jgoppert / aae451-notebookLinks
AAE 451 Aircraft Design
☆10Updated 4 years ago
Alternatives and similar repositories for aae451-notebook
Users that are interested in aae451-notebook are comparing it to the libraries listed below
Sorting:
- Blade Element Momentum Method for Propellers and Turbines☆74Updated last month
- Models for commercial aircraft design☆25Updated 5 years ago
- Vortex lattice method for inviscid lifting-surface aerodynamics☆45Updated 4 months ago
- Future Aircraft Sizing Tool☆107Updated last week
- Codes related to the analysis, design, and optimization of on-demand, electric vertical-takeoff-and-landing aircraft. A preprint of an up…☆44Updated 5 years ago
- Three-dimensional panel method for low-speed aerodynamics☆32Updated 2 weeks ago
- ☆38Updated last month
- This is where the tutorial scripts live☆26Updated 3 years ago
- Stripped down version of XFOIL as compiled python module☆107Updated 4 years ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆76Updated 3 weeks ago
- Nonlinear model of F16 flight dynamics.☆44Updated 8 months ago
- Vortex Lattice Method library written in Python☆44Updated 6 years ago
- Aircraft Design Recipes in Python☆127Updated last year
- A fully-featured flight simulator, capable of real-time lifting-line aerodynamic modelling.☆57Updated 3 years ago
- A Comprehensive Julia implementation of the Vortex Lattice Method☆55Updated last month
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆45Updated 10 months ago
- A fun, lightweight tool to visualize potential flows quickly!☆19Updated 11 months ago
- Computational Aerodynamics Lab☆30Updated 5 years ago
- xflrpy is a python enabled version of xflr5 for scripting and design optimization.☆78Updated 2 months ago
- ☆47Updated 3 months ago
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 years ago
- A python library for generating PDF XDSM diagrams.☆71Updated 4 months ago
- A Python module for modeling airfoils☆41Updated 2 years ago
- LOw Reynolds number Aircraft Analysis with Xfoil☆15Updated 5 years ago
- Blade Element Method implementation for propeller calculations.☆14Updated last year
- Fast and accurate aerodynamic modeling using general numerical lifting-line theory.☆122Updated last year
- CEASIOMpy is a Python conceptual aircraft design environment☆134Updated last week
- ezaero - Easy aerodynamics in Python☆33Updated 5 years ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆53Updated last month
- This project contains the UNIFIER19 C7A-HARW aircraft Flight Dynamics Simulator Simulink model and XPlane-11 model.☆25Updated last year