Results 11 to 20 of about 167,722 (364)

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

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

Full Coverage Discrete Hole Wall Cooling: Cooling Effectiveness [PDF]

open access: yesVolume 4: Heat Transfer; Electric Power, 1984
The development of a test facility for investigating full coverage discrete hole wall cooling for gas turbine combustion chamber wall cooling is described. A low temperature test condition of 750K mainstream temperature and 300K coolant temperature was used to investigate the influence of coolant flow rate at a constant cross flow Mach number ...
G.E. Andrews, M.L. Gupta, M.C. Mkpadi
openaire   +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

Pressure Gradient Effects on Film Cooling [PDF]

open access: yesVolume 4: Heat Transfer; Electric Power; Industrial and Cogeneration, 1995
Film cooling effectiveness was studied experimentally using a flat plate test facility with a single row of inclined round holes which injected high density, cryogenically cooled air. A pressure distribution representative of the suction side of a gas turbine blade was imposed on the test plate using a top wall contour.
Donald L. Schmidt, David G. Bogard
openaire   +1 more source

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

Effects of LoD and PoD in combined-hole film cooling [PDF]

open access: yes, 2017
Film cooling technique was used to provide thermal protection for turbine components from the hot combustion gases. Combined-hole film cooling system was introduced as a way to improve the film cooling performances.
Abdullah, Mohammad Kamil   +1 more
core   +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  

Surrogate-based optimization of a cratered cylindrical hole to enhance film-cooling effectiveness

open access: yesJournal of Thermal Science and Technology, 2016
A cratered film-cooling hole was investigated to determine the effect of shape parameters on film-cooling performance, and shape of the hole was optimized to improve film-cooling effectiveness.
Jun-Hee KIM, Kwang-Yong KIM
doaj   +1 more source

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

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