Results 1 to 10 of about 3,883 (153)

Numerical Investigation of the Effects of the Hole Inclination Angle and Blowing Ratio on the Characteristics of Cooling and Stress in an Impingement/Effusion Cooling System

open access: yesEnergies, 2023
Due to the uneven temperature field and temperature gradient introduced by an efficient cooling structure, the analysis of the stress field is necessary. In this study, the cooling characteristics and stress characteristics such as the thermal stress and
Haiwang Li   +4 more
doaj   +6 more sources

Influence of inhomogeneous porosity on effusion cooling [PDF]

open access: yesInternational Journal of Heat and Mass Transfer, 2019
Abstract Effusion cooling is an effective cooling technology which is considered as the next logical step of the cooling technology for gas turbine blades. Additive manufacturing technology makes it possible to fabricate effusion cooling structures in gas turbine blades with the optimal parameters and a low cost.
Gan Huang
exaly   +3 more sources

Effect of Holes Arrangement on Effusion Cooling Performance [PDF]

open access: yesEngineering and Technology Journal, 2014
The present work concentrates on the experimental investigation of effusion cooling performance for different whole pitch ratios. The film cooling effectiveness and local heat transfer coefficient for difference jet holes arrangement have been ...
Muwafag Sh. Alwan, Reyadh Ch. Al-Zachary
doaj   +2 more sources

Combined effect of upstream ramp and effusion cooling in combustion chamber liners of gas turbine

open access: yesJournal of Thermal Engineering, 2023
Effusion cooling technique is a highly efficient cooling method used to reduce the thermal stresses of combustion chamber liners in a gas turbine engine. The present study focuses on enhancing the adiabatic effectiveness of effusion cooling.
Yellu KUMAR   +3 more
doaj   +1 more source

Review of Advanced Effusive Cooling for Gas Turbine Blades

open access: yesEnergies, 2022
Turbine inlet temperature has continuously increased to improve gas turbine performance during the past few decades. Although internal convection cooling and traditional film cooling have contributed significantly to the current achievement, advanced ...
Wen Wang   +3 more
doaj   +1 more source

A Low Order Flow Network Model for Double-Wall Effusion Cooling Systems

open access: yesInternational Journal of Turbomachinery, Propulsion and Power, 2022
The high pressure turbine nozzle guide vane of a modern aeroengine experiences large heat loads and thus requires both highly effective internal and external cooling. This can be accomplished with double-wall effusion cooling, which combines impingement,
Michael van de Noort, Peter Ireland
doaj   +1 more source

Heat Transfer and Flow Performance of Impingement and Impingement/Effusion Cooling Systems [PDF]

open access: yesEngineering and Technology Journal, 2015
The current experimental study is made to investigate the heat transfer characteristics and pressure losses for both impingement and impingement/effusion cooling systems.The experiments are carried out on a metal test plate.The numerical work is made to ...
Assim H. Yousif   +2 more
doaj   +1 more source

Investigation of cooling performance degradation of impingement/effusion structure on pressure side of nozzle guide vane

open access: yesCase Studies in Thermal Engineering, 2022
The cooling performance of the impingent/effusion structure on the pressure side of nozzle guide vanes tested in an engine operating for the various duration of 100 h, 300 h, and 500 h was evaluated in this study via infrared thermal imaging.
Wei Zhang   +5 more
doaj   +1 more source

Experimental and numerical investigation of micro-scale effusion and transpiration air cooling on cascaded turbine blades

open access: yesCase Studies in Thermal Engineering, 2022
Micro cooling utilizing the micro-sized cooling hole or a porous structure on the surface is a promising technology in cooling applications of gas turbine blades.
Mingeon Kim   +3 more
doaj   +1 more source

Effects of Manufacturing Tolerances on Double-Wall Effusion Cooling

open access: yesJournal of Turbomachinery, 2023
Abstract As aeroengine designers seek to raise turbine entry temperatures for greater thermal efficiencies, novel cooling schemes are required to ensure that components can survive in increasingly hotter environments. By utilizing a combination of impingement cooling, pin-fin cooling, and effusion cooling, double-wall effusion cooling is
van de Noort, M   +2 more
openaire   +2 more sources

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