cfsengineering / CEASIOMpy
CEASIOMpy is a Python conceptual aircraft design environment
☆86Updated last week
Alternatives and similar repositories for CEASIOMpy:
Users that are interested in CEASIOMpy are comparing it to the libraries listed below
- 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
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆61Updated this week
- Stripped down version of XFOIL as compiled python module☆94Updated 3 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆63Updated 2 years ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆131Updated last week
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆16Updated 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…☆43Updated 7 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆41Updated 2 years ago
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- An implementation of the vortex-lattice method (VLM)☆30Updated last year
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆203Updated last week
- NASA's aircraft analysis, design, and optimization tool☆170Updated this week
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆39Updated this week
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆73Updated 10 months ago
- Aeroelastic Aircraft Design and Simulation Tool☆25Updated 6 years ago
- ☆33Updated 3 weeks ago
- The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…☆18Updated last month
- Multiphysics with OpenMDAO☆95Updated last month
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆90Updated this week
- CPACS - Common Parametric Aircraft Configuration Schema☆82Updated this week
- MACH: MDO of Aircraft Configurations with High fidelity☆123Updated last month
- Blade Element Momentum Method for Propellers and Turbines☆64Updated 2 weeks ago
- Source and vortex panel method codes referenced in my YouTube videos.☆92Updated 4 years ago
- A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superli…☆47Updated last year
- Some usefull routines for aeroelastic analysis with NASTRAN.☆19Updated 2 years ago
- Turbomachinery Blade and Flow path design tool☆35Updated this week
- OpenFOAM case files for simulating NACA foils.☆48Updated 2 weeks ago
- ezaero - Easy aerodynamics in Python☆32Updated 4 years ago
- Stripped down version of XROTOR as compiled python module☆18Updated 2 years ago
- A Python module for modeling airfoils☆34Updated last year