

Aerothermal Engineer with a PhD from ETH Zurich and 5+ years of expertise in turbine aerothermal systems, CFD modeling, gas dynamics, and combustion design applying for Aerothermal Engineer position (UR631210) at Rolls-Royce, Derby. Proven expertise in optimizing turbine combustors for hybrid power systems (SOFC/MGT), reducing emissions through advanced CFD and experimental validation. Skilled in 1D-3D computational tools (ANSYS Fluent, Chemkin), thermal modeling, and cross-disciplinary collaboration. Published in Combustion and Flame and Proc. Combust. Inst., with a focus on turbine-relevant aerothermal challenges. Seeking to leverage expertise in fluid mechanics and thermodynamics to enhance Rolls-Royce’s turbine aerothermal capabilities.
Actively pursuing Chartered Engineer status (Institution of Mechanical Engineers).
EU funded Hestia Project -2025 to 2026
EU funded NEXTMGT Project -2020 to 2024