Contact Dr Pavlos Zachos
- Tel: +44 (0) 1234 754633
- Email: p.zachos@cranfield.ac.uk
- ORCID
Areas of expertise
- Computational Fluid Dynamics
- Gas Turbines & Propulsion
- Instrumentation, Sensors and Measurement Science
- Power Systems & Turbines
Background
Dr. Pavlos Zachos holds the position of Reader in Propulsion Aerodynamics at the Centre of Propulsion and Thermal Power Engineering. He is a Rolls-Royce Royal Academy of Engineering Industrial Fellow, a Chartered Engineer through the Institute of Mechanical Engineers, a Fellow of AdvanceHE, and a visiting scholar at the University of Sydney, Australia. Pavlos is the acting Chair of a NATO Science and Technology committee focusing on propulsion system integration. He is appointed as a subject matter expert within various related AIAA Technical Committees through which he actively steers and supports delivery of the Institute's technical scope.
Dr. Zachos earned his PhD in gas turbine performance and aerodynamics from Cranfield University in 2010, receiving the Kings Norton Medal for outstanding doctoral research. He previously worked as a turbine designer for the Trent engine family at Rolls-Royce Derby.
Pavlos is a specialist in experimental and computational propulsion aerodynamics. His research interests include the aerodynamics of propulsion system integration and engine compatibility, NetZero aero-engine design and optimization, high-speed propulsion system aero integration, air induction system technology, high performance turbomachinery design, and inlet flow distortion. Since 2010, Dr. Zachos has led and delivered numerous research programmes, covering technology readiness levels (TRL) from 3 to 6+. His research endeavors are supported by major industrial partners such as Rolls-Royce, Boeing, Airbus, and MBDA, alongside various UK research councils (ATI, EPSRC, I-UK and the Royal Academy of Engineering). He has also secured major national grants from the UK Government, the UK Ministry of Defence, and the European Commission.
In his research, Dr. Zachos has pioneered advancements in propulsion system compatibility experimental testing by implementing non-intrusive optical flow diagnostic methods for inlet flow distortion measurements. His research findings have been instrumental in supporting aeroengine compatibility test campaigns within industrial settings as part of engine certification processes. Dr Zachos has also led the delivery of a dual-use, UK sovereign facility for supersonic propulsion system integration testing which is uniquely positioned to support research across a TRL range between 3 and 5+. This unique design characteristic makes the facility a vehicle for fundamental as well as industrial research programmes enabling the development, transition and pull-through of the outputs into higher TRL industrial settings for further exploitation by the UK Aerospace industry, which no other research institute offers in the broader area of supersonic propulsion integration aerodynamics.
Regarding his teaching responsibilities, Dr. Zachos owns and leads the delivery of the Turbomachinery and Blade Cooling module, a component of Cranfield's MSc program in Thermal Power and Propulsion. His teaching curriculum includes fundamentals of thermofluids science, compressible flow theory, gas dynamics, and the principles of turbomachinery design and performance. He is a former owner and module leader of Cranfield's Thermofluid Science taught module which formed part of many of the University's post-graduate programmes. Furthermore, he serves as the owner and course director for the Axial Compressor Design and Performance continuous professional development (CPD) programme, and he contributes to several other related CPD courses. To date, Dr. Zachos has successfully supervised over 15 doctoral students since 2010 as a primary supervisor.
Dr. Zachos is an active member of the American Society of Mechanical Engineers (ASME), a Senior Member of the American Institute of Aeronautics and Astronautics (AIAA), and a member of the Royal Aeronautical Society (RAeS). His publication record includes more than 70 refereed articles in journals and conference proceedings, demonstrating his contributions to the fields of applied aerodynamics and propulsion system performance and integration.
Research opportunities
Dr Zachos' research interests focus on the following areas:
- Applied aeorodynamics of propulsion systems
- Propulsion system integration, engine compatibility and distortion
- Supersonic flow aerodynamics
- High- and low- speed air induction system aerodynamics
- Inlet flow distortion
- Novel propulsion concepts and design optimisation
- Test rig design for high-speed propulsion system integration
- Aerodynamic measurements
- Non-intrusive metrology for aerodynamic applications
- Laser-based optical flow diagnostics
- Aerodynamic testing
- Industrial propulsion integration testing
- Applied computational fluid dynamics
Current activities
Dr Zachos currently leads a portfolio of research programmes in the broader area of propulsion system integration and compatibility with special focus on the development, maturing and demonstration of advanced, non-intrusive instrumentation capabilities for novel propulsion measurements, knowledge generation in aerodynamics to aid the development of next generation NetZero aircrafts and support of UK industry tests with novel measurements and data analytics.
His current professional activities focus on the delivery of a unique, dual-use UK sovereign aerodynamic testing facility for high-speed propulsion system integration measurements. This multi-year programme has received direct funding by the Defence Science and Technology Laboratory (Dstl) with the ambition to build and expand current measurement capabilities into supersonic flow regimes for engine compatiility testing. The facility is uniquely positioned to support research across a TRL range between 3 and 5+, which makes it a vehicle for fundamental as well as industrial research programmes enabling the development, transition and pull-through of the outputs into higher TRL industrial settings for further exploitation by the UK Aerospace industry.
In addition, Pavlos in collaboration with major industrial partners and various SMEs, pioneers industrial engine compatibility testing using non-intrusive measurement methods for dynamic inlet flow distortion characterisations at high TRL environments. As part of these programmes Pavlos' research group works closely with specialist SMEs to develop bespoke specialist instrumentation solutions for propulsion aero measurements, which subsequently find application in industrial measurements for aero-engine performance characterisation and certification.
Dr Zachos a visiting scholar at the University of Sydney, Australia since 2022. He is also the acting Chair of a NATO Science and Technology committee focusing on propulsion system integration. He is appointed as a subject matter expert within various related AIAA Technical Committees through which he actively steers and supports delivery of the Institute's technical scope.
Clients
- Rolls-Royce Holdings PLC
- Airbus SE
- Samsung Electronics Co., Ltd
- Defence Science and Technology Laboratory
- MBDA UK Ltd
Publications
Articles In Journals
- Migliorini M, Doll U, Lawson NJ, Melnikov SM, Steinbock J, .... (2025). Advancements on the use of Filtered Rayleigh Scattering (FRS) with machine learning methods for flow distortion in aero-engine intakes. Experimental Thermal and Fluid Science, 160
- Piovesan T, Zachos PK, MacManus DG, Kempaiah K, Michaelis D, .... (2025). Coupled fan-intake dynamic distortion characterization at crosswind conditions. AIAA Journal, 63(2)
- Piovesan T, Zachos PK, MacManus DG & Sheaf C. (2025). Unsteady swirl distortion in a short intake under crosswind conditions. AIAA Journal, 63(5)
- Migliorini M, Zachos PK, MacManus DG & Giannouloudis A. (2025). Experimental investigation of unsteady fan-intake interactions using time-resolved stereoscopic particle image velocimetry. Experimental Thermal and Fluid Science, 166
- Lawson NJ & Zachos PK. (2025). Brief Communication: measurement of boundary layer turbulent transition using an acoustic microphone unit. SAE International Journal of Aerospace, 18(2)
- Kempaiah KU, Piovesan T, Zachos PK, Michaelis D, Gebbink R, .... (2024). High-resolution turbofan intake flow characterization by automated stereoscopic-PIV in an industrial wind tunnel environment. Measurement Science and Technology, 35(2)
- Philippou AL, Zachos PK & MacManus DG. (2024). Aerodynamic instabilities in high-speed air intakes and their role in propulsion system integration. Aerospace, 11(1)
- Migliorini M, Zachos PK & MacManus DG. (2024). Evaluation of extreme value predictions for unsteady flow distortion of aero-engine intakes. Journal of Engineering for Gas Turbines and Power, 146(9)
- Doll U, Kapulla R, Dues M, Steinbock J, Melnikov S, .... (2023). Towards time-resolved multi-property measurements by filtered Rayleigh scattering: diagnostic approach and verification. Experiments in Fluids, 65(1)
- Doll U, Migliorini M, Baikie J, Zachos PK, Röhle I, .... (2022). Non-intrusive flow diagnostics for unsteady inlet flow distortion measurements in novel aircraft architectures. Progress in Aerospace Sciences, 130(April)
- Migliorini M, Zachos PK & MacManus DG. (2022). S-duct flow distortion with non-uniform inlet conditions. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 237(2)
- Logothetis DK, Zachos PK & Rogero J-M. (2022). Drag decomposition of a subsonic wing via a far-field, exergy-based method. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 237(7)
- Migliorini M, Zachos PK & MacManus DG. (2021). Novel method for evaluating intake unsteady flow distortion. Journal of Propulsion and Power, 38(1)
- McLelland G, MacManus DG, Zachos PK, Gil-Prieto D & Migliorini M. (2020). Influence of upstream total pressure profiles on S-duct intake flow distortion. Journal of Propulsion and Power, 36(3)
- Gil-Prieto D, Zachos PK, MacManus DG & McLelland G. (2018). Unsteady characteristics of S-duct intake flow distortion. Aerospace Science and Technology, 84
- D’Ambros A, Kipouros T, Zachos PK, Savill M & Benini E. (2018). Computational design optimization for S-ducts. Designs, 2(4)
- Orts-Gonzalez PL, Zachos PK & Brighenti GD. (2018). The impact of heat exchanger degradation on the performance of a humid air turbine system for power generation. Applied Thermal Engineering, 149
- Seetharama-Yadiyal V, Brighenti GD & Pavlos Z. (2018). Advanced gas turbine cycle performance modelling using response surface methods. The Aeronautical Journal, 122(1258)
- Brighenti GD, Zachos PK & Orts-Gonzalez PL. (2018). Part-load performance modelling of a reheated humid air turbine power cycle. Applied Thermal Engineering, 138
- Orts-Gonzalez PL, Zachos PK & Brighenti GD. (2018). Techno-economic analysis of a reheated humid air turbine. Applied Thermal Engineering, 137
- Gil-Prieto D, MacManus DG, Zachos PK & Bautista A. (2017). Assessment methods for unsteady flow distortion in aero-engine intakes. Aerospace Science and Technology, 72
- Gil-Prieto D, MacManus DG, Zachos PK, Tanguy G & Menzies KR. (2017). Convoluted intake distortion measurements using stereo particle image velocimetry. AIAA Journal, 55(6)
- Brighenti GD, Orts-Gonzalez PL, Sanchez-de-Leon L & Zachos PK. (2017). Design point performance and optimization of humid air turbine power plants. Applied Sciences, 7(4)
- Gil-Prieto D, MacManus DG, Zachos PK, Tanguy G, Wilson F, .... (2017). Delayed detached-eddy simulation and particle image velocimetry investigation of S-Duct flow distortion. AIAA Journal, 55(6)
- MacManus DG, Chiereghin N, Gil-Prieto D & Zachos PK. (2017). Complex aero-engine intake ducts and dynamic distortion. AIAA Journal, 55(7)
- Zachos PK. (2013). Modelling and Analysis of Turbofan Engines Under Windmilling Conditions. Journal of Propulsion and Power, 29(4)
- Grech N, Koupper C, Zachos PK, Pachidis V & Singh R. (2012). Considerations on the Numerical Modeling and Performance of Axial Swirlers Under Relight Conditions. Journal of Engineering for Gas Turbines and Power, 134(11)
- Grech N, Mehdi A, Zachos PK, Pachidis V & Singh R. (2012). Effect of Combustor Geometry on Performance of Airblast Atomizer Under Sub-Atmospheric Conditions. Engineering Applications of Computational Fluid Mechanics, 6(2)
- Terzis A, Kazakos C, Papadopoulos N, Kalfas A, Zachos PK, .... (2011). Effects of Swirl Velocities From Fan Assemblies Mounted on Lifting Surfaces. Journal of Engineering for Gas Turbines and Power, 133(3)
- Terzis A, Zachos P, Charnley B, Pachidis V & Kalfas AI. (2011). ON THE APPLICABILITY OF OIL AND DYE FLOW VISUALIZATION TECHNIQUE DURING THE DESIGN PHASE AND OPERATION OF EXPERIMENTAL RIGS. Journal of Flow Visualization and Image Processing, 18(3)
- Zachos PK, Aslanidou I, Pachidis V & Singh R. (2011). A Sub-idle Compressor Characteristic Generation Method With Enhanced Physical Background. Journal of Engineering for Gas Turbines and Power, 133(8)
- Zachos PK, Grech N, Charnley B, Pachidis V & Singh R. (2011). Experimental and Numerical Investigation of a Compressor Cascade at Highly Negative Incidence. Engineering Applications of Computational Fluid Mechanics, 5(1)
- Zachos PK, Pilidis P & Kalfas AI. (2010). Analysis of turbine performance degradation effects due to geometry variations between actual components and design Intent. The Aeronautical Journal, 114(1159)
- ZACHOS PK, PAPPA M, KALFAS AI, MANSOUR G, TSIAFIS I, .... (2008). Turbine Blading Performance Evaluation Using Geometry Scanning and Flowfield Prediction Tools. Journal of Power and Energy Systems, 2(6)
- Lawson NJ, Migliorini M, Doll U, Melnikov SM, Steinbock J, .... Pathway to non-intrusive in-flight flow diagnostics with Filtered Rayleigh Scattering (FRS). SAE International Journal of Aerospace
Conference Papers
- Migliorini M, Zachos PK, MacManus DG & Martin PG. (2025). Aerodynamic design of a high-speed intake test rig for propulsion integration research
- Piovesan T, Zachos PK, MacManus DG, Michaelis D, van Rooijen B, .... (2025). Use of non-intrusive flow diagnostics for aero-engine inlet flow distortion measurements in an industrial wind-tunnel
- Piovesan T, Zachos PK & MacManus DG. (2025). Total pressure distortion reconstruction methods from velocimetry data within an aero-engine intake at crosswind
- Ibanez C, Migliorini M, Giannouloudis A, Tejero F & Zachos PK. (2025). Cluster-based tracking method for the identification and characterisation of vortices
- Piovesan T, Zachos PK, MacManus DG & Sheaf C. (2024). Unsteady swirl distortion in a short intake under crosswind conditions
- Piovesan T, Migliorini M, Zachos PK & Tsoutsanis P. (2024). Dynamic swirl distortion characteristics in S-shaped diffusers using UCNS3D and time-resolved, stereo PIV methods
- Moreno M, Zachos PK, Gantt EJ, Tobaldini Neto L, Ferolla de Ambreu D, .... (2024). Summary of the 6th Propulsion Aerodynamics Workshop: NASA 1507 Inlet
- Migliorini M, Zachos PK, MacManus DG, Doll U, Dues M, .... (2024). Seeding-free inlet flow distortion measurements using filtered Rayleigh scattering: integration in a complex intake test facility
- Migliorini M, Zachos PK, MacManus DG & Giannouloudis A. (2024). Effect of a fan on the unsteady distortion of s-duct intakes
- Doll U, Kapulla R, Dues M, Steinbock J, Melnikov S, .... (2024). Towards time-resolved multi-property measurements by single-frequency FRS
- Dues M, Dues F, Melnikov S, Steinbock JJ, Doll U, .... (2024). 2D3C measurement of velocity, pressure and temperature fields in a intake flow of an air turbine by Filtered Rayleigh Sattering (FRS) and validation with LDV and PIV
- Doll U, Kapulla R, Steinbock J, Dues M, Migliorini M, .... (2023). Seeding-free inlet flow distortion measurement by filtered Rayleigh scattering: diagnostic approach and verification
- Migliorini M, Zachos PK & MacManus DG. (2023). Characterization of unsteady distortion events for S-duct intakes under non-uniform inlet conditions
- Moreno M, Migliorini M, Zachos PK, Haslam A & MacManus DG. (2023). Design and optimisation of a Mach 2.5 wind tunnel nozzle
- Migliorini M, Szymanski A, Zachos PK, MacManus DG & Martin PG. (2023). Design of a high-speed intake distortion simulator for propulsion integration research
- Migliorini M, Zachos PK, MacManus DG & Monnier V. (2022). A study on the development of the flow distortion downstream of an s-duct intake
- Piovesan T, Wenqiang Z, Vahdati M & Zachos PK. (2022). Investigations of the unsteady aerodynamic characteristics for intakes at crosswind
- Zhang W, Tiedemann B, Hegen S, Vahdati M, Zachos P, .... (2022). Non-Intrusive Flow distortion measurements within a Turbofan Intake (NIFTI)- De-risking the test campaigns with CFD analysis
- Terzis A, Zachos PK, Charnley BA & Kalfas AI. (2022). Application of oil and dye flow visualization in incompressible turbomachinery flows
- Migliorini M, Zachos PK & MacManus DG. (2019). An assessment on the unsteady flow distortion generated by an S-duct intake
- Migliorini M, Zachos PK & MacManus DG. (2019). The impact of inlet boundary layer thickness on the unsteady aerodynamics of S-duct intakes
- Guerrero-Hurtado M, Zachos PK, MacManus DG, Migliorini M & Trapani G. (2019). Unsteady swirl distortion characteristics for S-ducts using Lattice Boltzmann and time-resolved, stereo PIV methods
- Migliorini M, Zachos P & MacManus D. (2019). Correction: The impact of inlet boundary layer thickness on the unsteady aerodynamics of S-duct intakes
- Migliorini M, Zachos P & MacManus D. (2019). Correction: An assessment on the unsteady flow distortion generated by an S-duct intake
- Zubizarreta J, Anselmi E, Zachos P & Pachidis V. (2018). The impact of measurement uncertainty on heat exchanger performance measurements in a sCO2 test facility for power cycle applications
- Anselmi Palma E, Bunce I, Pachidis V, Zachos PK & Johnston M. (2018). An overview of the Rolls-Royce sCO2-test rig project at Cranfield University
- Zachos PK, Frascella M, MacManus DG & Gil-Prieto D. (2017). Pressure flowfield and inlet flow distortion metrics reconstruction from velocity data
- Tanguy G, MacManus DG, Zachos PK, Gil-Prieto D & Garnier E. (2017). Passive flow control study in an S-duct intake using Stereo Particle Image Velocimetry
- Tanguy G, MacManus DG, Zachos PK, Gil-Prieto D & Garnier E. (2016). Passive flow control study in a convoluted intake using Stereo Particle Image Velocimetry
- Gil-Prieto D, Zachos P, MacManus DG & Tanguy G. (2016). Convoluted Intake Distortion Measurements Using Stereo Particle Image Velocimetry
- Frascella M, Zachos PK, Gil-Prieto D & MacManus DG. (2016). Pressure flow field and inlet flow distortion metrics reconstruction from velocity data
- Brighenti G, Anselmi Palma E & Zachos PK. (2016). Parametric evaluation of S-CO2 Brayton cycles for bottoming applications
- Anselmi Palma E, Zachos PK, Collins R & Hassan M. (2016). Development of an experimental S-CO2 loop for bottoming cycle applications
- Gil-Prieto D, MacManus DG, Zachos PK, Tanguy G, Wilson F, .... (2016). Dynamic flow distortion investigation in an S-duct using DDES and SPIV data
- Zachos PK, MacManus DG & Chiereghin N. (2016). Flow distortion measurements in convoluted aero engine intakes
- Zachos PK, MacManus DG & Chiereghin N. (2015). Flow distortion measurements in convoluted aero engine intakes
- MacManus DG, Chiereghin N, Gil-Prieto D & Zachos PK. (2015). Complex aero-engine intake ducts and dynamic distortion
- Doligalski A, Sanchez de Leon L, Zachos PK & Pachidis V. (2014). Assessing the Potential of Gas-Recuperation in Reheated Gas Turbines Within Combined Gas-Steam Power Plants
- Sanchez de Leon L, Zachos PK & Pachidis V. (2013). A Comparative Assessment of Dry Gas Turbine Cycles for Marine Applications
- Lecoq M, Grech N, Zachos PK & Pachidis V. (2013). Probabilistic and Numerical Modelling of a Lobed Mixer at Windmilling Conditions
- Illana E, Grech N, Zachos PK & Pachidis V. (2013). Axial Compressor Aerodynamics Under Sub-Idle Conditions
- Piscopo G, Zachos PK & Pilidis P. (2013). Considerations on the Compression System Preliminary Design of a Short Haul Aircraft Propulsion System
- Koupper C, Grech N, Zachos PK, Pachidis V & Singh R. (2012). Considerations on the Numerical Modelling and Performance of Axial Swirlers Under Relight Conditions
- Zachos PK, Ruelke C, Pachidis V & Singh R. (2011). Compressor Blade Modelling Under Highly Negative Incedence
- Terzis A, Kazakos C, Zachos P, Kalfas A & Ott P. (2011). Swirl jet and crossflow interaction at low velocity ratios and incompressible flows
- Ruelke C, Terzis A, Zachos PK, Pachidis V & Singh R. (2010). Experimental evaluation and analytical modelling of the pressure loss through a compressor cascade operating at highly negative incidence
- Terzis A, Kazakos C, Papadopoulos N, Zachos PK, Pilidis P, .... (2010). The effect of the swirl velocity of a jet in cross flow typically used for turbine cooling applications
- Aslanidou I, Zachos PK, Pachidis V & Singh R. (2010). A Physically Enhanced Method for Sub-Idle Compressor Map Generation and Representation
- Terzis A, Kazakos C, Papadopoulos N, Kalfas AI, Zachos PK, .... (2010). Effects of the Swirl Velocity of a Jet in Crossflow From Fan Assemblies Mounted on Lifting Surfaces
- Kozaily J, Zachos PK, Pachidis V & Singh R. (2009). Gas Turbine Fuel Atomisation Dynamics Under Sub-atmospheric Conditions
- Gallar L, Pachidis V, Zachos PK & Singh R. (2009). Compressor IGV Off Design Performance and Loss Modelling
- Zachos PK, Pengue F, Pachidis V & Pilidis P. (2009). Flowfield Investigation of a Compressor Cascade at High Incidence—Part 2: Numerical Analysis
- Zachos PK, Pachidis V, Charnley B & Pilidis P. (2009). Flowfield Investigation of a Compressor Cascade at High Incidence—Part 1: Pneumatic Probe Measurements
- Laskaridis P & Zachos P. (2009). Effects of engine parameters on secondary power extraction and evaluation of engine performance penalties