Results 21 to 30 of about 13,478 (277)

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

Flow characterization of microscale effusion and transpiration air cooling on single blade

open access: yesCase Studies in Thermal Engineering, 2022
Micro cooling has drawn attention as the next-generation cooling technique that is better than film cooling for a high-temperature turbine blade. Not to reduce the gas turbine efficiency while having high blade cooling effectiveness, it recommends that ...
Mingeon Kim   +3 more
doaj   +1 more source

Experimental Study of Impingement Effusion-Cooled Double-Wall Combustor Liners: Thermal Analysis

open access: yesEnergies, 2021
A new experimental study is presented for a combustor with a double-wall cooling design. The inner wall at the hot gas side features effusion cooling with 7-7-7 laidback fan-shaped holes, and the outer wall at the cold side features an impingement hole ...
Thomas Jackowski   +2 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

Influence of Spanwise and Streamwise Film Hole Spacing on Adiabatic Film Effectiveness for Effusion-Cooled Gas Turbine Blades

open access: yesInternational Journal of Turbomachinery, Propulsion and Power, 2021
To meet the challenges of increased thermal loads and performance demands on aero-engine turbine blades, more advanced cooling techniques are required. This study used a modification of the well-known Goldstein equation to predict film effectiveness for ...
Matthew Courtis   +4 more
doaj   +1 more source

Deposition Characteristics of Particles with Different Diameters in an Impingement-Effusion Structure with a Double-Wall Blade [PDF]

open access: yesJournal of Applied Fluid Mechanics, 2023
Ingestion and deposition of fine particles on the surface of the coolant passage degrade the blade’s cooling performance. This paper proposes a deposition model to investigate the complex deposition characteristics of fine particles during repeated ...
W. Zhang, P. Zhang, Y. D. Wang
doaj   +1 more source

Computational Optimization of a Loosely-Coupled Strategy for Scale-Resolving CHT CFD Simulation of Gas Turbine Combustors

open access: yesEnergies, 2023
The accurate prediction of heat fluxes and, thus, metal wall temperatures of gas turbine (GT) combustor liners is a complicated and numerically expensive task.
Alberto Amerini   +2 more
doaj   +1 more source

Theory of cooling by flow through narrow pores [PDF]

open access: yes, 2006
We consider the possibility of adding a stage to a dilution refrigerator to provide additional cooling by ``filtering out'' hot atoms. Three methods are considered: 1) Effusion, where holes having diameters larger than a mean-free path allow atoms to ...
J. M. Ziman   +3 more
core   +3 more sources

Terrestrial analogs and thermal models for Martian flood lavas [PDF]

open access: yes, 2000
The recent flood lavas on Mars appear to have a characteristic “platy-ridged” surface morphology different from that inferred for most terrestrial continental flood basalt flows.
A. S. McEwen   +77 more
core   +1 more source

Unsteady Flow Field Characterization of Effusion Cooling Systems with Swirling Main Flow: Comparison Between Cylindrical and Shaped Holes

open access: yesEnergies, 2020
The presence of injectors with strongly swirled flows, used to promote flame stability in the combustion chambers of gas turbines, influences the behaviour of the effusion cooling jets and consequently of the liner’s cooling capabilities. For this reason,
Tommaso Lenzi   +4 more
doaj   +1 more source

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