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 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.
Parametric study of the vertical rise of a Rocket
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.
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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