BladeX - Python Blade Morphing

A set of tools that let you analyze the aerodynamic performance of wings and airfoils using models such as TaT,LLT and VLM.

A library for generating NACA foils

A minimal, dependency free utility for generating NACA and Bezier airfoils

PANKH (Panel Analysis of uNsteady Kinematics of Hovering airfoils) is a solver for studying unsteady aerodynamics of flapping and hovering airfoils using the unsteady vortex panel method. This repository includes the source code, example cases, and validation results.

Plota um perfil NACA 4 dígitos

Analysis And Computation Of Aerodynamics Parameters of a 4-digit NACA Airfoil With Flaps Using The Discrete Vortex Method (DVM)

Vertical wind turbine sandbox simulating the averaged torque on a three-blade vertical turbine with standard NACA blade profiles.

Panel method for steady multi-component 2D airfoil analysis using a linear vortex distribution | Python version

Python wrapper for the NACA456 airfoil coordinate generation program, provided by the Public Domain Aeronautical Software (PDAS), managed by Ralph Carmichael.