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Christos Mourouzidis

Lecturer

Cranfield University

United Kingdom

Research Interests

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About

Dr. Christos Mourouzidis is an Associate Professor at Cranfield University, UK. His research focuses on advanced propulsion systems, specifically in the areas of liquid hydrogen and ammonia-powered turbofans, integrated hybrid engine designs, and emissions reduction technologies. He has contributed to significant studies on the design and optimization of aircraft engines for future generations, emphasizing sustainability and performance enhancement.

Articles (12)

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2025

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2025

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2025

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2025

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2025

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2024

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2024

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2024

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2023

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2023

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2022

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2022

Collaborators (4)

David John Rajendran

Lecturer in Aero System Design for Future Propulsion Architectures

Cranfield University Cranfield School of Aerospace Transport and Manufacturing

UNITED KINGDOM

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Sajal Kissoon

Cranfield University

UNITED KINGDOM

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Ioannis Roumeliotis

Prof at Faculty of Engineering and Applied Science

Cranfield University

UNITED KINGDOM

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Theoklis Nikolaidis

Associate Professor in Gas Turbine Engineering and Thermal Engines Lab Lead

University of Patras

GREECE

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Christos Mourouzidis

Research Interests

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Articles (12)

Assessment of a liquid hydrogen conditioning system for retrofitting on kerosene designed turbofans

Hydrogen and Ammonia Powered Turbofan Design Implications for Next Generation of Aircraft Engines

Design space exploration of geared turbofans using alternative fuels

Installation effects of supersonic inlets on next-generation SST turbofan engines

Assessing uninstalled hydrogen-fuelled retrofitted turbofan engine performance

Abating CO2 and non-CO2 emissions with hydrogen propulsion

Integrated Hybrid Engine Cycle Design and Power Management Optimization

Ammonia for civil aviation: A design and performance study for aircraft and turbofan engine

Dynamic Simulation and Aircraft Level Assessment of CMC Implementation on GTF Engine

Design Methodology and Mission Assessment of Parallel Hybrid Electric Propulsion Systems

Design Optimization and Variable Geometries Implementation of a High Bypass Three-Shaft Turbofan Engine for EIS2050

Assessment of performance boundaries and operability of low specific thrust GUHBPR engines for EIS2025

Collaborators (4)

David John Rajendran

Sajal Kissoon

Ioannis Roumeliotis

Theoklis Nikolaidis

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