Contact Spyros Tsentis
Areas of expertise
- Electric and Hybrid Vehicles
- Gas Turbines & Propulsion
- Power Systems & Turbines
- Vehicle Aerodynamics
Background
Spyros received his 5-year diploma (integrated MEng) in 2020 from the Aristotle University of Thessaloniki (AUTh), Greece. He conducted his Master's Thesis on the performance analysis of a novel engine concept which utilizes hybrid air-breathing rocket cycle technology, under the supervision of Professor Anestis Kalfas.
Following his graduation, he worked as a Researcher within the "HECARRUS" Project (European Union, Horizon 2020, Research and Innovation Programme "Clean Sky 2") at the Laboratory of Fluid Mechanics and Turbomachinery (AUTh). His primary role within the project included the conceptual design and analysis of the Thermal Management System (TMS) of a small commuter aircraft utilizing hybrid-electric propulsion architectures, among others.
Spyros is a member of the ''AeroEngineS'' multi-platform application development team (available as web, android and iOS app). While conducting research in Greece, he programmed and developed 2 stand-alone templates focused on the performance simulation of a novel hybrid air-breathing rocket-cycle engine as well as a ramjet engine, thus widening the existing range of the application into the supersonic and hypersonic propulsion regimes. Following, he supervised the development of another template, able to simulate the performance of a Turbine-Based-Combined-Cycle (TBCC) engine.
Spyros has already co-supervised three M.Eng. students to completion, under the leading supervision of Professor Anestis Kalfas, at the Aristotle University of Thessaloniki, where he is also delivering guest lectures on high-speed propulsion systems.
Current activities
Currently, Spyros is undertaking his PhD on Aft-body Aerodynamics of Novel Propulsion Architectures within the Cranfield Air & Space Propulsion Institute, under the supervision of Professor Vassilios Pachidis, Professor Simon Prince and Dr Ioannis Goulos.
Publications
Articles In Journals
- Chatzistefanou A, Tsentis S & Kalfas A. (2025). Synergetic and Performance Characteristics of a High-Speed Precooled Propulsion Concept. Journal of Engineering for Gas Turbines and Power, 147(2)
- Tsentis S, Goulos I, Prince S, Pachidis V & Zmijanovic V. (2023). Propulsion Aerodynamics for a Novel High-Speed Exhaust System. Journal of Engineering for Gas Turbines and Power, 145(12)
- Gkoutzamanis VG, Tsentis SE, Valsamis Mylonas OS, Kalfas AI, Kyprianidis KG, .... (2022). Thermal Management System Considerations for a Hybrid-Electric Commuter Aircraft. Journal of Thermophysics and Heat Transfer, 36(3)
- Tsentis SE, Gkoutzamanis VG, Gaitanis AD & Kalfas AI. (2021). Multi-platform app-embedded model for hybrid air-breathing rocket-cycle engine in hypersonic atmospheric ascent. The Aeronautical Journal, 125(1291)
Conference Papers
- Tsentis S, Goulos I, Prince S, Pachidis V, Zmijanovic V, .... (2024). Wind Tunnel Installation Effects on the Base Flow for a High-Speed Exhaust System
- Tsentis S, Goulos I, Prince S, Pachidis V & Zmijanovic V. (2024). Cavity Impact on the Base Flow Unsteadiness for a High-Speed Exhaust System
- Tsentis S, Gaitanis A, Gkoutzamanis V & Kalfas A. (2024). A Comprehensive Educational App for Propulsion Systems
- Chatzistefanou A, Tsentis S & Kalfas A. (2024). Synergetic and Performance Characteristics of a High-Speed Pre-Cooled Propulsion Concept
- Tsentis S, Goulos I, Prince S, Pachidis V & Zmijanovic V. (2024). BASE FLOW CHARACTERISTICS FOR A SUB-SCALE HIGH-SPEED EXHAUST AT OVER-EXPANDED MODE
- Tsentis S, Goulos I, Prince S, Pachidis V & Zmijanovic V. (2023). Propulsion Aerodynamics for a Novel High-Speed Exhaust System
- Tsentis SE, Gkoutzamanis VG, Gaitanis AD & Kalfas AI. (2022). Multi-platform app-embedded model for hybrid air-breathing rocket-cycle engine in hypersonic atmospheric ascent
- Tsentis SE, Gkoutzamanis VG, Gaitanis AD & Kalfas AI. (2021). Multi-Platform App-Embedded Model for Hybrid Air-Breathing Rocket Cycle Engine in Hypersonic Atmospheric Ascent – CORRIGENDUM