Contact Professor Vassilios Pachidis
- Tel: +44 (0) 1234 754663
- Email: v.pachidis@cranfield.ac.uk
- ORCID
Areas of expertise
- Aeronautical Systems
- Computational Fluid Dynamics
- Environmental Impacts
- Gas Turbines & Propulsion
- Power Systems & Turbines
Background
Vassilios Pachidis is an Aerospace Engineer and Professor (Level III) of Propulsion Integration Engineering in the School of Aerospace, Transport and Manufacturing at Cranfield University. He first joined Cranfield as a member of research staff in 2001. His main research interests include power plant modelling, performance and certification; novel cycles; turbomachinery experimental, analytical and computational aerodynamics; propulsion system integration and environmental performance; thermal management; electrification and sustainability. He has an international standing built upon a well-established research track record. He has more than 15 years of experience in research, project management and income generation, and more than 15 years of experience in postgraduate teaching, learning and Continuous Professional Development. He is Principal Investigator (PI) in Horizon 2020, Horizon Europe, Clean Sky I & II, EPSRC, IUK and ATI Research Grants with a personal annual research income in excess of £1M.
Education
Prof Pachidis was educated at The University of Liverpool where he obtained a 1st Class Hons MEng degree Aerospace Engineering (graduated in 2000). Subsequently he joined Cranfield University and enrolled in the Aerospace Propulsion option of the Thermal Power MSc (graduated in 2001). He then became member of staff at Cranfield whilst pursuing a part-time PhD in Gas Turbine Advanced Performance Simulation which he completed in 4 years.
Teaching & Student Supervision
Has taught more than 700 postgraduates since 2002 and more than 150 Short Course delegates since 2006. Has supervised more than 165 MSc and 32 Doctoral Candidates to completion. Currently supervising 11 MSc and 14 Doctoral Candidates, 4 part-time.
Refereeing for High-impact Journals
Prof Pachidis acts as a referee for high-impact journals including; J. of Applied Mathematical Modelling, J. of Turbomachinery, J. of Engineering Failure Analyses, J. of Engineering for Gas Turbines and Power, J. of Aerospace Science and Technology, J. of Engineering Applications of Computational Fluid Mechanics.
Publications & Patents
More than 69 peer-reviewed papers in 4* and 3* journals and more than 98 fully peer-reviewed conference papers and 19 other conference publications to date. 17 joint patents filed with Rolls-Royce plc. with another 6 pending filing.
Awards and Honours
7 ASME/IGTI 'Best Paper' Awards in 2020, 2019, 2013, 2012, 2010, 2007 and 2006.
2 John P. Davis Awards ASME/IGTI Turbo Expo 2019 and 2020. Co-author with Dr David John Rajendran.
Rolls-Royce Howse-Ruffles Award 2015. Co-authored winning paper with Dr Aleixo Gonzalez.
The Cranfield School of Engineering 'Arthur Lefebvre Prize' in 2006 for Doctoral research.
The IMechE 'Whittle Reactionaries Medal' in 2002, for research in novel airframe-propulsion system integration.
Scholarship Award from 'Cranfield University' in 2000.
The 'Rolls-Royce plc. Prize' in 1999, for academic achievements.
Scholarship Award from 'The University of Liverpool' in 1996.
International Conference Contribution
Session Organizer, Session Chair or Co-Chair and Reviewer for all annual ASME Turbo Expo conferences since 2002.
Invited Keynote - Tandem Aerodays, Bucharest 2019, Panel Session 'Disruptive Game Changers'.
Panel Chair - Global Power & Propulsion Forum, Zurich, January 2017, 'Performance of Gas Turbines with Inter-turbine Reheat, Theory and Applications'.
Panel Chair & Invited Keynote - Global Power & Propulsion Forum, Zurich, January 2017, 'Very Low Specific Thrust Turbofan Engine Performance & Integration with the Aircraft'.
Panel Chair - ASME Turbo Expo 2017, Charlotte NC, June 2017, 'Inter-turbine Reheat Performance, Theory and Applications'.
Invited Keynote - Aerodays, October 2015, London, 'Clean Sky Technology Evaluator - Environmental Performance Assessment of Rotorcraft'.
Invited Keynote - ASME Turbo Expo, June 2015, Montreal, 'Clean Sky JTI - GRC Environmental Performance Assessments'.
Panel Chair - ASME Turbo Expo, June 2012, Copenhagen, Panel Session on 'Power plant Modelling to Support Environmental, Operational and Economic Decisions'.
Organized and carried out a daily workshop in 'GT Performance Simulation' hosted by the ASME-IGTI 'Aero Engine Life Management Conference' in London (2004).
Expert Committees and Memberships
External assessor for the Helmholtz Association (Germany), EPSRC (UK), the Killam Trusts (Canada & US), Agency of Quality Assurance and Accreditation in Higher Education (Cyprus), Hellenic Air Force, and others.
Co-author, UK Defence Solution Centre, White Paper, 'Cross Sector Innovation: Energising Defence Strand 7 - Powering the UK Space Strategy', CSI2-7-RP-7005-V1.0.
Point of Contact, ASME/IGTI 'Aircraft Engine Committee', 2021-2022.
Chair, 'Board of Past Chairs of Cycle Innovations Committee', ASME/IGTI, 2017-2019.
Chair, ASME/IGTI 'Cycle Innovations Committee', 2015-2017.
Vice-Chair, ASME/IGTI 'Cycle Innovations Committee', 2013-2015.
Clean Sky JTI - Technology Evaluator, Management and Steering Committee Member, 2008-2017.
Chair, 'Cycle Innovations and Power Systems', Global Power & Propulsion Society, since 2016.
Technical Team Member, NATO, SP-AVT-SP-003-19-444, 'Investigation of Sub-Idle Gas Turbine Performance'.
Technical Team Member, NATO, STO-AVT-333, 'Integration of Propulsion, Power, and Thermal Subsystem Models into Air Vehicle Conceptual Design'.
Fellow of the IMechE since October 2014 (member since December 2001).
Member of the ASME/IGTI since 2013.
Member of the RAeS since September 1999.
Current activities
Head of Centre for Propulsion and Thermal Power Engineering;
Propulsion is around 70 staff strong (including visiting academics) and one of the largest research and education activities within SATM, with a turnover of around £7m. The activity spans air, land and sea applications of gas turbines for power and propulsion. It is characterised by a very close integration of taught and short-course education and research, with 50-80 MSc students attending the Thermal Power course each year, and more than 80 full-time and part-time PhD students.
Director of the 'Rolls-Royce University Technology Centre (UTC) in Aero Systems Design, Integration & Performance' at Cranfield (Deputy Director 2008-2014);
The UTC is of major strategic importance to Cranfield due to its prestigious status and the business it attracts from Rolls-Royce and elsewhere (industry + academia). The UTC typically enrols more than 30 staff, more than 20 PhD candidates and more than 30 MSc candidates, with an annual research budget in excess of £4M.
Director of the 'Cranfield Air & Space Propulsion Institute' since Jan 2021;
The Institute supports a pan-university activity to promote and accelerate innovation across different disciplines and sectors in order to create new, revolutionary technologies for use in air and space propulsion. Key objective is to provide industry and academia with a pre-competitive environment for collaboration in low TRL research.
Clients
Cranfield interacts very widely with national and international research councils and organisations, (such as the ATI, the EPSRC, IUK, NASA, ESA, UKSA, DLR, NLR, ONERA and CIRA), industry and governments. It also values and develops long term relationships for the mutual benefit of its sponsors and itself. Within aerospace, these include Rolls-Royce, AIRBUS, SIEMENS, BOEING, Pratt & Whitney, SAFRAN Group, DSTL, BAE Systems, GKN, the MoD and many others.
Publications
Articles In Journals
- Lamprakis D, Rajendran DJ, Santhanakrishnan M, Coskun S, Roumeliotis I, .... (2025). On Leakage Flows in a Liquid Hydrogen Multistage Pump for Aircraft Engine Applications. Journal of Engineering for Gas Turbines and Power, 147(5)
- Vitlaris D, Rajendran DJ, Tunstall R, Whurr J & Pachidis V. (2025). On Hysteresis in a Variable Pitch Fan Transitioning to Reverse Thrust Mode and Back. Journal of Engineering for Gas Turbines and Power, 147(7)
- Anselmi Palma E, Kissoon S, Hann G, Pilidis P & Pachidis V. (2025). Engine strip and build lab: a practical approach to learning gas turbine engines. The Aeronautical Journal, 129(1331)
- Baena Mejías R, Saias CA, Roumeliotis I, Pachidis V & Bacic M. (2024). Assessment of hydrogen gas turbine-fuel cell powerplant for rotorcraft. International Journal of Hydrogen Energy, 50
- Rajendran DJ, Palaveev K, Anselmi E, Santhanakrishnan M & Pachidis V. (2024). Insights Into the Flow Field and Performance of a Boundary Layer Pump. Journal of Engineering for Gas Turbines and Power, 146(6)
- Vitlaris D, Rajendran DJ, Tunstall R, Whurr J & Pachidis V. (2024). On the Flow Physics During the Transition of a Variable Pitch Fan From Nominal Operation to Reverse Thrust Mode. Journal of Engineering for Gas Turbines and Power, 146(4)
- Coskun S, Rajendran DJ, Pachidis V & Bacic M. (2024). Control of flow separation over an aerofoil by external acoustic excitation at a high Reynolds number. Physics of Fluids, 36(1)
- Ghelani R, Roumeliotis I, Saias CA, Mourouzidis C, Pachidis V, .... (2024). Integrated Hybrid Engine Cycle Design and Power Management Optimization. Journal of Engineering for Gas Turbines and Power, 146(10)
- Sasi S, Mourouzidis C, Rajendran DJ, Roumeliotis I, Pachidis V, .... (2024). Ammonia for civil aviation: A design and performance study for aircraft and turbofan engine. Energy Conversion and Management, 307
- Mejias RB, Saias CA, Roumeliotis I, Pachidis V & Bacic M. (2024). Assessment of hydrogen gas turbine-fuel cell powerplant for rotorcraft. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 50
- Rajendran DJ, Santhanakrishnan M, Pachidis V & Messineo J. (2024). Flow field explorations and design improvements of a hybrid rocket motor LOx feed line. Acta Astronautica, 225
- Monokrousos N, Könözsy L, Pachidis V, Sozio E & Rossi F. (2024). A numerical approach to overcome the very-low Reynolds number limitation of the artificial compressibility for incompressible flows. Heliyon, 10(21)
- Eryilmaz I, Li H, Pachidis V, Laskaridis P, Zhu Z-Q, .... (2023). Performance and operability of an electrically driven propulsor. International Journal of Engine Research, 24(3)
- Ghelani R, Roumeliotis I, Saias CA, Mourouzidis C, Pachidis V, .... (2023). Design Methodology and Mission Assessment of Parallel Hybrid Electric Propulsion Systems. Journal of Engineering for Gas Turbines and Power, 145(3)
- Saias CA, Goulos I, Pachidis V & Bacic M. (2023). On the Effects of Optimal Implementation of Variable Rotor Speed and Power Management on Hybrid-Electric Rotorcraft. Journal of Engineering for Gas Turbines and Power, 145(3)
- 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)
- Saias CA, Roumeliotis I, Goulos I, Pachidis V & Bacic M. (2022). Design Exploration and Performance Assessment of Advanced Recuperated Hybrid-Electric Urban Air Mobility Rotorcraft. Journal of Engineering for Gas Turbines and Power, 144(3)
- 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)
- Eryilmaz I & Pachidis V. (2022). A design approach for controlled blade-off in overspeeding turbines. Engineering Failure Analysis, 138(August)
- Saias CA, Roumeliotis I, Goulos I, Pachidis V & Bacic M. (2022). Assessment of hydrogen fuel for rotorcraft applications. International Journal of Hydrogen Energy, 47(76)
- Nambiar VR & Pachidis V. (2022). Nacelle intake flow separation reduction at cruise condition using active flow control. Propulsion and Power Research, 11(3)
- Righi M, Pachidis V, Könözsy L, Giersch T & Schrape S. (2022). Experimental validation of a three-dimensional through-flow model for high-speed compressor surge. Aerospace Science and Technology, 128(September)
- Rajendran DJ, Tunstall R & Pachidis V. (2022). Estimation of Resultant Airframe Forces for a Variable Pitch Fan Operating in Reverse Thrust Mode. Journal of Engineering for Gas Turbines and Power, 144(12)
- Rajendran DJ & Pachidis V. (2021). Flow Distortion Into the Core Engine for an Installed Variable Pitch Fan in Reverse Thrust Mode. Journal of Turbomachinery, 143(7)
- Saias CA, Pellegrini A, Brown S & Pachidis V. (2021). Three-spool turbofan pass-off test data analysis using an optimization-based diagnostic technique. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 235(6)
- Vouros S, Polyzos ND, Goulos I & Pachidis V. (2021). Impact of optimized variable rotor speed and active blade twist control on helicopter blade–vortex interaction noise and environmental impact. Journal of Fluids and Structures, 104(July)
- Saias CA, Goulos I, Roumeliotis I, Pachidis V & Bacic M. (2021). Preliminary Design of Hybrid-Electric Propulsion Systems for Emerging Urban Air Mobility Rotorcraft Architectures. Journal of Engineering for Gas Turbines and Power, 143(11)
- Rajendran DJ & Pachidis V. (2021). On the Use of an Inflatable Rubber Lip to Improve the Reverse Thrust Flow Field in a Variable Pitch Fan. Journal of Engineering for Gas Turbines and Power, 143(11)
- Scullion C, Vouros S, Goulos I, Nalianda D & Pachidis V. (2021). Optimal Control of a Compound Rotorcraft for Engine Performance Enhancement. Journal of Engineering for Gas Turbines and Power, 143(2)
- Ferrer-Vidal LE, Pachidis V & Tunstall RJ. (2021). Generating axial compressor maps to zero speed. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 235(5)
- Ferrer-Vidal LE & Pachidis V. (2021). Numerical modeling of core compressor discharge for a windmilling aero engine. Aerospace Science and Technology, 108
- Templalexis I, Pachidis V & Aguirre HA. (2021). Comparative Assessment of Fouling Scenarios in an Axial Flow Compressor. Journal of Engineering for Gas Turbines and Power, 143(8)
- Vouros S, Goulos I, Scullion C, Nalianda D & Pachidis V. (2021). Impact of Tip-Vortex Modeling Uncertainty on Helicopter Rotor Blade–Vortex Interaction Noise Prediction. Journal of the American Helicopter Society, 66(1)
- Roumeliotis I, Mourouzidis C, Zafferetti M, Unlu D, Broca O, .... (2020). Assessment of Thermo-Electric Power Plants for Rotorcraft Application. Journal of Engineering for Gas Turbines and Power, 142(5)
- Polyzos ND, Vouros S, Goulos I & Pachidis V. (2020). Multi-disciplinary optimization of variable rotor speed and active blade twist rotorcraft: Trade-off between noise and emissions. Aerospace Science and Technology, 107
- Righi M, Pachidis V, Könözsy L, Zhao F & Vahdati M. (2020). Three-dimensional low-order surge model for high-speed axial compressors. Journal of the Global Power and Propulsion Society, 4
- Righi M, Pachidis V & Könözsy L. (2020). On the prediction of the reverse flow and rotating stall characteristics of high-speed axial compressors using a three-dimensional through-flow code. Aerospace Science and Technology, 99
- Righi M, Ferrer-Vidal LE & Pachidis V. (2020). Body-force and mean-line models for the generation of axial compressor sub-idle characteristics. The Aeronautical Journal, 124(1281)
- Ferrer-Vidal LE, Iglesias-Pérez A & Pachidis V. (2020). Characterization of axial compressor performance at locked rotor and torque-free windmill conditions. Aerospace Science and Technology, 101
- Cleton B, Anselmi E, Pellegrini A, Pachidis V & Laskaridis P. (2019). Effect of mixing Mach number and mixing efficiency on the preliminary cycle design of mixed high-BPR turbofans. Thermal Science and Engineering Progress, 10
- Rajendran DJ & Pachidis V. (2019). Fan Flow Field in an Installed Variable Pitch Fan Operating in Reverse Thrust for a Range of Aircraft Landing Speeds. Journal of Engineering for Gas Turbines and Power, 141(10)
- Vouros S, Goulos I & Pachidis V. (2019). Integrated methodology for the prediction of helicopter rotor noise at mission level. Aerospace Science and Technology, 89
- Ferrer-Vidal LE, Schneider M, Allegretti A & Pachidis V. (2019). A Loss and Deflection Model for Compressor Blading at High Negative Incidence. Journal of Turbomachinery, 141(12)
- Eryilmaz I, Guenchi B & Pachidis V. (2019). Multi-blade shedding in turbines with different casing and blade tip architectures. Aerospace Science and Technology, 87
- Eryilmaz I & Pachidis V. (2019). Turbine thermomechanical modelling during excessive axial movement and overspeed. The Aeronautical Journal, 123(1260)
- Pawsey L, Rajendran DJ & Pachidis V. (2018). Characterisation of turbine behaviour for an engine overspeed prediction model. Aerospace Science and Technology, 73
- Ortiz-Carretero J, Castillo Pardo A, Goulos I & Pachidis V. (2018). Impact of Adverse Environmental Conditions on Rotorcraft Operational Performance and Pollutant Emissions. Journal of Engineering for Gas Turbines and Power, 140(2)
- Righi M, Pachidis V, Könözsy L & Pawsey L. (2018). Three-dimensional through-flow modelling of axial flow compressor rotating stall and surge. Aerospace Science and Technology, 78
- Enconniere J, Ortiz-Carretero J & Pachidis V. (2018). Mission optimisation for a conceptual coaxial rotorcraft for taxi applications. Aerospace Science and Technology, 72
- Pellegrini A, Nikolaidis T, Pachidis V & Köhler S. (2017). On the performance simulation of inter-stage turbine reheat. Applied Thermal Engineering, 113
- Castillo Pardo A, Goulos I & Pachidis V. (2017). Modelling and analysis of coupled flap-lag-torsion vibration characteristics helicopter rotor blades. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 231(10)
- Enconniere J, Ortiz-Carretero J & Pachidis V. (2017). Mission performance analysis of a conceptual coaxial rotorcraft for air taxi applications. Aerospace Science and Technology, 69
- Templalexis I & Pachidis V. (2017). Simulation of Fouling in Axial Flow Compressor Using a Throughflow Method. Journal of Energy Engineering, 143(1)
- Ali F, Goulos I & Pachidis V. (2016). A Preliminary Design Tradeoff Study for an Advanced Propulsion Technology Rotorcraft at Mission Level. Journal of Engineering for Gas Turbines and Power, 138(1)
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d'Ippolito R. (2015). Design Space Exploration and Optimization of Conceptual Rotorcraft Powerplants. Journal of Engineering for Gas Turbines and Power, 137(12)
- Goulos I, Ali F, Tzanidakis K, Pachidis V & d'Ippolito R. (2015). A Multidisciplinary Approach for the Comprehensive Assessment of Integrated Rotorcraft–Powerplant Systems at Mission Level. Journal of Engineering for Gas Turbines and Power, 137(1)
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d’Ippolito R. (2015). Multidisciplinary design and optimisation of conceptual rotorcraft powerplants for operational performance and environmental impact. The Aeronautical Journal, 119(1217)
- Ali F, Goulos I & Pachidis V. (2015). An integrated methodology to assess the operational and environmental performance of a conceptual regenerative helicopter. The Aeronautical Journal, 119(1211)
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d'Ippolito R. (2015). Optimized Regenerative Powerplant Configurations Targeting Improved Rotorcraft Operational and Environmental Performance. Journal of the American Helicopter Society, 60(2)
- Goulos I & Pachidis V. (2015). Real-Time Aero-elasticity Simulation of Open Rotors With Slender Blades for the Multidisciplinary Design of Rotorcraft. Journal of Engineering for Gas Turbines and Power, 137(1)
- Goulos I, Pachidis V & Pilidis P. (2015). Flexible rotor blade dynamics for helicopter aeromechanics including comparisons with experimental data. The Aeronautical Journal, 119(1213)
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d'Ippolito R. (2015). Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off Between Rotorcraft Fuel Efficiency and Environmental Impact. Journal of Engineering for Gas Turbines and Power, 137(7)
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d'Ippolito R. (2015). Multi-objective Optimization of a Regenerative Rotorcraft Powerplant: Trade-off Between Overall Engine Weight and Fuel Economy. Journal of Engineering for Gas Turbines and Power, 137(12)
- Goulos I, Pachidis V & Pilidis P. (2014). Lagrangian formulation for the rapid estimation of helicopter rotor blade vibration characteristics. The Aeronautical Journal, 118(1206)
- Goulos I, Pachidis V & Pilidis P. (2014). Helicopter Rotor Blade Flexibility Simulation for Aeroelasticity and Flight Dynamics Applications. Journal of the American Helicopter Society, 59(4)
- Laskaridis P, Pachidis V & Pilidis P. (2014). Opportunities and challenges for distributed propulsion and boundary layer ingestion. Aircraft Engineering and Aerospace Technology, 86(6)
- Goulos I, Hempert F, Sethi V, Pachidis V, d'Ippolito R, .... (2013). Rotorcraft Engine Cycle Optimization at Mission Level. Journal of Engineering for Gas Turbines and Power, 135(9)
- Goulos I, Giannakakis P, Pachidis V & Pilidis P. (2013). Mission Performance Simulation of Integrated Helicopter–Engine Systems Using an Aeroelastic Rotor Model. Journal of Engineering for Gas Turbines and Power, 135(9)
- Gallar L, Volpe V, Salussolia M, Pachidis V & Jackson A. (2012). Thermodynamic Gas Model Effect on Gas Turbine Performance Simulations. Journal of Propulsion and Power, 28(4)
- Goulos I, Pachidis V, d’Ippolito R, Stevens J & Smith C. (2012). An Integrated Approach for the Multidisciplinary Design of Optimum Rotorcraft Operations. Journal of Engineering for Gas Turbines and Power, 134(9)
- 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, 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)
- Gallar L, Calcagni C, Llorens C & Pachidis V. (2011). Time accurate modelling of the secondary air system response to rapid transients. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 225(8)
- Gallar L, Arias M, Pachidis V & Singh R. (2011). Stochastic axial compressor variable geometry schedule optimisation. Aerospace Science and Technology, 15(5)
- Templalexis I, Pachidis V, Pilidis P & Kotsiopoulos P. (2010). The effect of upstream duct boundary layer growth and compressor blade lean angle variation on an axial compressor performance. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 224(8)
- Pachidis V, Templalexis I, Pilidis P & Kotsiopoulos P. (2010). A dynamic convergence control scheme for the solution of the radial equilibrium equation in through-flow analyses. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 224(7)
- Pachidis V, Pilidis P, Templalexis I, Barbosa JB & Nantua N. (2007). A de-coupled approach to component high-fidelity analysis using computational fluid dynamics. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 221(1)
- Pachidis V, Pilidis P, Texeira J & Templalexis I. (2007). A comparison of component zooming simulation strategies using streamline curvature. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 221(1)
- Pachidis V, Pilidis P, Marinai L & Templalexis I. (2007). Towards a full two dimensional gas turbine performance simulator. The Aeronautical Journal, 111(1121)
- Pachidis VA, Pilidis P, Alexander T, Kalfas A & Templalexis I. (2006). Advanced Performance Simulation of A Turbofan Engine Intake. Journal of Propulsion and Power, 22(1)
- Monokrousos N, Könözsy L, Pachidis V, Sozio E & Rossi F. Temperature-dependent solid material properties of GRCop-42 for an additively manufactured liquid rocket engine LOx cooling channel. Multidiszciplináris Tudományok, 14(3)
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
- Vitlaris D, Rajendran DJ, Tunstall R, Whurr J & Pachidis V. (2024). On Hysteresis in a Variable Pitch Fan Transitioning to Reverse Thrust Mode and Back
- Lamprakis D, Rajendran DJ, Santhanakrishnan M, Coskun S, Roumeliotis I, .... (2024). On Leakage Flows in a Liquid Hydrogen Multi-Stage Pump for Aircraft Engine Applications
- Rompokos P, Sasi S, Mourouzidis C, Roumeliotis I, Pachidis V, .... (2024). Integrated Performance Assessment and Decarbonising Potential for Aircraft Retrofitted With Sustainable Aviation Fuels
- Coskun S, Rajendran DJ, Pachidis V & Bacic M. (2024). Acoustic Excitation As a Flow Control Technique in a High-Speed Compressor Cascade
- 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
- Monokrousos N, Könözsy L, Pachidis V, Sozio E & Rossi F. (2024). NUMERICAL SOLUTION OF LOX FLOW IN A LIQUID ROCKET ENGINE ADDITIVELY MANUFACTURED COOLING CHANNEL
- Chen X, Isoldi A, Riaz A, Mourouzidis C, Keskin A, .... (2023). Evaluation of a Collaborative and Distributed Aircraft Design Environment, Enabled by Microservices and Cloud Computing
- Coskun S, Rajendran DJ, Pachidis V & Bacic M. (2023). Effect of Acoustic Excitation Amplitude on Flow Separation over NACA0015 Aerofoil for Near-Stall Angle-of-Attacks
- Coskun S, Rajendran DJ, Pachidis V & Bacic M. (2023). Control of Flow Separation in a High-speed Compressor Cascade Through Acoustic Excitation
- Kissoon S, Righi M, Pawsey L, Pachidis V, Tunstall R, .... (2023). A Characteristic-Based 1D Axial Compressor Model for Stall and Surge Simulations
- Ghelani R, Roumeliotis I, Saias CA, Mourouzidis C, Pachidis V, .... (2023). Integrated Hybrid Engine Cycle Design and Power Management Optimization
- Sasi S, Mourouzidis C, Roumeliotis I, Nikolaidis T, Pachidis V, .... (2023). Impacts of Alternative Aviation Fuels on Engine Cycle Design and Aircraft Mission Capability
- Palaveev K, Rajendran DJ, Anselmi E, Santhanakrishnan M & Pachidis V. (2023). Insights Into the Flow Field and Performance of a Boundary Layer Pump
- Vitlaris D, Rajendran DJ, Pachidis V, Tunstall R & Whurr J. (2023). On the Flow Physics During the Transition of a Variable Pitch Fan From Nominal Operation to Reverse Thrust Mode
- Ghelani R, Roumeliotis I, Saias CA, Mourouzidis C, Pachidis V, .... (2023). INTEGRATED HYBRID ENGINE CYCLE DESIGN AND POWER MANAGEMENT OPTIMIZATION
- Sasi S, Mourouzidis C, Roumeliotis I, Nikolaidis T, Pachidis V, .... (2023). IMPACTS OF ALTERNATIVE AVIATION FUELS ON ENGINE CYCLE DESIGN AND AIRCRAFT MISSION CAPABILITY
- van Heerden ASJ, Ippedico S, Rajendran DJ, Anselmi-Palma E, Roumeliotis I, .... (2023). Performance Analysis of an Engine-Mounted Compression System for Aircraft Environmental Control
- Tsentis S, Goulos I, Prince S, Pachidis V & Zmijanovic V. (2023). Propulsion Aerodynamics for a Novel High-Speed Exhaust System
- Coskun S, Pachidis V, Ubulom I & Bacic M. (2022). Improved Delayed Detached Eddy Simulations Applied to a NACA0015 Aerofoil Subject to Acoustic Excitation
- Tió FR, Azamar H & Pachidis V. (2022). A Method For The Characterization Of Fans Down To Zero Speed And Analysis Of Bypass Reverse Flow During Ground
- Anselmi E, Belleoud P, Roumeliotis I & Pachidis V. (2022). Update of the sCO2-Test Rig at Cranfield University
- Rajendran DJ, Tunstall R & Pachidis V. (2022). Estimation of Resultant Airframe Forces for a Variable Pitch Fan Operating in Reverse Thrust Mode
- Ghelani R, Roumeliotis I, Saias CA, Mourouzidis C, Pachidis V, .... (2022). Design Methodology and Mission Assessment of Parallel Hybrid Electric Propulsion Systems
- 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
- Rajendran DJ & Pachidis V. (2021). On the Use of an Inflatable Rubber Lip to Improve the Reverse Thrust Flow Field in a Variable Pitch Fan
- Scullion C, Vouros S, Goulos I, Nalianda D & Pachidis V. (2020). Optimal Control of a Compound Rotorcraft for Engine Performance Enhancement
- Roumeliotis I, Arena F, Liu Y, Vouros S, Pachidis V, .... (2020). Performance and Emission Assessment of Thermo-Electric Power Plant for Rotorcraft Propulsion
- Roumeliotis I, Castro L, Jafari S, Pachidis V, De Riberolles L, .... (2020). Integrated Systems Simulation for Assessing Fuel Thermal Management Capabilities for Hybrid-Electric Rotorcraft
- Roig Tió F, Ferrer-Vidal LE, Azamar Aguirre H & Pachidis V. (2020). Considerations on Axial Compressor Bleed for Sub-Idle Performance Models
- Larrieta O, Alonso R, Escobar ÓP, Eryilmaz I & Pachidis V. (2020). Design Space Exploration of Turbine Blade Shroud Interlock for Flutter Stability
- Templalexis I, Pachidis V & Hasani A. (2020). Comparative Assessment of Fouling Scenarios in an Axial Flow Compressor
- Rajendran DJ & Pachidis V. (2020). Flow Distortion Into the Core Engine for an Installed Variable Pitch Fan in Reverse Thrust Mode
- Righi M, Pachidis V, Könözsy L, Zhao F & Vadhati M. (2020). Three-dimensional low-order surge model for high-speed axial compressors
- Rajendran DJ, Bentley D, Aguirre HA, Tunstall R & Pachidis V. (2020). Development of a Research Model to Study the Operability of a Variable Pitch Fan Aero Engine In Reverse Thrust
- Righi M, Ferrer-Vidal LE, Allegretti A & Pachidis P. (2020). Low-order models for the calculation of compressor sub-idle characteristics
- Kissoon S, Fan Z, Mourouzidis C, Roumeliotis I & Pachidis V. (2020). Assessment of the performance boundaries of very low specific thrust direct-drive turbofan engines at aircraft level for EIS 2025
- Vouros S, Goulos I, Scullion C, Nalianda D & Pachidis V. (2019). Impact of wake modeling uncertainty on helicopter rotor aeroacoustic analysis
- Rajendran DJ & Pachidis V. (2019). Fan Flow Field in an Installed Variable Pitch Fan Operating in Reverse Thrust for a Range of Aircraft Landing Speeds
- Stevens J, Rademaker E, Scullion C, Vouros S, Nalianda D, .... (2019). Design evaluation and performance assessment of rotorcraft technology by 2050
- Aguirre HA, Pachidis V & Templalexis I. (2019). An Analytical Shock-Loss Model Fully Integrated to a Streamline Curvature Method for Axial-Flow Compressors
- Roumeliotis I, Mourouzidis C, Zafferetti M, Pachidis V, Broca O, .... (2019). Assessment of Thermo-Electric Power Plants for Rotorcraft Application
- Anselmi E, Bunce I & Pachidis V. (2019). An Overview of Initial Operational Experience With the Closed-Loop sCO2 Test Facility at Cranfield University
- Roumeliotis I, Nikolaidis T, Pachidis V, Broca O & Unlu D. (2018). Dynamic simulation of a rotorcraft hybrid engine in Simcenter Amesim
- 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 E, Bunce I, Pachidis V, Zachos P & Johnston M. (2018). An overview of the Rolls-Royce sCO2-test rig project at Cranfield University
- Ferrer-Vidal LE, Pachidis V & Tunstall RJ. (2018). An enhanced compressor sub-idle map generation method
- Eryilmaz I, Pawsey L & Pachidis V. (2018). Multidisciplinary methodology for turbine overspeed analysis
- Azamar H, Pachidis V & Templalexis I. (2017). Development of a streamline curvature axial-flow compressor performance simulator graphical-user-interface for design and research
- Azamar H, Pachidis V & Templalexis I. (2017). An improved streamline curvature-based design approach for transonic axial-flow compressor blading
- Ortiz-Carretero J, Castillo Pardo A, Pachidis V & Goulos I. (2017). Assessment of the Effect of Environmental Conditions on Rotorcraft Pollutant Emissions at Mission Level
- Pawsey L, Rajendran DJ & Pachidis V. (2017). Aerodynamic Performance of an Unlocated High Pressure Turbine Rotor With Worn Tip Seal Fins
- Enconniere J, Ortiz-Carretero J, Goulos I, Pachidis V, Smith C, .... (2017). The impact of clean sky technology on future 3500 lb single engine light rotorcraft
- Pawsey L, Rajendran DJ & Pachidis V. (2017). Aerodynamic performance of an un-located high-pressure turbine rotor
- Pawsey L, Rajendran DJ & Pachidis V. (2017). Aerodynamic performance of an unlocated high pressure turbine rotor with worn tip seal fins
- Templalexis I, Alexiou A, Pachidis V, Roumeliotis I & Aretakis N. (2016). Direct Coupling of a Two-Dimensional Fan Model in a Turbofan Engine Performance Simulation
- Ali F, Goulos I & Pachidis V. (2016). Improvements in the rotorcraft fuel economy and environmental impact through multiple-landing mission strategy
- Stevens J, Smith C, Thevenot L, D'Lppolito R, Gires E, .... (2016). CleanSky green rotorcraft new technologies - Maximizing noise and emissions benefits
- Stevens J, Smith C, Thevenot L, D'Ippolito R, Gires E, .... (2016). CleanSky green rotorcraft new technologies - Maximizing noise and emissions benefits
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d’Ippolito R. (2015). Design Space Exploration and Optimization of Conceptual Rotorcraft Powerplants
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d'Ippolito R. (2015). An advanced rotorcraft powerplant optimization at mission level: Towards high fidelity engine design optimization
- Ali F, Tzanidakis K, Goulos I, Pachidis V & D'Ippolito R. (2015). Conceptual design and optimisation of an advanced rotorcraft powerplant architecture
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d’Ippolito R. (2015). Multi-Objective Optimization of a Regenerative Rotorcraft Powerplant: Quantification of Fuel Economy and Environmental Impact
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d'Ippolito R. (2015). Multi-objective optimization of a regenerative rotorcraft powerplant: Quantification of overall engine weight and fuel economy
- Stevens J, Smith C, Pachidis V, Thevenot L & D'Ippolito R. (2015). Cleansky green rotorcraft noise and emissions benefits - Maximizing the impact of new technologies
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d'Ippolito R. (2015). Multi-objective Optimization of Conceptual Rotorcraft Powerplants: Trade-off between Rotorcraft Fuel Efficiency and Environmental Impact
- Ali F, Tzanidakis K, Goulos I, Pachidis V & d'Ippolito R. (2015). Multi-objective optimization of a regenerative rotorcraft powerplant: quantification of overall engine weight and fuel economy
- Smith C, Karamolegkos K, Goulos L, Pachidis V, Stevens J, .... (2014). Achieving rotorcraft noise and emissions reduction for 'Clean Sky' - The measurement of success
- Ali F, Goulos I, Tzanidakis K, Pachidis V & d’Ippolito R. (2014). A Multidisciplinary Approach for the Comprehensive Assessment of Integrated Rotorcraft–Powerplant Systems at Mission Level
- Fakhre A, Syed M, Goulos I & Pachidis V. (2014). A preliminary parametric study for an advanced propulsion technology helicopter
- Karamolegkos K, Goulos I, Pachidis V, Stevens J, Smith C, .... (2014). Helicopter Mission Analysis Using a Multidisciplinary Simulation Framework
- Pardo AC, Mehdi A, Pachidis V & MacManus DG. (2014). Numerical Study of the Effect of Multiple Tightly-Wound Vortices on a Transonic Fan Stage Performance
- Ali F, Tzanidakis K, Goulos I, Pachidis V & D'Ippolito R. (2014). Multidisciplinary design and optimization of conceptual powerplant configurations targeting improved rotorcraft operational performance
- 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
- Gonzalez A & Pachidis V. (2014). On the Numerical Simulation of Turbine Blade Tangling After a Shaft Failure
- Zoppellari S & Pachidis V. (2014). Unsteady Compressor Performance Assessment Using Euler Solvers
- Fakhre A, Tzanidakis K, Goulos I, Pachidis V & Ippolito RD. (2014). Optimized powerplant configurations for improved rotorcraft operational performance
- Goulos I & Pachidis V. (2014). Real-time simulation of rotor blade aeroelasticity for the multidisciplinary design of rotorcraft
- Goulos I & Pachidis V. (2014). Real-Time Simulation of Rotor Blade Aeroelasticity for the Multidisciplinary Design of Rotorcraft
- Fakhre A, Tzanidakis K, Goulos I, Pachidis V & D'Ippolito R. (2014). Optimized powerplant configurations for improved rotorcraft operational performance
- Fakhre A, Pachidis V, Goulos I, Pervier H & Tashfeen M. (2013). Helicopter mission analysis for a regenerative turboshaft engine
- Sanchez de Leon L, Zachos PK & Pachidis V. (2013). A Comparative Assessment of Dry Gas Turbine Cycles for Marine Applications
- Goulos I, Giannakakis P, Pachidis V & Pilidis P. (2013). Mission Performance Simulation of Integrated Helicopter–Engine Systems Using an Aeroelastic Rotor Model
- Fakhre A, Pachidis V, Goulos I, Tashfeen M & Pilidis P. (2013). Helicopter Mission Analysis for a Regenerated Turboshaft
- Goulos I, Hempert F, Sethi V, Pachidis V, d’Ippolito R, .... (2013). Rotorcraft Engine Cycle Optimization at Mission Level
- Ben Sghaier T, Mehdi A, Pachidis V & MacManus D. (2013). A Parametric Numerical Study of the Effects of Inlet Swirl Distortion on a Transonic Compressor Stage
- 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
- Goulos L, Hempert F, Sethi V, Pachidis V, d'Ippolito R, .... (2013). Rotorcraft engine cycle optimization at mission level
- Koupper C, Grech N, Zachos PK, Pachidis V & Singh R. (2012). Considerations on the Numerical Modelling and Performance of Axial Swirlers Under Relight Conditions
- Goulos I, Pachidis V, d’Ippolito R, Stevens J & Smith C. (2012). An Integrated Approach for the Multidisciplinary Design of Optimum Rotorcraft Operations
- McLelland G, di Cugno D, MacManus DG & Pachidis V. (2012). Boundary Conditions for Vortex CFD Simulations
- Castaneda J, Mehdi A, di Cugno D & Pachidis V. (2011). A Preliminary Numerical CFD Analysis of Transonic Compressor Rotors When Subjected to Inlet Swirl Distortion
- Zachos PK, Ruelke C, Pachidis V & Singh R. (2011). Compressor Blade Modelling Under Highly Negative Incedence
- Templalexis I, Pilidis P, Pachidis V & Kotsiopoulos P. (2011). Development of a Two-Dimensional Streamline Curvature Code
- 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
- Rojo I, Psarra A, Pachidis V & Pilidis P. (2010). Evaluation of the Energy Dissipated as Friction/Heat Between Turbines Following Shaft Failure
- Gallar L, Tzagarakis I, Pachidis V & Singh R. (2010). Compressor Performance 2D Modelling at Reverse Flow Conditions
- Aslanidou I, Zachos PK, Pachidis V & Singh R. (2010). A Physically Enhanced Method for Sub-Idle Compressor Map Generation and Representation
- Kipouros T, Pachidis V, Ghisu T & Templalexis I. (2010). Characterisation of the Uncertainties of the Operating Conditions in Turbomachinery Design
- Capozzi P, Psarra A, Pachidis V & Pilidis P. (2010). A Finite Element Approach of Turbines in Contact Following a Shaft Failure Event
- d'Ippolito R, Stevens J, Pachidis V, Berta A, Goulos I, .... (2010). A Multidisciplinary Simulation Framework for Optimization of Rotorcraft Operations and Environmental Impact
- Goulos I, Mohseni M, Pachidis V, D’Ippolito R & Stevens J. (2010). Simulation Framework Development for Helicopter Mission Analysis
- Goulos I, Pachidis V, Celis C, D’Ippolito R & Stevens J. (2010). Simulation Framework Development for Aircraft Mission Analysis
- Kozaily J, Zachos PK, Pachidis V & Singh R. (2009). Gas Turbine Fuel Atomisation Dynamics Under Sub-atmospheric Conditions
- Gallar L, Calcagni C, Pachidis V & Pilidis P. (2009). Development of a One-Dimensional Dynamic Gas Turbine Secondary Air System Model—Part I: Tool Components Development and Validation
- Calcagni C, Gallar L & Pachidis V. (2009). Development of a One-Dimensional Dynamic Gas Turbine Secondary Air System Model—Part II: Assembly and Validation of a Complete Network
- Gallar L, Pachidis V, Zachos PK & Singh R. (2009). Compressor IGV Off Design Performance and Loss Modelling
- Li YG, Marinai L, Gatto EL, Pachidis V & Philidis P. (2009). Multiple-Point Adaptive Performance Simulation Tuned to Aeroengine Test-Bed Data
- 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
- Gallar L, Arias M, Pachidis V & Pilidis P. (2009). Compressor Variable Geometry Schedule Optimisation Using Genetic Algorithms
- Psarra A, Pachidis V & Pilidis P. (2009). Finite Element Turbine Blade Tangling Modelling Following a Shaft Failure
- Pachidis V, Templalexis I & Pilidis P. (2009). A Dynamic Convergence Control Algorithm for the Solution of Two-Dimensional Streamline Curvature Methods
- Pachidis V, Templalexis I & Pilidis P. (2009). Convergence Stability of Through-Flow Analyses via the Implementation of the Secant and Bisection Iteration Schemes
- Templalexis I, Pachidis V & Kotsiopoulos P. (2009). Compensation of Intake Induced Flow Non-Uniformities With Compressor Blade Lean Angle Changes
- Muhammad Hassan Rizvi S, Ramsden KW & Pachidis V. (2009). Preliminary Design of a High Bypass Ratio Turbofan Engine
- Nikolaidis T, Pilidis P, Teixeira JA & Pachidis V. (2008). Water Film Formation on an Axial Flow Compressor Rotor Blade
- Rousselot S, Truffi D, Doulgeris G, Mistry S, Pachidis V, .... (2008). Generation of a Quasi 3-D Map of a Half-Embedded Ultra High Bypass Ratio Turbofan Intake on the Wing of a Broad Delta Wing Airframe
- Templalexis I, Pachidis V, Pilidis P & Kotsiopoulos P. (2008). The Effect of Blade Lean on the Solution of the Full Radial Equilibrium Equation
- Pachidis V, Pilidis P, Templalexis I & Marinai L. (2008). An Iterative Method for Blade Profile Loss Model Adaptation Using Streamline Curvature
- Pachidis V, Pilidis P & Li I. (2007). Training Future Gas Turbine Performance Engineers
- Bala A, Sethi V, LoGatto E, Pachidis V & Pilidis P. (2007). Study of VSV Effects on Performance via Integrated Aerodynamic Component Zooming Process
- Pachidis V, Pilidis P, Templalexis I & Kotsiopoulos P. (2007). 2D engine performance simulation using streamline curvature componentmodels
- Templalexis I, Pilidis P, Pachidis V & Kotsiopoulos P. (2007). A Fast Gas Turbine Engine Performance Analysis Tool Able to Capture Three Dimensional Effects
- Pachidis V, Pilidis P, Templalexis I & Marinai L. (2007). An Iterative Method for Blade Profile Loss Model Adaptation Using Streamline Curvature
- Pachidis V, Pilidis P, Templalexis I, Korakianitis T & Kotsiopoulos P. (2007). Prediction of Engine Performance Under Compressor Inlet Flow Distortion Using Streamline Curvature
- Templalexis IK, Kotsiopoulos P & Pachidis V. (2007). Intake - Compressor performance characteristic under inlet flow total pressure distortion
- Templalexis IK, Kotsiopoulos P & Pachidis V. (2007). Intake - Compressor performance characteristic under inlet flow total pressure distortion
- Pachidis V, Pilidis P, Templalexis I & Kotsiopoulos P. (2007). 2D engine performance simulation using streamline curvature componentmodels
- Templalexis I, Pilidis P, Pachidis V & Kotsiopoulos P. (2006). Development of a 2-D Compressor Streamline Curvature Code
- Melloni L, Kotsiopoulos P, Jackson A, Pachidis V & Pilidis P. (2006). Military Engine Response to Compressor Inlet Stratified Pressure Distortion by an Integrated CFD Analysis
- Pachidis V, Pilidis P, Templalexis I, Alexander T & Kotsiopoulos P. (2006). Prediction of Engine Performance Under Compressor Inlet Flow Distortion Using Streamline Curvature
- Templalexis I, Pilidis P, Pachidis V & Kotsiopoulos P. (2006). Quasi-Three-Dimensional Compressor Performance Simulation Using Streamline Curvature and Multi-Parallel Compressor Theory
- Pachidis V, Pilidis P, Talhouarn F, Kalfas A & Templalexis I. (2006). A Fully Integrated Approach to Component Zooming Using Computational Fluid Dynamics
- Templalexis I, Pilidis P, Guindeuil G, Lekas T & Pachidis V. (2005). 3D Simulation of a Convergent-Divergent Aero Engine Intake, Using Two Different CFD Methods
- Templalexis I, Pilidis P, Guindeuil G, Kotsiopoulos P & Pachidis V. (2005). Aero Engine Axi-Symmetric Convergent-Constant Area Intake 3D Simulation Using a Panel Method Approach
- Pachidis V, Pilidis P, Talhouarn F, Kalfas A & Templalexis I. (2005). A Fully Integrated Approach to Component Zooming Using Computational Fluid Dynamics
- Pachidis V, Pilidis P, Guindeuil G, Kalfas A & Templalexis I. (2005). A Partially Integrated Approach to Component Zooming Using Computational Fluid Dynamics
- Zilli A, Pachidis V, Jackson A & Pilidis P. (2005). CFD Investigation of the Performance of a Military HP Axial Turbine Subjected to Inlet Temperature Distortion
- Charalambous N, Ghisu T, Iurisci G, Pachidis V & Pilidis P. (2004). Axial Compressor Response to Inlet Flow Distortions by a CFD Analysis
- Pachidas VA & Singh R. (2002). Investigation of a Fuel Cell-Powered Blended Wing Body Airliner With Boundary Layer Re-Energization
- Ali F, Goulos I, Tzanidakis K, Pachidis V & D'Ippolito R. A multidisciplinary approach for the comprehensive assessment of integrated rotorcraft-powerplant systems at mission level