Aircraft design optimization made fast through computational graph transformations (e.g., automatic differentiation). Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.

NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, exposed to end-users in pure Python/NumPy.

Aerodynamic models of 3D wings using the Vortex Step Method

A mid-fidelity 3D free-wake solver for propellers, more accurate than BEMT. It simulates full wake development via a user-friendly GUI.

Flight Dynamics Project - UAV

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.

Coaxial Helicopter Design for Helicopter Emergency Medical Services (HEMS) Operations

Assignment Submission for the System Identification of Aerospace Vehicle (AE4320) course. Two Step Approach to Identify Aerodynamic Model - State Estimation and Parameter Estimation

Vectorial fields in fluids simulator.

CR25 SpaceConcordia 2025 solid rocketry project: a non-ordinary transition rocket due to new design required in-depth analysis. CFD simulation using OpenFOAM had been conducted to analyze aerodynamic forces on the airframe in different Angle of Attacks and Speeds

The project aims to simulate a rocket flight from ground to the Earth orbit

Machine learning-assisted optimisation of shuttlecock porosity using Gaussian Process Regression and Bayesian optimisation

Focused on the development of a simulator that simplifies and simulates the behaviour of an AeroSail system

Post-Processing tool for 2D steady-state CFD solutions based on unstructured grids.

An interactive 3D WebGL application that accelerates aerodynamic shape evaluation by comparing a traditional 3D CFD (Computational Fluid Dynamics) Solver side-by-side with an Instant SciML (Scientific Machine Learning) Neural Surrogate.

Aynı Ailden 2 Şok Dalgasının Kesişmesi Sonucu Oluşacak Akışın Genel Özelliklerini Hesaplamaktadır.

3D Vortex Lattice Method (VLM) implementation for a swept, tapered wing with elliptical loading comparison.

This project is about the determination and simulation of enviromental disturbances for a 1U CubeSat.

Python-based ODE solver for multi-stage rocketry, featuring automated risk assessment and impact distribution statistics.