Results 21 to 30 of about 1,878,968 (293)

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

Uncertainty quantification and film cooling

open access: yesComputers & Fluids, 2013
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
D'Ammaro, A, Montomoli, F
openaire   +5 more sources

Film-cooling hole optimization and experimental validation considering the lateral pressure gradient

open access: yesFrontiers in Mechanical Engineering, 2023
The flow in the turbine endwall region consists of the complicated secondary flow structures driven by the lateral pressure gradient, which heavily affects the performance of film cooling.
Hao Zhang   +4 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

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

Cooling Characteristics of Film-Cooled Turbine Blades [PDF]

open access: yesVolume 4: Heat Transfer; Electric Power, 1984
A series of experiments was performed to measure the cooling effectiveness of pin-fin type blades applicable to the first-stage blades of the high pressure turbine for the Advanced Gas Turbine of Japan (AGTJ-100A). Actual pin-fin type blades were used in three-dimensional hot cascade tests.
T. Abe   +5 more
openaire   +1 more source

Effect of an Upstream Unconnected Bulge on Film Cooling

open access: yesChemical Engineering Transactions, 2017
Film cooling technology is commonly used in a cooling system of gas turbines. For different upstream bulge configurations, the unconnected and connected configurations were used to investigate the film cooling effectiveness and downstream dimensionless ...
Q. Li   +5 more
doaj   +1 more source

Experimental study on a spray and falling-film cooling system

open access: yesCase Studies in Thermal Engineering, 2021
After spraying, the cooling medium retains potential cooling capability and, consequently, can form a falling film to further cool the downward area. In this paper, the flow patterns and the heat transfer coefficients are correlated respectively in the ...
Yuqi Huang   +3 more
doaj   +1 more source

EFFECTS OF INTERNAL COOLANT CROSSFLOW ON FILM-COOLING PERFORMANCE OF DOUBLE-JET AND CYLINDRICAL HOLES

open access: yes, 2022
In this paper, the effects of internal coolant crossflow on double-jet holes were simulated and compared with two rows of cylindrical holes under three blowing ratios (M = 0.5, 1.0, and 1.5), with an established and validated turbulence model.
Xie, Gongnan,   +4 more
core   +1 more source

Investigation on the Effect of Impingement Chamber Structure and Cooling Unit Number on Composite Cooling [PDF]

open access: yesJournal of Applied Fluid Mechanics
In order to deeply explore the influence and mechanism of the impingement chamber structure and the number of cooling units on the film cooling performance.
J. Liu, Z. Zhu, J. Chang, S. Ma, J. Sun
doaj   +1 more source

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