Describe aircraft configurations parametrically with pydantic
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Updated
Jan 15, 2023 - Python
Describe aircraft configurations parametrically with pydantic
Part 21 DOA Design Software written in Tkinter
The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and frequency domain as well as dynamic landing loads based on a generic landing gear module.
A Python script written to perform aircraft weight estimations and inertia calculations
UCSD SE262: Aircraft Structural Repair. Programs used to solve aircraft structural problems.
An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil
Wing optimization
An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
📈 Simulation of an oscillating airfoil
📈 Program that calculates design parameters for an ornithopter in level flight
Aircraft Design Resources - aircraft conceptual design framework
In this repository I publish the python code, that was part of my master thesis. The thesis can be found here, however its in German though, sry. :/
A Python implementation of the 1976 standard atmosphere model. Suitable to determine air properties at different altitudes.
Aircraft Conceptual Design Software
NeuralFoil is an airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
Airframe Finite Element Modeler
Ptera Software is a fast, easy-to-use, and open-source software package for analyzing flapping-wing flight.
CEASIOMpy is a Python conceptual aircraft design environment
NASA's aircraft analysis, design, and optimization tool
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