Outputs (10)

Broadband and transient aeroacoustic analysis of a CRM-based joined wing configuration at low speeds (2025)
Presentation / Conference Contribution

This study presents a computational investigation into the aeroacoustic performance of a Joined Wing (JW) configuration at low subsonic speeds. The modelled JW geometry, derived from NASA’s Common Research Model (CRM) configuration, consists of a fro... Read More about Broadband and transient aeroacoustic analysis of a CRM-based joined wing configuration at low speeds.

Wedged Gurney Flap for performance improvement of Vertical Axis Wind Turbines (2025)
Presentation / Conference Contribution

This study evaluates the wedged Gurney Flap (GF) on a three- straight-bladed Vertical Axis Wind Turbine (VAWT) using Computational Fluid Dynamics (CFD) simulations. The analysis considers the rotating effect of the blades at three different Tip Speed... Read More about Wedged Gurney Flap for performance improvement of Vertical Axis Wind Turbines.

Investigation of microjet engine inlet pressure distortions at angled inflow velocity conditions (2025)
Journal Article

The Armfield CM14 microjet axial flow turbine engine has been tested in open space at ambient conditions with engine inlet pressure at the aerodynamic interface plane (AIP) measured by a built-in pressure sensor for validating computational fluid dyn... Read More about Investigation of microjet engine inlet pressure distortions at angled inflow velocity conditions.

Transonic aerodynamic performance analysis of a CRM joined-wing configuration (2025)
Journal Article

This study examines the aerodynamic performance of a joined-wing (JW) aircraft design based on the NASA Common Research Model (CRM), aiming to assess its potential for efficient commercial transport or cargo aircraft at transonic speed (Mach 0.85). T... Read More about Transonic aerodynamic performance analysis of a CRM joined-wing configuration.

Dropped leading-edge aerofoil for improved aerodynamic and aeroacoustic performance (2024)
Presentation / Conference Contribution

Extended Abstract Ensuring the optimal performance of aerofoils is a critical engineering design challenge in aviation. The difficulty of enhancing aerodynamic efficiency whilst simultaneously reducing aeroacoustic emissions is well documented. Altho... Read More about Dropped leading-edge aerofoil for improved aerodynamic and aeroacoustic performance.

Drag reduction of lift-type vertical axis wind turbine with slit modified gurney flap (2024)
Journal Article

This study examines aerodynamic performance enhancement of Vertical Axis Wind Turbine (VAWT) blades with Gurney flap (GF) modified by slits. A quasi-3D computational fluid dynamics solution based on Reynolds-averaged Navier-Stokes model is employed t... Read More about Drag reduction of lift-type vertical axis wind turbine with slit modified gurney flap.

Aerodynamic performance optimisation of an aerofoil with combined leading-edge and trailing-edge morphing transformations (2024)
Presentation / Conference Contribution

The long-term strategy for aviation sustainability poses the need for more efficient aerodynamic designs. Many researchers have investigated innovative solutions offered by biologically inspired morphing wing concepts, with the leading- or trailing-e... Read More about Aerodynamic performance optimisation of an aerofoil with combined leading-edge and trailing-edge morphing transformations.

Micromechanical modeling of longitudinal compression behavior and failure mechanism of unidirectional carbon fiber reinforced aluminum composites involving initial fiber misalignment (2024)
Journal Article

A micromechanical model with realistic initial fiber misalignment (IFM) was developed to simulate the longitudinal compression behavior of unidirectional carbon fiber/aluminum composites. The matrix and fiber were modeled using ductile damage law and... Read More about Micromechanical modeling of longitudinal compression behavior and failure mechanism of unidirectional carbon fiber reinforced aluminum composites involving initial fiber misalignment.

Coupled morphing of leading and trailing-edge aerofoil for improved aerodynamic and aeroacoustic performance (2024)
Presentation / Conference Contribution

Event-triggered tracking control for switched nonlinear systems (2023)
Journal Article

In this paper, we study the output tracking control problem based on the event-triggered mechanism for cascade switched nonlinear systems. Firstly, an integral controller based on event-triggered conditions is designed, and the output tracking error... Read More about Event-triggered tracking control for switched nonlinear systems.