Generate volume meshes for OpenVSP generated surface meshes.
☆30Jun 10, 2021Updated 5 years ago
Alternatives and similar repositories for VSP2CFD
Users that are interested in VSP2CFD are comparing it to the libraries listed below. We may earn a commission when you buy through links labeled 'Ad' on this page.
Sorting:
- A Glyph script demonstrating how to automate viscous meshing for aircraft geometry.☆27Feb 27, 2025Updated last year
- ☆25Dec 18, 2017Updated 8 years ago
- Generate Free-Form Deformation boxes for SU2.☆20Jun 24, 2021Updated 5 years ago
- A Glyph script for generating NACA 4-series airfoil geometries and boundary layer meshes.☆29Jun 4, 2026Updated 3 weeks ago
- ☆10Aug 29, 2018Updated 7 years ago
- Managed Kubernetes at scale on DigitalOcean • AdDigitalOcean Kubernetes includes the control plane, bandwidth allowance, container registry, automatic updates, and more for free.
- cgnsUtilities is a collection of functions for working with CGNS grids.☆11Apr 2, 2026Updated 2 months ago
- ☆54Apr 17, 2018Updated 8 years ago
- Airfoil Library created with Xoptfoil2☆12Jan 10, 2026Updated 5 months ago
- A Glyph script for generating NACA 4-series airfoil geometries.☆26Jun 24, 2021Updated 5 years ago
- OpenMDAO 2020 Reverse Hackathon☆16Aug 23, 2024Updated last year
- A parametric aircraft geometry tool☆789Jun 21, 2026Updated last week
- Stripped down version of XFOIL as compiled python module☆111Jun 16, 2021Updated 5 years ago
- Python Version of MachUp (Numerical Lifting-Line Method)☆18Mar 8, 2019Updated 7 years ago
- Extract spline geometries from 3D ACIS Modeler .SAT files☆17May 2, 2019Updated 7 years ago
- Deploy to Railway using AI coding agents - Free Credits Offer • AdUse Claude Code, Codex, OpenCode, and more. Autonomous software development now has the infrastructure to match with Railway.
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆32May 31, 2025Updated last year
- Vortex Lattice Method library written in Python☆44Oct 3, 2019Updated 6 years ago
- ☆13Apr 8, 2024Updated 2 years ago
- APM Plane, APM Copter, APM Rover source☆12Mar 27, 2024Updated 2 years ago
- NASTRAN is the NASA Structural Analysis System, a finite element analysis program (FEA) completed in the early 1970's.☆11Feb 28, 2018Updated 8 years ago
- Source and vortex panel method codes referenced in my YouTube videos.☆117Sep 27, 2020Updated 5 years ago
- A set of tools to solve potential flows past bodies on a Cartesian grid☆13Sep 23, 2024Updated last year
- An interactive demo of AeroSandbox, powered by Dash☆30Feb 17, 2025Updated last year
- ☆155Mar 25, 2023Updated 3 years ago
- Wordpress hosting with auto-scaling - Free Trial Offer • AdFully Managed hosting for WordPress and WooCommerce businesses that need reliable, auto-scalable performance. Cloudways SafeUpdates now available.
- A friendly library for multidisciplinary analysis and optimization on HPC☆23Jun 17, 2026Updated last week
- ☆340Aug 12, 2022Updated 3 years ago
- Multibody Dynamics Simulation Solver 多刚体动力学求解程序☆24Apr 23, 2026Updated 2 months ago
- The CEED high-order Field and Mesh Specification☆16Sep 10, 2021Updated 4 years ago
- Qt orm 框架☆14Jul 16, 2021Updated 4 years ago
- Airfoil optimization with Xfoil☆54Jan 12, 2022Updated 4 years ago
- ☆11Jan 28, 2023Updated 3 years ago
- MORTon Indexer (Z-order) Fortran environment☆12Mar 2, 2026Updated 3 months ago
- UC Berkeley, National Instruments & Autodesk Collaborative Research Project☆23Nov 1, 2016Updated 9 years ago
- Deploy on Railway without the complexity - Free Credits Offer • AdConnect your repo and Railway handles the rest with instant previews. Quickly provision container image services, databases, and storage volumes.
- Converter utility to convert APC PE0 files to OpenVSP BEM format☆30Oct 4, 2022Updated 3 years ago
- ☆51Sep 26, 2025Updated 9 months ago
- V-cycle Multigrid method for 2D Poisson Equation☆14Oct 30, 2015Updated 10 years ago
- Example case for OpenFOAM overset meshing with dynamic meshes. This case has two contra rotating 60mm propellers that are inline with one…☆10May 3, 2021Updated 5 years ago
- DATCOM-XL is a transparent and easy to use aircraft aerodynamic derivative estimation tool.☆11Apr 11, 2024Updated 2 years ago
- OpenFOAM Additions; Code that was geared to specific purposes and meant to be easily used by others.☆15Apr 8, 2014Updated 12 years ago
- Numerical Lifting-Line Algorithm☆47Aug 10, 2019Updated 6 years ago