Msc Research Student
• Conducted in-depth investigation into the merits of hybrid and/or distributed propulsion systems in aircraft, focusing on the integration of power management for adding or subtracting significant power from the engine at various points in the flight envelope.• Utilized PROOSIS to model and analyze the design-point and off-design gas turbine thermal performance of NASA's N+3 Engine, contributing to the evaluation of its efficiency and effectiveness in real-world operating conditions.• Integrated the N+3 Engine into the NASA STARC ABL aircraft and conducted a comprehensive comparative analysis to identify the advantages and assess the performance of the integrated system, demonstrating strong skills in system integration, performance evaluation, and data analysis.