Carlos Xisto
I'm an 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 aero-engines for mid-century applications with special interest in hydrogen powered propulsion systems. 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.
Showing 45 publications
The heat transfer potential of compressor vanes on a hydrogen fueled turbofan engine
Compact heat exchangers for hydrogen-fueled aero engine intercooling and recuperation
Fan Stage Design and Performance Optimization for Low Specific Thrust Turbofans
FAN STAGE DESIGN AND PERFORMANCE OPTIMIZATION FOR LOW SPECIFIC THRUST TURBOFANS
Development of an aerodynamic analysis tool for boundary layer ingestion concept design
Design and performance of liquid hydrogen fueled aircraft for year 2050 EIS
Multipoint aerodynamic design of ultrashort nacelles for ultrahigh-bypass-ratio engines
DESIGN AND PERFORMANCE OF LIQUID HYDROGEN FUELLED AIRCRAFT FOR YEAR 2050 EIS
Numerical modeling of laminar-turbulent transition in an interconnecting compressor duct
MULTIPOINT AERODYNAMIC DESIGN OF A NACELLE FOR AN ELECTRIC FAN
Multidisciplinary assessment of a year 2035 turbofan propulsion system
Effect of heat exchanger integration in aerodynamic optimization of an aggressive S-duct
EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT
Estimation of Design Parameters and Performance for a State-of-the-Art Turbofan
Techno-economic review of alternative fuels and propulsion systems for the aviation sector
Conceptual Design of a Compressor Vane- HEX for LH2 Aircraft Engine Applications
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
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
Aeroelastic Analysis of a Cycloidal Rotor Under Various Operating Conditions
The Efficiency of a Pulsed Detonation Combustor-Axial Turbine Integration
Assessment of CO2 and NOx emissions in intercooled pulsed detonation turbofan engines
First and Second Law Analysis of Radical Intercooling Concepts
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
Scale effects on conventional and intercooled turbofan engine performance
A Search for the “ULTIMATE” Aero-Engine
An outlook for radical aero engine intercooler concepts
Numerical Computations of MHD Flow on Hypersonic and Re-Entry Vehicles
Design of an innovative off road hybrid vehicle by energy efficiency criteria
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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Showing 7 research projects
Fan Alternatives for Next Generation engines 2 (FANG2)
Minimum environmental impact ultra-efficient cores for aircraft propulsion
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)