convexengineering / SPaircraft
Models for commercial aircraft design
☆25Updated 4 years ago
Related projects ⓘ
Alternatives and complementary repositories for SPaircraft
- This is where the tutorial scripts live☆22Updated 2 years ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆36Updated 3 months ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆53Updated last week
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- Vortex lattice method for inviscid lifting-surface aerodynamics☆41Updated last month
- Modified USAF Aircraft DATCOM☆20Updated 12 years ago
- Blade Element Momentum Method for Propellers and Turbines☆58Updated last month
- ☆29Updated 2 months 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
- OpenMDAO 2020 Reverse Hackathon☆14Updated 2 months ago
- A python library for generating PDF XDSM diagrams.☆59Updated 11 months ago
- Stripped down version of XROTOR as compiled python module☆17Updated last year
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆19Updated 2 months ago
- A Python module for modeling airfoils☆30Updated 11 months ago
- A python interface for DATCOM. Provides export/ parsing capabilities.☆27Updated 12 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆32Updated this week
- A pre/post processor for PANAIR☆14Updated 3 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆77Updated 2 weeks ago
- ezaero - Easy aerodynamics in Python☆31Updated 4 years ago
- Future Aircraft Sizing Tool☆63Updated this week
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆15Updated 5 years ago
- ☆37Updated last year
- An OpenMETA model for the conceptual design of an autonomous transport aircraft, inspired by Vahana from A^3 by Airbus.☆12Updated 3 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆38Updated 2 years ago
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆39Updated 4 years ago
- An implementation of the vortex-lattice method (VLM)☆25Updated last year
- A Glyph script demonstrating how to automate viscous meshing for aircraft geometry.☆22Updated 3 years ago
- conceptual design of vtol platforms☆13Updated 5 years ago
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆23Updated last year