Contact Dr Evangelia Pontika
Areas of expertise
- Electric and Hybrid Vehicles
- Environmental Impacts
- Flight Physics
- Gas Turbines & Propulsion
Background
General Background
Evangelia Pontika is a Research Fellow in Propulsion Performance and Fleet Management within the Hybrid Electric Propulsion Group at the Centre for Propulsion and Thermal Power Engineering. Her research activities include gas turbine engine life consumption, engine life management, flight path analysis and propulsion integration of green and sustainable power generation technologies.
Evangelia has developed a multi-platform aero-engine performance simulation app within the Laboratory of Fluid Mechanics and Turbomachinery at Aristotle University, which is currently used for educational purposes in Aerospace Courses in Greece and Sweden. At Cranfield University, she has developed engine life consumption tools and engine life management methods. She also has experience in the aircraft integration of electric and hybrid-electric propulsion systems as well as their environmental and performance assessment.
Evangelia has advised and supervised 6 MSc theses within the Thermal Power and Propulsion MSc Course. She has also acted as a reviewer for ASME Turbo Expo, the Global Power & Propulsion Society and AIAA conferences. Evangelia has collaborated with several industrial and academic organisations including: Lufthansa Technik, Rolls Royce, SAFRAN, Aristotle University of Thessaloniki, Sheffield University, Mälardalen University, Delft University of Technology, DLR, University of Genoa, Eindhoven University of Technology, Karlsruhe Institute of Technology and others.
Education
Evangelia holds a Diploma in Mechanical Engineering with specialisation in Aeronautics and Engines (BEng+MEng) from Aristotle University of Thessaloniki (2017) and a PhD in Aerospace Propulsion from Cranfield University (2021) on the topic of "Hot Corrosion Damage Modelling in Aero-Engines based on Performance and Flight Mission Analysis for Fleet Characterisation".
Awards & Honours
- EPSRC Early Career Researcher - Exploratory Impact Award (2024)
- Best Paper Award, ASME Turbo Expo 2018 (2019)
- Scholarship for a fully funded PhD at Cranfield University sponsored by Lufthansa Technik (2017)
Research opportunities
Gas Turbine Engine Life Consumption
Engine Life Management
Hybrid Electric Propulsion Integration
Current activities
Evangelia is currently working in the EU Horizon Project FlyECO and is leading the task for the gas turbine design exploration, performance and integration with solid oxide fuel cells for a highly integrated power propulsion system using hydrogen. She is supervising MSc and PhD projects, contributes to lectures and she is a debuty course director for two short courses. Finally, Evangelia is the custodian of the in-house aircraft performance software.
Projects:
- Impact aircraft fleet operations on hot corrosion damage and prescribed maintenance actions, EPSRC Exploratory Impact Award (2024)
- PINES (Propulsion Integration of Novel Engine Systems), funded by UKRI (2021-2024) : investigated performance and life management opportunities for novel engines
- FutPrint50 (FUTure PRopulsion and INTegration: towards a hybrid-electric 50-seat regional aircraft), EU Horizon 2020 project (2020-2023) : contributed to the aircraft integration of electrified propulsion systems, their performance and environmental assessment
- Chemically Induced Damage Mechanisms in Gas Turbines, funded by Lufthansa Technik (2017-2021) : developed a multidisciplinary framework for the prediction of hot corrosion damage in aero-engines
Clients
Evangelia has collaborated with several industrial and academic organisations including: Lufthansa Technik, Rolls Royce, SAFRAN, Aristotle University of Thessaloniki, Sheffield University, Mälardalen University, Delft University of Technology, DLR, University of Genoa, Eindhoven University of Technology, Karlsruhe Institute of Technology and others.
Publications
Articles In Journals
- Asli M, König P, Sharma D, Pontika E, Huete J, .... (2024). Thermal management challenges in hybrid-electric propulsion aircraft. Progress in Aerospace Sciences, 144
- Pontika E, Laskaridis P, Nikolaidis T & Koster M. (2024). Hot Corrosion Damage Modeling in Aeroengines Based on Performance and Flight Mission. Journal of Thermophysics and Heat Transfer
- Aslanidou I, Zimmerman N, Pontika E, Kalfas AI & Kyprianidis KG. (2021). Reforming heat and power technology course using student feedback to enhance learning experience. International Journal of Mechanical Engineering Education, 49(4)
Conference Papers
- He Z, Pontika E & Laskaridis P. (2024). Toward Net Zero: an Engine Electrification Strategy Approach of Fuel Cell and Steam Injection
- Zammit Mangion D, Pontika E, Zammit-Mangion R & pilidis P. (2024). Mission Definition and Flight Performance Analysis of a Hydrogen Technology C-130J Flying Demonstrator
- Zaghari B, Zhou T, Enalou HB, Pontika E & Laskaridis P. (2023). The Impact of Multi-Stack Fuel Cell Configurations on Electrical Architecture for a Zero Emission Regional Aircraft
- Pontika E, Zaghari B, Zhou T, Enalou HB & Laskaridis P. (2023). Integrated Mission Performance Analysis of Novel Propulsion Systems: Analysis of a Fuel Cell Regional Aircraft Retrofit
- Pontika E, Laskaridis P, Nikolaidis T & Koster M. (2023). Hot Corrosion Damage Modelling in Aero Engines based on Performance and Flight Mission Analysis
- Pontika E, Laskaridis P, Montana Gonzalez F, Jacobs W & Mills A. (2023). Mapping the Effect of Variable HPT Blade Cooling on Fuel Burn, Engine Life and Emissions for Fleet Optimization using Active Control
- Zaghari B, Kiran A, Sinnige T, Pontika E, Enalou HB, .... (2023). The Impact of Electric Machine and Propeller Coupling Design on Electrified Aircraft Noise and Performance
- Zhou T, Enalou HB, Pontika E, Zaghari B & Laskaridis P. (2022). Minimising the effect of degradation of fuel cell stacks on an integrated propulsion architecture for an electrified aircraft
- Pontika E, Laskaridis P, Nikolaidis T & Koster M. (2020). Comparison of Sodium Sulphate Deposition Rate Models Based on Operational Factors Influencing Hot Corrosion Damage in Aero-Engines
- Pontika EC, Kalfas AI & Aslanidou I. (2019). AeroEngineS: Multi-Platform Application for Aero Engine Simulation and Compressor Map Operating Point Prediction
- Aslanidou I, Zaccaria V, Pontika E, Zimmerman N, Kalfas AI, .... (2018). Teaching Gas Turbine Technology to Undergraduate Students in Sweden