OpenMDAO / POEMsLinks
Proposals for OpenMDAO Enhancements
☆18Updated 4 months ago
Alternatives and similar repositories for POEMs
Users that are interested in POEMs are comparing it to the libraries listed below
Sorting:
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆79Updated this week
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆247Updated 4 months ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆154Updated last week
- Web application for multidisciplinary design analysis and optimization☆33Updated 2 months ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆173Updated last month
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆53Updated 3 months ago
- OpenMDAO solvers and drivers to handle specific methods.☆12Updated 4 months ago
- Stripped down version of XFOIL as compiled python module☆109Updated 4 years ago
- Multiphysics with OpenMDAO☆117Updated last month
- 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…☆76Updated 4 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…☆27Updated this week
- XDSM generator written in javascript.☆12Updated last year
- The Python XFOIL optimization toolbox can be used to optimize airfoils for a specific operating range, and might be useful to you for its…☆50Updated 8 years ago
- A python library for generating PDF XDSM diagrams.☆71Updated 5 months ago
- Blade Element Momentum Method for Propellers and Turbines☆77Updated 2 months ago
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 years ago
- Multidisciplinary Airplane Research Integrated Library☆11Updated 6 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆136Updated this week
- ☆40Updated 3 weeks ago
- NASA's aircraft analysis, design, and optimization tool☆250Updated this week
- Aeroelastic Aircraft Design and Simulation Tool☆29Updated 7 years ago
- MACH: MDO of Aircraft Configurations with High fidelity☆149Updated 3 months ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆81Updated 3 years ago
- ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.☆293Updated 2 months ago
- A pre/post processor for PANAIR☆21Updated 5 years ago
- CPACS - Common Parametric Aircraft Configuration Schema☆98Updated 2 weeks ago
- Numerical Manufacturing And Design Tool (NuMAD) -- A design tool for wind and water turbine composite blades☆39Updated 2 years ago
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆42Updated 2 months ago
- A python based blade parametrization tool☆71Updated last year
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆79Updated last year