VahanaOpenSource / vtol_sizing
conceptual design of vtol platforms
☆14Updated 6 years ago
Alternatives and similar repositories for vtol_sizing
Users that are interested in vtol_sizing are comparing it to the libraries listed below
Sorting:
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆40Updated last month
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆40Updated 2 months ago
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆19Updated 3 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…☆22Updated 3 months ago
- ☆38Updated last month
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆64Updated this week
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆31Updated 8 months ago
- Multiphysics with OpenMDAO☆102Updated last week
- Aeroelastic Composite Beam Analysis Tool☆17Updated 8 years ago
- Turbomachinery Blade and Flow path design tool☆44Updated 3 weeks ago
- Blade Element Momentum Method for Propellers and Turbines☆67Updated 3 weeks ago
- A Python module for modeling airfoils☆36Updated last year
- This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil☆10Updated 2 months ago
- Vortex Lattice for Aeroelasticity☆12Updated 7 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆45Updated 2 years ago
- Stripped down version of XROTOR as compiled python module☆22Updated 2 years ago
- Vortex lattice method for inviscid lifting-surface aerodynamics☆43Updated 5 months ago
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆16Updated 6 years ago
- An implementation of the vortex-lattice method (VLM)☆31Updated last year
- A Glyph script demonstrating how to automate viscous meshing for aircraft geometry.☆23Updated 2 months ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆66Updated 2 years ago
- Stripped down version of XFOIL as compiled python module☆99Updated 3 years ago
- XDSM generator written in javascript.☆12Updated 10 months ago
- OpenMDAO 2020 Reverse Hackathon☆14Updated 8 months ago
- High-aspect-ratio composite wing nonlinear aeroelastic toolbox☆15Updated 5 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆105Updated this week
- Aeroelastic Aircraft Design and Simulation Tool☆27Updated 7 years ago
- Scripts for Dynamics of Flexible Aircraft☆20Updated last month
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆25Updated last month