Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
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Updated
May 23, 2024 - Python
Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
Flight mechanics utils
This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL)
This paper graphically presents the evolutions of several variables during the re-entry of two types of vehicles: Ballistic and Supporters
Flight mechanics atmospheric reentry study for ballistic capsules and lifting vehicles
Study of the dynamics of atmospheric reentry
Python package to compute the characteristics of an airplane or an airfoil based on simple flight mechanics equations.
Professional MATLAB/Simulink implementation of the longitudinal flight dynamics of the Cessna 172S Skyhawk.
A comprehensive introduction to the principles governing the flight performance of fixed-wing aircraft, aimed at undergraduate students in aerospace engineering.
MATLAB-based glider design and trajectory simulation for maximum range under fixed design constraints.
Rocket Simulation is a real-time 3D rocket flight simulator that models realistic physics, including thrust, drag, gravity, and fuel consumption. Users can control rocket parameters, explore atmospheric layers, and monitor flight data in an interactive 3D environment built with Three.js and Vite.
Calcolatore prestazioni di decollo e atterraggio per aeromobili — metodo di integrazione numerica di Meccanica del Volo
MATLAB flight mechanics mission simulation and aircraft performance study
Conceptual aircraft design and flight mechanics analysis developed with OpenVSP and MATLAB.
Parametric study of the vertical rise of a Rocket
Python-based tool for preliminary aircraft performance analysis including range, endurance, lift, drag, and flight dynamics.
A Python-based Aircraft Flight Performance Simulator for aerodynamic analysis, aircraft performance calculations, and flight mechanics.
This project was done as part of a Master's Thesis by Reggie Johanes at the Faculty of Aerospace Engineering, TU Delft. For a complete report please refer to the TU Delft repository link below.
Aircraft mission analysis: climb/cruise/descent simulation, implicit trim solving, and payload-range sizing in Python
Project developed for 220027 course at ESEIAAT-UPC during fall 2021. Submitted for grading on dec. 19th, but will still be updated in the following months.
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