Publication: "Toward Radar Cross Section Prediction in Hypersonic Plasma Environments: A Preliminary Assessment Under Variable Flight Conditions", Proceedings of the International Conference on Fluid Dynamics and Electromagnetic Characterization (2026).
05/2025 – 06/2025, Staged Combustion Cycle Preliminary Sizing, Analysis of propulsive performance and preliminary sizing of a liquid rocket engine using a fuel-rich staged combustion cycle.,
09/2025 – 10/2025, 2D NACA 4412 Airfoil Trailing Edge Separation, Study on turbulence modeling for separated flow over an airfoil, with validation against experimental and high-fidelity reference data.,
02/2025 – 03/2025, Backward-facing step flow, Investigation of flow expansion in a duct with backward-facing step, analyzing the influence of domain geometries and Reynolds numbers.,
10/2024 – 12/2024, Analysis and simulation of aircraft dynamic behavior., The work focuses on the analysis and simulation of aircraft dynamics, with the aim of understanding the behavior of the vehicle under different flight conditions and evaluating its stability and performance.,
07/2024 – 09/2024, Experimental analysis of ceramic diborides in a plasma wind tunnel, The thesis investigates the behavior of sintered ceramic diborides exposed to high-enthalpy flows for potential use in hypersonic thermal protection systems. Experiments were performed in the SPES plasma wind tunnel at Mach 3 and up to 15 MJ/kg, using non-intrusive diagnostics to measure surface temperatures. The work includes a comparative analysis of two material compositions and a preliminary assessment of high-enthalpy effects on their surfaces.