2015
DOI: 10.1016/j.cja.2015.08.017
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Numerical investigation on the flow structures in a narrow confined channel with staggered jet array arrangement

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Cited by 11 publications
(1 citation statement)
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“…Figure 2 shows the turbine schematic and the components that use impingement cooling. These sketches are taken from different sources and more details on cooling configurations of these turbine components can be found in these references [52][53][54][55][56]. The combustor liner and shroud use arrays of jet holes that are usually customized for those individual components.…”
Section: Key Aspects Of Impingement Heat Transfer Related To Gas-turbine Technologiesmentioning
confidence: 99%
“…Figure 2 shows the turbine schematic and the components that use impingement cooling. These sketches are taken from different sources and more details on cooling configurations of these turbine components can be found in these references [52][53][54][55][56]. The combustor liner and shroud use arrays of jet holes that are usually customized for those individual components.…”
Section: Key Aspects Of Impingement Heat Transfer Related To Gas-turbine Technologiesmentioning
confidence: 99%