Carlos Xisto
Mer information om Carlos Xisto hittar du på Chalmers engelska sidor.
Visar 56 publikationer
Moving towards TRL 3 Intercooling Integration for Hydrogen Fueled Aircraft
GENERALIZED METHOD FOR THE CONCEPTUAL DESIGN OF COMPACT HEAT EXCHANGERS
EXPERIMENTAL AND NUMERICAL STUDY ON THE EFFECT OF OGV CLOCKING ON ICD PERFORMANCE
Generalized Method for the Conceptual Design of Compact Heat Exchangers
Compact Heat Exchangers with Curved Fins for Hydrogen Turbofan Intercooling
The heat transfer potential of compressor vanes on a hydrogen fueled turbofan engine
Compact heat exchangers for hydrogen-fueled aero engine intercooling and recuperation
LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS
Compact Heat Exchangers With Curved Fins for Hydrogen Turbofan Intercooling
Analysis of Blade Aspect Ratio’s Influence on High-Speed Axial Compressor Performance
A brief introduction to Aeronautics
MODELLING A HYDROGEN FUELLED COMPOSITE CYCLE AEROENGINE
Lessons Learned from Project Based Teaching in Aerospace at Chalmers
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
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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Visar 9 forskningsprojekt
EXperimental Aircraft for European Leadership In Aviation (EXAELIA)
FläktAlternativ för Nästa Generations motorer 2 (FANG2)
Minimum environmental impact ultra-efficient cores for aircraft propulsion
Pathways for a sustainable introduction of hydrogen into the aviation sector
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)