geoffreynyaga / Kenya-One-Project
Aircraft Conceptual Design Software
☆32Updated 2 years ago
Alternatives and similar repositories for Kenya-One-Project:
Users that are interested in Kenya-One-Project are comparing it to the libraries listed below
- CEASIOMpy is a Python conceptual aircraft design environment☆85Updated this week
- A python wrapper of the Panair/A502 panel code.☆14Updated 2 years ago
- Vortex lattice method for inviscid lifting-surface aerodynamics☆42Updated 2 months ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆62Updated 2 years ago
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆16Updated 5 years ago
- A Python module for modeling airfoils☆34Updated last year
- An object-oriented Python 3 GUI and API for single- and multi-element parametric airfoil design, analysis, and optimization☆17Updated this week
- Fast and accurate aerodynamic modeling using general numerical lifting-line theory.☆105Updated 8 months ago
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- ✈️ Aircraft Design Tool☆24Updated last year
- A pre/post processor for PANAIR☆14Updated 4 years ago
- Simple GUI for PROFOIL☆14Updated 4 months ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆38Updated 2 weeks ago
- Aircraft Design Recipes in Python☆109Updated 10 months ago
- ☆31Updated 2 weeks ago
- Airfoil optimization with Xfoil☆50Updated 3 years ago
- Aeroelastic Aircraft Design and Simulation Tool☆25Updated 6 years ago
- An implementation of the vortex-lattice method (VLM)☆28Updated last year
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆60Updated this week
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆200Updated this week
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆38Updated 4 years ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆19Updated 2 years ago
- Aircraft Design Resources - aircraft conceptual design framework☆14Updated 4 years ago
- conceptual design of vtol platforms☆13Updated 6 years ago
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆73Updated 9 months ago
- CPACS - Common Parametric Aircraft Configuration Schema☆81Updated last month
- ☆47Updated 4 years ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆37Updated 7 months ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆131Updated 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…☆69Updated 3 years ago