naca

BladeX - Python Blade Morphing

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 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

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

自动化 NACA 翼型 CFD 流程与气动系数数据库：多块钝后缘网格、Fluent RANS/URANS、工况矩阵扫掠，以及 Cursor Skills（问询/收敛/波动升级/对比报告）。

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

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

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.

Plota um perfil NACA 4 dígitos

Get NACA airfoil with more points

Aerodynamic performance analysis of NACA 6-series airfoils using XFLR5 compared to NACA TN-2502 experimental data.

aerodynamic section synthesizer