arktools / pydatcom
A python interface for DATCOM. Provides export/ parsing capabilities.
☆27Updated 12 years ago
Related projects: ⓘ
- Vortex Lattice Method library written in Python☆41Updated 4 years ago
- This is where the tutorial scripts live☆22Updated 2 years ago
- Creates a 3D model of a Digital DATCOM compatible aircraft in Matlab☆17Updated 2 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆70Updated last month
- ☆10Updated this week
- Modified USAF Aircraft DATCOM☆20Updated 12 years ago
- An implementation of the vortex-lattice method (VLM)☆25Updated last year
- Aircraft Design Recipes in Python☆98Updated 5 months ago
- Future Aircraft Sizing Tool☆44Updated this week
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆15Updated 5 years ago
- A fully-featured flight simulator, capable of real-time lifting-line aerodynamic modelling.☆48Updated 2 years ago
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆68Updated 4 months ago
- Fast and accurate aerodynamic modeling using general numerical lifting-line theory.☆92Updated 3 months ago
- PyAVL is a python based gui interface to the Athena Vortex Lattice (AVL) program for aerodynamic and other analysis☆11Updated 12 years ago
- Codes related to the analysis, design, and optimization of on-demand, electric vertical-takeoff-and-landing aircraft. A preprint of an up…☆33Updated 4 years ago
- 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…☆61Updated 3 years ago
- Based on the 1976 USAF STABILITY AND CONTROL DIGITAL DATCOM PROGRAM, the tool is designed to provide a simpler AND more convenient form i…☆21Updated 2 years ago
- Stripped down version of XROTOR as compiled python module☆16Updated last year
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆57Updated last year
- A pre/post processor for PANAIR☆13Updated 3 years ago
- Stripped down version of XFOIL as compiled python module☆87Updated 3 years ago
- Python Version of MachUp (Numerical Lifting-Line Method)☆18Updated 5 years ago
- xflrpy is a python enabled version of xflr5 for scripting and design optimization.☆46Updated last year
- This project contains the UNIFIER19 C7A-HARW aircraft Flight Dynamics Simulator Simulink model and XPlane-11 model.☆24Updated 3 months ago
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆38Updated 4 years ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆192Updated last month
- ezaero - Easy aerodynamics in Python☆30Updated 3 years ago
- A python wrapper of the Panair/A502 panel code.☆14Updated 2 years ago