Carlos Xisto
I'm a Senior Researcher (associate professor) at the Division of Fluid Dynamics, Dep. of Mechanics and Maritime Sciences. My main research interest revolves around the development of radical propulsion concepts for aerospace. My main fields of expertise include compressible flow, computational fluid dynamics, turbomachinery, gas turbine performance, pulsed detonation combustion, plasma dynamics, and magnetohydrodynamics. I'm actively engaged in the investigation of novel concepts of gas turbine engines for mid-century applications. I am also supervising the development of magnetohydrodynamic and plasma dynamic numerical models, to predict the generation and manipulation of weakly ionized plasma flow in hypersonic aircraft or re-entry vehicles. My ambition is to take part in the development of concepts that could significantly improve the efficiency of air transport and contribute to a sustainable and greener future in aviation.
Visar 23 publikationer
Development of fuel and heat management systems for liquid hydrogen powered aircraft
Feasibility Study of a Radical Vane-Integrated Heat Exchanger for Turbofan Engine Applications
Conceptual Design of a Compressor Vane- HEX for LH2 Aircraft Engine Applications
Assessment of CO2 and NOx emissions in intercooled pulsed detonation turbofan engines
Concetual design of ultra-efficient cores for mid-century aircraft turbine engines
Aeroelastic Analysis of a Cycloidal Rotor Under Various Operating Conditions
The Efficiency of a Pulsed Detonation Combustor-Axial Turbine Integration
First and Second Law Analysis of Radical Intercooling Concepts
Assessment of CO2 and NOx emissions in intercooled pulsed detonation turbofan engines
Numerical analysis of a multi-species MHD model for plasma layer control of re-entry vehicles
Scale effects on conventional and intercooled turbofan engine performance
Parametric Analysis of a Large-scale Cycloidal Rotor in Hovering Conditions
First and second law analysis of radical intercooling concepts
Analytical model for the performance estimation of pre-cooled pulse detonation turbofan engines
A Search for the “ULTIMATE” Aero-Engine
Design of an innovative off road hybrid vehicle by energy efficiency criteria
An outlook for radical aero engine intercooler concepts
Numerical Computations of MHD Flow on Hypersonic and Re-Entry Vehicles
Ultra low emission technology innovations for mid-century aircraft turbine engines
Temperature Oscillations in the Wall of a Cooled Multi Pulsejet Propeller for Aeronautic Propulsion
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Visar 5 forskningsprojekt
IMOTHEP - Investigation and Maturation of Technologies for Hybrid Electric Propulsion
Enabling cryogenic hydrogen-based CO2-free air transport (ENABLEH2)
Virtuell Integrerad Demonstrator för turbomaskiner (VIND)
Ultra Low emission Technology Innovations for Mid-century Aircraft Turbine Engines (ULTIMATE)
Engine Module Validators (ENOVAL)