OpenMDAO / RevHack2020Links
OpenMDAO 2020 Reverse Hackathon
☆15Updated last year
Alternatives and similar repositories for RevHack2020
Users that are interested in RevHack2020 are comparing it to the libraries listed below
Sorting:
- Multidisciplinary Airplane Research Integrated Library☆11Updated 5 years ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆69Updated last week
- ☆16Updated last month
- Scripts for Dynamics of Flexible Aircraft☆20Updated 4 months ago
- ☆22Updated 2 weeks ago
- Stripped down version of XFOIL as compiled python module☆103Updated 4 years ago
- A finite element method for beam-like structures.☆12Updated 2 months ago
- An implementation of the vortex-lattice method (VLM)☆36Updated 2 years ago
- The Python XFOIL optimization toolbox can be used to optimize airfoils for a specific operating range, and might be useful to you for its…☆48Updated 8 years ago
- A python library for generating PDF XDSM diagrams.☆67Updated this week
- 2-dimensional airfoil aerodynamics library☆13Updated 2 years ago
- ☆39Updated 5 months ago
- ☆13Updated last year
- CPACS - Common Parametric Aircraft Configuration Schema☆93Updated 3 months ago
- Blade Element Momentum Method for Propellers and Turbines☆70Updated last week
- Models for commercial aircraft design☆25Updated 5 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆70Updated 2 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆45Updated 6 months ago
- CEASIOMpy is a Python conceptual aircraft design environment☆116Updated last month
- A pre/post processor for PANAIR☆17Updated 4 years ago
- Web application for multidisciplinary design analysis and optimization☆31Updated this week
- The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…☆26Updated this week
- ezaero - Easy aerodynamics in Python☆33Updated 4 years ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆160Updated 2 months ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆126Updated last month
- Ducted Axisymmetric Propulsor Evaluation☆13Updated last week
- MACH: MDO of Aircraft Configurations with High fidelity☆136Updated this week
- 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…☆73Updated 4 years ago
- ☆12Updated last week
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆46Updated last month