usuaero / MachLine
A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
☆40Updated last month
Alternatives and similar repositories for MachLine:
Users that are interested in MachLine are comparing it to the libraries listed below
- ☆37Updated 3 weeks ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆19Updated 3 years ago
- ☆49Updated 4 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆44Updated 2 years ago
- A Python module for modeling airfoils☆36Updated last year
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆30Updated 7 months ago
- Blade Element Momentum Method for Propellers and Turbines☆65Updated 2 weeks ago
- Multiphysics with OpenMDAO☆100Updated this week
- A pre/post processor for PANAIR☆15Updated 4 years ago
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆24Updated this week
- conceptual design of vtol platforms☆14Updated 6 years ago
- ☆49Updated 7 years ago
- Vortex lattice method for inviscid lifting-surface aerodynamics☆43Updated 4 months ago
- Stripped down version of XROTOR as compiled python module☆21Updated 2 years ago
- Python tool to genreate 2D meshes around airfoils☆31Updated 2 weeks ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆40Updated last week
- High-aspect-ratio composite wing nonlinear aeroelastic toolbox☆15Updated 5 years ago
- Aeroelastic Composite Beam Analysis Tool☆17Updated 8 years ago
- An implementation of the vortex-lattice method (VLM)☆31Updated last year
- CEASIOMpy is a Python conceptual aircraft design environment☆95Updated this week
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆23Updated last year
- Post-processing framework to predict rotor noise using PSU-WOPWOP from CAMRAD II simulation results☆14Updated last month
- Turbomachinery Blade and Flow path design tool☆43Updated last week
- This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil☆10Updated last month
- ezaero - Easy aerodynamics in Python☆33Updated 4 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆65Updated 2 years ago
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…☆20Updated 2 months ago
- Converter utility to convert APC PE0 files to OpenVSP BEM format☆21Updated 2 years ago
- MACH: MDO of Aircraft Configurations with High fidelity☆125Updated 2 weeks ago