RCAIDE.Library.Components.Airfoils

Airfoils#

Airfoils module providing classes and methods for defining and analyzing aircraft airfoil geometries

This module contains implementations of various airfoil types including general airfoils and specific NACA series airfoils. It provides functionality for defining airfoil geometry.

Notes

The airfoil classes in this module are designed to work with RCAIDE’s aerodynamic analysis tools and can be integrated into complete aircraft configurations. Airfoil data can be imported from external sources or generated using geometric definitions.

See also

RCAIDE.Library.Components.Wings

Wing components that utilize airfoil definitions

RCAIDE.Framework.Analyses.Aerodynamics

Aerodynamic analysis tools that work with airfoil components

Modules

Airfoil(*args, **kwarg)

Base class for defining airfoil geometries and their aerodynamic characteristics

Biconvex_Airfoil(*args, **kwarg)

Class for generating Bi-convex airfoil geometries.

NACA_4_Series_Airfoil(*args, **kwarg)

Class for generating NACA 4-series airfoil geometries.

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