A python library for the design and development of turbomachinery in rocket applications.
TurboRocket is a python library enabling the design of turbomachinery components for liquid rocket propulsion systems.
The main goal of this project is to create a set of tools that can be used by designers to create simplified models to assess turbomachinery performance.
Use the package manager pip to install the TurboRocket library.
pip install turboRocket# Need to fill this out at somepoint describing an example use case for the turboRocket library.Pull requests are more than welcome. If major changes are intended, please open an issue thread to discuss the change.
As of current, github issues are being internally used to develop core functionality of the library.
Key contributors to this library are:
- Elias Aoubala (
EliasAoubala) - Craig Orrock