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Effect of lid height and blowing ratio on film cooling effectiveness of a novel lidded hole configuration (2022)
Journal Article

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

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.