Model configurations of a blade trailing-edge internal cooling passage with staggered elliptic pin-fins in streamwise and spanwise are adopted for numerical investigation using computational fluid dynamics (CFD). Grid refinement study is performed at first to identify a baseline mesh, followed by validation study of passage total pressure loss, which gives 2 and 4 discrepancies respectively for two chosen configurations in comparison with experimental measurements. Further investigations are focused on evaluation of wall heat transfer coefficient (HTC) of both pin-fin and end walls, and it is found that CFD predicted pin-fin wall HTC are generally in good agreement with test data for the streamwise staggered elliptic pin-fins, but not the s...
In order to achieve higher thermal efficiency and power output, the gas turbine inlet temperature of...
Increasing the firing temperatures in gas turbines require better, and highly efficient means of hea...
Detailed measurements of the heat transfer coefficient (htc) distributions on the internal surfaces ...
Model configurations of a blade trailing-edge internal cooling passage with staggered elliptic pin-f...
This paper studies the effect of mesh topologies such as hybrid and structured meshes on the evaluat...
Turbine blades are often exposed to the ‘hot’ gas environment and thus it is essential to apply effe...
Detailed flow visualization and heat transfer investigations under uniform heat flux boundary condit...
In modern turbine blades, pressure-side cutbacks with film-cooling slots stiffened with lands and pi...
Heat transfer and pressure characteristics in a rectangular channel are experimentally explored in d...
The air outlet hole of lower edge plate of turbine blade can influence the flow and heat transfer pe...
In this paper detailed experimental measurements and computational predictions of heat transfer coef...
A common way to cool the tip is to use serpentine passages with 180-deg turn under the blade tip-cap...
Detailed measurements of the heat transfer coefficient distributions on the internal surfaces of a n...
The heat transferred to the turbine blade is substantially increased as the turbine inlet temperatur...
In certain regions of turbine aerofoils, cooling system designers need to cool the blades with conve...
In order to achieve higher thermal efficiency and power output, the gas turbine inlet temperature of...
Increasing the firing temperatures in gas turbines require better, and highly efficient means of hea...
Detailed measurements of the heat transfer coefficient (htc) distributions on the internal surfaces ...
Model configurations of a blade trailing-edge internal cooling passage with staggered elliptic pin-f...
This paper studies the effect of mesh topologies such as hybrid and structured meshes on the evaluat...
Turbine blades are often exposed to the ‘hot’ gas environment and thus it is essential to apply effe...
Detailed flow visualization and heat transfer investigations under uniform heat flux boundary condit...
In modern turbine blades, pressure-side cutbacks with film-cooling slots stiffened with lands and pi...
Heat transfer and pressure characteristics in a rectangular channel are experimentally explored in d...
The air outlet hole of lower edge plate of turbine blade can influence the flow and heat transfer pe...
In this paper detailed experimental measurements and computational predictions of heat transfer coef...
A common way to cool the tip is to use serpentine passages with 180-deg turn under the blade tip-cap...
Detailed measurements of the heat transfer coefficient distributions on the internal surfaces of a n...
The heat transferred to the turbine blade is substantially increased as the turbine inlet temperatur...
In certain regions of turbine aerofoils, cooling system designers need to cool the blades with conve...
In order to achieve higher thermal efficiency and power output, the gas turbine inlet temperature of...
Increasing the firing temperatures in gas turbines require better, and highly efficient means of hea...
Detailed measurements of the heat transfer coefficient (htc) distributions on the internal surfaces ...