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Contact

Visit Abdulnaser Sayma

C111, College Building

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Postal Address

City, University of London
Northampton Square
London
EC1V 0HB
United Kingdom

About

Overview

Professor Sayma obtained BSc in Mechanical Engineering with Distinction from Birzeit University in Palestine in 1987, MSc in Energy Technology from Salford University in 1990 and PhD from UMIST in 1994. His thesis topic was Finite Element model for dense gas dispersion in the atmosphere. He joined the Aeronautics department at Imperial College London in 1994 on EPSRC funded project as a research assistant where he worked on the development of an external aerodynamic compressible flow model introducing boundary layer grids and viscous effects in the Euler solver.

In 1996, he joined the Rolls Royce Vibration University Technology Centre (VUTC) at the Department of Mechanical Engineering, Imperial College London, where he stayed for about 9 years. He progressed to a Research Fellow, Senior Research Fellow and then Principal Research Fellow. In 2001, he was awarded the title RolIs Royce reaserch fellow at Imperial College and in 2003 he was awarded a Royal Academy of Engineering Senior Research Fellow co-funded by Rolls-Royce Plc. During his spell at the VUTC, he was one of two main developers for the unsteady aerodynamics and aeroelatisity code AU3D which has been the main aeroelasticity system at Rolls Royce. He also contributed to several major aero-engine projects including analysis of compressors, fans, turbines, rotating cavities, intake and bypass ducts and downstream nozzles.

In 2005 he became a Senior Lecturer in Computational Mechanics at Brunel University. A year later, he was given a Chair in Computational Fluid Dynamics at the University of Sussex where he worked at the Thermo-Fluid Mechanics Research Centre (TFMRC) at the Department of Engineering and Design. He continued to lead research in unsteady compressible flow in turbomacinery, where he focused on industrial gas turbines and micro-gas turbines. He held several senior administrative positions, the last of which was the Director of Research and Knowledge Exchange for the School of Engineering and Informatics. He also introduced a new MSc in Sustainable Energy Technology.

In January 2013, he joined City University London as a Professor of Energy Engineering. He is currently leading EU FP7 consortium for conducting research and demonstration of a concentrated solar power system powering a small-scale micro-gas turbine. He is also conducting research in waste heat recovery using small scale Organic Rankine Cycle (ORC) in addition to continued activity in turbomachinery CFD and aeroelasticity.He has been an active member of the European Turbine Network (ETN), based in Brussels, which coordinates European industrial gas turbine activities across the whole value chain. He has been the chairman of the Cycle Efficiency Technical Committee and he is currently a member of the ETN project board.

Qualifications

Diploma Certificate of Advanced Teaching and Learning, Imperial College London, 2004
PhD Finite Element Modelling (CFD) of Dense Gas Dispersion in the Atmosphere, UMIST, 1994
MSc Energy Technology for Developing Countries, Salford University, 1990
BSc Mechanical Engineering, Birzeit University, 1987

Employment

01/2013 - to date City University London, Professor
12/2006 - 12/2013 University of Sussex, Professor of Computational Fluid Dynamics
12/2005 - 11/2006 Brunel University, Senior Lecturer in Computational Mechanics
02/1994 - 11/2005 Imperial College London, Research Assistant, Research Fellow, Senior research Fellow, Principal Research Fellow, Royal Society Senior Research Fellow

Membership of professional bodies

2007 Institution of Mechanical Engineers, Fellow
2004 High Education Academy, Fellow
1998 Royal Aeronautical Society, Member

Research

Research interests

- Unsteady Aerodynamics and Aeroelaticity
- Gas Turbines for jet propulsion
- Industrial gas Turbines
- Micro-gas turbines
- Energy systems including solar power and waste heat recovery

Publications

Books (3)

  1. Sayma, A. Computational Fluid Dynamics. Bookboon. ISBN 978-87-7681-430-4.
  2. Long, C. and Sayma, N. Heat Transfer. Bookboon. ISBN 978-87-7681-432-8.
  3. Long, C. and Sayma, N. Heat Transfer: Exercises. Bookboon. ISBN 978-87-7681-433-5.

Chapters (6)

  1. Sayma, A., Vahdati, M., Wu, X. and Imregun, M. (2003). Recent developments in unsteady flow modelling for turbomachinery aeroelasticity. In Elder, R.L., Towlidakis, A. and Yates, M.K. (Eds.), Advnaces of CFD in Fluid Machinery Design IMechE.
  2. Vahdati, M., Sayma, A. and Imregun, M. (1999). Case studies in Turbomachinery Aeroelasticity using an integrated 3D non-linear method. In Sieverding, C.H. and Fransson, T.H. (Eds.), Aeroelasticity in axial-flow turbomachines, Lecture Series Karman Institute for Fluid Dynamics.
  3. Sayma, A., Vahdati, M., Green, J.S. and Imregun, M. (1998). Whole-assembly flutter analysis of a low pressure turbine blade. In Fransson ed, T.H. (Ed.), Unsteady Aerodynamics and Aeroelasticity of Turbomachines (pp. 347–359). Kluwer Academic Publishers, Dordrecht.
  4. Sbardella, L., Sayma, A. and Imregun, M. (1998). Semi-unstructured mesh generator for flow calculations in axial turbomachinery blading. In Fransson, T.H. (Ed.), Unsteady Aerodynamics and Aeroelasticity of Turbomachines (pp. 541–554). Kluwer Academic Publishers, Dordrecht.
  5. Piero, J. and Sayma, A. (1996). A 3-D unstructured multigrid Navier-Stokes solver. In Morton, K.W. and Baines, M.J. (Eds.), Numerical Methods for Fluids Dynamics Oxford University Press.
  6. Sayma, A. Gas Turbines for Marine Applications. In Carlton, J., Jukes, P. and Sang, C.-.Y. (Eds.), Encyclopedia of Maritime and Offshore Engineering, online John Wiley & Sons, Ltd.. ISBN 978-1-118-47640-6.

Conference Papers and Proceedings (36)

  1. Arroyo, A., McLorn, M., Fabian, M., White, M. and Sayma, A.I. (2016). Rotor-dynamics of different shaft configurations for a 6 KW micro gas turbine for concentrated solar power. .
  2. White, M. and Sayma, A.I. (2016). Investigating the effect of changing the working fluid on the three-dimensional flow within organic rankine cycle turbines. .
  3. Li, Y.L. and Sayma, A. (2014). Numerical investigation of VSVs mal-schedule effects in a threestage axial compressor. .
  4. Nucara, P. and Sayma, A. (2012). Effects of using Hydrogen-rich syngas in industrial gas turbines while maintaining fuel flexibility on a multistage axial compressor design. .
  5. Li, Y. and Sayma, A. (2012). Effects of blade damage on the performance of a transonic axial compressor rotor. .
  6. Moghaddam, E.R., Coren, D., Long, C. and Sayma, A. (2011). A numerical investigation of moment coefficient and flow structure in a rotor-stator cavity with rotor mounted bolts. .
  7. Wang, F., Sayma, A.I., Peng, Z.J. and Huang, Y. (2011). A multi-section droplet combustion model for spray combustion simulation. .
  8. Nucara, P. and Sayma, A. (2011). Effects of using Hydrogen-rich Syngas in industrial gas turbines while maintaining fuel flexibility on compressor design. .
  9. Bohari, B. and Sayma, A. (2010). CFD analysis of effects of damage due to bird strike on fan performance. .
  10. Wang, F., Leboeuf, F., Huang, Y., Zhou, L.X. and Sayma, A.I. (2010). An algebraic sub-grid scale turbulent combustion model. .
  11. Swalen, M.J.P., Koenig, C.S., Sayma, A.I. and Khir, A.W. (2010). CFD MODELLING OF A BI-DIRECTIONAL AXIAL FLOW LVAD. .
  12. Wang, F., Leboeuf, F., Huang, Y., Zhou, L.X., Sayma, A.I. and ASME, (2010). AN ALGEBRAIC SUB-GRID SCALE TURBULENT COMBUSTION MODEL. .
  13. Patel, K.N., Koenig, C.S., Sayma, A.I. and Khir, A.W. (2009). TRANSIENT BEHAVIOR OF DIFFERENT IMPELLER DESIGN OF A PULSATILE AXIAL FLOW LVAD: A COMPUTATIONAL STUDY. .
  14. Swalen, M.J.P., Koenig, C.S., Sayma, A.I. and Khir, A.W. (2009). COMPUTATIONAL STUDY OF A NOVEL AXIAL FLOW PUMP AS LVAD. .
  15. Swalen, M.J.P., Koenig, C.S., Sayma, A.I. and Khir, A.W. (2008). DEVELOPMENT OF A NOVEL VENTRICULAR ASSIST DEVICE (VAD). .
  16. Sayma, A.I. (2007). Steady-flow analysis of low pressure compression system for turbofan engines. .
  17. Sladojević, I., Sayma, A.I. and Imregun, M. (2007). Influence of stagger angle variation on aerodynamic damping and frequency shifts. .
  18. Sayma, A.I., Vahdti, M., Imregun, M. and Marshal, J. (2007). Low-pressure compression system effects on fan assembly forced response. .
  19. Saiz, G., Imregun, M. and Sayma, A.I. (2006). A multi blade-row linearised analysis method for flutter and forced response predictions in turbomachinery. .
  20. Sladojević, I., Petrov, E.P., Imregun, M. and Sayma, A.I. (2006). Forced response variation of aerodynamically and structurally mistuned turbo-machinery rotors. .
  21. Wilson, M.J., Imregun, M. and Sayma, A.I. (2006). The effect of stagger variability in gas turbine fan assemblies. .
  22. Di Mare, L., Simpson, G. and Sayma, A.I. (2006). Fan forced response due to ground vortex ingestion. .
  23. Di Mare, L., Simpson, G., Mueck, B. and Sayma, A.I. (2006). Effect of bleed flows on flutter and forced response of core compressors. .
  24. Di Mare, L., Sayma, A.I., Coupland, J. and Imregun, M. (2005). Acoustic liner models in a general purpose CFD code. .
  25. Wilson, M.J., Imregun, M. and Sayma, A.I. (2005). The effect of stagger variability in gas turbine fan assemblies. .
  26. Sladojević, J., Petrov, E.P., Sayma, A.I., Imregun, M. and Green, J.S. (2005). Investigation of the influence of aerodynamic coupling on response levels of mistuned bladed DISCS with weak structural coupling. .
  27. Wu, X., Sayma, A.I., Vahdati, W. and Imregun, M. (2004). Computational techniques for aeroelasticity and aero-acoustic analyses of aero-engine fan assemblies. .
  28. Cand, M., Sayma, A.I. and Imregun, M. (2004). 3-Dimensional noise propagation using a Cartesian grid. .
  29. Wu, X., Vahdati, M., Sayma, A.I. and Imregun, M. (2003). A numerical investigation of aeroacoustic fan blade flutter. .
  30. Bréard, C., Sayma, A., Imregun, M., Wilson, A.G. and Tester, B.J. (2001). A CFD-based non-linear model for the prediction of tone noise in lined ducts. .
  31. Bréard, C., Vahdati, M., Sayma, A.I. and Imregun, M. (2000). An integrated time-domain aeroelasticlty model for the prediction of fan forced response due to inlet distortion. .
  32. Bréard, C., Imregun, M., Sayma, A. and Vahdati, M. (1999). Flutter stability analysis of a complete fan assembly. .
  33. Bréard, C., Imregun, M., Sayma, A. and Vahdati, M. (1999). Flutter stability analysis of a complete fan assembly. .
  34. Vahdati, M., Sayma, A. and Imregun, M. (1998). Prediction of high and low engine order forced responses for an LP turbine blade. .
  35. Sayma, A.I., Vahdati, M. and Imregun, M. (1998). Forced response analysis of an intermediate pressure turbine using a nonlinear aeroelasticity model. .
  36. Betts, P.L. and Sayma, A.I. (1992). On the suppression of pressure checkerboarding with bilinear-constant mixed interpolation. .

Journal Articles (36)

  1. Ioannou, E. and Sayma, A.I. (2017). Full annulus numerical study of hot streaks propagation in a hydrogen-rich syngas-fired heavy duty axial turbine. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 231(5), pp. 344–356. doi:10.1177/0957650917706861.
  2. White, M., Sayma, A.I. and Markides, C.N. (2017). Supersonic flow of non-ideal fluids in nozzles: An application of similitude theory and lessons for ORC turbine design and flexible use considering system performance. Journal of Physics: Conference Series, 821(1) . doi:10.1088/1742-6596/821/1/012002.
  3. White, M. and Sayma, A.I. (2016). Improving the economy-of-scale of small organic rankine cycle systems through appropriate working fluid selection. Applied Energy, 183, pp. 1227–1239. doi:10.1016/j.apenergy.2016.09.055.
  4. White, M. and Sayma, A.I. (2015). The Application of Similitude Theory for the Performance Prediction of Radial Turbines Within Small-Scale Low-Temperature Organic Rankine Cycles. Journal of Engineering for Gas Turbines and Power, 137(12) . doi:10.1115/1.4030836.
  5. Li, Y.L. and Sayma, A.I. (2015). Computational fluid dynamics simulations of blade damage effect on the performance of a transonic axial compressor near stall. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 229(12), pp. 2242–2260. doi:10.1177/0954406214553828.
  6. White, M. and Sayma, A.I. (2015). System and component modelling and optimisation for an efficient 10 kWe low-temperature organic Rankine cycle utilising a radial inflow expander. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 229(7), pp. 795–809. doi:10.1177/0957650915574211.
  7. White, M. and Sayma, A.I. (2015). The one-dimensional meanline design of radial turbines for small scale low temperature organic rankine cycles. Proceedings of the ASME Turbo Expo, 2C . doi:10.1115/GT2015-42466.
  8. White, M. and Sayma, A.I. (2015). The impact of component performance on the overall cycle performance of small-scale low temperature organic Rankine cycles. IOP Conference Series: Materials Science and Engineering, 90(1) . doi:10.1088/1757-899X/90/1/012063.
  9. SAYMA, A., Moghadam, E.R. and Long, C.A. (2013). Numerical investigation of moment coefficient and flow structure in a rotor stator cavity with rotor mounted bolts. Proceedings of the Institution of Mechanical Engineers Part A: Journal of Power and Energy, 227(3) .
  10. SAYMA, A. (2011). Towards virtual testing of compression systems in gas turbine engines. NAFEMS International Journal of CFD Case Studies .
  11. di Mare, L., Imregun, M., Green, J.S. and Sayma, A.I. (2010). A numerical study of labyrinth seal flutter. Journal of Tribology, 132(2), pp. 1–7. doi:10.1115/1.3204774.
  12. Cooke, A., Childs, P., Sayma, N. and Long, C.A. (2009). A disc to air heat flux error and uncertainty analysis applied to a turbomachinery test rig design. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 223(3), pp. 659–674. doi:10.1243/09544062JMES1158.
  13. Chassaing, J.C., Sayma, A.I. and Imregun, M. (2008). A combined time and frequency domain approach for acoustic resonance prediction. Journal of Sound and Vibration, 311(3-5), pp. 1100–1113. doi:10.1016/j.jsv.2007.10.006.
  14. Bartels, R.E. and Sayma, A.I. (2007). Computational aeroelastic modelling of airframes and turbomachinery: progress and challenges. Philos Trans A Math Phys Eng Sci, 365(1859), pp. 2469–2499. doi:10.1098/rsta.2007.2018.
  15. Wilson, M.J., Imregun, M. and Sayma, A.I. (2007). The effect of stagger variability in gas turbine fan assemblies. Journal of Turbomachinery, 129(2), pp. 404–411. doi:10.1115/1.2437776.
  16. Vahdati, M., Sayma, A.I., Imregun, M. and Simpson, G. (2007). Multibladerow forced response modeling in axial-flow core compressors. Journal of Turbomachinery, 129(2), pp. 412–422. doi:10.1115/1.2436892.
  17. Vahdati, M., Sayma, A.I., Freeman, C. and Imregun, M. (2005). On the use of atmospheric boundary conditions for axial-flow compressor stall simulations. Journal of Turbomachinery, 127(2), pp. 349–351. doi:10.1115/1.1861912.
  18. Wu, X., Vahdati, M., Sayma, A. and Imregun, M. (2005). Whole-annulus aeroelasticity analysis of a 17-bladerow WRF compressor using an unstructured Navier-Stokes solver. International Journal of Computational Fluid Dynamics, 19(3), pp. 211–223. doi:10.1080/10618560410001715554.
  19. Sayma, A.I., Vahdati, M., Lee, S.J. and Imregun, M. (2003). Forced response analysis of a shaft-driven lift fan. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 217(10), pp. 1125–1138. doi:10.1243/095440603322517144.
  20. Sayma, A.I., Kim, M. and Smith, N.H.S. (2003). Leading-edge shape and aeroengine fan blade performance. Journal of Propulsion and Power, 19(3), pp. 516–519.
  21. Bréard, C., Sayma, A.I., Vahdati, M. and Imregun, M. (2002). Aeroelasticity analysis of an industrial gas turbine combustor using a simplified combustion model. Journal of Fluids and Structures, 16(8), pp. 1111–1126. doi:10.1006/jfls.2002.0466.
  22. Sayma, A.I., Bréard, C., Vahdati, M. and Imregun, M. (2002). Aeroelasticity analysis of air-riding seals for aero-engine applications. Journal of Tribology, 124(3), pp. 607–616. doi:10.1115/1.1467086.
  23. Vahdati, M., Sayma, A.I., Bréard, C. and Imregun, M. (2002). Computational study of intake duct effects on fan flutter stability. AIAA Journal, 40(3), pp. 408–418.
  24. Bréard, C., Vahdati, M., Sayma, A.I. and Imregun, M. (2002). An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion. Journal of Engineering for Gas Turbines and Power, 124(1), pp. 196–208. doi:10.1115/1.1416151.
  25. Barakos, G., Vahdati, M., Sayma, A.I., Bréard, C. and Imregun, M. (2001). A fully distributed unstructured Navier-Stokes solver for large-scale aeroelasticity computations. Aeronautical Journal, 105(1041-1050), pp. 419–426.
  26. Vahdati, M., Sayma, A.I., Marshall, J.G. and Imregun, M. (2001). Mechanisms and prediction methods for fan blade stall flutter. Journal of Propulsion and Power, 17(5), pp. 1100–1108. doi:10.2514/2.5850.
  27. Sayma, A.I., Vahdati, M. and Imregun, M. (2000). Multi-bladerow fan forced response predictions using an integrated three-dimensional time-domain aeroelasticity model. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 214(12), pp. 1467–1483. doi:10.1243/0954406001523425.
  28. Sayma, A.I., Vahdati, M. and Imregun, M. (2000). Turbine forced response prediction using an integrated non-linear analysis. Proceedings of the Institution of Mechanical Engineers, Part K: Journal of Multi-body Dynamics, 214(1), pp. 45–60.
  29. Sayma, A.I., Vahdati, M., Sbardella, L. and Imregun, M. (2000). Modeling of three-dimensional viscous compressible turbomachinery flows using unstructured hybrid grids. AIAA journal, 38(6), pp. 945–954.
  30. Sbardella, L., Sayma, A.I. and Imregun, M. (2000). Semi-structured meshes for axial turbomachinery blades. International Journal for Numerical Methods in Fluids, 32(5), pp. 569–584. doi:10.1002/(SICI)1097-0363(20000315)32:5<569::AID-FLD975>3.0.CO;2-V.
  31. Sayma, A.I., Vahdati, M. and Imregun, M. (2000). An Integrated Nonlinear Approach for Turbomachinery Forced Response Prediction. Part I: Formulation. Journal of Fluids and Structures, 14(1), pp. 87–101. doi:10.1006/jfls.1999.0253.
  32. Vahdati, M., Sayma, A.I. and Imregun, M. (2000). An Integrated Nonlinear Approach for Turbomachinery Forced Response Prediction. Part II: Case Studies. Journal of Fluids and Structures, 14(1), pp. 103–125. doi:10.1006/jfls.1999.0254.
  33. Sayma, A.I., Vahdati, M., Imregun, M. and Green, J.S. (1998). Whole-assembly flutter analysis of a low-pressure turbine blade. Aeronautical Journal, 102(1018), pp. 459–463.
  34. Sayma, A.I. and Betts, P.L. (1998). Numerical modelling of thermal radiation absorption during the dispersion of dense gas clouds in the atmosphere. International Journal for Numerical Methods in Fluids, 26(7), pp. 837–850.
  35. Sayma, A.I. and Betts, P.L. (1997). A finite element model for the simulation of dense gas dispersion in the atmosphere. International Journal for Numerical Methods in Fluids, 24(3), pp. 291–317.
  36. Li, Y. and Sayma, A.I. Computational Fluid Dynamics Simulation of Surge in a Three Stage Axial Compressor. International Journal of Turbines & Sustainable Energy Systems, 1(1) . doi:10.4273/ijtses.1.1.04.

Patents (2)

  1. Simpson, G. (2008). Design of vanes for exposure to Vibration Loading. Patent no. US7909580 B2
  2. Vahdati, M. and Sayma, A. (2008). METHOD OF MODELING THE ROTATING STALL OF A GAS TURBINE ENGINE. Patent no. US 7,643,975 B2