Gas turbine blades are usually cooled by using ribbed serpentine internal cooling passages
which are fed by extracted compressor air. The individual straight ducts are connected by …

Gas turbine blades are usually cooled by using ribbed serpentine internal cooling passages,
which are fed by extracted compressor air. The individual straight ducts are connected by …

The ribbed serpentine blade cooling system is a typical configuration in the modern gas
turbine airfoil. In this study, the experimental and the numerical efforts were carried out to …

Internal cooling channels with differing aspect ratios are typically found in gas turbine blades
due to the varying thickness of the blade from the leading to trailing edge. These serpentine …

Serpentine, multi-pass cooling passages are used in cooling advanced gas turbine blades.
In the open literature, most internal cooling studies use a fixed cross-sectional area for multi …

Internal cooling channels with differing aspect ratios are typically found in gas turbine blades
due to the varying thickness of the blade from the leading to trailing edge. These serpentine …

This numerical study examined the effects of a curved turning vane on the heat transfer and
pressure loss of a four-pass internal cooling channel. Three-dimensional omega-based …

The ribbed serpentine blade cooling system is a typical configuration in the modern gas
turbine airfoil. In this study, experimental and the numerical efforts were carried out to …

The gas turbine blade/vane internal cooling is achieved by circulating the compressed air
through the cooling channels inside the turbine blade. Cooling channel geometries vary to fit …

The gas turbine blade/vane internal cooling is achieved by circulating compressed air
through the cooling channels inside the turbine blade. Cooling channel geometries vary to fit …