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.

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.

A library for generating NACA foils

GPU-accelerated NACA airfoil analysis and optimization tool for Apple Silicon, written in Rust.

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

End-to-end CFD automation pipeline using Python & OpenFOAM to analyze and optimize NACA airfoils.

Parametric modeling, aerodynamic analysis, and design evolution of classical NACA airfoil families.

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

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

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

Plota um perfil NACA 4 dígitos

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

aerodynamic section synthesizer

Comparative CFD analysis: NACA 2412 vs NLF airfoils · ~44% L/D improvement at cruise

Explainable least-squares matching workflow for NACA 0012 pressure coefficient curves using Python, SQLite, and Bokeh.

Scientific analysis comparing XFLR5 simulations with wind tunnel experiments for NACA airfoils — computes lift/drag coefficients and generates publication-quality visualizations