VahanaOpenSource / vtol_sizingLinks
conceptual design of vtol platforms
☆17Updated 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:
- The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…☆26Updated last week
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆51Updated 2 weeks ago
- ☆38Updated last week
- CEASIOMpy is a Python conceptual aircraft design environment☆129Updated last week
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆45Updated 8 months ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆74Updated this week
- Turbomachinery Blade and Flow path design tool☆65Updated last month
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆19Updated 6 years ago
- The Python XFOIL optimization toolbox can be used to optimize airfoils for a specific operating range, and might be useful to you for its…☆48Updated 8 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆52Updated 3 years ago
- Vortex Lattice for Aeroelasticity☆13Updated 8 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆73Updated 3 years ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆168Updated 3 weeks ago
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆38Updated 5 months ago
- Aeroelastic Composite Beam Analysis Tool☆19Updated 9 years ago
- Vortex Lattice Method library written in Python☆42Updated 6 years ago
- 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…☆74Updated 4 years ago
- Stripped down version of XFOIL as compiled python module☆105Updated 4 years ago
- Aeroelastic Aircraft Design and Simulation Tool☆29Updated 7 years ago
- Some usefull routines for aeroelastic analysis with NASTRAN.☆21Updated 3 years ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆239Updated last month
- This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil☆14Updated 8 months ago
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 years ago
- A pre/post processor for PANAIR☆18Updated 4 years ago
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆40Updated this week
- CPACS - Common Parametric Aircraft Configuration Schema☆97Updated last month
- NASA's aircraft analysis, design, and optimization tool☆235Updated 2 weeks ago
- A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superli…☆58Updated 3 months ago
- Multiphysics with OpenMDAO☆112Updated 2 months ago
- MACH: MDO of Aircraft Configurations with High fidelity☆145Updated 2 weeks ago