Online search of airfoils (aerofoil) in the databases filtering by name, thickness and camber

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

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 picture.

(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 Max camber 0% at 0% chord

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 Database Source dat file

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

Details: Dat file: Parser (fx63137-il) WORTMANN FX 63-137 AIRFOIL Wortmann FX 63-137 human power aircraft airfoil (Liver Puffin) airfoil Max thickness 13.7% at 30.9% chord.

Details of airfoil (aerofoil)(mh32-il) MH 32 8.7% Martin Hepperle MH 32 for F3E and F3B

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 dat file

Details: Dat file: Parser (naca0008-il) NACA 0008 NACA 0008 airfoil Max thickness 8% at 30% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format