OpenMDAO / POEMs
Proposals for OpenMDAO Enhancements
☆16Updated last month
Alternatives and similar repositories for POEMs:
Users that are interested in POEMs are comparing it to the libraries listed below
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆61Updated last week
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆91Updated last week
- OpenMDAO solvers and drivers to handle specific methods.☆11Updated last week
- ☆37Updated 2 weeks ago
- Multiphysics with OpenMDAO☆98Updated last week
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆147Updated this week
- ☆12Updated 2 months ago
- OpenMDAO 2020 Reverse Hackathon☆14Updated 7 months ago
- Blade Element Momentum Method for Propellers and Turbines☆65Updated last month
- Web application for multidisciplinary design analysis and optimization☆31Updated last week
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆40Updated last month
- Multidisciplinary Airplane Research Integrated Library☆10Updated 5 years ago
- Stripped down version of XFOIL as compiled python module☆94Updated 3 years ago
- ☆16Updated last week
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆206Updated this week
- CEASIOMpy is a Python conceptual aircraft design environment☆94Updated this week
- XDSM generator written in javascript.☆12Updated 9 months ago
- A python library for generating PDF XDSM diagrams.☆61Updated last month
- An implementation of the vortex-lattice method (VLM)☆31Updated last year
- A Comprehensive Julia implementation of the Vortex Lattice Method☆50Updated 2 months ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆43Updated 2 years ago
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆28Updated 6 months ago
- Aeroelastic Aircraft Design and Simulation Tool☆26Updated 7 years ago
- The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…☆19Updated 2 months ago
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆38Updated 4 years ago
- Python interface for XFOIL. The objective of this library is to be able to be able to call XFOIL from Python iteratively for any simulati…☆71Updated 4 years ago
- Vortex lattice method for inviscid lifting-surface aerodynamics☆42Updated 3 months ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆63Updated 2 years ago
- ☆12Updated 5 years ago
- A pre/post processor for PANAIR☆14Updated 4 years ago