Contact Dr David John Rajendran
- Tel: +44 (0) 1234 754571
- Email: D.Rajendran@cranfield.ac.uk
- ORCID
Areas of expertise
- Computational Fluid Dynamics
- Computing, Simulation & Modelling
- Design, Strategy & Innovation
- Gas Turbines & Propulsion
Background
David John is a Lecturer within the Rolls-Royce University Technology Centre for Aero Systems Design, Integration and Performance at Cranfield University. He specialises in aero systems design for future propulsion architectures. David graduated with distinction in his bachelor's degree in Aeronautical Engineering from Madras Institute of Technology, India. After his graduation, he worked at the Gas Turbine Research Establishment in the design and development of turbines for various applications. Thereafter, he enrolled in the Gas Turbine Technology Master's degree at Cranfield University. In his Master's programme, his research looked into the turbine aerodynamic behaviour in overspeed conditions. Subsequently, he did his doctoral research within the Rolls-Royce University Technology Centre at Cranfield University where he explored the design space of using Variable Pitch Fans for reverse thrust in future efficient, environment friendly, civil gas turbines.
David has received several prestigious awards in both the academia and the industry like the stipendiary fellowship of the Aeronautics Research and Development Board, Government of India 2009, Rear Admiral A K Hando Trophy 2010, Government of India Young Scientist Award 2014, Royal Aeronautical Society (RAeS) NE Rowe Award 2016 and Cranfield Branch Annual Lecture Award 2016, Roy Fedden Memorial Prize 2017, American Society of Mechanical Engineers (ASME) Turbo Expo Best Paper Awards 2019 and 2020, Lord Kings Norton Medal 2020, and the ASME John P Davis Award 2020 and 2021. He has a total of 22 high impact journal and conference publications along with a editorial role for a special issue of Journal of Aerospace Sciences and Technologies. He has jointly filed 10 patent applications to date. He is a Member of the RAeS, ASME and the Aeronautical Society of India. He has been member of several peer review and preliminary design review committees, concept study and funding bid development teams, and has contributed in the organization of several high profile conferences and working committees. He is a peer-reviewer for several International gas turbine conferences, Journal of Aerospace Sciences and Technologies and the ASME Turbo Expo.
Research opportunities
David's research expertise is in integrated system design space exploration with different levels of modelling fidelity. Interdisciplinary design and research challenges with a focus on fluid dynamic design optimization across aerospace, energy and other industries are welcome for Masters and doctoral projects. Design exploration studies to optimize fluid processes with a focus on NetZero and future sustainable aviation are particularly welcome.
Current activities
David's research interests include development of robust high fidelity methods for numerical flow solutions in complete integrated systems and system level interdependency explorations to develop optimum aerodynamic designs for future propulsion architectures. He plays an active role in InnovateUK project PINES led by Rolls-Royce plc. and in several other industrially funded doctoral programmes and projects. David's research expertise in flow modelling is used in several other EU and industry funded projects within the Centre. He is also involved in integrated modelling of experimental facilities, exploration of unconventional flows, design code development for quick concept studies, exploratory flow modelling with hydrogen and supercritical fluids, and multi-disciplinary optimization.
Clients
Rolls-Royce plc.
InnovateUK
Siemens Industry Software Limited.
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)
- 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)
- 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
- Bakogianni A, Anselmi Palma E, Rajendran DJ, Bufalari L, Talluri L, .... (2024). Multidisciplinary design and manufacturing of a Tesla pump prototype. Applied Thermal Engineering, 255
- 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
- Freschi R, Bakogianni A, Rajendran DJ, Anselmi Palma E, Talluri L, .... (2023). Flow field explorations in a boundary layer pump rotor for improving 1D design codes. Designs, 7(1)
- Rajendran DJ, Palaveev K, Anselmi Palma E, Santhanakrishnan M & Pachidis V. (2023). 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. (2023). 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)
- 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)
- 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)
- 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)
- Pawsey L, Rajendran DJ & Pachidis V. (2017). Characterisation of turbine behaviour for an engine overspeed prediction model. Aerospace Science and Technology, 73
- Sasi S, Mourouzidis C, Rajendran DJ & Roumeliotis I. Hydrogen & Ammonia Powered Turbofan Design Implications For Next Generation Of Aircraft Engines. Journal of Engineering for Gas Turbines and Power