012-il) NACA 0012 AIRFOILS NACA 0012 airfoil Max thickness 12% at 30% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source …