Contact Dr Sangkeun Kang
Areas of expertise
- Aircraft Design
- Gas Turbines & Propulsion
Background
Sangkeun Kang is currently a Researcher in the Centre for Propulsion Engineering. Notable projects include the Application of Chemical Steam to Turboprop Aircraft Propulsion Units and the Assessment of Engine Operability for Gas Turbine-based Hybrid Propulsion Systems.
BEng in Aerospace Engineering (2014-2019), The University of Manchester, UK
MSc Thermal Power (Aerospace Propulsion) (2019-2020), Cranfield University, UK
Current activities
Currently a PhD student for Integrated Thermal Management System for eVTOL systems in the Centre for Propulsion Engineering
Highly interested in sustainable Aircraft Propulsion systems to create solutions for climate change issues, including Full electric and Hybrid Electric Propulsion.
Publications
Articles In Journals
- Kang S, Saias CA, Roumeliotis I & Broca O. (2025). Design and simulation of eVTOL aircraft Thermal Management System. Journal of Engineering for Gas Turbines and Power, 147(6)
- Kang S, Roumeliotis I, Zhang J, Broca O & Pachidis V. (2022). Assessment of engine operability and overall performance for parallel hybrid electric propulsion systems for a single-aisle aircraft. Journal of Engineering for Gas Turbines and Power, 144(4)
- Kang S, Saias CA, Roumeliotis I & Broca O. Preliminary Design of Integrated Power and Thermal Management Systems for Hybrid Electric VTOL Aircraft Architecture. Journal of Engineering for Gas Turbines and Power
Conference Papers
- Rompokos P, Kang S & Roumeliotis I. (2025). Integrated design and operation assessment of a preheating system for liquid hydrogen fuelled engines
- Kang S, Saias CA, Roumeliotis I & Broca O. (2025). Preliminary design of integrated power and thermal management systems for hybrid electric VTOL aircraft architecture
- Kang S, Saias C, Roumeliotis I & Broca O. (2024). Design and Simulation of eVTOL Aircraft Thermal Management System
- Kang S, Saias CA, Roumeliotis I & Broca O. (2023). On the design of integrated thermal management systems for eVTOL aircraft
- Kang S, Roumeliotis I, Zhang J, Pachidis V & Broca O. (2021). Assessment of engine operability and overall performance for parallel hybrid electric propulsion systems for a single-aisle aircraft