SLOSH-ML is a Matlab graphical user interface designed to analyze rocket propellant sloshing in space launch vehicles

Interactive courseware that introduces foundational-level concepts as taught in introductory courses in fluid mechanics.

Simple software created to quickly output aircraft landing gear design geometry during a year long iterative design process. This allowed for complex trade off analysis with other design team members.

A program to calculate the parameters of a turbofan engine (Matlab).

FEM of dynamic beams

Numerical and Analytical Flow Solution over Joukowski Aerofoil, Using O-grid Meshing Method and PSOR solving algorithm.

Developed a missile guidance and ballistic control system for autonomous mid-air and surface-to-air target chase and interception

This repository contains the source code for a modified Beddoes-Leishman dynamic stall model

Programi iz knjige Stajni trap letelica.

My matlab code (Numerical Analysis, Simulation)

PteraControls is a tool for designing control systems for flapping wing vehicles.

The study aims to develop a preliminary design of a fixed-wing aerodyne (Business Jet) able to carry a reduced number of people in intercontinental flights at the maximum possible Mach number.

Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.

Algorithms regarding spacecraft attitude determination and control.

Educational Vibration programs for Octave. Intended for undergraduate and early graduate students.

Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink

Simple J2 propagator modeled in Simulink