adeharo9 / NACA-airfoil-generator
Airfoil generator of NACA 4, 5 and 6 Series
☆23Updated 6 years ago
Related projects: ⓘ
- Vortex Lattice Method library written in Python☆41Updated 4 years ago
- An implementation of the vortex-lattice method (VLM)☆25Updated last year
- Stripped down version of XFOIL as compiled python module☆87Updated 3 years ago
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆17Updated 2 weeks ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆37Updated 2 years ago
- A pre/post processor for PANAIR☆13Updated 3 years ago
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆22Updated last year
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆38Updated 4 years ago
- Generate 4 and 5 digit NACA airfoil sections☆34Updated 2 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆57Updated last year
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆15Updated 5 years ago
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆68Updated 4 months ago
- Generate volume meshes for OpenVSP generated surface meshes.☆25Updated 3 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆70Updated last month
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆34Updated 2 months 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…☆61Updated 3 years ago
- Some usefull routines for aeroelastic analysis with NASTRAN.☆17Updated 2 years ago
- Multiphysics with OpenMDAO☆47Updated last month
- 2-dimensional airfoil aerodynamics library☆12Updated last year
- Aeroelastic Composite Beam Analysis Tool☆16Updated 7 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆29Updated 2 weeks ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆48Updated this week
- A MATLAB tool for the mean-line design optimization of axial turbines☆26Updated 3 years ago
- Scripts for Dynamics of Flexible Aircraft☆13Updated 3 months ago
- ☆29Updated last month
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆18Updated 2 years ago
- Stripped down version of XROTOR as compiled python module☆16Updated last year
- conceptual design of vtol platforms☆13Updated 5 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…☆38Updated 7 years ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆192Updated last month