MIT-LAE / pyNA
the python Noise Assessment tool to assess aircraft noise during take-off and landing operations
☆20Updated last year
Related projects ⓘ
Alternatives and complementary repositories for pyNA
- A semi-empirical code for modeling the acoustics of propellers and turbines☆13Updated last year
- Tools for computational aeroacoustics☆16Updated 4 months ago
- Blade Element Momentum Method for Propellers and Turbines☆59Updated 2 months ago
- Collection of Python functions for prediction of turbulence-flat plate interaction noise using Amiet's model☆16Updated 2 years ago
- ☆29Updated 3 months ago
- Meshless large eddy simulation through the reformulated vortex particle method☆76Updated this week
- ☆16Updated 2 months ago
- A Comprehensive Julia implementation of the Vortex Lattice Method☆49Updated last week
- ☆14Updated last year
- Medium fidelity aircraft-propulsion system design and optimization.☆28Updated last week
- Vortex lattice method for inviscid lifting-surface aerodynamics☆42Updated last week
- Pure Julia Implementation of Geometrically Exact Beam Theory☆90Updated 3 months ago
- A toolbox meant for aircraft design analyses.☆43Updated 5 months ago
- Julia wrapper to OpenMDAO☆18Updated 9 months ago
- Three-dimensional panel method for low-speed aerodynamics☆27Updated this week
- Multiphysics with OpenMDAO☆49Updated 3 months ago
- Wind farm tools based in Julia☆16Updated 4 months ago
- Marine Hydrodynamics☆28Updated 2 years ago
- Stripped down version of XROTOR as compiled python module☆17Updated last year
- Three-dimensional panel method for high-Reynolds aerodynamics.☆12Updated 3 years ago
- A lightweight boundary element method library for hydrodynamics and aerodynamics.☆9Updated last month
- A Julia package for Aeroacoustics☆27Updated 5 months ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆54Updated this week
- ezaero - Easy aerodynamics in Python☆31Updated 4 years ago
- Models for commercial aircraft design☆25Updated 4 years ago
- Blade element momentum theory approach to calculate blade forces at varying inflow angles☆9Updated 5 years ago
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆40Updated 4 years ago
- Jupyter Notebooks for AE6310: Optimization for the Design of Engineering Systems☆14Updated 11 months ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆36Updated 4 months ago