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Dr Djamel Rezgui
Dr Djamel Rezgui
MEng, PhD
Lecturer
Area of research
Aeroelastic Stability of Smart Nonlinear Helicopter Rotor Structures
Research summary
Research Interests
- Nonlinear rotor blade aeroelasticity and stability.
- Dynamics of smart helicopter rotors.
- Periodically forced and self-excited systems.
- Piece-wise smooth systems.
- Dynamics or coupled rotating-stationary structures.
- Applications of bifurcation and continuation methods for engineering problems.
- Experimental continuation techniques.
- Dynamic substructuring.
- Nonlinear modal analysis.
- Autogyro flight mechanics.
- Flight mechanics and control of Rotary UAVs and MAVs.
- Design concepts of wind and marine turbines.
- Energy harvesting using nonlinear design and control concepts.
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Biography
Djamel Rezgui is a lecturer at the University of Bristol, with an interest in the dynamics of nonlinear oscillatory aero-systems. His research is focused on using continuation methods and bifurcation theory, to increase the understanding of the behaviour and stability of nonlinear aeroelastic and aeromechanic rotor systems. Example applications include understanding the stability of the autogyro rotors at high speed conditions and the aeroelastic stability of helicopter rotor blades. Djamel's research also involved combining experimental techniques with continuation and bifurcation analysis. Djamel graduated and acquired his Master’s degree in Aerospace Engineering in 2004 and completed his PhD in ...
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Selected publications
- Rezgui, D, Lowenberg, MH, Jones, M & Monteggia, C 2012, Towards Industrialisation of Bifurcation Analysis in Rotorcraft Aeroelastic Problems. in: American Institue of Aeronautics and Astronautics: AIAA Atmospheric Flight Mechanics Conference.
- Rezgui, D, Lowenberg, M, Jones, M & Monteggia, C 2011, Application of Continuation and Bifurcation Methods to Aeroelastic Rotor Blade Stability. in: 37th European Rotorcraft Forum, Milan, Italy.
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Recent publications
- Rezgui, D, Lowenberg, M & Bunniss, P 2010, Flap-lag stability of helicopter rotor blades using continuation and bifurcation methods. in: 3rd International Conference on Dynamics, Vibration & Control, Hangzhou, China.
- Lowenberg, M, Rezgui, D & Bunniss, P 2009, Experimental evaluation of numerical continuation and bifurcation methods applied to autogyro rotor blade aeromechanical stability. in: 7th International Conference on Multibody Systems, Nonlinear Dynamics and Control (IDETC), San Diego, CA, USA. ASME, pp. 379 - 387
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