Educational Vibration programs. Intended for undergraduate and early graduate students.
An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil
A comprehensive solution for designing and optimizing student-built liquid rocket engines.
GELATO: GEneric LAunch Trajectory Optimizer
Bolted Joint Stress Field Model
Basic ISA Calculator for Python projects
A Python implementation of the 1976 standard atmosphere model. Suitable to determine air properties at different altitudes.
A curated list of tools, frameworks, resources, and educational content for Aerospace Engineering.
Fatigue and fracture package
Structural analysis of the aileron of a Boeing 737
A python repository for compressible aerodynamics
Script de monitoramento de telemetria para missões espaciais, cansat e foguetemodelismo.
The program developed helps to identify aircraft with its position, velocity and flight information to detect aircraft in breach of Air Law over a controlled Airspace (London) using ADS-B data streams
Black-Box optimization of a rotor's shape using Projected Gradient Descent
This is a full cycle code for the PT6A-114 engine. The code was developed for AERO 417 Aerospace Propulsion. In this repository, you will find the code for the engine, as well as the basic engine specs and code results
A series of Python-based tools useful for the analysis of satellite missions.
This is an attempt to develop a code to obtain the reentry trajectory of a space vehicle which a certain velocity, altitude and rentry angle. There are many thing that can be included to make this more sophisticated and changes to obtain more accurate and real life results.
Hohmann transfer orbit modeling with Hall-Effect thruster integration, implemented in Python, C++ and MATLAB with 3D visualization and validated delta-V calculations for LEO to GEO missions
An implementation of the method of characteristics for supersonic nozzle design written in Python.
JARVIS provides a graphical user interface for simulating rocket launches. Users can input various parameters related to the rocket's mass, drag coefficient, cross-sectional area, air density, and motor burn time. The application runs the simulation and visualizes the results, including altitude and velocity over time.
Add a description, image, and links to the aerospace-engineering topic page so that developers can more easily learn about it.
To associate your repository with the aerospace-engineering topic, visit your repo's landing page and select "manage topics."