Results 21 to 30 of about 3,391,667 (362)

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

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

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

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

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

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

Experimental investigation of liquid film cooling in hypersonic flow

open access: yesThe Physics of Fluids, 2019
Film cooling is generally considered as a promising active cooling technology for developing thermal protection systems of hypersonic vehicles; however, most of experimental and numerical studies of film cooling mainly concentrated on gaseous film ...
苑朝凯   +3 more
semanticscholar   +1 more source

Experimental Study of a Novel Non-Packing Closed Evaporative Cooling Tower with Vertical 3D Deformation Tubes

open access: yesEnergies, 2022
The closed evaporative cooling tower (CECT) is widely used in the field of industrial cooling. At present, most CECTs still mainly adopt the horizontal-tube falling-film cooling method.
Aimin Tu   +5 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

Occurrence of Hysteresis like behavior of resistance of $Sb_2 Te_3$ film in heating-cooling cycle

open access: yes, 2004
Experimental observations of a peculiar behavior observed on heating and cooling ${\rm Sb_2Te_3}$ films at different heating and cooling rate are detailed. The film regained its original resistance, forming a closed loop, on the completion of the heating-
A.G. Vedeshwar   +14 more
core   +1 more source

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