VISUAL PREVIEW

Airfoil Library

HIGH REYNOLDS PROFILES (GA & TRANSPORT)
NACA 2412 Standard GA Main Wing
NACA 2415 Utility/Cargo Root Section
NACA 0012 Symmetric / Aerobatic Standard
NACA 0015 Deep Symmetric Control Surface
NACA 23012 Modern Airliner / Transport
NACA 23015 High-Lift Cargo Transport
NACA 4412 High-Lift STOL Utility
NACA 4415 Heavy Payload Utility
NACA 1412 High Speed Efficiency
NACA 0018 Extreme Aerobatic / Structural
NACA 2418 Thick Root Assembly Section
NACA 23018 Heavy Root Transport Joint
NACA 0009 Horizontal / Vertical Tail Fin
NACA 0006 High-Speed Thin Tail Surface
NACA 2410 Thin Propeller Root Region
NACA 4418 Ultra High Camber Root
NACA 23021 Deep Spar Heavy Transport
NACA 0021 Thick Control Blade Standard
NACA 2421 Structural Root Truss Section
NACA 2424 Extreme Thickness Root Base

NACA Airfoil Profiles

What are NACA Airfoils?

Developed by the National Advisory Committee for Aeronautics, these profiles are defined by mathematical equations allowing for precise aerodynamic analysis.

NACA 4-Digit

Simple profiles defined by max camber, position, and thickness. E.g., NACA 2412.

NACA 5-Digit

Advanced profiles for specific lift coefficients and camber positions. E.g., NACA 23012.

NACA 6-Series

Laminar flow airfoils designed to minimize drag at high speeds. This tool uses exact NASA TM 4741 specifications.

Export Formats

  • DAT: Compatible with XFOIL and CFD tools.
  • CSV: For spreadsheet analysis.
  • SVG: Scalable vector graphics for CAD.