About
Alex Novoselov serves as Assistant Professor in the Department of Mechanical Engineering at the University of Utah's College of Engineering, specializing in combustion dynamics and sustainable energy systems.
His research encompasses:
- Hydrogen and ammonia combustion for decarbonization
- Turbulent boundary layer flashback phenomena
- Deflagration to detonation transition (DDT)
- Hybrid rocket propulsion systems
- Cool flame dynamics and low-temperature combustion
Recent publications (2020-2025) reveal a strong computational focus using Large Eddy Simulation and manifold-based reduced-order models to address safety challenges in gas turbines and rocket engines. His work increasingly investigates ammonia/hydrogen blends as sustainable aviation fuels while maintaining core expertise in flashback dynamics.
Dr. Novoselov mentors undergraduate researchers through the Summer Program for Undergraduate Research (SPUR), emphasizing project relevance, achievable milestones, and presentation skill development. His NSF CAREER award supports fundamental research on lean hydrogen flame stability in gas turbines.
His computational research group develops advanced simulation frameworks for complex reacting flows, contributing to next-generation propulsion and power generation technologies.
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