All Outputs (3)

Effect of lid height and blowing ratio on film cooling effectiveness of a novel lidded hole configuration (2022)
Journal Article
Guelailia, A., Khorsi, A., Slimane, S. A., Blala, H., Slimane, A., Salem, H., & Bouferrouk, A. (2022). Effect of lid height and blowing ratio on film cooling effectiveness of a novel lidded hole configuration. Proceedings of the Institution of Mechanical Engineers, Part E: Journal of Process Mechanical Engineering, 236(6), 2599-2607. https://doi.org/10.1177/09544089221095665

Film cooling is one of the promising technologies used for protecting rocket nozzles and turbine blades from combustion chamber hot gases. This paper proposes a novel shape of film cooling injection hole, called lidded hole, that can offer significan... Read More about Effect of lid height and blowing ratio on film cooling effectiveness of a novel lidded hole configuration.

The effects of a morphed trailing-edge flap on the aeroacoustic and aerodynamic performance of a 30P30N Aerofoil (2022)
Journal Article
Watkins, J., & Bouferrouk, A. (2022). The effects of a morphed trailing-edge flap on the aeroacoustic and aerodynamic performance of a 30P30N Aerofoil. Acoustics, 4(1), 248-267. https://doi.org/10.3390/acoustics4010015

This paper presents initial results on the aeroacoustic and aerodynamic effects of morphing the trailing-edge flap of the 30P30N aerofoil, over five flap deflections (5–25◦ ), at an 8◦ angle of attack and a Reynolds number of Re = 9.2 × 105 . The Ffo... Read More about The effects of a morphed trailing-edge flap on the aeroacoustic and aerodynamic performance of a 30P30N Aerofoil.

Effects of an unsteady morphing wing with seamless side-edge transition on aerodynamic performance (2022)
Journal Article
Abdessemed, C., Bouferrouk, A., & Yao, Y. (2022). Effects of an unsteady morphing wing with seamless side-edge transition on aerodynamic performance. Energies, 15(3), Article 1093. https://doi.org/10.3390/en15031093

This paper presents an unsteady flow analysis of a 3D wing with a morphing trailing edge flap (TEF) and a seamless side-edge transition between the morphed and static parts of a wing by introducing an unsteady parametrization method. First, a 3D stea... Read More about Effects of an unsteady morphing wing with seamless side-edge transition on aerodynamic performance.