In the current research, effects of the layout of film holes near the first-stage vane leading edge on the endwall cooling and phantom cooling of the vane suction side surface were numerically studied. The computational results indicate that the case with a positive film-hole angle achieves a higher cooling effectiveness level on the endwall and vane suction side surface compared to the case with a corresponding negative film-hole angle. Furthermore, the location of the film hole has a significant influence on the cooling performance of the endwall and vane suction side surface. In addition, the case with a smaller distance from film holes to the vane stagnation also attains a slightly higher cooling effectiveness (phantom cooling effective...
Film-cooling-air ejection from the suction surface of a turbine vane was investigated. This investig...
This study aims to investigate the cooling performance of various film cooling holes, including comb...
Detailed experiments were carried out to obtain the film cooling effectiveness distribution on the s...
In the current research, effects of the layout of film holes near the first-stage vane leading edge ...
Endwall film cooling upstream of the leading edge (LE) of a vane presents a relatively complex flow ...
In order to study the effect of thermal barrier coating deposition inside the film holes of turbine ...
Purpose: Endwall film cooling protects vane endwall by coolant coverage, especially at the leading e...
The aim of this work is oriented to increase film cooling effectiveness value through numerical inve...
Endwall film cooling is a significant cooling method to protect the endwall region and the junction ...
The present paper shows the results of an experimental investigation on film cooling of a nozzle van...
The effects of wall thickness and hole shape variation on a full-coverage film cooled turbine vane a...
Researchers in gas turbine field take great interest in the cooling performance on the first-stage v...
An experimental study was conducted in a simulated three vane linear cascade to determine the effect...
The film cooling and heat transfer on the endwall especially in the junction region of a vane/blade ...
In gas turbine development, the direction has been higher turbine inlet temperatures to increase the...
Film-cooling-air ejection from the suction surface of a turbine vane was investigated. This investig...
This study aims to investigate the cooling performance of various film cooling holes, including comb...
Detailed experiments were carried out to obtain the film cooling effectiveness distribution on the s...
In the current research, effects of the layout of film holes near the first-stage vane leading edge ...
Endwall film cooling upstream of the leading edge (LE) of a vane presents a relatively complex flow ...
In order to study the effect of thermal barrier coating deposition inside the film holes of turbine ...
Purpose: Endwall film cooling protects vane endwall by coolant coverage, especially at the leading e...
The aim of this work is oriented to increase film cooling effectiveness value through numerical inve...
Endwall film cooling is a significant cooling method to protect the endwall region and the junction ...
The present paper shows the results of an experimental investigation on film cooling of a nozzle van...
The effects of wall thickness and hole shape variation on a full-coverage film cooled turbine vane a...
Researchers in gas turbine field take great interest in the cooling performance on the first-stage v...
An experimental study was conducted in a simulated three vane linear cascade to determine the effect...
The film cooling and heat transfer on the endwall especially in the junction region of a vane/blade ...
In gas turbine development, the direction has been higher turbine inlet temperatures to increase the...
Film-cooling-air ejection from the suction surface of a turbine vane was investigated. This investig...
This study aims to investigate the cooling performance of various film cooling holes, including comb...
Detailed experiments were carried out to obtain the film cooling effectiveness distribution on the s...