Results 21 to 30 of about 12,641 (263)

Experimental Study on the Improvement of the Film Cooling Effectiveness of Various Modified Configurations Based on a Fan-Shaped Film Cooling Hole on a Flat Plate

open access: yesEnergies, 2023
Modern gas turbines have evolved by increasing the turbine inlet temperature (TIT) to improve performance. This development has led to a demand for cooling techniques.
Seokmin Kim   +3 more
doaj   +1 more source

Experimental Study on the Improvement of Film Cooling Effectiveness of Various Modified Configurations Based on a Fan-Shaped Film Cooling Hole on an Endwall

open access: yesEnergies, 2023
Several studies have previously been conducted to improve the cooling performance of film cooling. However, most of the research has conducted experiments with film cooling holes on flat plates, and thus, the results of these studies do not encompass the
Seokmin Kim   +3 more
doaj   +1 more source

Determination of Film Cooling Effectiveness and Heat Transfer Coefficient Simultaneously on a Flat Plate

open access: yesEnergies, 2022
In this paper, flat plate film cooling with two rows of compound angle cylindrical film cooling holes was investigated. A data processing method was evaluated which could determine the film cooling effectiveness and heat transfer coefficient ...
Mingjie Zhang
doaj   +1 more source

Effects of Turbulence Promoters of Gas Turbine Blades on Film Cooling Performance

open access: yesJournal of Thermal Science and Technology, 2012
The effects of orientation of turbulence promoting ribs in the internal cooling air passage on the film cooling performance of outer surface of gas turbine blades have been studied experimentally.
Yukiko AGATA   +3 more
doaj   +1 more source

Numerical Study on Film-Cooling Effectiveness for Various Film-Cooling Hole Schemes

open access: yesASME-JSME-KSME 2011 Joint Fluids Engineering Conference: Volume 1, Symposia – Parts A, B, C, and D, 2011
Film-cooling has been widely used as the important alternative to protect the turbine blade. Since the film-cooling hole geometry is one of the most influential parameters for film-cooling performance, various film-cooling hole schemes have been developed to increase cooling performance for the past few decades.
S.M. Kim, K.D. Lee, K.Y. Kim
openaire   +2 more sources

Experimental Investigation on the Effects of DBD Plasma on the Film Cooling Effectiveness of a 30-Degree Slot

open access: yesApplied Sciences, 2017
The effects of dielectric barrier discharge (DBD) plasma on the film cooling effectiveness of a 30-degree slot was experimentally investigated in a low-speed wind tunnel.
Ye Jee Kim   +3 more
doaj   +1 more source

Numerical Investigation on Film Cooling Mechanism with Different Coolant Delivery Configurations

open access: yesJournal of Applied Fluid Mechanics, 2021
Kidney vortex has significant impact on film cooling effectiveness, and different kinds of film cooling hole geometry and configuration are developed to weaken or eliminate kidney vortex.
Y. T. Jiang   +4 more
doaj  

Numerical Computation and Optimization of Turbine Blade Film Cooling

open access: yesAdvances in Mechanical Engineering, 2014
The effect of film cooling parameters on the cooling effectiveness of an actual turbine blade is studied numerically. Film cooling parameters such as the hole shape, holes distribution, blowing ratio, streamwise angle, and spanwise angle are investigated
Ahmed M. Elsayed   +2 more
doaj   +1 more source

Film cooling modeling of a turbine vane with multiple configurations of holes

open access: yesCase Studies in Thermal Engineering, 2018
Film cooling flow is important for gas turbine thermal protection. But it is difficult to predict the film cooling flow performances. The aim of this paper is to modeling the film cooling flow of a turbine vane with endwall film cooling, showerhead film ...
J.H. Liu, Y.B. Liu, L. Liu
doaj   +1 more source

Numerical study on film cooling mechanism and characteristics of cylindrical holes with branched jet injections

open access: yesPropulsion and Power Research, 2013
The film cooling mechanism and characteristics of a row of cylindrical holes with branched jet injections were investigated by numerical simulation. Three geometries for the branched jet injection holes and four blowing ratios were considered.
Yu Yao, Jingzhou Zhang, Yang Yang
doaj   +1 more source

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