By means of time-resolved thermal infrared technique, an experimental investigation of the
effect of transverse trench on unsteady film cooling performances of backward cylindrical …

Grain depth-of-cut, which is the predominant factor determining the surface morphology,
grinding force, and subsurface damage, has a significant impact on the surface quality of the …

The high pressure turbine nozzle guide vane of a modern aeroengine experiences large
heat loads and thus requires both highly effective internal and external cooling. This can be …

Oleo-damping performance is a key factor affecting the landing gear buffer performance,
while the flow discharge coefficient determines buffer damping force. For improving the …

Abstract Full-scale Computational Fluid Dynamics (CFD) numerical simulations can
accurately predict the heat flux and metal wall temperature of gas turbine combustor liners …

Quasi-transpiration cooling schemes such as Double-Wall Effusion Cooling allow the
Nozzle Guide Vanes of High Pressure Turbines in modern aeroengines to experience high …

Gas turbine design has been characterized over the years by a continuous increase of the
maximum cycle temperature, justified by a corresponding increase of cycle efficiency and …

This study investigates the discharge coefficient of a cylindrical hole with gas jets in liquid
crossflow in a cavitation tunnel. Utilizing the Π theorem, the research examines the …

An experimental study was performed on the discharge coefficients of laidback fan-shaped
holes under different internal coolant crossflow orientations. The influence of the geometric …

This study combines the experimental and numerical simulation methods to deeply analyze
the impact of liquid crossflow on the discharge coefficient of a gas jet hole on a flat plate …