This repo contains the architecture for a mid-fidelity wing-propeller optimisation model.
The directory structure is as follow:
Section | Content |
---|---|
docs | References to literature used for the slipstream code |
examples | Example cases |
python_src | Wrapped code for python package, including compiled code |
src | Source cod |
tests | Test suite, using unittest |
Code:
- Python3
- numpy
- OpenMDAO
- RETHORST
- OpenAeroStruct (FORK - JExalto)
- unittest
Copyright (c) 2023 Joaquin Exalto - This repository is licensed with a MIT license and is available as opensource. More information about the license is included within the LICENSE
file.