usuaero / panairwrapper
A python wrapper of the Panair/A502 panel code.
☆14Updated 2 years ago
Alternatives and similar repositories for panairwrapper:
Users that are interested in panairwrapper are comparing it to the libraries listed below
- A pre/post processor for PANAIR☆14Updated 4 years ago
- An implementation of the vortex-lattice method (VLM)☆30Updated last year
- Stripped down version of XROTOR as compiled python module☆18Updated 2 years ago
- ☆33Updated 3 weeks ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆63Updated 2 years ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆19Updated 3 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆86Updated last week
- 3D Vortex Panel Method☆15Updated 8 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆38Updated this week
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆41Updated 2 years ago
- High-aspect-ratio composite wing nonlinear aeroelastic toolbox☆15Updated 5 years ago
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆38Updated 4 years ago
- Aeroelastic Aircraft Design and Simulation Tool☆25Updated 6 years ago
- Generate volume meshes for OpenVSP generated surface meshes.☆27Updated 3 years ago
- An archive of the programs provided by Joseph Katz and Allen Plotkin in their book Low-Speed Aerodynamics☆15Updated last year
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆23Updated last year
- Generate and plot the contour of an airfoil using the PARSEC parameterization☆17Updated 10 years ago
- ☆24Updated 6 years ago
- Aeroelastic Composite Beam Analysis Tool☆17Updated 8 years ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆39Updated this week
- 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…☆69Updated 3 years ago
- Blade Element Momentum Method for Propellers and Turbines☆64Updated 2 weeks ago
- Turbomachinery Blade and Flow path design tool☆35Updated this week
- Converter utility to convert APC PE0 files to OpenVSP BEM format☆20Updated 2 years ago
- A Python module for modeling airfoils☆34Updated last year
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆23Updated last year
- ☆47Updated 6 years ago
- Stripped down version of XFOIL as compiled python module☆94Updated 3 years ago
- Multiphysics with OpenMDAO☆96Updated last month
- Computational Aerodynamics Lab☆23Updated 4 years ago