| Name | parafoil JSON |
| Version |
0.0.1
JSON |
| download |
| home_page | None |
| Summary | under development |
| upload_time | 2025-09-07 16:35:01 |
| maintainer | None |
| docs_url | None |
| author | Open Orion |
| requires_python | >=3.8 |
| license | MIT |
| keywords |
|
| VCS |
 |
| bugtrack_url |
|
| requirements |
No requirements were recorded.
|
| Travis-CI |
No Travis.
|
| coveralls test coverage |
No coveralls.
|
<p align="center">
<img src="./assets/logo.svg" alt="drawing" width="500"/>
</p>
<p align="center">the open source parametric airfoil generator</p>
# About
ParaFoil is a declarative tool that parametrically generates turbomachinery and aircraft airfoils and passages with B-splines. The purpose is to generate airfoil shapes from different parameters during fluid simulation optimizations.
# Install
```
pip install git+https://github.com/OpenOrion/parafoil.git#egg=parafoil
```
## Other Versions
```
# Version 1
pip install git+https://github.com/OpenOrion/parafoil.git@1.0.0#egg=parafoil
```
# Example
## Airfoil
```python
import numpy as np
from parafoil import CamberThicknessAirfoil
airfoil = CamberThicknessAirfoil(
inlet_angle=np.radians(40.0),
outlet_angle=np.radians(-20.0),
stagger_angle=np.radians(0.0),
upper_thick_prop=[0.035, 0.14, 0.14, 0.035, 0.007],
lower_thick_prop=[0.035, 0.14, 0.14, 0.035, 0.007],
leading_prop=0.5,
trailing_prop=0.5,
chord_length=1
)
airfoil.visualize(include_camber_ctrl_pnts=True)
```
## Passage
```python
from parafoil import TurboRowPassage
passage = TurboRowPassage(
airfoil=airfoil,
spacing_to_chord=1.0,
leading_edge_gap_to_chord=0.25,
trailing_edge_gap_to_chord=0.25,
)
passage.visualize()
```
# Devlopement Setup
```
git clone https://github.com/OpenOrion/parafoil.git
cd parafoil
pip install -r requirements_dev.txt
```
# Help Wanted
Right now there are some items such as CFD meshing and adding more shaping. Please join the [Discord](https://discord.gg/H7qRauGkQ6) for project communications and collaboration.
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